AD-PA Compliance Status Report I-DPCC...S TCCA CF-92-22 FAA 94-04-02 TCCA CF-2003-02 Bombardier SB215-A3040 SoREM AD CF-2003-02 Scheda analisi AD - N/A ENGINE REAR MOUNT STRUTS CLOSED:

A.D. Compliance Status

A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Delivery Date: Dec 07

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS

EXPIRATION REPETITIVE

ACTIONS DESCRIPTION

NOTES (COMPLIANCE DATE)

A Applicable (to be Incorp.) D Deleted

R Applicable Repetitive I Incorporated

N Not Applicable Y Yes effective

Revision n° 1

pag. 1 of 4 S Superseded N Not effective

Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCC Compliance Status

A N FAA

77-17-13 - - - - NLG DOORS

CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N

A N FAA

77-13-05 - - - -

MISSING RIVETS IN BULKHEAD


A N TCCA

CF-90-11R2 FAA 93-16-06R2

Bombardier SB215-A435

SoREM Scheda analisi AD

JUNE. 10, 1994 N/A

RUDDER-AILERON INTERCONNECT TAB (TO PREVENT POSSIBILE

FLUTTER)

CLOSED: NOT EFFECTIVE AS PER POWERED AILERON

SYSTEM INSTALLED

S TCCA

CF-92-22

FAA 94-04-02 TCCA CF-2003-

02



- N/A ENGINE REAR

MOUNT STRUTS

CLOSED: SUPERSEDED BY AD CF-2003-02

I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314


SoREM Scheda Analisi PA

N/A ENGINE FIRE-WIRE DETECTION LOOP

CLOSED: AD COMPLIED WITH

ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING

SYSTEM

I Y FAA

97-11-08 - - - -

AFM - LIMITATION SECTION - POWER

LEVERS

CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION

PAGE 8

A N TCCA

CF-96-02R1 ENAC 1999-268 - - - -

CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES NOT APPLICABLE AS PER AD

EFFECTIVITY

A N TCCA

CF-2002-14 FAA 2004-26-08

ENAC 02-167

Bombardier SB215-4234

SoREM DT CL-61-4234

MARCH 04, 2003 N/A PCU BACKUP

PRESSURE VALVE

NOT APPLICABLE AS PER VALVE INCORPORATED AT

MANUFACTURE

R N ENAC 00-496

FAA 2002-12-12 - - - WING TO FUSELAGE

FRAME ANGLES NOT APPLICABLE AS PER AD

EFFECTIVITY

S - FAA

2003-04-06 ENAC 03-067

FAA 2006-22-05

SoREM

DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343

March 16, 2003 N/A INU Honeywell Primus II

RNZ-850/ -851

REF TO COMPONENTS

SUPERSEDED BY FAA 2006-22-05

R Y TCCA

CF-2003-02 FAA 2004-10-04

ENAC 03-251

Bombardier SB215-A4287R2

SoREM BM-CL-71-A4287

BM-CL-71-A4287R2 SMJC 31 and 32

WITHIN 50 F/H SINCE FEBRUARY

28, 2003

EVERY 250 F/H REPETITIVE ACTION

FOLLOWED BY SoREM SMJC #31 and #32

ENGINE REAR MOUNT STRUTS

OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 ON 29/08/2011 (W/O

11/308); 194.25 FH TO GO

28/09/2003

R Y FAA

2004-21-05 -

SCHEDA ANALISI Disposizione Tecnica

DT-CL-21-01

A 500 heater Hrs Total or 100 heater hrs TIS from 19/11/04

(whichever occurs later)

100 Hrs funzion. 24 Months

PRESSURE DECAY TEST and CABIN

HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA

2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A

REGOLATORE CARBURANTE CON VALVOLE SHUTOFF

A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA

2005-18-05 - - - -

LOWER CAPS OF THE WING FRONT SPAR AND

REAR SPAR

CLOSED NOT APPLICABLE AS PER AD EFFECTIVITY

A N EASA

2006-0375 - Scheda Analisi AD Dec. 29, 2006 -

CARLING TECHNOLOGIES

SWITCHES

CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY

N N FAA

2006-22-05 EASA 2006-479 Scheda Analisi AD - N/A

INTEGRATED NAVIGATION UNITS

REF TO COMPONENTS

Supersedes FAA 2003-04-06

R Y TCCA

CF-2008-29 FAA 2009-05-04 ENAC 2008-316

SMJC-60 Mar 8, 2009

BEFORE AND AFTER EVERY FIRE SEASON

OR AT SIX MONTH INTERVAL,

WHICHEVER IS SHORTER TIME

PERIOD

RUDDER LOWER TORQUE TUBE UPPER BEARING

OPEN: AD COVERED BY SMJC 60 CARRIED OUT ON 04/04/2011(W/O

11/019 ADD 2) EXPIRED OCT 03, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2 ENAC 2011-88

Bombardier SB 215 -A4424 Jun 01, 2011

FIRST INSPECTION WITHIN 50 FC FROM

20 DEC 2010; THEREAFTER REPEAT

PERRFORM AN INSPECTION BEFORE

100 FC WITH TERMINATING ACTION NOT LATER THAN Jun

01, 2011.

INSPECTION OF THE EMERGENCY WATER DUMP

PULLEY BRACKET AND STRUCTURE

CLOSED SB 215-A4424 PART B EMBODIED ON 01/06/2011 (W/0 11/019 ADD 2)

R Y TCCA

CF-2011-35

Bombardier SB 215-A4450;

Bombardier SB 215-A4451

ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;

Ref. To AD-PA Compliance Components


Liquid Penetrant & Eddy Current Inspection on MLG Upper Member

Forward Lug

REF. TO AD-PA COMPLIANCE COMPONENTS

EASA/TCA/FAA/ENAC


Eng. Type:

PW123AF

Eng. S/N. :

AF0086 Manuf. date:

AUG 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION NOTES




Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance AF0086.doc

I Y TCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A

O-RING DETERIORATION DURING FUEL FILTER COVER INSTALLATION

- CLOSED - AD COMPLIED WITH AT

DELIVERY

I Y TCCA

CF-90-22R1 RAI 91-296

P&WC SB21018R1

30/06/94 N/A OIL SYSTEM INSPECTION

DUE TO BEARING DETERIORATION


DELIVERY

A N TCA

CF-91-02 -

P&WC SB20946R1

31/10/91 N/A TO PREVENT IN FLIGHT

TORQUE FLUCTUATIONS

- CLOSED – N/A DUE TO ENGINE S/N AD COMPLIED WITH AT

DELIVERY

I Y TCCA

CF-91-26R1 RAI 91-347

P&WC SB20914R3

SB21053 31/03/92 N/A

TO IMPROVE THE RETENTION OF THE

P2.5/P3 TUBE ASSEMBLY.


DELIVERY

S Y TCCA

CF-92-03R1 RAI 93-284 - - N/A

INTERNAL OIL FIRES INTERCOMPRESSOR

CASE (ICC)

- CLOSED – SUPERSEDED BY TCCA CF-92-03R2

I Y TCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065

30/06/94 N/A INTERNAL OIL FIRES IN

THE ICC.


DELIVERY

EASA/TCA/FAA/ENAC


Eng. Type:

PW123AF

Eng. S/N. :

AF0086 Manuf. date:

AUG 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS






Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance AF0086.doc

A N TCCA

CF-94-01

FAA 94-03-02 Amdt 39-8808

RAI 94-001 P&WC SIL 307

Since 14/01/94

1000⇔2000 cycles N/A

REPLACEMENT HP TURBINE DISK

- CLOSED - NOT EFFECTIVE FOR

ENGINES S/N 109022 AND SUBSEQUENT

I Y TCCA

CF-96-22 ENAC 96-353

P&WC SB21077R7 SB21364R1 SB21373R3

First nozzle replacement or within 30/11/98

Whichever occurs first

N/A REPLACEMENT OF FUEL

NOZZLES LOCKING PLATES AND “O” RINGS

- CLOSED - ALL SBs RELATED TO AD

EMBODIED AD COMPLIED WITH

A N TCCA

CF-2000-34 FAA 2003-16-04

ENAC 01-065 P&WC

SB 21100R2

all spare heaters within 02/03/01

installed p/n 10718 before 31/08/02

N/A ENGINE PW100 SERIES

FUEL HEATERS

- CLOSED – NOT APPLICABLE FOR

ENGINES S/N 109036 AND SUB’S

A N TCCA

CF-2002-10 ENAC 02-090

- CLOSED – N/A AS PER ENGINE MODEL

I Y TCCA

CF-2002-34 FAA 2004-20-01

ENAC 02-448

P&WC SB21562R0/R1/R2

SB21669 SOREM DT-CL-73-04

Within 400 f/h or “C/2” Inspection

1200 f/h or 3A Final Action within 2400 f/h

or 23/8/2004

INSPECTION /MODIFICATION OF MECHANICAL FUEL

CONTROL UNIT

- CLOSED - POST SB21562

28/09/2003

EASA/TCA/FAA/ENAC


Eng. Type:

PW123AF

Eng. S/N. :

AF0094 Manuf. date:

DEC 2006

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS






Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCC Left Engine

I Y TCCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



DELIVERY

I Y TCCA

CF-90-22R1 RAI 91-296

P&WC SB21018R1




DELIVERY

A N TCCA

CF-91-02 -

P&WC SB20946R1


TORQUE FLUCTUATIONS - CLOSED –

N/A DUE TO ENGINE S/N

I Y TCCA

CF-91-26R1 RAI 91-347

P&WC SB20914R3

SB21053 31/03/92 N/A




DELIVERY

S TCCA

CF-92-03R1 RAI 93-284 - - N/A


CASE (ICC)


I Y TCCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC.


DELIVERY

EASA/TCA/FAA/ENAC


Eng. Type:

PW123AF

Eng. S/N. :

AF0094 Manuf. date:

DEC 2006

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS






Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCC Left Engine

A N TCCA

CF-94-01

FAA 94-03-02 Amdt 39-8808

RAI 94-001 P&WC SIL 307

Since 14/01/94



- CLOSED – NOT EFFECTIVE FOR


I Y TCCA

CF-96-22 ENAC 96-353

P&WC SB21077R7 SB21364R1 SB21373R3







A N TCCA

CF-2000-34 FAA 2003-16-04

ENAC 01-065 P&WC

SB 21100R2




FUEL HEATERS



A N TCCA

CF-2002-10 ENAC 02-090

P&WC SB 21914R4

Next shop visit or before 31/12/03


N/A PW118, PW120 and PW121

INTERCOMPRESSOR CASE FIRE


I Y TCCA

CF-2002-34 FAA 2004-20-01

ENAC 02-448





or 23/8/2004


CONTROL UNIT


28/09/2003


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

20070112 Manuff. date:

JAN 2007

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance 200707112

I Y FAA

93-06-06 - H.S.

ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided

transfer tube

- CLOSED – AD COMPLIED WITH

P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420

H.S. ASB 14SF-61-A59R6

SB -67R2/-81R2/-82R1

5000 Hrs (PostMod HS SB

14SF-61-82)

Shaft Torque Check 5000 Hrs.

PCU INSPECTION/ MODIFICATION

OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82.

CHECK COVERED BY O/H PROCEDURE (TTG 1177.30 FH – REF. TO ENG AF0086)

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1

since 09/05/96 300 cycles or within

28/02/97 500 cycles

BLADE INSPECTION / MODIFICATION


BLADE #1 S/N 2007010567

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



BLADE #2 S/N 2007010568

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



BLADE #3 S/N 2007010569

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



BLADE #4 S/N 2007010822


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


JAN 2007

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2

PCU mod –A48 10.500 Hrs

10.500 Hours

CRITICAL PARTS INSPECTION: PCU, TRNSFER TUBE,

ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE INSPECTED DURING LAST

O/H (TTG 633.10 FH)

R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: ACTUATOR INSPECTED DURING LAST

O/H (TTG 633.10 FH)

R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: PCU INSPECTED DURING LAST SHOP VISIT

(TTG 1177.30 FH)

28/09/2003

A N FAA

2006-24-07 Scheda Analisi PA Jan 3, 2007

- CLOSED – NOT APPLICABLE AS PER

PROPELLER MODEL

A N FAA

US-2011-04-02 ENAC 2011-68 ADE issued Apr 15, 2011

NOT APPLICABLE AS PER PROPELLER MODEL


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

20070111 Manuf. date:

JAN 2007

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION




N Not Applicable Y Yes effective pag. 1 of 2

S Superseded N Not effective

Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance 20070111.doc

I Y FAA

93-06-06 - H.S.

ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrated

transfer tube


P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)

Shaft Torque Check 5000 Hrs



CHECK COVERED BY O/H PROCEDURE (TTG 197.10 FH – REF.TO ENG AF0094)

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97

500 cycles up-to incorporating of HS SB 14SF-61-A92



BLADE #1 S/N 2007010564

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




BLADE #2 S/N 2007010565

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



BLADE #3 S/N 2007010566

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



BLADE #4 S/N 2006070373

I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY


O/H (TTG 633.25 FH)


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


JAN 2007

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY


O/H (TTG 633.25 FH)

I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: PCU INSPECTED DURING LAST O/H

(TTG 197.10 FH)

28/09/2003

A N FAA



PROPELLER MODEL

A N FAA




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCC Components Compliance Status

A N FAA

81-21-05 - - Nov 19, 1981 N/A

ARTEX ELT Battery not usable in salt environment

CLOSED: NOT APPLICABLE – SUBJECT ELT BATTERY NOT

INSTALLED

A N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 - N/A N/A

Ni-Cd batterie con celle in polistirolo

CLOSED: NOT APPLICABLE - TEMPERATURE SENSING

INSTALLED ON BATTERIES EMBODIED

S - RAI

82-113 - - - - -

CLOSED: SUPERS. BY ENAC 96-348

N N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782 - N/A N/A Ni-Cd batteries

CLOSED: CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF

FAA 72-19-04

S - RAI

88-052 - - - - - SUPERS. BY ENAC 88-096

R Y RAI

88-096 FAR 43

Appendix E Norma di lavoro

NL-CL-34-06 19/11/2005 24 Months

ALTIMETER AND STATIC PRESSURE SYSTEM

OPEN: TEST CARRIED OUT ON 13/05/2011 (W/O 11/019 ADD 2) (NEXT DUE WITHIN 12/05/2013)

I Y ENAC 96-052

FAA FAR 91.21 - N/A N/A USE OF PORTABLE

ELETTRONIC DEVICES CLOSED: AFM UPDATED – CREW

INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -

Within 500 Hrs (TIS) or 12 mths from 14/11/96


COMBUSTION CHAMBER DECAY TEST (JANITROL)

CLOSED: NOT APPLICABLE - HEATER MODEL B4500

(CERAMIC COMBUSTION TUBE) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N ENAC 97-167

FAA 97-11-10 - - N/A PURITAIN-BENNETT

CREW OXYGEN MASKS

CLOSED: NOT APPLICABLE - SCOTT OXYGEN MASKS

INSTALLED

N N TCCA

CF-95-16 ENAC 97-221

Marathon Power SB 111692-014

27/07/96 N/A PCB SERIES PC-250 MODIFICATION OR

REMOVAL

CLOSED: NOT APPLICABLE AS PER INVERTER INSTALLED

(Serie MSI-800)

N N ENAC 97-274


CREW OXYGEN MASKS

CLOSED: NOT APPLICABLE - AVOX OXYGEN MASKS

INSTALLED

N N ENAC 99-231

FAA 99-08-21 - - N/A

PURITAIN-BENNETT CREW OXYGEN MASKS


INSTALLED

S - ENAC 00-018

FAA 99-23-22 Norma di Lavoro

NL-CL-34-07 Apr 17, 2000 Every 90 days TRANSPONDER MODO

“C” INSPECTION/TEST

CLOSED: SUPERSEDED BY ENAC 00-209

N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686

Engineering Instruction

EI 004/00 18/05/00 N/A

TRANSPONDER MODO “C”

CLOSED: NOT APPLICABLE AD RESCINDED APR. 12, ‘00

SUPERSEDES ENAC 00-018


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


S - ENAC 01-173

FAA 2001-08-01 Scheda Analisi PA May 2, 2001 N/A FUEL SHUT-OFF VALVES

P/N 14D11 o 23D04


A N ENAC 01-368

FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A

FUEL SHUT-OFF VALVES P/N 14D11 o 23D04

P/N installed on A/C: J20C30

CLOSED: NOT APPLICABLE AS PER FUEL SHUT-OFF P/N

INSTALLED Supersedes ENAC 01-173

N N ENAC 01-442

FAA 2001-18-05 - Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.

CLOSED: NOT APPLICABLE PER P/N

I Y ENAC 01-470

FAA 2001-22-14 SoREM

DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER

DISCHARGER

CLOSED: P/N AFFECTED CHECKED. WALTER KIDDE

CARTRIDGES INSTALLED ON

I Y TCCA

CF-2002-14 ENAC 02-167

BOMBARDIER SB215-3108 SB215-4234

SoREM BM-CL-61-4234

04/03/2003 N/A

PROPELLER CONTROL UNIT

BACKUP PRESSURE RELIEF VALVE

CLOSED: SB 215-4234 INCORPORATED

I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


RNZ -850/ -851

CLOSED: NOT APPLICABLE, INU P/N 7510100-732 (#1) AND

7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


28/09/2003

N N FAA

2003-23-05 ENAC 2004-003 ENAC-2004-073

- December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili

CLOSED: NOT APPLICABLE

HOSES INSTALLATI P/N 114040-4

R Y FAA

2004-21-05 Amdt.39-13826

- Scheda Analisi PA DT-CL-21-01

A 500 heater Hrs or 100 heater Hrs TIS

since 19/11/04 (whichever occurs

later)

100 Hrs (TIS) or

24 Months

PRESSURE DECAY TEST ed Operational Test del

CABIN HEATER (JANITROL)

OPEN: HEATER TIME IN SERVICE CHECKED:

60,35 HOURS TEST NOT YET PERFORMED

A N FAA



CLOSED: NOT APPLICABLE AS PER HEATER INSTALLED

R Y EASA

2006-0265 -

Scheda Analisi PA ESP-4-34-001

Within Mar 13, 2007

24 Months MODE “S” and “C”

TRANSPONDERS CHECK

OPEN: CARRIED OUT DURING ANNUAL

CHECK ON 6/6/2011 (W/O 11/019)

NEXT DUE WITHIN 5/06/2013

A N EASA

2006-0269 - Scheda Analisi PA - -

MODE “S” TRANSPONDERS

CLOSED: NOT APPLICABLE AS PER MODEL INSTALLED

A N FAA

2006-18-08 - Scheda Analisi AD Oct. 11, 2006 -

GOODYEAR NOSE WHEEL TIRES

CLOSED: NOT APPLICABLE AS PER

GOODYEAR TIRES NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA

2006-19-04 - Scheda Analisi AD - -


CLOSED: NOT APPLICABLE AS PER PART NUMBER NOT

INSTALLED

N N FAA

2006-22-05 ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU


COMPONENT MODIFIED (REF TO

FAA-2003-04-06)

