AS350B2 s/n 2364 SE-JFL - cdn-3.thejameslist.com s/n 2364 SE-JFL 1. ... AS355F1, AS355F2, AS355N, AS355NP, EC130B4, ... Rotorcraft Flight Manual - Chapter Normal Procedures

STATUS REPORT INDEX AS350B2 s/n 2364 SE-JFL

1. OVERVIEW STATUS AIRFRAME INSPECTIONS

2. AD, ASB, MOD AIRFRAME

3. STATUS! COMPONENT AIRFRAME

4. OVERVIEW STATUS ENGINE INSPECTIONS

5. AD, ASB, MOD ENGINE

6. STATUS! COMPONENT ENGINE

7. MODIFICATIONS – STC

8. BASIC WEIGHT & BALANCE

9. REMAINING REMARKS

10. REPETITIVE (NATIONAL) REQUIREMENTS

AIRFRAME INSP REF TOL Note Last perf. A/C TT Remaining time

SLL (various) 04-10-00 - See Binder tab No.3 -

Time Limits/Maintenace Checks

(various)04-20-00 - 5270,2FH / 34216TC -

Components subject to TBO

(various)05-10-00 - See Binder tab No.3 -

Components subject to OTL

(various)05-11-00 - See Binder tab No.3 -

Components subject to OC 05-12-00 - 5270,2FH / 34216TC -

BFF/ 0 -/ TA/ ALF 05-20-00 0 DAILY DAILY

10FH 05-20-01 1FH DAILY DAILY

10FH / 7D 05-20-02 0 DAILY DAILY

150FH / 12M insp 05-21-00 15FH/36D 5270,2FH / 2015-12-07 5420,2FH / 2016-12-07

150FH insp 05-21-01 15FH 5270,2FH 5420,2FH

12M insp 05-21-02 36D 2015-12-07 2016-12-07

600FH / 24M insp 05-22-00 60FH/73D 5270,2FH / 2015-12-07 5870,2FH / 2017-12-07

Scheduled Airframe Inspections

600FH / 24M insp 05-22-00 60FH/73D 5270,2FH / 2015-12-07 5870,2FH / 2017-12-07

600FH insp 05-22-01 60FH 5270,2FH 5870,2FH

24M insp 05-22-02 73D 2015-12-07 2017-12-07

1200FH / 48M insp 05-23-00 120FH/146D 5270,2FH / 2015-12-07 6470,2FH / 2019-12-07

1200FH insp 05-23-01 120FH 5270,2FH 6470,2FH

48M insp 05-23-02 146D 2015-12-07 2019-12-07

144M insp 05-24-02 180D 2015-12-07 2027-12-07

Specific periodic intervals (various) 05-25-00 -5270,2FH / 34216TC /

2015-12-07-

Punctual Intervals (various) 05-26-00 -5270,2FH / 34216TC /

2015-12-07-

ATA Appl.AD

classAD number

Issue

DateSubject

Appr. Holder / Type

Design.

Effective

date

Expire

datePerformed SB Rec.

65 N/A EADFAA 2015-22-53

(EASA 2015-0178)2015-10-30

Tail Rotor Control

SUPERSEDES FAA EAD 2015-22-52

Applicability: AS350B3 helicopters with a dual hydraulic

system installed, certificated in any category.

AIRBUS HELICOPTERS

AS 350

2015-11-02

N/A. AS350 B3

model only.

67.00.66

SIN 2944-

S-29

65 N/A EADFAA 2015-22-52

(EASA 2015-0178)2015-10-28

Tail Rotor Control

SUPERSEDED BY FAA EAD 2015-22-53

Applicability: AS350B3 helicopters with a dual hydraulic

system installed, certificated in any category.

AIRBUS HELICOPTERS

AS 350

2015-10-29

N/A. AS350 B3

model only.

67.00.66

SIN 2944-

S-29

65 Y AD 2015-0195 2015-09-23

Tail Rotor Drive – Drive Shaft Bearings – Inspection /

Replacement

SUPERSEDES AD F-1998-173-073

Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters,

and AS 355 E, F, F1, F2, N and NP helicopters, all serial

numbers, if equipped with tail rotor (TR) drive shaft bearings

as indicated in Table 1 of this AD.

AIRBUS HELICOPTERS

AS 350

AS 355

2015-10-07 165FH

New

driveshaft

bearings

installed 2015-

11-03. Next

insp: A/CTT

5435,2.

01.00.70 165FH

63 N/A AD FAA 2015-17-11 2015-09-29

Main Rotor System

Applicability: AS350B, AS350BA, AS350B1, AS350B2,

AS350B3,AS350C, AS350D, AS350D1, AS355E, AS355F,

AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2

helicopters with a swashplate assembly with rotating star,

part number (P/N) 350A371003-04, 350A371003-05,

350A371003-06, 350A371003-07, or 350A371003-08,

certificated in any category.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2015-09-29 165FH

2015-04-10

P/N affected,

but repair not

performed =

AD N/A. Test

iaw ASB

performed to

confirm.

62.00.34 No

- N/A AD 2015-0178 2015-08-26

Rotorcraft Flight Manual - Chapter Normal Procedures - Engine

prestart Check / Run-up Check / Engine and Rotor Shutdown -

Amendment

Applicability: AS 350 B3 helicopters, all serial numbers, if

equipped with a dual hydraulic system, production

modification (mod) OP 3082, or mod OP 3346.

AIRBUS HELICOPTERS

AS 3502015-08-31 2015-09-07

67.00.66

SIN 2944-

S-29

63 N/A PAD 15-104 2015-08-03

Rotor Drive - Main Gearbox Main and Bottom Casings -

Inspection/Replacement


equipped with MGB main casing P/N 350A32-3156-21 (fitted

on assembly P/N 350A32-3156-01), or P/N 350A32-3156-22

(fitted on assembly P/N 350A32-3156-02), or P/N 350A32-

3121-04, or P/N 350A32-3121-06, or if equipped with MGB

bottom casing (sump) P/N 350A32-3119-05.

AIRBUS HELICOPTERS

AS 350- 165FH/6M - 01.00.68

63 Y PAD 15-105 2015-08-03

Rotor Drive - Main Gearbox Bottom Casing -


Applicability: AS 350 B1, B2 and AS 355 E, F, F1, F2, N

helicopters, all serial numbers, if equipped with MGB bottom

casing (sump) P/N 350A32-3119-03 or P/N 350A32-3119-05.

AIRBUS HELICOPTERS

AS 350

AS 355

- 165FH/6M

2015-12-04:

The recorded TC

on MGB sump is

34216 /FH is

5270,2. No

further action is

required until

TC has reached

93700 (PHAB

WO 17220006).

01.00.56

01.00.69

.05 y AD 2015-0132 2015-07-08

Time Limits / Maintenance Checks - Aitworthiness Limitations

/ Maintenance Requirements - Implementation

SUPERSEDES AD 2013-0088

Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 D, AS

350 B1, AS 350 B2, AS 350 B3, EC 130 T2 and EC 130 B4

helicopters, all serial numbers.

AIRBUS HELICOPTERS

AS 350 / EC 1302015-07-22 2016-07-22

Perf iaw AMP

AS350B2 SE-

JFL 2015-11-

27 / PHAB

CAMO

SE.MG.0107

AS350B2

ALS

REVISION

005

67 N/A PAD 15-087 2015-06-24

Rotor Flight Control - Tail Rotor Control Stop Screws -

Modification


Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS

350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers

(s/n), if equipped with adjustable primary yaw stop in the

baggage compartment which corresponds to modification

(MOD) 071908, or MOD 171912, or MOD