A N EASA

2006-0366 - Scheda Analisi PA Dec 14, 2006 - LIFE RAFT


AIRCRAFT MODEL

A N EASA

2006-0286R1 - Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders

CLOSED: NOT APPLICABLE: P/N NOT

INSTALLED

A N EASA

2007-0256 - Scheda Analisi PA Sep 19, 2007 - Seat Restraint System


INSTALLED

A N EASA

2007-0294 ENAC 2009-060 Scheda Analisi PA - -

APU Turbine wheel life limit reduction

CLOSED: NOT EFFECTIVE AS PER

APU NOT INSTALLED ON SOREM CL415

FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA

2009-0200 - Scheda Analisi AD Sep 22, 2010 N/A

Navigation – Mode A/C Transponder – Check /

Modification

CLOSED: NOT EFFECTIVE: P/N NOT

INSTALLED

N N FAA

2009-20-10 - Scheda Analisi AD Jan 17, 2010 N/A

Autopilot – servo motors modification

CLOSED: NOT EFFECTIVE AS PER P/N

INSTALLED

S - CF 2009-42 - SOREM ESB-4-32-4414

(SMJC 063)

Part I within 50Fh Part II: within 750 Fc Part III: every 750 Fc

Every 750 Flight cycles

Special Inspection of Accumulator Screw Caps

CLOSED: SUPERSEDED BY CF

2009-42R1 (PART I CARRIED OUT ON NOV

26, 2009)

R Y CF 2009-42R1 - SOREM ESB-4-32-

4414R1 - Every 750 Flight

cycles Special Inspection of

Accumulator Screw Caps

OPEN: AD COVERED BY SMJC-63

PERFORMED ON 20/04/2011 (W/O 11/019 ADD 2) 668 FC TO GO

A N EASA

2009-0251 - Scheda Analisi AD Nov 26, 2009 N/A

Portable Halon 1211 Fire Extinguisher

CLOSED: NOT EFFECTIVE: S/N NOT

INSTALLED

A N EASA

2009-0262R1 Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A


NOT EFFECTIVE: S/N NOT INSTALLED

A N EASA

2009-0278 - Scheda Analisi AD Jan 22, 2010 N/A



INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N TCA

CF-2009-44 - Scheda Analisi AD Jul 01, 2011 N/A

ELT-Potential Failure to Transmit the Required 406MHz Coded Signal


INSTALLED

N N EASA

2010-003R1 - Scheda Analisi AD 18 Apr, 2010 N/A

TDR-94 and TDR-94D transponders

CLOSED: NOT EFFECTIVE : P/N NOT

INSTALLED

Y N EASA

2010-0062R1 - Scheda Analisi AD 14 Apr 2010 N/A


NOT EFFECTIVE: P/N NOT INSTALLED

A Y FAA

2010-07-02 - Scheda Analisi AD 31 Ott 2012 N/A

Honeywell Primus II RNZ 850()/-851

CLOSED INU #1 AND INU #2

ALREADY MODIFIED”

N N EASA

2010-0067 - Scheda Analisi AD 26 Apr, 2010 N/A


CLOSED - NOT EFFECTIVE: P/N NOT

INSTALLED

N N EASA

2010-30 Scheda Analisi SIB N/A N/A

Risks in Transporting Lithium Batteries in Cargo by

Aircraft

CLOSED - NOT APPLICABLE SINCE

INAER FLEET IS NOT OPERATING IN CARGO

TRANSPORT CONFIGURATION

N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer –

Erroneous Airspeed and Altitude Indications

CLOSED - NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N FAA

2011-01-09 Scheda Analisi AD 9/06/2011 N/R

B/E Aerospace protective breathing equipment P/N 119003-11 inspection for

B/A Aerospace S.B. 119003-35-6 compliance.

CLOSED: NOT APPLICABLE AS PER P/N NOT INSTALLED

N N EASA

2011-0043 Scheda Analisi AD 30/04/2013 N/R

Gables Engineering Mode S Transponder Control Panel

Modification


ON THE A/C TYPE

N N EASA


ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement


ON THE A/C TYPE

N N FAA

2011-11-04

Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire

Extinguisher


NOT INSTALLED

N N EASA

2010-0204 ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A



NOT INSTALLED

N N FAA 2011-14-

08 Scheda Analisi AD

Aug 19,2014 or 6500 FH from Aug

19,2011 N/A

B/E Aerospace pax oxy mask inspection


NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCC s/n 2066

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)




Revision n° 1


Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2011-35 - ESB-4-32-A4451 Rev 01

First incorporation: Within 50 Flight Hrs

upon receipt of Bombardier SB 215-

A4451

To be repeated every 165 land landings

Inspection of the MLG Upper Member forward lug using

eddy current method

FIRST INCORPORATION: CLOSED WITH WO

11/183 ON JUL 22, 11; REPETITIVE ACTION:

OPEN; TO GO: 91 LANDINGS

A Y TCCA

CF-2011-35 - ESB-4-32-A4450 Rev 01 November 11, 2011 N/A


liquid penetrant method

OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Delivery Date: Oct 18, 94

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCD Compliance Status

A N FAA

77-17-13 - - - - NLG DOORS


A N FAA

77-13-05 - - - -



A N TCCA

CF-90-11R2 FAA 93-16-06R2



JUNE. 10, 1994 N/A


FLUTTER)


SYSTEM INSTALLED

S TCCA

CF-92-22

FAA 94-04-02 TCCA CF-2003-

02



- N/A ENGINE REAR

MOUNT STRUTS


I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314




CLOSED: AD COMPLIED WITH ENGINE FIRE DETECTION SYSTEM CONNECTED TO AIRCRAFT FIRE WARNING

SYSTEM

I Y FAA

97-11-08 - - - -


LEVERS

CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION

SECTION PAGE 8

A N TCCA

CF-96-02R1 ENAC 1999-268 - - - -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS

PER AIRCRAFT S/N

A N TCCA

CF-2002-14 FAA 2004-26-08

ENAC 02-167


SoREM DT CL-61-4234


PRESSURE VALVE

CLOSED: NOT APPLICABLE AS PER AIRCRAFT AND ENGINE

SERIAL NUMBERS

R N ENAC 00-496


FRAME ANGLES CLOSED: NOT APPLICABLE AS

PER AIRCRAFT S/N

S - FAA

2003-04-06 ENAC 03-067

FAA 2006-22-05

SoREM

DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343


RNZ-850/ -851 CLOSED: SUPERSEDED BY

FAA 2006-22-05

R Y TCCA

CF-2003-02 FAA 2004-10-04

ENAC 03-251





28, 2003




OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 10/080 – 74 FH

TO GO

28/09/2003

R Y FAA

2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA



A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA

2005-18-05 - - - -


REAR SPAR


A N EASA



SWITCHES


N N FAA



REF TO COMPONENTS


R Y TCCA

CF-2008-29 FAA 2009-05-04 ENAC 2008-316

SMJC-60 Mar 8, 2009




PERIOD


OPEN: TO BE CARRIED OUT ON MAR 28,

11 (AD COVERED BY SMJC 60) INAER W.O. 11/017

NEXT DUE WITHIN SEP 27, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2 ENAC 2011-88






01, 2011.

INSPECTION OF THE EMERGENCY WATER

DUMP PULLEY BRACKET AND STRUCTURE

OPEN PART A TO BE ACCOMPLISHED

WITH SMJC-062 PLANNED TERMINATING ACTION PART B INCLUDED IN W.O. 11/017

PERFORMED APR 18, 11

R Y TCCA

CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCD Components Compliance Status

A N FAA

81-21-05 - - Nov 19, 1981 N/A



INSTALLED

A N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 - N/A N/A




S - RAI

82-113 - - - - -


N N TCCA

CF-96-21



FAA 72-19-04

S - RAI

88-052 - - - - - SUPERS. BY ENAC 88-096

R Y RAI

88-096 FAR 43


NL-CL-34-06 19/11/2005 24 Months


OPEN: TEST CARRIED OUT ON JAN 22, 2010 (NEXT DUE WITHIN

JAN 21, 2012)

I Y ENAC 96-052



INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N ENAC 97-167


CREW OXYGEN MASKS


INSTALLED

N N TCCA

CF-95-16 ENAC 97-221



REMOVAL


(Serie MSI-800)

N N ENAC 97-274


CREW OXYGEN MASKS


INSTALLED

N N ENAC 99-231

FAA 99-08-21 - - N/A



INSTALLED

S - ENAC 00-018





N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


EI 004/00 18/05/00 N/A





A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368






N N ENAC 01-442



I Y ENAC 01-470



DISCHARGER



I Y TCCA

CF-2002-14 ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


RNZ -850/ -851


7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


28/09/2003

N N FAA

2003-23-05 ENAC 2004-003 - December 24, 2005 N/A

Titeflex Corporation, Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months




285.54 HOURS TEST NOT YET PERFORMED

A N FAA



CLOSED: NOT APPLICABLE BY

COMPONENT P/N 91E18-1 INSTALLED

R Y EASA

2006-0265 - Scheda Analisi PA

Within Mar 13, 2007


TRANSPONDERS CHECK

OPEN: CARRIED OUT DURING LAST ANNUAL

CHECK W.O. 10/080 NEXT DUE WITHIN

13/06/2012

A N EASA




A N FAA




GOODYEAR TIRES P/N INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA




N N FAA



7510100-731 (#2) INSTALLED

A N EASA



AIRCRAFT MODEL

A N EASA



P/N INSTALLED

A N EASA



P/N INSTALLED

A N EASA





FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA



Modification


INSTALLED

N N FAA




INSTALLED

S - CF 2009-42 - SOREM ESB-4-32-4414

(SMJC 063)




CLOSED: SUPERSEDED BY CF 2009-42R1 (PART I &

PART II CARRIED OUT O DURING THE LAST ANNUAL CHECK W.O.

10/080)

R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight



OPEN: AD COVERED BY SMJC-63 – 664

FLIGHT CYCLES TO GO

A N EASA



CLOSED: NOT EFFECTIVE AS PER S/N

INSTALLED

A N EASA




NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N EASA




INSTALLED

N N TCA




INSTALLED

N N EASA




NOT INSTALLED

Y N EASA

2010-0062 - Scheda Analisi AD 14 Apr 2010 N/A



NOT INSTALLED

A Y FAA



OPEN: APPLICABLE AND EFFECTIVE DUE

TO NEW REQUIREMENTS

NOT YET PERFOMED

N N EASA



NOT EFFECTIVE AS PER P/N NOT INSTALLED

N N EASA



Aircraft

NOT APPLICABLE SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT

CONFIGURATION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________




NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010

N N FAA





N N EASA



Modification


ON THE A/C TYPE

N N EASA

2011-0090R1 ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator


ON THE A/C TYPE

N N EASA




ON THE A/C TYPE

N N FAA

2011-11-04


Extinguisher


NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCD s/n 2003

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA




NOT INSTALLED

N N FAA 2011-14-



19,2011 N/A



NOT INSTALLED

R Y TCCA

CF-2011-35 - ESB-4-32-A4451 Rev 01



A4451



eddy current method

OPEN: FIRST

INCORPORATION NOT YET PERFORMED

A Y TCCA




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Delivery Date: Jan 94

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCE Compliance Status

A N FAA

77-17-13 - - - - NLG DOORS


A N FAA

77-13-05 - - - -



A N TCCA

CF-90-11R2 FAA 93-16-06R2



JUNE. 10, 1994 N/A


FLUTTER)


SYSTEM INSTALLED

S TCCA

CF-92-22

FAA 94-04-02 TCCA CF-2003-

02



- N/A ENGINE REAR

MOUNT STRUTS


I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA

97-11-08 - - - -


LEVERS


SECTION PAGE 8

A N TCCA

CF-96-02R1 ENAC 1999-268 - - - -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS

PER AIRCRAFT S/N

A N TCCA

CF-2002-14 FAA 2004-26-08

ENAC 02-167


SoREM DT CL-61-4234


PRESSURE VALVE


SERIAL NUMBERS

R N ENAC 00-496


FRAME ANGLES CLOSED: NOT APPLICABLE AS

PER AIRCRAFT S/N

S - FAA

2003-04-06 ENAC 03-067

FAA 2006-22-05

SoREM

DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343


RNZ-850/ -851 CLOSED: SUPERSEDED BY

FAA 2006-22-05

R Y TCCA

CF-2003-02 FAA 2004-10-04

ENAC 03-251





28, 2003




OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 11/006 – 128 FH

TO GO

28/09/2003

R Y FAA

2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA



A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA

2005-18-05 - - - -


REAR SPAR


A N EASA



SWITCHES


N N FAA



REF TO COMPONENTS


R Y TCCA

CF-2008-29 FAA 2009-05-04 ENAC 2008-316

SMJC-60 Mar 8, 2009




PERIOD


OPEN: TO BE CARRIED OUT WITH(AD

COVERED BY SMJC 60) INAER W.O. 11/036 ON JUN 13, 11

NEXT DUE WITHIN DEC 12, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2 ENAC 2011-88






01, 2011.



CLOSED PART A ACCOMPLISHED WITH

SMJC-062 TERMINATING ACTION

PERFORMED WITH W.O. 11/006 ON 12/04/11

R Y TCCA

CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



Eng. Type:

PW123AF

Eng. S/N. :

AF0022 Manuf. date: May 1997

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD Compliance Status – Engine 1 AF0022

I Y TCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A


CLOSED: AD COMPLIED WITH AT DELIVERY

I Y RAI

91-296 TCA CF-90-22R1

P&WC SB21018R1




I N TCA

CF-91-02 -

P&WC SB20946R1


TORQUE FLUCTUATIONS CLOSED: NA DUE TO ENGINE S/N

I Y RAI

91-347 TCA CF-91-26R1

P&WC SB20914R3

SB21053 31/03/92 N/A




S RAI

93-284 TCA CF-92-03R1 - - N/A


CASE (ICC)


SUPERSEDED BY CF-92-03R2

I Y TCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC.



Eng. Type:

PW123AF

Eng. S/N. :


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


A N RAI

94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808

P&WC SIL 307 Since 14/01/94



CLOSED: NOT EFFECTIVE FOR ENGINES S/N 109022

AND SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR

TO DELIVERY

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2




FUEL HEATERS

CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036

AND SUBSEQUENT

N N ENAC 02-090

TCA CF-2002-10 P&WC

SB 20914 R4

At the next scheduled engine

shop visit, or before 31 December 2003, whichever occurs

first



CLOSED: N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT

CLOSED: AD COMPLIED WIYH AT DELIVERY

(NO REPEATITIVE ACTION) CKD ON ENG CHK LIST

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0059 Manuf. date: DEC 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


I Y TCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



I Y RAI

91-296 TCA CF-90-22R1

P&WC SB21018R1




I N TCA

CF-91-02 -

P&WC SB20946R1


TORQUE FLUCTUATIONS CLOSED: N/A TO ENGINE S/N

I Y RAI

91-347 TCA CF-91-26R1

P&WC SB20914R3

SB21053 31/03/92 N/A




S RAI

93-284 TCA CF-92-03R1 - - N/A


CASE (ICC)


SUPERSEDED BY CF-92-03R2

I Y TCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC. CLOSED: AD COMPLIED WITH

AT DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0059 Manuf. date: DEC 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


A N RAI

94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808




CLOSED: nOT EFFECTIVE FOR ENGINES S/N 109022 AND

SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





CLOSED: ALL SBs RELATED TO AD EMBODIED PRIOR TO

DELIVERY

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2




FUEL HEATERS CLOSED: NOT APPLICABLE FOR ENGINES S/N 109036 AND SUB’S

N N ENAC 02-090

TCA CF-2002-10 P&WC

SB 20914 R4



first




I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT

CLOSED: AS COMPLIED WITH AT DELIVERY

(NO REPEATITIVE ACTION) CKD ON ENG LIST

28/09/2003


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


Aug 17, 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report prop1 sn 20010616 CE

I Y FAA

93-06-06 - H.S.


transfer tube


P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)




INSPECTED DURING LAST O/H. (every 2000 FH) 1441.44 FH TO GO

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLOSED: NOT APPLICABLE FOR BLADE #1 S/N 890293-

19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLOSED: NOT APPLICABLE FOR BLADE #2 S/N

200007012-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



200108014-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



2005070453

I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY


O/H. (every 2000 FH) 319.15 FH TO GO


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


Aug 17, 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY



I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: PCU INSPECTED DURING LAST O/H..

(every 2000 FH) 1441.44 FH TO GO

A N FAA


CLOSED: NOT APPLICABLE AS PER PROPELLER

MODEL

A N FAA



MODEL


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

930703 Manuf. date:

May 07, 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


I Y FAA

93-06-06 - H.S.


transfer tube

CLÒSED: AD COMPLIED WITH

P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)





A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLÒSED: NOT APPLICABLE FOR BLADE #1 S/N

200106017-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLÒSED: NOT APPLICABLE FOR BLADE #2 S/N

2005070454-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLÒSED: BLADE #3 S/N 882976-19 MODIFIED AS PER ASB 14SF-61-A92R1

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLÒSED: NOT APPLICABLE FOR BLADE #4 S/N 9910026-

19

I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY




Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

930703 Manuf. date:

May 07, 2001

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY


O/H. (every 2000 FH)

1125.09 FH TO GO

I Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: PCU INSPECTED DURING LAST O/H.


A N FAA


CLÒSED: NOT APPLICABLE AS PER PROPELLER

MODEL

A N FAA


CLÒSED: NOT APPLICABLE AS PER PROPELLER

MODEL


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCE Components Compliance Status

A N FAA

81-21-05 - - Nov 19, 1981 N/A



INSTALLED

A N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 - N/A N/A




S - RAI

82-113 - - - - -


N N TCCA

CF-96-21



FAA 72-19-04

S - RAI

88-052 - - - - - SUPERS. BY ENAC 88-096

R Y RAI

88-096 FAR 43


NL-CL-34-06 19/11/2005 24 Months


OPEN TEST CARRIED OUT ON SEP 27, 2010 WITH W.O. 10/319

(NEXT DUE WITHIN SEP 24, 2012)

I Y ENAC 96-052



INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N ENAC 97-167


CREW OXYGEN MASKS


INSTALLED

N N TCCA

CF-95-16 ENAC 97-221



REMOVAL


(Serie MSI-800)

N N ENAC 97-274


CREW OXYGEN MASKS


INSTALLED

N N ENAC 99-231

FAA 99-08-21 - - N/A



INSTALLED

S - ENAC 00-018





N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


EI 004/00 18/05/00 N/A





A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368






N N ENAC 01-442



I Y ENAC 01-470



DISCHARGER



I Y TCCA

CF-2002-14 ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


RNZ -850/ -851


7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


28/09/2003

N N FAA

2003-23-05 ENAC 2004-003 - December 24, 2005 N/A

Titeflex Corporation, Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN: HEATER TIME IN SERVICE CHECKED: 92 HEATER TIME TO GO OR WITHIN 04/03/12

A N FAA





R Y EASA

2006-0265 - Scheda Analisi PA

Within Mar 13, 2007


TRANSPONDERS CHECK


CHECK W.O. 11/006

A N EASA




A N FAA






A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA




N N FAA



7510100-731 (#2) INSTALLED

A N EASA



AIRCRAFT MODEL

A N EASA



P/N INSTALLED

A N EASA



P/N INSTALLED

A N EASA





FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA



Modification


INSTALLED

N N FAA




INSTALLED

S - CF 2009-42 - SOREM ESB-4-32-4414

(SMJC 063)




CLOSED: SUPERSEDED BY CF 2009-42R1 (PART I &

PART II CARRIED OUT O DURING THE LAST ANNUAL CHECK W.O.

10/080)

R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight



OPEN: AD COVERED BY SMJC-63 – OPEN:

TO GO 51 FC

A N EASA




INSTALLED

A N EASA




NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N EASA




INSTALLED

N N TCA




INSTALLED

N N EASA




NOT INSTALLED

Y N EASA

2010-0062 - Scheda Analisi AD 14 Apr 2010 N/A



NOT INSTALLED

A Y FAA




TO NEW REQUIREMENTS

NOT YET PERFOMED”

N N EASA




N N EASA



Aircraft


CONFIGURATION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________




NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010

N N FAA





N N EASA



Modification


ON THE A/C TYPE

N N EASA



ON THE A/C TYPE

N N EASA




ON THE A/C TYPE

N N FAA

2011-11-04


Extinguisher


NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCE s/n 2004

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA




NOT INSTALLED

N N FAA 2011-14-



19,2011 N/A



NOT INSTALLED

R Y TCCA

CF-2011-35 - ESB-4-32-A4451 Rev 01



A4451



eddy current method

OPEN: FIRST

INCORPORATION CARRIED OUT WITH

W.O. 11/186 ON JUL 22, 11

REPETITIVE ACTION WITHIN 131 LL

A Y TCCA




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Delivery Date: Sep 01

EFFE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS EXPIRATION REPETITIVE

ACTIONS DESCRIPTION NOTES (COMPLIANCE DATE)

A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective

Revision n° 1


Date:

Sep 09, 11 Prepared by:

________________________

Approved by:

________________________

I-DPCF Compliance Status

A N FAA 77-17-13

- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N

A N FAA 77-13-05

- - - - MISSING RIVETS IN BULKHEAD


A N TCCA CF-90-11R2 FAA 93-16-06R2



JUNE. 10, 1994 N/A RUDDER-AILERON

INTERCONNECT TAB (TO PREVENT POSSIBILE

FLUTTER)

CLOSED: NOT EFFECTIVE AS PER POWERED AILERON SYSTEM

INSTALLED

S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02



- N/A ENGINE REAR MOUNT STRUTS


I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA 97-11-08

- - - - AFM - LIMITATION SECTION - POWER

LEVERS


SECTION PAGE 8

A N TCCA CF-96-02R1

ENAC 1999-268 - - - - CLOSED: AD ISSUED JUST TO CANCEL PREVIOUS REVISION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AIRCRAFT S/N

A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234

MARCH 04, 2003 N/A PCU BACKUP PRESSURE VALVE


SERIAL NUMBERS

R N ENAC 00-496

FAA 2002-12-12 - - - WING TO FUSELAGE FRAME ANGLES


S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343

March 16, 2003 N/A INU Honeywell Primus II RNZ-850/ -851

CLOSED: SUPERSEDED BY FAA 2006-22-05

R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003




OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 WO 11/246 – 129.04

FH TO GO

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


A N FAA 2004-25-16R1 - Scheda Analisi AD Jan. 05, 2005 N/A


A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05

- - - - LOWER CAPS OF THE

WING FRONT SPAR AND REAR SPAR


A N EASA 2006-0375

- Scheda Analisi AD Dec. 29, 2006 - CARLING

TECHNOLOGIES SWITCHES


N N FAA 2006-22-05

EASA 2006-479 Scheda Analisi AD - N/A INTEGRATED NAVIGATION UNITS

REF TO COMPONENTS Supersedes

FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


OPEN: CARRIED OUT ON APR 05, 11 WITH W.O. 11/045 R1 (AD

COVERED BY SMJC 60) NEXT DUE WITHIN OCT 05, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


R Y TCCA CF-2010-38R2

ENAC 2010-443 Bombardier SB 215 -A4424 Jun 01, 2011




100 FC WITH TERMINATING ACTION NOT LATER THAN 01

Jun 2011.



CLOSED: PART B TERMINATING ACTION PERFORMED WITH W.O. 11/045 R1

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



Eng. Type:

PW123AF

Eng. S/N. :

109083 Manuf. date:

SEPT 1995

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________


I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



DELIVERY

I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A

OIL SYSTEM INSPECTION DUE TO BEARING DETERIORATION

- CLOSED - SB21018 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED WITH

A N TCA CF-91-02

- P&WC SB20946R1 31/10/91 N/A TO PREVENT IN FLIGHT

TORQUE FLUCTUATIONS

- CLOSED – N/A DUE TO ENGINE S/N AD COMPLIED WITH AT

DELIVERY

I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053

31/03/92 N/A TO IMPROVE THE

RETENTION OF THE P2.5/P3 TUBE ASSEMBLY.


S Y RAI 93-284

TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR

CASE (ICC)


I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065

30/06/94 N/A INTERNAL OIL FIRES IN THE ICC.


DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

109083 Manuf. date:

SEPT 1995

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________


I Y RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808

P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A REPLACEMENT HP

TURBINE DISK


DELIVERY

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3







A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2



N/A ENGINE PW100 SERIES FUEL HEATERS



A N ENAC 02-090

TCA CF-2002-10 - CLOSED –

N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT


DELIVERY (NO REPETETIVE ACTION)

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0071 Manuf. date:

JUN 20, 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________

I-DPCF Left Engine

I Y TCCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



DELIVERY

I Y TCCA CF-90-22R1

RAI 91-296 P&WC SB21018 (last R6) 30/06/94 N/A



A N TCCA CF-91-02




I Y TCCA CF-91-26R1

RAI 91-347 P&WC

SB20914 (last R4) SB21053 (last R2)




S TCCA CF-92-03R1

RAI 93-284 - - N/A INTERNAL OIL FIRES INTERCOMPRESSOR

CASE (ICC)


I Y TCCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065



DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0071 Manuf. date:

JUN 20, 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________

I-DPCF Left Engine

A N TCCA CF 94-01

FAA 94-03-02 Amdt 39-8808

RAI 94-001 P&WC SIL 307 Since 14/01/94

1000⇔2000 cycles N/A REPLACEMENT HP TURBINE DISK



I Y TCCA CF-96-22

ENAC 96-353

P&WC SB21077R7 SB21364R1 SB21373R3







A N TCCA CF-2000-34

FAA 2003-16-04 ENAC 01-065

P&WC SB 21100R2






A N TCCA CF-2002-10

ENAC 02-090

P&WC SB 21914R4





- CLOSED – N/A AS PER ENGINE

MODEL

I Y TCCA CF-2002-34

FAA 2004-20-01 ENAC 02-448





or 23/8/2004


CONTROL UNIT

- CLOSED - AD COMPLIED WITH

(NO REPETETIVE ACTION)

28/09/2003


Prop. Type:

Hamilton Sundstrand 14SF-19

Prop. S/N. :


FEBRUARY 19, 1997

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________


I Y FAA 93-06-06 - H.S.

ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrided transfer tube


P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)




CHECK COVERED BY O/H PROCEDURE (TTG 966.08

FH)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles BLADE INSPECTION /

MODIFICATION

- CLOSED – BLADE #1 S/N 882969-19 APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


BLADE #3 S/N 889087-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


BLADE #4 S/N 889089-19


Prop. Type:


Prop. S/N. :


FEBRUARY 19, 1997

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 2


Date:


________________________

Approved by:

________________________


R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2

PCU mod –A48 10.500 Hrs 10.500 Hours

CRITICAL PARTS INSPECTION: PCU, TRANSFER TUBE,

ACTUATOR ASSEMBLY


O/H (TTG 1379.39 FH)

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


CRITICAL PARTS INSPECTION: PCU,

TRNSFER TUBE, ACTUATOR ASSEMBLY


O/H (TTG 1379.39 FH)

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: PCU INSPECTED DURING LAST SHOP VISIT

(TTG 966.08 FH)

28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 - CLOSED –


A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED –



Prop. Type:


Prop. S/N. :

921236 Manuf. date:

FEB 1994

EFFE

CT

P.A. / A.D. Other

Authority issues



A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective pag. 1 of 2 S Superseded N Not effective

Date:


________________________

Approved by:

________________________


I Y FAA 93-06-06 - H.S.

ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1) nitrated transfer tube


P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)

Shaft Torque Check 5000 Hrs




FH)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


BLADE #3 S/N 200006034-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


BLADE #4 S/N 200107038-19

I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H (TTG 800.19 FH)


Prop. Type:


Prop. S/N. :

921236 Manuf. date:

FEB 1994

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H (TTG 800.19 FH)

I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: PCU INSPECTED DURING LAST O/H

(TTG 16.45 FH)

28/09/2003

A N FAA 2006-24-07



A N FAA US-2011-04-02




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________

I-DPCF Components Compliance Status

A N FAA 81-21-05

- - Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment


INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 - N/A N/A Ni-Cd batterie con celle in

polistirolo



S - RAI 82-113

- - - - - CLOSED: SUPERS. BY ENAC 96-348

N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052

- - - - - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E

Norma di lavoro NL-CL-34-06 19/11/2005 24 Months ALTIMETER AND STATIC

PRESSURE SYSTEM OPEN: TEST CARRIED OUT ON

FEB 27, 2010 (NEXT DUE WITHIN FEB 25, 2012)

I Y ENAC 96-052

FAA FAR 91.21 - N/A N/A USE OF PORTABLE ELETTRONIC DEVICES

CLOSED: AFM UPDATED – CREW INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


N N ENAC 97-167

FAA 97-11-10 - - N/A PURITAIN-BENNETT CREW OXYGEN MASKS


INSTALLED

N N TCCA CF-95-16

ENAC 97-221 Marathon Power SB 111692-014 27/07/96 N/A

PCB SERIES PC-250 MODIFICATION OR

REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231


CREW OXYGEN MASKS CLOSED: NOT APPLICABLE -

SCOTT OXYGEN MASKS INSTALLED

S - ENAC 00-018

FAA 99-23-22 Norma di Lavoro NL-CL-34-07 Apr 17, 2000 Every 90 days


INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686

Engineering InstructionEI 004/00 18/05/00 N/A TRANSPONDER MODO

“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368

FAA 2001-17-13 Scheda Analisi PA Aug 28, 2001 N/A FUEL SHUT-OFF VALVES

P/N 14D11 o 23D04 P/N installed on A/C: J20C30



N N ENAC 01-442



I Y ENAC 01-470

FAA 2001-22-14 SoREM DT CL-26-02 Jun 10, 2003 N/A FIRE EXTINGUISHER

DISCHARGER CLOSED: P/N AFFECTED

CHECKED. WALTER KIDDE CARTRIDGES INSTALLED ON

I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343

March 16, 2003 N/A INU Honeywell Primus II RNZ -850/ -851


7510100-731 (#2) INSTALLED

28/09/2003

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N FAA 2003-23-05

ENAC 2004-003 ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months









R Y EASA 2006-0265 - Scheda Analisi PA

ESP-4-34-001 Within

Mar 13, 2007 24 Months MODE “S” and “C” TRANSPONDERS CHECK

OPEN: CARRIED OUT WITH ON FEB 27, 2010. NEXT DUE WITHIN FEB

25, 2012

A N EASA 2006-0269

- Scheda Analisi PA - - MODE “S” TRANSPONDERS


A N FAA 2006-18-08 - Scheda Analisi AD Oct. 11, 2006 - GOODYEAR

NOSE WHEEL TIRES



EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04

- Scheda Analisi AD - - MODE “S” TRANSPONDERS


N N FAA 2006-22-05

ENAC 2006-479 Scheda Analisi AD Dec 1, 2006 N/A Honeywell Primus INU


7510100-731 (#2) INSTALLED

A N EASA 2006-0366

- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT CLOSED: NOT

APPLICABLE AS PER AIRCRAFT MODEL

A N EASA 2006-0286R1

- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders CLOSED: NOT

APPLICABLE AS PER P/N INSTALLED

A N EASA 2007-0256

- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System CLOSED: NOT


A N EASA 2007-0294

ENAC 2009-060 Scheda Analisi PA - - APU Turbine wheel life limit reduction



FLEET

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200

- Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /

Modification


INSTALLED

N N FAA 2009-20-10

- Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification


INSTALLED

S - CF 2009-42 - SOREM ESB-4-32-4414 (SMJC 063)

Part I within 50Fh Part II: within 750 Fc

Part III: every 750 Fc



CLOSED: SUPERSEDED BY CF 2009-42R1 (PART

I CARRIED OUT ON NOV 26, 2009)

R Y CF 2009-42R1 Enac 2010-183 FAA 2011-03-08

SOREM ESB-4-32-4414R1 - Every 750 Flight




PERFORMED ON FEB 19, 02– 541 FLIGHT

CYCLES TO GO

A N EASA 2009-0251

- Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher


INSTALLED

A N EASA 2009-0262R1

Enac 2010-33 Scheda Analisi AD Feb 10, 2010 N/A Portable Halon 1211 Fire Extinguisher

NOT EFFECTIVE AS PER S/N NOT INSTALLED

A N EASA 2009-0278

- Scheda Analisi AD Jan 22, 2010 N/A Portable Halon 1211 Fire Extinguisher


INSTALLED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N TCA CF-2009-44

- Scheda Analisi AD Jul 01, 2011 N/A ELT-Potential Failure to Transmit the Required 406MHz Coded Signal


INSTALLED

N N EASA 2010-003R1

- Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders


NOT INSTALLED

Y N EASA 2010-0062R1

- Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher


A Y FAA 2010-07-02

- Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851


TO NEW REQUIREMENTS

NOT YET PERFOMED”

N N EASA 2010-0067



N N EASA 2010-30

Scheda Analisi SIB N/A N/A Risks in Transporting

Lithium Batteries in Cargo by Aircraft


CONFIGURATION



NOT APPLICABLE AS PER A/C TYPE, REFER

TO ADE ISSUED DATED NOV 09, 2010

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N FAA 2011-01-09

Scheda Analisi AD 9/06/2011 N/R



NOT APPLICABLE AS PER P/N NOT INSTALLED

N N EASA 2011-0043

Scheda Analisi AD 30/04/2013 N/R Gables Engineering Mode S Transponder Control Panel

Modification


P/N NOT INSTALLED ON THE A/C TYPE

N N EASA 2011-0090R1

ENAC 2011-202 Scheda Analisi AD 27/07/2011 N/R Oxygen mask regulator CLOSED: NOT

APPLICABLE AS PER P/N NOT INSTALLED ON

THE A/C TYPE

N N EASA 2011-0103

Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas

P/N 21-41 ( ) series Mod/Replacement



N N FAA

2011-11-04

Scheda Analisi AD 14 Apr 2010 N/A Portable Halon 1211 Fire Extinguisher


NOT INSTALLED

N N EASA 2010-0204

ENAC 2011-164 Scheda Analisi AD Oct 20, 2010 N/A TDR-94 and TDR-94D transponders


NOT INSTALLED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCF s/n 2059

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N FAA 2011-14-08

Scheda Analisi AD Aug 19,2014 or

6500 FH from Aug 19,2011

N/A B/E Aerospace pax oxy mask inspection


NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451


Inspection of the MLG Upper Member forward lug using eddy current method

FIRST INCORPORATION:

CLOSED (REF TO WO 11/187);

REPETITIVE ACTION: OPEN; TO GO: 70

LANDINGS

A Y TCCA CF-2011-35

- ESB-4-32-A4450 Rev 01 November 11, 2011 N/A

Inspection of the MLG Upper Member forward lug

using liquid penetrant method

OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Delivery Date: Apr 04

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Compliance Status

A N FAA 77-17-13


A N FAA 77-13-05



A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)


INSTALLED

S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02





I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA 97-11-08


LEVERS


SECTION PAGE 8

A N TCCA CF-96-02R1



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234



SERIAL NUMBERS

R N ENAC 00-496



S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003


FOLLOWED BY INAER SMJC #31 and #32


OPEN: INSPECTION COVERED BY INAER SMJC 31 AND 32 AND

CARRIED OUT WITH W.O. 11/283 (NEXT DUE WITHIN 147.40 FH)

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

OPEN: HEATER TIME IN SERVICE CHECKED ON AUG 05, 2010:

96.53 HOURS TEST NOT YET PERFORMED REF

TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




A N EASA 2006-0375




N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


OPEN: COVERED BY SMJC 60 PERFORMED WITH WO 11/022

NEXT DUE ON NOV 11, 2011


Eng. Type:

PW123AF

Eng. S/N. :

AF0024 Manuf. date:

SEPTEMBER 1993

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Left Engine

I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A


CLOSED: FUEL PUMP P/N: 5008269H INSTALLED (Post

SB21360) AD COMPLIED WITH

I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A


CLOSED: SB21018 EMBODIED AS PER BUILD SPEC 723. AD COMPLIED

WITH

A N TCA CF-91-02


TORQUE FLUCTUATIONS CLOSED: N/A DUE TO

ENGINE S/N

I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053



CLOSED: SB21053 EMBODIED AS PER BUILD

SPEC 723. AD COMPLIED WITH

S RAI 93-284


CASE (ICC)

CLOSED: SUPERSEDED BY TCA CF-92-03R2

I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065


CLOSED: SBs EMBODIED AS PER BUILD SPEC 723.


Eng. Type:

PW123AF

Eng. S/N. :

AF0024 Manuf. date:

SEPTEMBER 1993

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Left Engine

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK

CLOSED: HP DISK P/N: 3041511 INSTALLED. AD COMPLIED WITH

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





CLOSED: FUEL NOZZLES OVERHAULED DURING

LAST SHOP VISIT. SB21373 INTRODUCED.

AD COMPLIED WITH

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2





AND SUB’S

A N ENAC 02-090

TCA CF-2002-10 P&WC SB 21914R4






I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT



28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

109041 Manuf. date:

SEPTEMBER 1993

EFFE

CT

A.D. PA-ENAC ISSUED DOCUMENTS EXPIRATION REPETITIVE



Date:


________________________

Approved by:

________________________

I-DPCH Right Engine

I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A


CLOSED: FUEL PUMP P/N: 5008269H INSTALLED (Post

SB21360 AD COMPLIED WITH

I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A




A N TCA CF-91-02



ENGINE S/N

I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053





S - RAI 93-284


CASE (ICC)


I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065


CLOSED: SBs EMBODIED AS PER BUILD SPEC 723.

AD COMPLIED WITH


Eng. Type:

PW123AF

Eng. S/N. :

109041 Manuf. date:

SEPTEMBER 1993

EFFE

CT

A.D. PA-ENAC ISSUED DOCUMENTS EXPIRATION REPETITIVE



Date:


________________________

Approved by:

________________________

I-DPCH Right Engine

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK

CLOSED: HP DISK P/N: 3041511

INSTALLED. AD COMPLIED WITH

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





CLOSED: FUEL NOZZLES OVERHAULED DURING

LAST SHOP VISIT. SB21373 INTRODUCED.

AD COMPLIED WITH

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2





AND SUB’S

A N ENAC 02-090

TCA CF-2002-10 P&WC SB 21914R4






I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT



28/09/2003


Prop. Type:


Prop. S/N. :

960340 Manuf. date:

MARCH 1996

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Right Propeller

I Y FAA 93-06-06 - H.S.



P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN: PCU HOURS: 1469.58 INSPECTION PERFORMED

EVERY O/H AD COMPLIED WITH

(NEXT DUE WITHIN 530.02)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION CLOSED: NOT APPLICABLE

FOR BLADE #1 S/N 889085-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

CLOSED: BLADE #2 S/N 880302-19 MODIFIED (ref to

SISAM DECLARATION) AD COMPLIED WITH

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #3 S/N 200010014-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #4 S/N 2009040360-19


Prop. Type:


Prop. S/N. :

960340 Manuf. date:

MARCH 1996

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Right Propeller

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE HOURS: (TSO): 758.00

INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)

AD COMPLIED WITH (NEXT DUE WITHIN 1242.00)

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: ACTUATOR HOURS (TSO): 758.00



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: PCU HOURS (TSN): 1469.58



28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE

AS PER PROPELLER MODEL

A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE



Prop. Type:


Prop. S/N. :


JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Left Propeller

I Y FAA 93-06-06 - H.S.


CLOSED: AD COMPLIED WITH P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN: PCU HOURS: 1469.58

INSPECTION PERFORMED EVERY O/H


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #1 S/N 2009050173-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #2 S/N 2009050174-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #3 S/N 2009040361-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #4 S/N 2009050175-19


Prop. Type:


Prop. S/N. :


JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE HOURS: TSO: N/A; TTSN:

758.00 INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)


R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: ACTUATOR HOURS TSO: N/A; TTSN: 758.00



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY




28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL

A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL


Prop. Type:


Prop. S/N. :


JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCH Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052


R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM OPEN: CARRIED OUT DURING LAST ANNUAL CHECK (W.O.

11/022). NEXT DUE WHITIN 3/06/13

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231




S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470




I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


CLOSED: INU#1 #2 REPLACED ON 08/04/04

W/O SOREM 04/028 NOTIFIED TO THE CREW – INFO

INSERTED IN AFM

28/09/2003


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N FAA 2003-23-05

ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation, Tubi Flessibili



N N FAA 2003-23-05




R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN: HEATER TIME IN SERVICE CHECKED ON

AUG 05, 2010: 96.53 HOURS

TEST NOT YET PERFORMED






ESP-4-34-001 Within


OPEN: COVERED BY ANN-AT-10

(REF W.O. 11/022)

A N EASA 2006-0269




NOSE WHEEL TIRES




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04



N N FAA 2006-22-05



7510100-731 (#2) INSTALLED

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256



A N EASA 2007-0294




FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED








R Y CF 2009-42R1 - SOREM ESB-4-32-

4414R1 (SMJC 063)





OPEN: COVERED BY SOREM ESB-4-32-4414

(SMJC 063; PERF. WITH WO 11/022)

616 CYCLES TO GO

A N EASA 2009-0251



INSTALLED

Y N EASA 2009-0262R1


CLOSED:NOT EFFECTIVE AS PER S/N

NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA

2010-0062R1



NOT INSTALLED

A Y FAA 2010-07-02

- Scheda Analisi AD 31 Oct 2012 N/A Honeywell Primus II RNZ 850()/-851

OPEN: INU #1 AND INU #2 TO

BE PERFORMED

N N EASA 2010-0067



NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2010-30

Scheda Analisi SIB N/A N/A Risks in Transporting Lithium Batteries in Cargo by Aircraft

CLOSED: NOT APPLICABLE SINCE

SOREM FLEET IS NOT OPERATING IN CARGO


N N CF-2010-37 Enac 2010-397 Scheda Analisi AD N/A N/A Air Data Computer – Erroneous Airspeed and Altitude Indications

CLOSED: NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010

N N FAA 2011-01-09


B/E Aerospace protective breathing equipment P/N 119003-11 inspection for B/A Aerospace S.B. 119003-35-6 compliance.


N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE

N N EASA 2011-0103

Scheda Analisi AD 03/12/2011 N/R ELT TRI-BAND Antennas P/N 21-41 ( ) series Mod/Replacement




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCH s/n 2062

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08

Scheda Analisi AD Aug 19,2014 or 6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01

First incorporation:

Within 50 Flight Hrs upon receipt of Bombardier SB 215-A4451

To be repeated every 165 land

landings

Inspection of the MLG Upper Member forward lug using eddy

current method




LANDINGS

A Y TCCA CF-2011-35

- ESB-4-32-A4450 Rev 01

November 11, 2011 N/A

Inspection of the MLG Upper Member forward lug using liquid

penetrant method OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Delivery Date: May 01

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Compliance Status

A N FAA 77-17-13


A N FAA 77-13-05



A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)


INSTALLED

S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02





I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA 97-11-08


LEVERS


SECTION PAGE 8

A N TCCA CF-96-02R1



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234



SERIAL NUMBERS

R N ENAC 00-496



S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003





FH TO GO

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




A N EASA 2006-0375




N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


OPEN: CARRIED OUT WITH W.O. 11/002

(AD COVERED BY SMJC 60) NEXT DUE WITHIN SET 30, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________








01, 2011.



CLOSED: PART A TO BE ACCOMPLISHED WITH SMJC-062

(W.O. 10/269) TERMINATING ACTION PART B PERFORMED

WITH W.O. 11/011

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



Eng. Type:

PW123AF

Eng. S/N. :

AF0087 Manuf. date:

AUGUST 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Right Engine

I Y TCA CF-90-21 -

P&WC SB20355 (last R1) SB20897 (last R3)

30/04/91 N/A O-RING DETERIORATION

DURING FUEL FILTER COVER INSTALLATION


AT DELIVERY

I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018 (last R6) 30/06/94 N/A



AT DELIVERY

A N TCA CF-91-02

- P&WC SB20946 (last R2) 31/10/91 N/A TO PREVENT IN FLIGHT


ENGINE S/N

I Y RAI 91-347

TCA CF-91-26R1 P&WC





AT DELIVERY

S - RAI 93-284


CASE (ICC)


I Y TCA CF-92-03R2

- P&WC

SB20957 (last R5) SB20962 (last R4) SB21065 (last R7)



AT DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0087 Manuf. date:

AUGUST 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Right Engine

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK


AND SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077 (last R8) SB21364 (last R1) SB21373 (last R3)





CLOSED: ALL SBs RELATED TO AD EMBODIED

AD COMPLIED WITH

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB21100 (last R3)





AND SUBSEQUENT

A N ENAC 02-090

TCA CF-2002-10 P&WC SB 21914R4






I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT


AT DELIVERY (NO REPETETIVE ACTION)

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0081 Manuf. date:

JAN 27, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Left Engine

I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A



A N TCA CF-91-02



ENGINE S/N

I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053




S - RAI 93-284


CASE (ICC)


I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065




Eng. Type:

PW123AF

Eng. S/N. :

AF0081 Manuf. date:

JAN 27, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Left Engine

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK


AND SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





CLOSED: ALL SBs RELATED TO AD EMBODIED

AD COMPLIED WITH

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2





AND SUB’S

A N ENAC 02-090

TCA CF-2002-10 P&WC SB 21914R4






I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT



28/09/2003


Prop. Type:


Prop. S/N. :

971016 Manuf. date:

OCT 1997

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI right propeller

I Y FAA 93-06-06 - H.S.



P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82


FH)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #1 S/N 890287-19

N/A AS PER SERIAL NUMBER

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #2 S/N 890289-19


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #3 890290-19 N/A AS PER SERIAL

NUMBER

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #4 2007010560-19



Prop. Type:


Prop. S/N. :

971016 Manuf. date:

OCT 1997

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI right propeller

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H (every 2000 Fh) TTG 1488.30 FH

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H. (every 2000 Fh) TTG 1488.30 FH

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: PCU INSPECTED DURING LAST SHOP VISIT.

(every 2000 Fh) TTG 626.07 FH

28/09/2003

A N FAA 2006-24-07



A N FAA US-2011-04-02




Prop. Type:


Prop. S/N. :


AUG 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI left propeller

I Y FAA 93-06-06 - H.S.



P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN: PCU COMPLIANT WITH HS-SB14SF-61-82


FH)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #1 S/N 880300

APPLIED FINAL MODIFICATION HS SB 14SF-61-A92 BY SISAM

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #2 S/N 200105011


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED – BLADE #3 S/N 200108013


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION




Prop. Type:


Prop. S/N. :


AUG 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI left propeller

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H (every 2000 Fh) TTG 415.12 FH

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





O/H. (every 2000 Fh) TTG 415.12 FH

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2





(every 2000 Fh) TTG 162.52 FH

28/09/2003

A N FAA 2006-24-07



A N FAA US-2011-04-02




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCI Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052

- - - - - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM

OPEN TEST CARRIED OUT ON LH&RH ALTIMETER ON JUL

22,2011WITH W.O. 11/011 R1. (NEXT DUE WITHIN JUL 21, 2013)

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231




S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470




I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


28/09/2003

N N FAA 2003-23-05


Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN: NEW HEATER INSTALLED DURING

ANNUAL CHECK W.O. 11/011 R1. TIME IN

SERVICE CHECKED: 0 HOURS. TEST NOT YET

PERFORMED





R Y EASA 2006-0265 - Scheda Analisi PA Within



CHECK W.O. 11/011 R1. NEXT DUE JUL 21, 2013

A N EASA 2006-0269




NOSE WHEEL TIRES




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04



N N FAA 2006-22-05



7510100-731 (#2) INSTALLED

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256



A N EASA 2007-0294




FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED







I & PART II CARRIED OUT O DURING THE

LAST ANNUAL CHECK W.O. 10/080)

R Y CF 2009-42R1 - ESB-4-32-4414R1 - Every 750 Flight cycles


OPEN: AD COVERED BY SMJC-63 – OPEN:

TO GO 486 FC

A N EASA 2009-0251



INSTALLED

A N EASA 2009-0262R1



NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


A N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA 2010-0062



NOT INSTALLED

A Y FAA 2010-07-02

- Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851


TO NEW REQUIREMENTS

NOT YET PERFOMED”

N N EASA 2010-0067



N N EASA 2010-30




CONFIGURATION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________






N N FAA 2011-01-09





N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE

N N EASA 2011-0103





N N FAA

2011-11-04



N N EASA 2010-0204



NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCI s/n 2058

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N FAA 2011-14-08


6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451




CLOSED (REF TO WO 11/011 R1);


LANDINGS

A Y TCCA CF-2011-35




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009


EFFE

CT

P.A. / A.D. Other

Authority issues



A Applicable (to be Incorp.) D Deleted R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective Pag. 1 of 4 S Superseded N Not effective

Date:

Sept 09, 11 Prepared by:

________________________

Approved by:

________________________

I-DPCO Compliance Status

A N FAA 77-17-13

- - - - NLG DOORS - CLOSED -

NOT APPLICABLE AS PER AIRCRAFT S/N

A N FAA 77-13-05


- CLOSED - NOT APPLICABLE AS PER

AIRCRAFT S/N

A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)

- CLOSED - NOT EFFECTIVE AS PER

POWERED AILERON SYSTEM INSTALLED

S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02




- CLOSED – SUPERSEDED BY

AD CF-2003-02

I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314






SYSTEM

I Y FAA 97-11-08


LEVERS

- CLOSED - AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION

PAGE 8

A N TCCA CF-96-02R1

ENAC 1999-268 - - - - - CLOSED -

AD ISSUED JUST TO CANCEL PREVIOUS REVISION


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES - CLOSED -


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234



AIRCRAFT AND ENGINE SERIAL NUMBERS

R N ENAC 00-496



AIRCRAFT S/N

S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


- CLOSED - SUPERSEDED BY

FAA 2006-22-05

R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003




- OPEN - COVERED SMJC 31 & SMJC 32 –

NEXT DUE: WITHIN 217.23 FH

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




AIRCRAFT S/N

A N EASA 2006-0375



- CLOSED - NOT APPLICABLE AS PER AD

EFFECTIVITY

N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


- OPEN - CARRIED OUT DURING LAST ANNUAL CHECK W.O. 11/018

NEXT DUE: WITHIN SEP 26, 2011


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2






01, 2011.



CLOSED ESB-4-42-A4424 PART B TERMINATING ACTION

PERFORMED ON 15/02/2011 REF. WO 11/018

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;



LIQUID PENETRANT & EDDY CURRENT INSPECTION ON

MLG UPPER MEMBER FORWARD LUG

OPEN


Eng. Type:

PW123AF

Eng. S/N. :

109073 Manuf. date:

DECEMBER 1994

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Engine 109073 - I-DPCO RH.doc

I Y TCA CF-90-21

- P&WC




- CLOSED- AD COMPLIED BY

SB20355 AND SB20897 INCORPORATION

PRIOR TO DELIVERY (SEE ENGINE TECHNICAL LOG)

I Y TCA CF-91-02


TORQUE FLUCTUATIONS


SB20946 INCORPORATION PRIOR TO DELIVERY

(SEE ENGINE TECHNICAL LOG)

I Y RAI 91-296






I Y RAI 91-347

TCA CF-91-26R1 P&WC







I Y TCA

CF-92-03R2 Supersedes RAI 93-284

-


30/06/94 N/A INTERNAL OIL FIRES INTERCOMPRESSOR

CASE (ICC)


SB20957, SB20962 AND SB21065 INCORPORATION


S RAI 93-284


CASE (ICC)

SUPERSEEDED BY

TCA CF-92-03R2


Eng. Type:

PW123AF

Eng. S/N. :

109073 Manuf. date:

DECEMBER 1994

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Engine 109073 - I-DPCO RH.doc

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808

P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A

REPLACEMENT HIGH PRESSURE TURBINE DISK (APPLICABLE TO ENGINE

INCORPORATING HPT DISK P/N 3035711 OR 3038411)

- CLOSED- NOT APPLICABLE

DUE TO INSTALLED HPT DISK P/N DIFFERENT TO THE ONES

INTO EFFECTIVITY (SEE ENGINE TECHNICAL LOG)

I Y ENAC 96-353

TCA CF-96-22


First nozzle replacement or within

30/11/98 whichever occurs first



- CLOSED- AD COMPLIED-WITH


A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04





- CLOSED- NOT APPLICABLE FOR ENGINES

S/N 109036 AND SUBS

N N ENAC 02-090

TCA CF-2002-10 - - - - NOT APPLICABLE AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01

P&WC SB21669

(INSPECTION)

P&WC SB21562 (last R2) (MODIFICATION)

SOREM DT-CL-73-04

400 F/H

1200 F/H (REPETITIVE INSPECTION)

4500 F/H

(FINAL MODIFICATION)


CONTROL UNIT

- CLOSED- FINAL MODIFICATION COMPLIED

BY SB21562 INCORPORATION (SEE ENGINE TECHNICAL LOG)

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0009 Manuf. date:

OCTOBER 1996

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Engine AF0009 - I-DPCO LH.doc

I Y TCA CF-90-21

- P&WC







I Y TCA CF-91-02


TORQUE FLUCTUATIONS




I Y RAI 91-296






I Y RAI 91-347

TCA CF-91-26R1 P&WC







I Y TCA

CF-92-03R2 Supersedes RAI 93-284

-


30/06/94 N/A INTERNAL OIL FIRES INTERCOMPRESSOR

CASE (ICC)




S RAI 93-284


CASE (ICC)

SUPERSEDED BY

TCA CF-92-03R2


Eng. Type:

PW123AF

Eng. S/N. :

AF0009 Manuf. date:

OCTOBER 1996

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Engine AF0009 - I-DPCO LH.doc

A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808

P&WC SIL 307 Since 14/01/94 1000⇔2000 cycles N/A

REPLACEMENT HIGH PRESSURE TURBINE DISK (APPLICABLE TO ENGINE

INCORPORATING HPT DISK P/N 3035711 OR 3038411)

- CLOSED- NOT APPLICABLE

DUE TO INSTALLED HPT DISK P/N DIFFERENT TO THE ONES

INTO EFFECTIVITY (SEE ENGINE TECHNICAL LOG)

I Y ENAC 96-353

TCA CF-96-22


First nozzle replacement or within

30/11/98 whichever occurs first



- CLOSED- AD COMPLIED-WITH


A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04





- CLOSED- NOT APPLICABLE FOR ENGINES

S/N 109036 AND SUBS

N N ENAC 02-090

TCA CF-2002-10 - - - - NOT APPLICABLE AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01

P&WC SB21669

(INSPECTION)

P&WC SB21562 (last R2) (MODIFICATION)

SOREM DT-CL-73-04

400 F/H

1200 F/H (REPETITIVE INSPECTION)

4500 F/H

(FINAL MODIFICATION)


CONTROL UNIT

- CLOSED- FINAL MODIFICATION COMPLIED

BY SB21562 INCORPORATION (SEE ENGINE TECHNICAL LOG)

28/09/2003


Prop. Type:


Prop. S/N. :

991013 Manuf. date:

OCTOBER 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Propeller 991013 - I-DPCO.doc

I Y FAA 93-06-06

- H.S. ASB 14SF-61-A61 06/09/93 N/A TITANIUM (A1)

nitrided transfer tube

- CLOSED- COMPLIED-WITH

AS PER TRANSFER TUBE P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1

5000 Hrs TIS (Post

HS SB 14SF-61-82)

5000 Hrs TIS (Post

HS SB 14SF-61-82) PCU TORQUE CHECK

- OPEN- INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)

242.41 F/H TO GO

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97



- CLOSED- NOT APPLICABLE FOR

BLADE #1 S/N 9910014-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




BLADE #2 S/N 9910015-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




BLADE #3 S/N 9910016-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97




BLADE #4 S/N 9910017-19

I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




- OPEN- TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH

(prop. O/H) 226.32 F/H TO GO


Prop. Type:


Prop. S/N. :

991013 Manuf. date:

OCTOBER 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - Propeller 991013 - I-DPCO.doc

I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




- OPEN- ACTUATOR INSPECTION

SCHEDULED EVERY 2000 FH (prop. O/H)

226.32 F/H TO GO

I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




- OPEN- PCU INSPECTION


242.41 F/H TO GO 28/09/2003

A N FAA 2006-24-07

- - Jan 3, 2007 - - - CLOSED-


A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 - CLOSED -



Prop. Type:


Prop. S/N. :

941009 Manuf. date:

OCTOBER 1994

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCD Left Propeller

I Y FAA 93-06-06 - H.S.



P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN: PCU INSPECTION PERFORMED EVERY O/H


A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #1 S/N 2009060223-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #1 S/N 2009081091-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #3 S/N 2009060219-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




FOR BLADE #4 S/N 2009031495-19


Prop. Type:


Prop. S/N. :

941009 Manuf. date:

OCTOBER 1994

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCD Left Propeller

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: TRANSFER TUBE HOURS: (TSO): 428.24


AD COMPLIED WITH (NEXT DUE WITHIN: 1571.36)

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: ACTUATOR HOURS (TSO): 428.24



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




OPEN: PCU HOURS (TSO): 847.40



28/09/2003

A N FAA 2006-24-07



A N FAA US-2011-04-02




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCO Components Compliance Status

A N FAA 81-21-05


-CLOSED- NOT APPLICABLE – SUBJECT ELT

BATTERY NOT INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo

-CLOSED- NOT APPLICABLE -

TEMPERATURE SENSING INSTALLED ON BATTERIES

EMBODIED

S - RAI 82-113

- - - - - -CLOSED- : SUPERS. BY ENAC 96-348

N N TCCA CF-96-21


-CLOSED- CF96-21 ISSUED TO CANCEL THE

APPLICABILITY OF FAA 72-19-04

S - RAI 88-052

- - - - - -CLOSED- SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM

-OPEN- CARRIED OUT DURING LAST ANNUAL CHECK W.O. 11/018;

NEXT DUE: WITHIN APR 25, 2013

I Y ENAC 96-052


-CLOSED- AFM UPDATED – CREW

INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -





HEATER MODEL B4500 (CERAMIC COMBUSTION TUBE)

INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N ENAC 97-167




N N TCCA CF-95-16



REMOVAL

-CLOSED- NOT APPLICABLE AS PER

INVERTER INSTALLED (Serie MSI-800)

N N ENAC 97-274




N N ENAC 99-231


CREW OXYGEN MASKS



S - ENAC 00-018



INSPECTION/TEST

-CLOSED- SUPERSEDED BY ENAC 00-209

N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”

-CLOSED- NOT APPLICABLE

AD RESCINDED APR. 12, ‘00



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04

-CLOSED- SUPERSEDED BY ENAC 01-368

A N ENAC 01-368



-CLOSED- NOT APPLICABLE AS PER FUEL

SHUT-OFF P/N INSTALLED Supersedes ENAC 01-173

N N ENAC 01-442


-CLOSED- NOT APPLICABLE PER P/N

I Y ENAC 01-470


DISCHARGER

-CLOSED- P/N AFFECTED CHECKED.

WALTER KIDDE CARTRIDGES INSTALLED ON

I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A



-CLOSED- SB 215-4234 INCORPORATED

I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


-CLOSED- NOT APPLICABLE, INU P/N

7510100-732 (#1) AND 7510100-731 (#2) INSTALLED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


28/09/2003

N N FAA 2003-23-05

ENAC 2004-003 Enac 2004-073 - December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili

-CLOSED- NOT APPLICABLE


R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



-OPEN- HEATER TIME IN

SERVICE CHECKED: 238.36 HOURS TEST NOT YET PERFORMED



-CLOSED- NOT APPLICABLE BY



ESP-4-34-001 Within


-OPEN- CARRIED OUT DURING LAST ANNUAL CHECK

W.O. 11/018; NEXT DUE: WITHIN APR

27, 2013

A N EASA 2006-0269


-CLOSED- NOT APPLICABLE AS

PER MODEL INSTALLED


NOSE WHEEL TIRES


PER GOODYEAR TIRES P/N

INSTALLED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04



PER MODEL INSTALLED

N N FAA 2006-22-05


-CLOSED- NOT APPLICABLE, INU P/N 7510100-732 (#1) AND 7510100-731 (#2)

INSTALLED

A N EASA 2006-0366

- Scheda Analisi PA Dec 14, 2006 - LIFE RAFT -CLOSED-

NOT APPLICABLE AS PER AIRCRAFT MODEL

A N EASA 2006-0286R1

- Scheda Analisi PA Sep 9, 2006 - Oxygen Cylinders -CLOSED-

NOT APPLICABLE AS PER P/N INSTALLED

A N EASA 2007-0256

- Scheda Analisi PA Sep 19, 2007 - Seat Restraint System -CLOSED-

NOT APPLICABLE AS PER P/N INSTALLED

A N EASA 2007-0294


-CLOSED- NOT EFFECTIVE AS

PER APU NOT INSTALLED ON SOREM

CL415 FLEET

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200


Modification

-CLOSED- NOT EFFECTIVE AS PER P/N INSTALLED

N N FAA 2009-20-10








- CLOSED - SUPERSEDED BY CF


26, 2009)

R Y CF 2009-42R1 - SOREM ESB-4-32-4414 - Every 750 Flight cycles


CLOSED: PART I (CARRIED OUT ON NOV

26, 2009) OPEN: PART II and Part

III COVERED BY SMJC-63 PERFORMED:DURING LAST ANNUAL CHECK

W.O. 11/018; NEXT DUE WITHIN 559 FLIGHT

CYCLES TO GO

A N EASA 2009-0251


-CLOSED- NOT EFFECTIVE AS PER S/N INSTALLED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


Y N EASA 2009-0262R1



PER S/N NOT INSTALLED

N N EASA 2009-0278



N N TCA CF-2009-44



N N EASA 2010-003R1



PER P/N NOT INSTALLED

Y N EASA

2010-0062R1




A Y FAA 2010-07-02


-OPEN- APPLICABLE AND

EFFECTIVE DUE TO “NEW

REQUIREMENTS”; NOT YET PERFORMED

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2010-0067



N N EASA 2010-30



- CLOSED - NOT APPLICABLE

SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT

CONFIGURATION



- CLOSED - NOT APPLICABLE AS

PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010

N N FAA 2011-01-09





N N EASA 2011-0043


Modification


ON THE A/C TYPE

N N EASA 2011-0090R1


APPLICABLE AS PER P/N NOT INSTALLED

ON THE A/C TYPE

EASA/TCA/FAA/ENAC


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCO s/n 2009

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2011-0103




ON THE A/C TYPE

N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08


6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451






LANDINGS

A Y TCCA CF-2011-35




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCR Compliance Status

A N FAA 77-17-13

- - - - NLG DOORS - CLOSED -


A N FAA 77-13-05



AIRCRAFT S/N

A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)



S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02





AD CF-2003-02

I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314






SYSTEM

I Y FAA 97-11-08


LEVERS


PAGE 8

A N TCCA CF-96-02R1

ENAC 1999-268 - - - - - CLOSED -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES - CLOSED -


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234



AIRCRAFT AND ENGINE SERIAL NUMBERS

R N ENAC 00-496



AIRCRAFT S/N

S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



FAA 2006-22-05

A N TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003




- CLOSED - NOT APPLICABLE SINCE REAR

MOUNTS P/N 87110047-001 INSTALLED IN PRODUCTION

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




AIRCRAFT S/N

A N EASA 2006-0375




EFFECTIVITY

N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD

RUDDER LOWER TORQUE TUBE UPPER

BEARING

- OPEN - AD COMPLIED WITH

ON APR 14, 2011. NEXT DUE OCT 13, 2011 (AD COVERED BY SMJC

60)


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2






01, 2011.



CLOSED ESB-4-42-A4424 PART B TERMINATING ACTION

PERFORMED ON 10/05/2011 REF. WO 11/069

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;



LIQUID PENETRANT & EDDY CURRENT

INSPECTION ON MLG UPPER MEMBER FORWARD LUG

OPEN


Eng. Type:

PW123AF

Eng. S/N. :

AF0124 Manuf. date:

JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - AF0124 - Engine1 - I-DPCR (WIP).doc

I Y TCA CF-90-21 -




- CLOSED- FUEL PUMP P/N: 3117094-02 INSTALLED (Post SB21360)

I Y RAI 91-296



- CLOSED- SB21018 EMBODIED AS PER

BUILD SPEC 723.

A N TCA CF-91-02


TORQUE FLUCTUATIONS - CLOSED-


I Y RAI 91-347

TCA CF-91-26R1 P&WC


31/03/92 N/A ENGINE FIRE DUE TO OIL

ACCUMULATING IN THE ICC CAVITY.

- CLOSED- SB21053 AND SB20914

EMBODIED AS PER BUILD SPEC 723.

S - RAI 93-284

TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES IN THE ICC.

- CLOSED- SUPERSEEDED BY TCA CF-

92-03R2

I Y TCA CF-92-03R2

- P&WC


21211 (last R6)


- CLOSED- SBs EMBODIED AS PER

BUILD SPEC 723.


Eng. Type:

PW123AF

Eng. S/N. :

AF0124 Manuf. date:

JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


1000⇔2000 cycles

N/A REPLACEMENT HP TURBINE DISK

- CLOSED- HP DISK P/N 3041511

INSTALLED

I Y ENAC 96-353

TCA CF-96-22






- CLOSED- SBs INTRODUCED AT

MANUFACTURE

I Y ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04



installed p/n 10718

before 31/08/02


- CLOSED- FUEL HEATER P/N: 10839F

(Post SB21519)

A N ENAC 02-090

TCA CF-2002-10 - - N/A INTERCOMPRESSOR CASE FIRE

- CLOSED- N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01




1200 f/h or 3A Final Action within

2400 f/h or 23/8/2004


CONTROL UNIT

- CLOSED- MFCU P/N 3244857-15

INSTALLED (Post SB21562)


Eng. Type:

PW123AF

Eng. S/N. :

AF0126 Manuf. date:

JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y TCA CF-90-21 -


30/04/91 N/A

O-RING DETERIORATION


- CLOSED- FUEL PUMP P/N: 3117094-02 INSTALLED (Post SB21360)

I Y RAI 91-296


OIL SYSTEM INSPECTION DUE TO

BEARING DETERIORATION

- CLOSED- SB21018 EMBODIED AS PER BUILD

SPEC 723

A N TCA CF-91-02

- P&WC SB20946 (last R2) 31/10/91 N/A

TO PREVENT IN FLIGHT TORQUE

FLUCTUATIONS

- CLOSED- N/A DUE TO ENGINE S/N

I Y RAI 91-347

TCA CF-91-26R1 P&WC


31/03/92 N/A ENGINE FIRE DUE TO

OIL ACCUMULATING IN THE ICC CAVITY.

- CLOSED- SB21053 AND SB20914 EMBODIED

AS PER BUILD SPEC 723

S - RAI 93-284

TCA CF-92-03R1 - - N/A INTERNAL OIL FIRES IN THE ICC.

- CLOSED- SUPERSEEDED BY TCA CF-92-

03R2

I Y TCA CF-92-03R2

- P&WC


21211 (last R6)


- CLOSED- SBs EMBODIED AS PER BUILD

SPEC 723


Eng. Type:

PW123AF

Eng. S/N. :

AF0126 Manuf. date:

JUNE 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


1000⇔2000 cycles


- CLOSED- HP DISK P/N 3041511 INSTALLED

I Y ENAC 96-353

TCA CF-96-22




N/A

REPLACEMENT OF FUEL NOZZLES

LOCKING PLATES AND “O” RINGS

- CLOSED- SBs INTRODUCED AT

MANUFACTURE

I Y ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04



installed p/n 10718

before 31/08/02


- CLOSED- FUEL HEATER P/N 10839F (Post

SB21519)

A N ENAC 02-090

TCA CF-2002-10 - - N/A INTERCOMPRESSOR CASE FIRE

- CLOSED- N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





2400 f/h or 23/8/2004


CONTROL UNIT

- CLOSED- MFCU P/N 3244857-15 INSTALLED

(Post SB21562)


Prop. Type:


Prop. S/N. :


JULY 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - 20090710 - Propeller 1 - I-DPCR (WIP).doc

I Y FAA 93-06-06 - H.S.




R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1

5000 Hrs (PostMod HS

SB 14SF-61-82)

Shaft Torque Check

5000 Hrs


- OPEN- INSPECTION SCHEDULED EVERY

2000 FH (prop. O/H) 1425.13 F/H TO GO

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1

since 09/05/96 300 cycles or

within 28/02/97 500 cycles BLADE INSPECTION /

MODIFICATION - CLOSED-:

NOT APPLICABLE - BLADE #1 S/N 2009060220-19 INSTALLED

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2

6000 Hrs or 3 years since February 7,

1997

10.500 Hours


ACTUATOR ASSEMBLY




Prop. Type:


Prop. S/N. :


JULY 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY



1425.13 F/H TO GO

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY

- OPEN- PCU INSPECTION SCHEDULED

EVERY 2000 FH (prop. O/H) 1425.13 F/H TO GO

28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 - CLOSED-


A N FAA US-2011-04-02




Prop. Type:


Prop. S/N. :


AUGUST 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y FAA 93-06-06 - H.S.




R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


SB 14SF-61-82)

Shaft Torque Check

5000 Hrs


- OPEN- INSPECTION SCHEDULED EVERY

2000 FH (prop. O/H) 1425.13 F/H TO GO

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

- CLOSED-: S/N 882977-19 INSTALLED ON 31/05/10 AS PER W.O. 10/103

ALREADY MODIFIED

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY




Prop. Type:


Prop. S/N. :


AUGUST 2009

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY



1425.13 F/H TO GO

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY

- OPEN- PCU INSPECTION SCHEDULED

EVERY 2000 FH (prop. O/H) 1425.13 F/H TO GO

28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 - CLOSED-


A N FAA US-2011-04-02




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


_______________________

Approved by:

________________________

I-DPCR Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052

- - - - - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM OPEN

TEST CARRIED OUT ON SEP 30, 2009 (NEXT DUE SEP 28, 2011)

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


_______________________

Approved by:

________________________


N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231



INSTALLED

S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


_______________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470




I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A



CLOSED: SB 215-4234 INCORPORATED IN PRODUCTION

I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________


28/09/2003

N N FAA 2003-23-05




R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN HEATER TIME IN

SERVICE CHECKED: 5.40 HOURS

TEST NOT YET PERFORMED







ESP-4-34-001 Within


OPEN LAST PERFORMANCE

DURING ANNUAL INSPECTION

07/06/2011. (COVERED BY ANN-AT-10)

NEXT DUE: ANNUAL INSPECTION

A N EASA 2006-0269




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________



NOSE WHEEL TIRES



A N FAA 2006-19-04



N N FAA 2006-22-05



7510100-731 (#2) INSTALLED

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________


A N EASA 2007-0294




FLEET

N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED






A/C DELIVERED WHEN AD REV. 1 WAS

ALREADY ISSUED.

R Y CF 2009-42R1 - SOREM ESB-4-32-4414 - Every 750 Flight cycles


OPEN AD COVERED BY INAER SMJC 063 (723 FCY TO

GO)

Y N EASA 2009-0251



INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________


Y N EASA 2009-0262R1



Y N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA

2010-0062R1



A Y FAA 2010-07-02


CARRIED OUT ON MAY 28, 10. BOTH INU # 1

AND # 2 ARE IN COMPLIANCE


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________


N N EASA 2010-0067



N N EASA 2010-30



NOT APPLICABLE SINCE INAER FLEET IS

NOT OPERATING IN CARGO TRANSPORT

CONFIGURATION





N N FAA 2011-01-09





N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCR s/n 2074

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


_______________________

Approved by:

________________________


N N EASA 2011-0103





N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08


6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451






LANDINGS

A Y TCCA CF-2011-35




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Delivery Date: Feb 27, 98

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCT Compliance Status

A N FAA

77-17-13 - - - - NLG DOORS


A N FAA

77-13-05 - - - -



A N TCCA

CF-90-11R2 FAA 93-16-06R2



JUNE. 10, 1994 N/A


FLUTTER)


SYSTEM INSTALLED

S TCCA

CF-92-22

FAA 94-04-02 TCCA CF-2003-

02



- N/A ENGINE REAR

MOUNT STRUTS


I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314






SYSTEM

I Y FAA

97-11-08 - - - -


LEVERS

CLOSED: AFM REV. 12 ISSUED WITH THE NOTE IN LIMITATION SECTION

PAGE 8

A N TCCA

CF-96-02R1 ENAC 1999-268 - - - -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES NOT APPLICABLE AS PER AD

EFFECTIVITY

A N TCCA

CF-2002-14 FAA 2004-26-08

ENAC 02-167


SoREM DT CL-61-4234


PRESSURE VALVE


MANUFACTURE

R N ENAC 00-496



EFFECTIVITY

S - FAA

2003-04-06 ENAC 03-067

FAA 2006-22-05

SoREM

DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343


RNZ-850/ -851

REF TO COMPONENTS


R Y TCCA

CF-2003-02 FAA 2004-10-04

ENAC 03-251





28, 2003




OPEN: CARRIED OUT WITH SMJC 31 & SMJC 32 ON 08/07/2011 (W/O

11/129); 39.52 FH TO GO

28/09/2003

R Y FAA

2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA



A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA

2005-18-05 - - - -


REAR SPAR

CLOSED NOT APPLICABLE AS PER AD EFFECTIVITY

A N EASA



SWITCHES


N N FAA



REF TO COMPONENTS


R Y TCCA

CF-2008-29 FAA 2009-05-04 ENAC 2008-316

SMJC-60 Mar 8, 2009




PERIOD



11/099) NEXT DUE WITHIN NOV 30, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2 ENAC 2011-88






01, 2011.



CLOSED SB 215-A4424 PART B EMBODIED

ON 31/05/2011 (W/0 11/099)

R Y TCCA

CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



Eng. Type:

PW123AF

Eng. S/N. :

AF0014 Manuf. date:

DECEMBER 5, 1996

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCT righr engine

I Y TCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



I Y RAI

91-296 TCA CF-90-22R1

P&WC SB21018R1




I Y TCA

CF-91-02 -

P&WC SB20946R1



AD COMPLIED WITH

I Y RAI

91-347 TCA CF-91-26R1

P&WC SB20914R3

SB21053 31/03/92 N/A




S RAI

93-284 TCA CF-92-03R1 - - N/A


CASE (ICC)


I Y TCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC. - CLOSED –

AD COMPLIED WITH


Eng. Type:

PW123AF

Eng. S/N. :

AF0014 Manuf. date:

DECEMBER 5, 1996

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCT righr engine

A N RAI

94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808






I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3






A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2




FUEL HEATERS



A N ENAC 02-090

TCA CF-2002-10 - CLOSED –

N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT



28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0095 Manuf. date:

DEC 2006

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCT Left Engine

I Y TCCA

CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A



DELIVERY

I Y TCCA

CF-90-22R1 RAI 91-296

P&WC SB21018R1




DELIVERY

A N TCCA

CF-91-02 -

P&WC SB20946R1




I Y TCCA

CF-91-26R1 RAI 91-347

P&WC SB20914R3

SB21053 31/03/92 N/A




DELIVERY

S TCCA

CF-92-03R1 RAI 93-284 - - N/A


CASE (ICC)


I Y TCCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC.


DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0095 Manuf. date:

DEC 2006

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCT Left Engine

A N TCCA

CF-94-01

FAA 94-03-02 Amdt 39-8808

RAI 94-001 P&WC SIL 307

Since 14/01/94





I Y TCCA

CF-96-22 ENAC 96-353

P&WC SB21077R7 SB21364R1 SB21373R3







A N TCCA

CF-2000-34 FAA 2003-16-04

ENAC 01-065 P&WC

SB 21100R2




FUEL HEATERS



A N TCCA

CF-2002-10 ENAC 02-090

P&WC SB 21914R4






I Y TCCA

CF-2002-34 FAA 2004-20-01

ENAC 02-448





or 23/8/2004


CONTROL UNIT


28/09/2003


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


FEB 1997

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCT right propeller

I Y FAA

93-06-06 - H.S.


transfer tube


P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)




CHECK COVERED BY O/H PROCEDURE (2000FH)

932.30 TO GO

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


NOT APPLICABLE FOR BLADE #1 S/N 9910019-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


NOT APPLICABLE FOR BLADE #3 S/N 2008061377

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles




Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :


FEB 1997

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCT right propeller

R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

TRANSFER TUBE INSPECTED DURING LAST


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

ACTUATOR INSPECTED DURING LAST O/H. (every

2000 FH) 1394.34 FH TO GO

R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

PCU INSPECTED DURING LAST O/H on 16/09/03.

(every 2000 FH) 932.30 TO GO

28/09/2003

A N FAA



A N FAA




Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

930508 Manuf. date:

17/05/93

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 10

Prepared by:

________________________

Approved by:

________________________

I-DPCT Left Propeller

I Y FAA

93-06-06 - H.S.


transfer tube CLOSED: AD COMPLIED WITH

P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



OPEN:

PCU INSPECTION PERFORMED EVERY O/H

(NEXT DUE WITHIN 1381.12 FH)

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLOSED: PERFORMED by SISAM ASB –A92R1 FOR

BLADE #1 S/N 879627-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLOSED: PERFORMED by SISAM ASB –A92R1 FOR BLADE #2 S/N 879628-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles


CLOSED: PERFORMED by SISAM ASB –A92R1 FOR BLADE #3 S/N 879626-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


28/02/97 500 cycles



200105014-19


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

930508 Manuf. date:

17/05/93

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 10

Prepared by:

________________________

Approved by:

________________________

I-DPCT Left Propeller

R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: ACTUATOR INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


10.500 Hours


ACTUATOR ASSEMBLY

OPEN: PCU INSPECTION SCHEDULED EVERY 2000 FH (prop. O/H)

AD COMPLIED WITH (NEXT DUE WITHIN 1381.12

FH)

28/09/2003

A N FAA



MODEL

A N FAA




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________

I-DPCT Components Compliance Status

A N FAA

81-21-05 - - Nov 19, 1981 N/A



INSTALLED

A N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 - N/A N/A




S - RAI

82-113 - - - - -


N N TCCA

CF-96-21



FAA 72-19-04

S - RAI

88-052 - - - - - SUPERS. BY ENAC 88-096

R Y RAI

88-096 FAR 43


NL-CL-34-06 19/11/2005 24 Months


OPEN: TEST CARRIED OUT ON JUL 29, 2010, W.O. 09/382 (NEXT

DUE WITHIN JUL 27, 2012)

I Y ENAC 96-052



INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N ENAC 97-167


CREW OXYGEN MASKS


INSTALLED

N N TCCA

CF-95-16 ENAC 97-221



REMOVAL


(Serie MSI-800)

N N ENAC 97-274


CREW OXYGEN MASKS


INSTALLED

N N ENAC 99-231

FAA 99-08-21 - - N/A



INSTALLED

S - ENAC 00-018





N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


EI 004/00 18/05/00 N/A





A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368






N N ENAC 01-442



I Y ENAC 01-470



DISCHARGER



I Y TCCA

CF-2002-14 ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


RNZ -850/ -851


7510100-731 (#2) INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


28/09/2003

N N FAA

2003-23-05 ENAC 2004-003 ENAC-2004-073

- December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months





A N FAA



CLOSED: NOT APPLICABLE AS PER HEATER INSTALLED

R Y EASA

2006-0265 -

Scheda Analisi PA ESP-4-34-001

Within Mar 13, 2007


TRANSPONDERS CHECK

OPEN: CARRIED OUT DURING LAST ANNUAL CHECK W.O. 09/382 ON JUL 29, 2010 NEXT DUE

WITHIN JUL 2012

A N EASA




A N FAA






A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


A N FAA



CLOSED: NOT APPLICABLE AS PER PART NUMBER NOT

INSTALLED

N N FAA




FAA-2003-04-06)

A N EASA



AIRCRAFT MODEL

A N EASA



INSTALLED

A N EASA



INSTALLED

A N EASA





FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N EASA



Modification


INSTALLED

N N FAA




INSTALLED

S - CF 2009-42 - SOREM ESB-4-32-4414

(SMJC 063)






26, 2009)

R Y CF 2009-42R1 - SOREM ESB-4-32-

4414R1 - Every 750 Flight




PERFORMED ON 19/04/2011 (W/O 11/066)

596 FC TO GO

A N EASA



CLOSED: NOT EFFECTIVE: S/N NOT

INSTALLED

A N EASA



NOT EFFECTIVE: S/N NOT INSTALLED

A N EASA




INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N TCA




INSTALLED

N N EASA



CLOSED: NOT EFFECTIVE : P/N NOT

INSTALLED

Y N EASA

2010-0062R1 - Scheda Analisi AD 14 Apr 2010 N/A


NOT EFFECTIVE: P/N NOT INSTALLED

A Y FAA



INU #1 COMPLIED INU #2 TO BE

PERFOMED WITHIN OCT 31, 12”

N N EASA



CLOSED - NOT EFFECTIVE: P/N NOT

INSTALLED

N N EASA



Aircraft

CLOSED - NOT APPLICABLE SINCE

INAER FLEET IS NOT OPERATING IN CARGO




CLOSED - NOT APPLICABLE AS PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


N N FAA





N N EASA



Modification


ON THE A/C TYPE

N N EASA



ON THE A/C TYPE

N N EASA




ON THE A/C TYPE

N N FAA

2011-11-04


Extinguisher


N N EASA




NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCT s/n 2029

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION

NOTES (COMPLIANCE

DATE)





Date:

Sep 09, 11

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2011-35 - ESB-4-32-A4451 Rev 01



A4451



eddy current method


CLOSED (REF TO WO 11/195 ON 22/07/11);

REPETITIVE ACTION: 91 LL TO GO

A Y TCCA




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Delivery Date: Jun ‘98

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________

I-DPCU Compliance Status

A N FAA 77-17-13

- - - - NLG DOORS CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY

A N FAA 77-13-05



A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)


INSTALLED

S TCCA CF-92-22

FAA 94-04-02





I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA 97-11-08


LEVERS


SECTION PAGE 8

A N TCCA CF-96-02R1



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 - - - MLG AXLES CLOSED: NOT APPLICABLE AS PER AD EFFECTIVITY

A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234


CLOSED: NOT APPLICABLE AS PER VALVE INCORPORATED AT

MANUFACTURE

R N ENAC 00-496



S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


REF TO COMPONENTS


R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003




OPEN: INSPECTION COVERED BY SOREM SMJC 31 AND 32 AND

CARRIED OUT WITH W.O. 09/279. NEXT DUE WITHIN A/C FH 4279

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




A N EASA 2006-0375




N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD

RUDDER LOWER TORQUE TUBE UPPER

BEARING

OPEN: CARRIED OUT ON OCT 05, 10 (AD COVERED BY SMJC 60). EXPIRED ON APR 05, 2010 AND ALREADY PLANNED WITH W.O.

11/038


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030


EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________








01, 2011.



OPEN: PART B, TERMINATING ACTION, PLANNED WITH W.O. 11/038

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________

I-DPCQ Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052

- - - - - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM

OPEN: CARRIED OUT DURING WITH W.O. 09/073. NEXT DUE PLANNED WITH W.O. 11/038

Supersedes ENAC 88-095

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231




S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Revision n° 1


Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470


DISCHARGER

CLOSED: P/N AFFECTED CHECKED AND REMOVED.


FEB 05, 02

I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


CLOSED: INU#1 #2 REPLACED. NOTIFIED TO THE CREW – INFO

INSERTED IN AFM


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


28/09/2003

N N FAA 2003-23-05


Tubi Flessibili


HOSES INSTALLED P/N 114040-4

R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN: HEATER TIME IN SERVICE 278.00

HOURS. 222.00 HOURS TO GO TO THE TEST






ESP-4-34-001 Within


OPEN: CARRIED OUT DURING

WITH W.O. 09/073. NEXT DUE PLANNED

WITH W.O. 11/038

A N EASA 2006-0269




NOSE WHEEL TIRES




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04



N N FAA 2006-22-05



COMPONENT MODIFIED (REF TO FAA

2003-04-06)

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256



A N EASA 2007-0294




FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED







I CARRIED OUT ON NOV 2009)

R Y CF 2009-42R1 - SOREM ESB-4-32-4414 (SMJC 063)





CLOSED: (PART I CARRIED OUT ON NOV

2009) OPEN: PART II AND PART III - NOT YET

PERFORMED. ISSUED SMJC 063: 160 FLIGHT

CYCLES TO GO

A N EASA 2009-0251



INSTALLED

Y N EASA 2009-0262R1




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA

2010-0062R1



A Y FAA 2010-07-02

- Scheda Analisi AD ESB-4-34-2010-07-02 31 Oct 2012 N/A Honeywell Primus II RNZ

850()/-851

OPEN: INCORPORATION TO

BE VERIFIED. INSPECTION PLANNED

WITH W.O. 11/038

N N EASA 2010-0067




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N EASA 2010-30




CONFIGURATION





N N FAA 2011-01-09





N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE

N N EASA 2011-0103






A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCU s/n 2030

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Revision n° 1


Date:


________________________

Approved by:

________________________


N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08


6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451




PLANNED (REF TO WO 11/038);

REPETITIVE ACTION: OPEN TO BE

CONSEQUENTLY PLANNED.

A Y TCCA CF-2011-35




OPEN

EFFE

CT

pag. 1 o

I-DPCV Co

A N

A N

A N

S

I Y

I Y

A N

P.A. / A.D.

of 4 A ApR ApN NoS Su

ompliance Status

FAA 77-17-13

FAA 77-13-05

TCCA CF-90-11R2

TCCA CF-92-22

ENAC 95-064

FAA 97-11-08

TCCA CF-96-02R

A.D. C

. Other

Authorityissues

pplicable (to be pplicable Repetot Applicable uperseded

-

-

2 FAA 93-16-06R

FAA 94-04-02TCCA CF-2003

02

TCCA CF-92-10R1

-

1 ENAC 1999-26

Compli

y ISSUEDDOCUMEN

Incorp.) D Dtitive I I

Y YN N

-

-

R2

BombardieSB215-A43

SoREMScheda analis

2 3-

BombardieSB215-A304

SoREMScheda analisP&WC: SB20 SB21 SB21 SB21

BombardieSB215-A306

SoREMScheda Analis

-

68 -

ance SD NTS EXPIRA

Deleted Incorporated Yes effective Not effective

-

-

er 35

si AD

JUNE. 10

er 40

si AD

-

0914 113 211 314

er 60

si PA

-

-

Status

ATION REPEACT

Date:

Sep 09,

, 1994

A/C Type:

CaC

ETITIVE TIONS

11 Prepared

________

-

- M

N/A IN(T

N/A

N/A E

- S

-

anadair CL-415

DESCRIPTIO

by:

______________

NLG DOORS

MISSING RIVETSBULKHEAD

RUDDER-AILERONTERCONNECT TO PREVENT POSSI

FLUTTER)

ENGINE REARMOUNT STRUT

ENGINE FIRE-WIDETECTION LOO

AFM - LIMITATIOSECTION - POW

LEVERS

-

A/C Reg. :

D

ON (COMP

____

Approved b

_________

CLOSED:PER

S IN CLOSED:PER

ON TAB BILE

CLOSED: NPOWERE

R TS

CLOSEA

IRE OP

CLOSEDENGINSYSTEAIRCRA

ON WER

CLOSED:WITH THE

SE

CLOSEDCANCEL

I-DPCVs/n 20

Delivery Date: Jul

NOTES PLIANCE DAT

by:

______________

: NOT APPLICABLE AR AIRCRAFT S/N


NOT EFFECTIVE AS PED AILERON SYSTE

INSTALLED

D: SUPERSEDED BYAD CF-2003-02

D: AD COMPLIED WITNE FIRE DETECTION EM CONNECTED TO AFT FIRE WARNING

SYSTEM

: AFM REV. 12 ISSUEE NOTE IN LIMITATIOECTION PAGE 8

: AD ISSUED JUST TPREVIOUS REVISIO

V 035 l 98

E)

___

AS

AS

PER M

Y

TH

ED ON

TO ON

EFFE

CT

pag. 2 o

I-DPCV Co

R N

A N

R N

S -

R Y

R Y

P.A. / A.D.


ompliance Status

ENAC 00-265

TCCA CF-2002-14

ENAC 00-496

FAA 2003-04-06

TCCA CF-2003-02

FAA 2004-21-05

A.D. C

. Other

Authorityissues


FAA 2004-03-1

4 FAA 2004-26-0

ENAC 02-167

FAA 2002-12-1

6 ENAC 03-067

FAA 2006-22-0

2 FAA 2004-10-0

ENAC 03-251

5 -

Compli

y ISSUEDDOCUMEN


Y YN N

13 -

08 7

BombardieSB215-423

SoREMDT CL-61-42

12 -

7 05

SoREMDT-CL-34-

DT-CL-34-0BM-CL-34-4

04 1

BombardieSB215-A4287

SoREMBM-CL-71-A4

BM-CL-71-A42SMJC 31 and

SCHEDA ANADisposizione Te

DT-CL-21-

ance SD NTS EXPIRA


-

er 34

234

MARCH 04

-

-05 07R1 4343

March 16

er 7R2

4287 287R2 d 32

WITHIN 5SINCE FEB

28, 20

28

ALISI ecnica -01

A 500 hHrs Total heater hrfrom 19/

(whicheoccurs l

Status

ATION REPEACT

Date:

Sep 09,

4, 2003

6, 2003

50 F/H BRUARY 003

EVERREPETIT

FOLLOWESMJC #

8/09/2003

eater or 100 rs TIS /11/04 ever later)

100 Hr24 M

A/C Type:

CaC

ETITIVE TIONS

11 Prepared

________

-

N/A

- W

N/A IN

RY 250 F/H TIVE ACTION ED BY SoREM #31 and #32

EN

rs funzion. Months

P

O

anadair CL-415

DESCRIPTIO

by:

______________

MLG AXLES

PCU BACKUPPRESSURE VAL

WING TO FUSELAFRAME ANGLE

U Honeywell PrimRNZ-850/ -851

NGINE REAR MOSTRUTS

PRESSURE DECTEST and CABI

HEATER (JANITROL)

OPERATIONAL TE

A/C Reg. :

D

ON (COMP

____

Approved b

_________

CLOSED:PER

P VE

CLOSED:PER AIR

SE

AGE ES

CLOSED:PER

mus II

CLOSEF

OUNT OPEN: INS

SOREM CARRIED

(NEXT D

CAY N

EST

REF T

I-DPCVs/n 20

Delivery Date: Jul

NOTES PLIANCE DAT

by:

______________


: NOT APPLICABLE ARCRAFT AND ENGINEERIAL NUMBERS


D: SUPERSEDED BYFAA 2006-22-05

PECTION COVEREDSMJC 31 AND 32 ANOUT WITH W.O. 10/3

DUE WITHIN 55.56 FH

TO COMPONENTS

V 035 l 98

E)

___

AS

AS E

AS

Y

D BY D 344 H)

EFFE

CT

pag. 3 o

I-DPCV Co

A N 2

R N

A N

N N

R Y

P.A. / A.D.


ompliance Status

FAA 2004-25-16R

FAA 2005-18-05

EASA 2006-0375

FAA 2006-22-05

TCCA CF-2008-29

A.D. C

. Other

Authorityissues


R1 -

5 -

5 -

5 EASA 2006-47

9 FAA 2009-05-0ENAC 2008-31

Compli

y ISSUEDDOCUMEN


Y YN N

Scheda Analis

-

Scheda Analis

79 Scheda Analis

04 16 SMJC-60

ance SD NTS EXPIRA


si AD Jan. 05,

-

si AD Dec. 29,

si AD -

Mar 8, 2

Status

ATION REPEACT

Date:

Sep 09,

2005

2006

2009

BEFOREEVERY F

OR AT INT

WHICSHOR

P

A/C Type:

CaC

ETITIVE TIONS

11 Prepared

________

N/A CV

A/

- LO

WIN

-

N/A N

E AND AFTER FIRE SEASON SIX MONTH

TERVAL, CHEVER IS RTER TIME ERIOD

RU

anadair CL-415

DESCRIPTIO

by:

______________

REGOLATORECARBURANTE CVALVOLE SHUTO/B/C 14D11 o A/B

23D04

OWER CAPS OF NG FRONT SPAR

REAR SPAR

CARLING TECHNOLOGIE

SWITCHES

INTEGRATEDNAVIGATION UN

UDDER LOWER TORTUBE UPPER BEARI

A/C Reg. :

D

ON (COMP

____

Approved b

_________

E CON OFF B/C/P

REF T

THE R AND CLOSED:

PER

ES CLOSED:PER

D ITS

REF TS

FA

RQUE ING

OPEN: CEXPIREA/C CU

M

I-DPCVs/n 20

Delivery Date: Jul

NOTES PLIANCE DAT

by:

______________

TO COMPONENTS


: NOT APPLICABLE AR AD EFFECTIVITY

TO COMPONENTS Supersedes

AA 2003-04-06

COVERED BY SMJC 6ED ON SEP 29, 2010 URRENTLY UNDER

MAINTENANCE

V 035 l 98

E)

___

AS

AS

60

EFFE

CT

pag. 4 o

I-DPCV Co

R Y

R Y

P.A. / A.D.


ompliance Status

TCCA CF-2010-38R

TCCA CF-2011-35

A.D. C

. Other

Authorityissues


R2 ENAC 2011-8

5 Bombardier SB

215-A4450; Bombardier SB

215-A4451

Compli

y ISSUEDDOCUMEN


Y YN N

8 Bombardier SB -A4424

B

B

ESB-4-32-A44501;

ESB-4-32-A44501;

ance SD NTS EXPIRA


215 Jun 01,

50 Rev

51 Rev

Ref. To ACompliaCompon

Status

ATION REPEACT

Date:

Sep 09,

2011

FIRST IWITHIN

20 DTHEREAF

PERRINSPECT

100 TERMINANOT LAT

01

AD-PA ance nents

Ref. TComCom

A/C Type:

CaC

ETITIVE TIONS

11 Prepared

________

NSPECTION 50 FC FROM

DEC 2010; FTER REPEAT RFORM AN TION BEFORE FC WITH

ATING ACTION TER THAN Jun 1, 2011.

INE

To AD-PA mpliance mponents

LiqCM

anadair CL-415

DESCRIPTIO

by:

______________

NSPECTION OF TMERGENCY WA

DUMP PULLEYBRACKET ANDSTRUCTURE

quid Penetrant & Current InspectionMLG Upper Mem

Forward Lug

A/C Reg. :

D

ON (COMP

____

Approved b

_________

THE ATER Y D

PART A TW

PLATERM

A/C CUM

Eddy n on ber

REF. TOC

I-DPCVs/n 20

Delivery Date: Jul

NOTES PLIANCE DAT

by:

______________

OPEN TO BE ACCOMPLISHEWITH SMJC-062

NNED PART B AS MINATING ACTION URRENTLY UNDER

MAINTENANCE

AD-PA COMPLIANCCOMPONENTS

V 035 l 98

E)

___

ED

CE


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



pag. 1 of 9 A Applicable (to be Incorp.) D Deleted Date:


________________________

Approved by:

________________________ R Applicable Repetitive I Incorporated N Not Applicable Y Yes effective S Superseded N Not effective

I-DPCV Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052


R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM

OPEN: CARRIED OUT WITH W.O. 08/422. EXPIRED ON 04/05/11

A/C CURRENTLY UNDER MAINTENANCE

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues





________________________

Approved by:



N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231




S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues





________________________

Approved by:



S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470




I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


CLOSED: INU#1 #2 REPLACED ON 09/04/04

W/O SOREM 04/209 NOTIFIED TO THE CREW – INFO

INSERTED IN AFM

28/09/2003


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



N N FAA 2003-23-05




N N FAA 2003-23-05




R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months



OPEN: HEATER TIME IN SERVICE:







ESP-4-34-001 Within


OPEN: PERFORMED WITH W.O. 10/047.

EXPIRED. A/C CURRENTLY

UNDER MAINTENANCE

A N EASA 2006-0269




NOSE WHEEL TIRES




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



A N FAA 2006-19-04



N N FAA 2006-22-05



7510100-731 (#2) INSTALLED

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256



A N EASA 2007-0294




FLEET


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED








R Y CF 2009-42R1 - SOREM ESB-4-32-

4414R1 (SMJC 063)





OPEN: COVERED BY SOREM ESB-4-32-4414 (SMJC 063; 59 CYCLES

TO GO)

A N EASA 2009-0251



INSTALLED

Y N EASA 2009-0262R1




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



N N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA

2010-0062R1



NOT INSTALLED

A Y FAA 2010-07-02


OPEN: INU #1 COMPLIED WITH / INU #2 TO BE PERFORMED

N N EASA 2010-0067



NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



N N EASA 2010-30







NOV 09, 2010

N N FAA 2011-01-09




N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE

N N EASA 2011-0103





A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCV s/n 2035

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)



________________________

Approved by:



N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08




NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01




landings


current method

OPEN: FIRST

INCORPORATION NOT YET PERFORMED

A Y TCCA CF-2011-35

- ESB-4-32-A4450 Rev 01





A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Delivery Date: Nov 11, 1998

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCW Compliance Status

A N FAA

77-17-13 NLG DOORS

NOT APPLICABLE AS PER AD EFFECTIVITY

A N FAA

77-13-05



A N TCCA

CF-90-11R2 FAA 93-16-06R2



JUNE. 10, 1994 N/A


FLUTTER)

NOT EFFECTIVE AS PER POWERED AILERON SYSTEM

INSTALLED

S TCCA

CF-92-22 FAA 94-04-02



N/A ENGINE REAR

MOUNT STRUTS

SUPERSEDED BY AD CF-2003-02

I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314






SYSTEM

I Y FAA

97-11-08


LEVERS


PAGE 8

A N TCCA

CF-96-02R1 ENAC 1999-268



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 MLG AXLES NOT APPLICABLE AS PER AD

EFFECTIVITY

A N TCCA

CF-2002-14 FAA 2004-26-08

ENAC 02-167


SoREM DT CL-61-4234


PRESSURE VALVE


MANUFACTURE

R N ENAC 00-496

FAA 2002-12-12 WING TO FUSELAGE


EFFECTIVITY

S FAA

2003-04-06 ENAC 03-067

SoREM

DT-CL-34-05 DT-CL-34-07R1 BM-CL-34-4343


RNZ-850/ -851

REF TO COMPONENTS


A N TCCA

CF-2003-02 FAA 2004-10-04

ENAC 03-251





28, 2003




AD IS APPLIED TO REAR MOUNTS P/N 87110016-009 AND -011.

P/N 87110047-001 INSTALLED DURING PRODUCTION AD NOT APPLICABLE

28/09/2003

R Y FAA

2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


A N FAA



A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA

2005-18-05 -


REAR SPAR


A N EASA

2006-0375 Scheda Analisi AD Dec. 29, 2006


SWITCHES


N N FAA

2006-22-05 EASA 2006-479 Scheda Analisi AD N/A


REF TO COMPONENTS


R Y TCCA

CF-2008-29 FAA 2009-05-04 ENAC 2008-316

SMJC-60 Mar 8, 2009




PERIOD



11/112) NEXT DUE WITHIN NOV 27, 11


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036


EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2 ENAC 2011-88






01, 2011.



CLOSED SB 215-A4424 PART B EMBODIED

ON 27/05/2011 (W/0 11/109)

R Y TCCA

CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;




Forward Lug



Eng. Type:

PW123AF

Eng. S/N. :

109063 Manuf. date:

DEC 17, 1994

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - 109063 - Engine1 - I-DPCW

I Y TCA

CF-90-21 -




- CLOSED - AD COMPLIED BY


PRIOR TO DELIVERY

I Y RAI

91-296 TCA CF-90-22R1





SB21018R1 INCORPORATION PRIOR TO DELIVERY

A N TCA

CF-91-02 -



TORQUE FLUCTUATIONS CLOSED: N/A AS PER

ENGINE S/N

I Y RAI

91-347 TCA CF-91-26R1


31/03/92 N/A ENGINE FIRE DUE TO OIL

ACCUMULATING IN THE ICC CAVITY.


SB20914R3 AND SB21053 INCORPORATION

PRIOR TO DELIVERY

S RAI

93-284 TCA CF-92-03R1 - - N/A

INTERNAL OIL FIRES INTERCOMPRESSOR CASE

(ICC)

SUPERSEADED BY

TCA CF-92-03R2

I Y TCA

CF-92-03R2 -


21211 (last R6)

30/06/94 N/A INTERNAL OIL FIRES IN THE

ICC.



PRIOR TO DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

109063 Manuf. date:

DEC 17, 1994

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - 109063 - Engine1 - I-DPCW

A N RAI

94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


1000⇔2000 cycles

N/A REPLACEMENT HP

TURBINE DISK

CLOSED: NOT EFFECTIVE FOR


I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3





- CLOSED -

ALL SBs RELATED TO AD EMBODIED PRIOR

TO DELIVERY

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2


installed p/n 10718

before 31/08/02


FUEL HEATERS

CLOSED NOT APPLICABLE FOR


A N ENAC 02-090

TCA CF-2002-10 CLOSED: N/A AS PER

ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





2400 f/h or 23/8/2004


CONTROL UNIT

- CLOSED - MFCU p/n: 324485715

INSTALLED. AD COMPLIED WITH

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0052 Manuf. date:

SEP 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - AF0052 - Engine2 - I-DPCW

I Y TCA

CF-90-21 -


30/04/91 N/A




DELIVERY

I Y TCCA

CF-90-22R1 RAI 91-296

P&WC SB21018R1

30/06/94 N/A




DELIVERY

A N TCA

CF-91-02 -



TORQUE FLUCTUATIONS

- CLOSED – N/A DUE TO ENGINE S/N

I Y TCCA

CF-91-26R1 RAI 91-347

P&WC SB20914R3

SB21053 31/03/92 N/A




DELIVERY

S TCCA

CF-92-03R1 RAI 93-284 - - N/A


CASE (ICC)


I Y TCCA

CF-92-03R2 -

P&WC SB20957R3 SB20962R2

SB21065


THE ICC.


DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0052 Manuf. date:

SEP 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS







Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - AF0052 - Engine2 - I-DPCW

A N TCCA

CF-94-01

FAA 94-03-02 Amdt 39-8808

RAI 94-001 P&WC SIL 307

Since 14/01/94

1000⇔2000 cycles

N/A REPLACEMENT HP

TURBINE DISK



I Y TCCA

CF-96-22 ENAC 96-353

P&WC SB21077R7 SB21364R1 SB21373R3



N/A





A N TCCA

CF-2000-34 FAA 2003-16-04

ENAC 01-065 P&WC

SB 21100R2


installed p/n 10718

before 31/08/02


FUEL HEATERS



A N TCCA

CF-2002-10 ENAC 02-090

P&WC SB 21914R4



N/A

PW118, PW120 and PW121



I Y TCCA

CF-2002-34 FAA 2004-20-01

ENAC 02-448





2400 f/h or 23/8/2004


CONTROL UNIT


28/09/2003


Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

991213 Manuf. date:

DECEMBER 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - 991213 - Propeller 1 - I-DPCW

I Y FAA

93-06-06 - H.S.


transfer tube

- CLOSED – P/N 814829-1 INSTALLED AD COMPLIED WITH

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


SB 14SF-61-82)

Shaft Torque Check

5000 Hrs



CHECK COVERED BY O/H PROCEDURE (2000 FH) 208.02

FH TO GO

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1


within 28/02/97 500 cycles


CLOSED: NOT APPLICABLE FOR BLADE #1 S/N 9912024-19

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE INSPECTED DURING LAST O/H.



Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

991213 Manuf. date:

DECEMBER 1999

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY

OPEN: ACTUATOR INSPECTED DURING LAST O/H.


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours


ACTUATOR ASSEMBLY



28/09/2003

A N FAA



A N FAA




Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

950205 Manuf. date:

Feb 20, 1995

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

__________________

Approved by:

____________________


I Y FAA

93-06-06 - H.S.


transfer tube

- CLOSED – P/N 814829-1 INSTALLED AD COMPLIED WITH

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)

Shaft Torque Check

5000 Hrs



CHECK COVERED BY O/H PROCEDURE (2000 FH) 1774.09

FH TO GO

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1





BLADE S/N 2009090165

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




- CLOSED - BLADE #2 S/N 879794

MODIFIED BY ASB-A92.R1

A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1






A N ENAC

96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




- CLOSED - BLADE #4 S/N 880299


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2

6000 Hrs or 3 years since

February 7, 1997 10.500 Hours


ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE INSPECTED DURING LAST O/H.



Prop. Type:

Hamilton Sundstrand

14SF-19

Prop. S/N. :

950205 Manuf. date:

Feb 20, 1995

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION






Date:

Sep 09, 2011

Prepared by:

__________________

Approved by:

____________________


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




ACTUATOR ASSEMBLY

OPEN: ACTUATOR INSPECTED DURING LAST O/H.


R Y ENAC

97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2




ACTUATOR ASSEMBLY



28/09/2003

A N FAA



A N FAA




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________

I-DPCW Components Compliance Status

A N FAA

81-21-05 Nov 19, 1981 N/A


APPLICABLE ELT BATTERY NOT INSTALLED

A N TCCA

CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 N/A N/A


TEMPERATURE SENSING INSTALLED ON BATTERIES

EMBODIED

S RAI

82-113 SUPERS. BY ENAC 96-348

N N TCCA

CF-96-21


CF96-21 ISSUED TO CANCEL THE APPLICABILITY OF

FAA 72-19-04

S RAI

88-052 SUPERS. BY ENAC 88-096

R Y RAI

88-096 FAR 43


NL-CL-34-06 19/11/2005 24 Months


CARRIED OUT DURING ACCOMPLISHMENT OF AD EASA

2006-0265 (MAR 8, 2011, W.O 11/09)

I Y ENAC 96-052

FAA FAR 91.21 N/A N/A USE OF PORTABLE

ELETTRONIC DEVICES

- CLOSED - AFM UPDATED – CREW

INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -




NOT APPLICABLE HEATER MODEL B4500

(CERAMIC COMBUSTION TUBE)


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


N N ENAC 97-167

FAA 97-11-10 - N/A PURITAIN-BENNETT

CREW OXYGEN MASKS

NOT APPLICABLE SCOTT OXYGEN MASKS

INSTALLED

N N TCCA

CF-95-16 ENAC 97-221



REMOVAL

NOT APPLICABLE AS PER INVERTER INSTALLED

(Serie MSI-800)

N N ENAC 97-274


CREW OXYGEN MASKS


INSTALLED

N N ENAC 99-231


CREW OXYGEN MASKS


INSTALLED

S ENAC 00-018




Superseded by ENAC 00-209

N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


EI 004/00 18/05/00 N/A


NOT APPLICABLE AD RESCINDED APR. 12, ‘00



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


S ENAC 01-173


P/N 14D11 o 23D04

NOT APPLICABLE AS PER HEATER INSTALLED

Supers. By ENAC 01-368

A N ENAC 01-368






N N ENAC 01-442

FAA 2001-18-05 Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.

NOT APPLICABLE PER P/N

I Y ENAC 01-470



DISCHARGER

- CLOSED - P/N AFFECTED CHECKED.


I Y TCCA

CF-2002-14 ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A



- CLOSED - SB215-4234 IS INCORPORATED

DURING PRODUCTION

I Y ENAC 03-067

FAA 2003-04-06

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


RNZ -850/ -851

- CLOSED - INU P/N 7510100-732 (#1) AND 7510100-731 (#2) INSTALLED

28/09/2003


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


N N FAA

2003-23-05 ENAC 2004-003 -

December 24, 2005

N/A Titeflex Corporation,

Tubi Flessibili

NOT APPLICABLE HOSES INSTALLATI

P/N 114040-4

N N FAA

2003-23-05 ENAC 2004-073 -

December 24, 2005

N/A Titeflex Corporation,

Tubi Flessibili

NOT APPLICABLE HOSES INSTALLATI

P/N 114040-4

R Y FAA

2004-21-05 Amdt.39-13826


A 500 heater Hrs or 100 heater Hrs

TIS since 19/11/04


100 Hrs (TIS) or

24 Months

PRESSURE DECAY TEST ed Operational Test del CABIN

HEATER (JANITROL)

HEATER TIME IN SERVICE CHECKED:

258,00 HOURS TEST NOT YET PERFORMED

A N FAA





R Y EASA

2006-0265 -

Scheda Analisi PA NL CL-34-04 Ed. 2

Within Mar 13, 2007


TRANSPONDERS CHECK

CARRIED OUT DURING LAST ANNUAL CHECK

W.O. 11/053 ON SEP 01, 2011 NEXT DUE WITHIN

AUG 31, 2013

A N EASA

2006-0269 - Scheda Analisi PA MODE “S” TRANSPONDERS

N/A AS PER MODEL NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


A N FAA

2006-18-08 Scheda Analisi AD Oct. 11, 2006


NOT APPLICABLE AS PER


A N FAA

2006-19-04 Scheda Analisi AD MODE “S” TRANSPONDERS

N/A AS PER PART NUMBER NOT

INSTALLED

N N FAA


NOT APPLICABLE AS PER COMPONENT MODIFIED (REF TO

FAA-2003-04-06)

A N EASA

2006-0366 Scheda Analisi PA Dec 14, 2006 LIFE RAFT


A N EASA

2006-0286R1 Scheda Analisi PA Sep 9, 2006 Oxygen Cylinders


A N EASA

2007-0256 Scheda Analisi PA Sep 19, 2007 Seat Restraint System



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


A N EASA

2007-0294 ENAC 2009-060 Scheda Analisi PA


NOT EFFECTIVE AS PER APU NOT

INSTALLED ON SOREM CL415 FLEET

N N EASA

2009-0200 Scheda Analisi AD Sep 22, 2010 N/A


Modification


N N FAA

2009-20-10 Scheda Analisi AD Jan 17, 2010 N/A



S - CF 2009-42 - SOREM ESB-4-32-

4414 (SMJC 063)

Part I within 50Fh Part II: within 750

Fc Part III: every

750 Fc





26, 2009)

R Y CF 2009-42R1 Enac 2010-183

FAA 2011-03-08 SOREM ESB-4-32-

4414R1 Every 750 Flight

cycles Special Inspection of Accumulator

Screw Caps

CLOSED PART II:: PERFORMED WITH WO 10/293 ON SEP 1, 2010;

OPEN: PART III: 621 FLIGHT CYCLES TO GO

Y N EASA

2009-0251 Scheda Analisi AD Nov 26, 2009 N/A




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


Y N EASA




N N EASA




INSTALLED

N N TCA

CF-2009-44 Scheda Analisi AD Jul 1, 2011 N/A

ELT-Potential Failure to Transmit the Required 406MHz Coded

Signal


N N EASA

2010-003R1 Scheda Analisi AD 18 Apr, 2010 N/A



Y N EASA

2010-0062


Extinguisher


A Y FAA

2010-07-02 Scheda Analisi AD 31 Ott 2012 N/A


OPEN: NOT YET PERFOMED

INU 1 AND INU 2 TO BE MODIFIED”


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


N N EASA

2010-0067 Scheda Analisi AD 26 Apr, 2010 N/A



NOT INSTALLED

N N EASA


Risks in Transporting Lithium Batteries in Cargo by Aircraft






NOV 09, 2010

N N FAA




N N EASA



Modification


ON THE A/C TYPE

N N EASA



ON THE A/C TYPE


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCW s/n 2036

Components

EF

FE

CT

P.A. / A.D. Other

Authority issues

ISSUED DOCUMENTS


ACTIONS DESCRIPTION





Revision n° 2


Date:

Sep 09, 2011

Prepared by:

________________________

Approved by:

________________________


N N EASA




ON THE A/C TYPE

N N FAA

2011-11-04


Extinguisher


N N EASA




NOT INSTALLED

R Y TCCA

CF-2011-35 -

ESB-4-32-A4451 Rev 01




landings


current method


CLOSED (REF TO WO 11/053R2);

REPETITIVE ACTION: 151 LL TO GO

A Y TCCA

CF-2011-35 -

ESB-4-32-A4450 Rev 01

November 11, 2011

N/A Inspection of the MLG Upper

Member forward lug using liquid penetrant method

OPEN

A.D. Compliance Status A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCY Compliance Status

A N FAA 77-17-13


A N FAA 77-13-05



A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)


INSTALLED

S TCCA CF-92-22

FAA 94-04-02 TCCA CF-2003-

02





I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314





SYSTEM

I Y FAA 97-11-08


LEVERS


SECTION PAGE 8

A N TCCA CF-96-02R1



Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234



SERIAL NUMBERS

R N ENAC 00-496



S - FAA 2003-04-06

ENAC 03-067 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003


FOLLOWED BY INAER SMJC #31 and #32



FH TO GO

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05




A N EASA 2006-0375




N N FAA 2006-22-05



FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


OPEN: CARRIED OUT WITH W.O. 11/100 (AD COVERED BY SMJC

60) NEXT DUE NOV 29, 2011

A.D. Compliance Status Eng. Type:

PW123AF

Eng. S/N. :


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD Compliance Status – AF0023

I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A


CLOSED: AD COMPLIED BY SB20355 AND SB20897

INCORPORATION PRIOR TO DELIVERY


I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A


CLOSED: AD COMPLIED BY SB21018R1 INCORPORATION


I N TCA CF-91-02


TORQUE FLUCTUATIONS



I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053



CLOSED: AD COMPLIED BY SB20914R3 AND SB21053



S RAI 93-284


CASE (ICC)

CLOSED: SUPERSEADED BY TCA CF-92-03R2

I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065


CLOSED: AD COMPLIED BY SB20957, SB20962 AND SB21065




PW123AF

Eng. S/N. :


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK


AND SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3






TO DELIVERY (SEE ENGINE TECHNICAL LOG)

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2




CLOSED: : NOT APPLICABLE FOR ENGINES S/N 109036

AND SUB’S

N N ENAC 02-090

TCA CF-2002-10 P&WC SB 20914 R4



first




I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT

CLOSED: FINAL MODIFICATION COMPLIED BY

SB21562 INCORPORATION DATED 21/06/04 W.O.

CV005/04-24


PW123AF

Eng. S/N. :

AF0079 Manuf. date: Nov 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y TCA CF-90-21 -

P&WC SB20355R1

SB20897 30/04/91 N/A


CLOSED: AD COMPLIED BY SB20355 AND SB20897



I Y RAI 91-296

TCA CF-90-22R1 P&WC SB21018R1 30/06/94 N/A




I N TCA CF-91-02


TORQUE FLUCTUATIONS



I Y RAI 91-347

TCA CF-91-26R1 P&WC

SB20914R3 SB21053



CLOSED: AD COMPLIED BY SB20914R3 AND SB21053



S RAI 93-284


CASE (ICC)

SUPERSEADED BY

TCA CF-92-03R2

I Y TCA CF-92-03R2

- P&WC

SB20957R3 SB20962R2

SB21065


CLOSED: AD COMPLIED BY SB20957, SB20962 AND SB21065




PW123AF

Eng. S/N. :

AF0079 Manuf. date: Nov 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


TURBINE DISK


AND SUBSEQUENT

I Y ENAC 96-353

TCA CF-96-22

P&WC SB21077R7 SB21364R1 SB21373R3






TO DELIVERY (SEE ENGINE TECHNICAL LOG)

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04

P&WC SB 21100R2





AND SUB’S

N N ENAC 02-090

TCA CF-2002-10 P&WC SB 20914 R4



first




I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





or 23/8/2004


CONTROL UNIT

CLOSED: ENGINE IS POST SB 21562, NO FURTHER ACTION

REQUIRED (SEE ENGINE TECHNICAL LOG)

A.D. Compliance Status Prop. Type:


Prop. S/N. :


Aug 17, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09 , 11 Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report prop1 sn 20010810

I Y FAA 93-06-06 - H.S.


CLOSED: P/N 814829-1 INSTALLED

AD COMPLIED WITH

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)



PCU HOURS: 749.27 INSPECTION PERFORMED

EVERY O/H (NEXT DUE WITHIN 1250.33)

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200107049-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200107050-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200108010-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200210034-19



Prop. S/N. :


Aug 17, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09 , 11 Prepared by:

________________________

Approved by:

________________________


I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE HOURS: TTSN: N/A; TSO:



I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: ACTUATOR HOURS: TTSN: N/A; TSO: 1444.57



I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY




A N FAA 2006-24-07



A N FAA US-2011-04-02





Prop. S/N. :


May 07, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09,11 Prepared by:

________________________

Approved by:

________________________


I Y FAA 93-06-06 - H.S.


CLOSED: P/N 814829-1 INSTALLED

AD COMPLIED WITH

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)





(NEXT DUE WITHIN 381.19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200105010-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


200105012-10

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


2007080733-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION




Prop. S/N. :


May 07, 2001

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE TTSN: N/A; TSO: 884.49



I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: ACTUATOR HOURS TTSN: N/A; TSO: 884.49



I Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY




A N FAA 2006-24-07



A N FAA US-2011-04-02




Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCY Components Compliance Status

A N FAA 81-21-05



INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782


polistirolo



S - RAI 82-113


N N TCCA CF-96-21



FAA 72-19-04

S - RAI 88-052

- - - - - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E

Norma di lavoro NL-CL-34-06R2 19/11/2005 24 Months ALTIMETER AND STATIC

PRESSURE SYSTEM OPEN: TEST CARRIED OUT ON DEC 13 2009 WITH W.O. 09/380

(NEXT DUE WITHIN DEC 07, 2011)

I Y ENAC 96-052



N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -







Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N ENAC 97-167



INSTALLED

N N TCCA CF-95-16



REMOVAL


(Serie MSI-800)

N N ENAC 97-274



INSTALLED

N N ENAC 99-231




S - ENAC 00-018



INSPECTION/TEST


N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”




Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


S - ENAC 01-173


P/N 14D11 o 23D04


A N ENAC 01-368





N N ENAC 01-442



I Y ENAC 01-470




I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A




I Y ENAC 03-067

FAA 2003-04-06 FAA 2006-22-05

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343



7510100-731 (#2) INSTALLED


Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


28/09/2003

N N FAA 2003-23-05


Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826




later)

100 Hrs (TIS) or

24 Months










NL-34-004 Within


OPEN: CARRIED OUT DURING ANNUAL CHK; LAST WITH WO 11/020. NEXT DUE APR 27, 2012

A N EASA 2006-0269




NOSE WHEEL TIRES




Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


A N FAA 2006-19-04



N N FAA 2006-22-05




SCHEDA ANALISI 2006-22-05)

A N EASA 2006-0366



A N EASA 2006-0286R1



A N EASA 2007-0256



A N EASA 2007-0294




FLEET


Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0200


Modification


INSTALLED

N N FAA 2009-20-10



INSTALLED








R Y CF 2009-42R1 - SOREM ESB-4-32-4414 SMJC 063 - Every 750 Flight



OPEN: PERFORMED:WITH W.O. 10/136-PART 2; PART III DUE WITHIN

490 FC

A N EASA 2009-0251



INSTALLED

Y N EASA 2009-0262R1



NOT INSTALLED


Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2009-0278



INSTALLED

N N TCA CF-2009-44



INSTALLED

N N EASA 2010-003R1



NOT INSTALLED

Y N EASA

2010-0062R1



NOT INSTALLED

A Y FAA 2010-07-02


OPEN: INU #1 , INU #2 TO BE PERFORMED

N N EASA 2010-0067



NOT INSTALLED


Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N EASA 2010-30









NOV 09, 2010

N N FAA 2011-01-09





N N EASA 2011-0043


Modification



N N EASA 2011-0090R1



THE A/C TYPE

N N EASA 2011-0103






Canadair CL-415

A/C Reg. :

I-DPCY s/n 2047

Components

EFFE

CT

P.A. / A.D. Other

Authority issues



(COMPLIANCE DATE)


Date:


________________________

Approved by:

________________________


N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08


6500 FH from Aug 19,2011



NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01



A4451






LANDINGS

A Y TCCA CF-2011-35




OPEN


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Delivery Date: April 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

I-DPCZ Compliance Status

A N FAA 77-17-13

NLG DOORS - CLOSED -


A N FAA 77-13-05



EFFECTIVITY

A N TCCA CF-90-11R2 FAA 93-16-06R2





FLUTTER)



S TCCA CF-92-22

FAA 94-04-02



N/A ENGINE REAR MOUNT STRUTS


AD CF-2003-02

I Y ENAC 95-064

TCCA CF-92-10R1

P&WC: SB20914 SB21113 SB21211 SB21314






SYSTEM

I Y FAA 97-11-08


LEVERS


PAGE 8

A N TCCA CF-96-02R1

ENAC 1999-268 - CLOSED -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R N ENAC 00-265

FAA 2004-03-13 MLG AXLES - CLOSED -


A N TCCA CF-2002-14

FAA 2004-26-08 ENAC 02-167


SoREM DT CL-61-4234


- CLOSED - NOT APPLICABLE AS PER VALVE

INCORPORATED AT MANUFACTURE

R N ENAC 00-496

FAA 2002-12-12 WING TO FUSELAGE FRAME ANGLES


EFFECTIVITY

S FAA 2003-04-06

ENAC 03-067

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


- CLOSED - REF TO COMPONENTS

SUPERSEDED BY

FAA 2006-22-05

R Y TCCA CF-2003-02

FAA 2004-10-04 ENAC 03-251





28, 2003




- OPEN - CARRIED OUT WITH SMJC 31 & 32

WITH W.O. 11/225, 76.11 FH TO GO

28/09/2003

R Y FAA 2004-21-05 -


DT-CL-21-01





HEATER (JANITROL)

OPERATIONAL TEST

REF TO COMPONENTS


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________




A/B/C 14D11 o A/B/C/P 23D04

REF TO COMPONENTS

R N FAA 2005-18-05

- LOWER CAPS OF THE



EFFECTIVITY

A N EASA 2006-0375

Scheda Analisi AD Dec. 29, 2006 CARLING



EFFECTIVITY

N N FAA 2006-22-05

EASA 2006-479 Scheda Analisi AD N/A INTEGRATED NAVIGATION UNITS


FAA 2003-04-06

R Y TCCA CF-2008-29

FAA 2009-05-04 ENAC 2008-316 SMJC-60 Mar 8, 2009




PERIOD


- OPEN - COVERED BY SMJC 60; TO BE

PERFORMED WITHIN 31/10/2011


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048


EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


R Y TCCA

CF-2010-38R2






01, 2011.



-CLOSED- TERMINATING ACTION

COMPLETED WITH WO 11/070

R Y TCCA CF-2011-35



ESB-4-32-A4450 Rev 01;

ESB-4-32-A4451 Rev 01;



LIQUID PENETRANT & EDDY CURRENT INSPECTION ON

MLG UPPER MEMBER FORWARD LUG



Eng. Type:

PW123AF

Eng. S/N. :

AF0055 Manuf. date:

OTT 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09,2011

Prepared by:

________________________

Approved by:

________________________

AD-PA Compliance Status Report - AF0055 - Engine1 - I-DPCZ

I Y TCA CF-90-21 -


30/04/91 N/A



-CLOSED- AD COMPLIED WITH AT

DELIVERY

I Y RAI 91-296





DELIVERY

A N TCA CF-91-02

- P&WC SB20946 (last R2) 31/10/91 N/A


FLUCTUATIONS

-CLOSED- N/A DUE TO ENGINE S/N AD COMPLIED WITH AT

DELIVERY

I Y RAI 91-347

TCA CF-91-26R1 P&WC





DELIVERY

S RAI 93-284


CASE (ICC)

CLOSED- SUPERSEDED BY TCA CF-

92-03R2

I Y TCA CF-92-03R2

- P&WC


21211 (last R6)



DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0055 Manuf. date:

OTT 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09,2011

Prepared by:

________________________

Approved by:

________________________


A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


1000⇔2000 cycles


-CLOSED- NOT EFFECTIVE FOR


I Y ENAC 96-353

TCA CF-96-22




N/A




DELIVERY

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04



installed p/n 10718

before 31/08/02




A N ENAC 02-090

TCA CF-2002-10 -CLOSED- N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





2400 f/h or 23/8/2004


CONTROL UNIT


DELIVERY (NO REPETITIVE ACTION)

28/09/2003


Eng. Type:

PW123AF

Eng. S/N. :

AF0080 Manuf. date:

DEC 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09,2011

Prepared by:

________________________

Approved by:

________________________


I Y TCA CF-90-21 -


30/04/91 N/A




DELIVERY

I Y RAI 91-296





DELIVERY

A N TCA CF-91-02

- P&WC SB20946 (last R2) 31/10/91 N/A


FLUCTUATIONS

-CLOSED- N/A DUE TO ENGINE S/N AD COMPLIED WITH AT

DELIVERY

I Y RAI 91-347

TCA CF-91-26R1 P&WC





DELIVERY

S RAI 93-284


CASE (ICC)

CLOSED- SUPERSEDED BY TCA CF-

92-03R2

I Y TCA CF-92-03R2

- P&WC


21211 (last R6)



DELIVERY


Eng. Type:

PW123AF

Eng. S/N. :

AF0080 Manuf. date:

DEC 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09,2011

Prepared by:

________________________

Approved by:

________________________


A N RAI 94-001

TCA CF 94-01 FAA 94-03-02 Amdt 39-8808


1000⇔2000 cycles




I Y ENAC 96-353

TCA CF-96-22




N/A




DELIVERY

A N ENAC 01-065

TCA CF-2000-34 FAA 2003-16-04



installed p/n 10718

before 31/08/02




A N ENAC 02-090

TCA CF-2002-10 -CLOSED- N/A AS PER ENGINE MODEL

I Y ENAC 02-448

TCA CF-2002-34 FAA 2004-20-01





2400 f/h or 23/8/2004


CONTROL UNIT


DELIVERY (NO REPETITIVE ACTION)

28/09/2003

EASA/TCA/FAA/ENAC


Prop. Type:


Prop. S/N. :


OCT 28, 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report Propeller 1 I-DPCZ

I Y FAA 93-06-06 - H.S.



P/N 814829-1

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


14SF-61-82)






A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION NOT APPLICABLE FOR

BLADE #1 S/N

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




BLADE #2 S/N

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




BLADE #3 S/N

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1




BLADE #4 S/N

EASA/TCA/FAA/ENAC


Prop. Type:


Prop. S/N. :


OCT 28, 1999

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report Propeller 1 I-DPCZ

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: TRANSFER TUBE HOURS: TTSN :N/A; TSO:



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: ACTUATOR HOURS: TTSN :N/A; TSO:



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2



ACTUATOR ASSEMBLY

OPEN: PCU HOURS (TSO): 31.03



28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 NOT APPLICABLE AS PER PROPELLER MODEL

A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 NOT APPLICABLE AS PER PROPELLER MODEL


Prop. Type:


Prop. S/N. :


JAN 30, 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - 20000125 - Propeller 2 - I-DPCZ

I Y FAA 93-06-06 - H.S.


-CLOSED- P/N 814829-1 INSTALLED

AD COMPLIED WITH

R Y ENAC 96-004

supersedes 95-046

FAA 95-22-12 Amdt 39-9420


SB -67R2/-81R2/-82R1


SB 14SF-61-82)

Shaft Torque Check

5000 Hrs





A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION

-CLOSED- NOT APPLICABLE FOR BLADE

#1 S/N 882399-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


#2 S/N 890123-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


#3 S/N 890124-19

A N ENAC 96-177

FAA 96-08-02 Amdt 39-9568

H.S. ASB 14SF-61-A95R1/-

A93/A92R1



MODIFICATION


#4 S/N 890126-19


Prop. Type:


Prop. S/N. :


JAN 30, 2000

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________

AD-PA Compliance Status Report - 20000125 - Propeller 2 - I-DPCZ

R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours



OPEN: TRANSFER TUBE HOURS: TTSN :N/A; TSO: 1625.34



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours



OPEN: ACTUATOR HOURS TTSN :N/A; TSO: 1625.34



R Y ENAC 97-034

FAA 96-25-20 Amdt 39-9863

H.S. ASB 14SF-61-70R2


1997

10.500 Hours



OPEN: PCU HOURS (TSO): 516.12 INSPECTION SCHEDULED EVERY

2000 FH (prop. O/H) AD COMPLIED WITH

(NEXT DUE WITHIN 1483.48) 28/09/2003

A N FAA 2006-24-07

Scheda Analisi PA Jan 3, 2007 -CLOSED-


A N FAA US-2011-04-02

ENAC 2011-68 ADE issued Apr 15, 2011 CLOSED: NOT APPLICABLE AS PER PROPELLER MODEL


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:

Sep 09 2011 Prepared by:

________________________

Approved by:

________________________

I-DPCZ Components Compliance Status

A N FAA 81-21-05

Nov 19, 1981 N/A ARTEX ELT Battery not usable in salt environment

CLOSED: NOT APPLICABLE, SUBJECT ELT BATTERY NOT

INSTALLED

A N TCCA CF-96-21

FAA 72-19-04 Amdt. 39-1782

RAI 74-225 N/A N/A Ni-Cd batterie con celle in

polistirolo



S RAI 82-113

- CLOSED - SUPERS. BY ENAC 96-348

N N TCCA CF-96-21


- CLOSED - CF96-21 ISSUED TO CANCEL THE

APPLICABILITY OF FAA 72-19-04

S RAI 88-052

- CLOSED - SUPERS. BY ENAC 88-096

R Y RAI 88-096

FAR 43 Appendix E


PRESSURE SYSTEM - OPEN -

CARRIED OUT ON JAN 28, 2010; NEXT DUE WITHIN JAN 26, 2012

I Y ENAC 96-052

FAA FAR 91.21 N/A N/A USE OF PORTABLE ELETTRONIC DEVICES

- CLOSED - AFM UPDATED – CREW

INFORMED

N N ENAC 96-348

FAA 96-20-07 Amdt 39-9773 -





HEATER MODEL B4500 (CERAMIC COMBUSTION TUBE)


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N ENAC 97-167

FAA 97-11-10 - N/A PURITAIN-BENNETT CREW OXYGEN MASKS



N N TCCA CF-95-16



REMOVAL


INVERTER INSTALLED (Serie MSI-800)

N N ENAC 97-274




N N ENAC 99-231




S ENAC 00-018



INSPECTION/TEST

- CLOSED - Superseded by ENAC 00-209

N N ENAC 00-209

FAA 99-23-22 Amdt. 39-11686


“C”


AD RESCINDED APR. 12, ‘00



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


S ENAC 01-173


P/N 14D11 o 23D04


HEATER INSTALLED

Supers. By ENAC 01-368

A N ENAC 01-368




HEATER INSTALLED


N N ENAC 01-442

FAA 2001-18-05 Nov 20, 2001 N/A GOODYEAR TIRE AND RUBBER COMPANY.

- CLOSED - NOT APPLICABLE PER P/N

I Y ENAC 01-470


DISCHARGER

- CLOSED - P/N AFFECTED CHECKED.


I Y TCCA CF-2002-14

ENAC 02-167


SoREM BM-CL-61-4234

04/03/2003 N/A



- CLOSED - SB215-4234 IS INCORPORATED

DURING PRODUCTION

I Y ENAC 03-067

FAA 2003-04-06

SoREM DT-CL-34-05

DT-CL-34-07R1 BM-CL-34-4343


- CLOSED - INU P/N 7510100-732 (#1) AND 7510100-731 (#2) INSTALLED

28/09/2003


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N FAA 2003-23-05

ENAC 2004-003 - December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili



N N FAA 2003-23-05

ENAC 2004-073 - December 24, 2005 N/A Titeflex Corporation,

Tubi Flessibili



R Y FAA

2004-21-05 Amdt.39-13826


A 500 heater Hrs or 100 heater Hrs

TIS since 19/11/04


100 Hrs (TIS) or

24 Months

PRESSURE DECAY TEST ed Operational Test del CABIN

HEATER (JANITROL)

- OPEN - HEATER TIME IN

SERVICE CHECKED: 126.36 HOURS AT JAN

20, 2010; TEST NOT YET PERFORMED





PER HEATER INSTALLED


ESP-4-34-001 Within


- OPEN - CARRIED OUT DURING LAST ANNUAL CHECK:

(CRS DATED: 13/06/2011)

A N EASA 2006-0269

- Scheda Analisi PA MODE “S” TRANSPONDERS - CLOSED -

N/A AS PER MODEL NOT INSTALLED


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


A N FAA 2006-18-08 Scheda Analisi AD Oct. 11, 2006 GOODYEAR

NOSE WHEEL TIRES


PER GOODYEAR TIRES NOT

INSTALLED

A N FAA 2006-19-04

Scheda Analisi AD MODE “S” TRANSPONDERS - CLOSED -

N/A AS PER PART NUMBER NOT

INSTALLED

N N FAA 2006-22-05



PER COMPONENT MODIFIED (REF TO

FAA-2003-04-06)

A N EASA 2006-0366

Scheda Analisi PA Dec 14, 2006 LIFE RAFT - CLOSED -


A N EASA 2006-0286R1

Scheda Analisi PA Sep 9, 2006 Oxygen Cylinders - CLOSED -


A N EASA 2007-0256

Scheda Analisi PA Sep 19, 2007 Seat Restraint System - CLOSED -



A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


A N EASA 2007-0294

ENAC 2009-060 Scheda Analisi PA APU Turbine wheel life limit reduction

- CLOSED - NOT EFFECTIVE AS

PER APU NOT INSTALLED ON SOREM

CL415 FLEET

N N EASA 2009-0200

Scheda Analisi AD Sep 22, 2010 N/A Navigation – Mode A/C Transponder – Check /

Modification



N N FAA 2009-20-10

Scheda Analisi AD Jan 17, 2010 N/A Autopilot – servo motors modification



S - CF 2009-42 - SOREM ESB-4-32-

4414 (SMJC 063)

Part I within 50FhPart II: within 750

Fc Part III: every

750 Fc



- CLOSED - SUPERSEDED BY CF


26, 2009)

R Y CF 2009-42R1 Enac 2010-183 Scheda Analisi AD Every 750 Flight cycles


- OPEN - CARRIED OUT WITH

ESB-4-32-4414R1 (SMJC 63 PERFORMED ON JUL 22, 2010); NEXT DUE: 547 CYCLES

Y N EASA 2009-0251

Scheda Analisi AD Nov 26, 2009 N/A Portable Halon 1211 Fire Extinguisher




A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


Y N EASA 2009-0262R1




N N EASA 2009-0278


- CLOSED - NOT EFFECTIVE AS PER P/N INSTALLED

N N TCA CF-2009-44

Scheda Analisi AD Jul 1, 2011 N/A ELT-Potential Failure to Transmit

the Required 406MHz Coded Signal



N N EASA 2010-003R1

Scheda Analisi AD 18 Apr, 2010 N/A TDR-94 and TDR-94D transponders



Y N EASA

2010-0062R1




A Y FAA 2010-07-02

Scheda Analisi AD 31 Ott 2012 N/A Honeywell Primus II RNZ 850()/-851

- OPEN - TO BE INTRODUCED ON BOTH INU 1 & 2.


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N EASA 2010-0067

Scheda Analisi AD 26 Apr, 2010 N/A TDR-94 and TDR-94D transponders



N N EASA 2010-30



SINCE SOREM FLEET IS NOT OPERATING IN CARGO TRANSPORT

CONFIGURATION



PER A/C TYPE, REFER TO ADE ISSUED DATED

NOV 09, 2010

N N FAA 2011-01-09




N N EASA 2011-0043


Modification


ON THE A/C TYPE

N N EASA 2011-0090R1



THE A/C TYPE


A/C Type:

Canadair CL-415

A/C Reg. :

I-DPCZ s/n 2048

Componenti

EFFE

CT

P.A. / A.D. Other

Authority issues




Date:


________________________

Approved by:

________________________


N N EASA 2011-0103



ON THE A/C TYPE

N N FAA

2011-11-04



NOT INSTALLED

N N EASA 2010-0204



NOT INSTALLED

N N FAA 2011-14-08




NOT INSTALLED

R Y TCCA CF-2011-35

- ESB-4-32-A4451 Rev 01




landings


current method




LANDINGS

A Y TCCA CF-2011-35

- ESB-4-32-A4450 Rev 01




Documents

AD-PA Compliance Status Report I-DPCC...S TCCA CF-92-22 FAA 94-04-02 TCCA CF-2003-02 Bombardier SB215-A3040 SoREM AD CF-2003-02 Scheda analisi AD - N/A ENGINE REAR MOUNT STRUTS CLOSED: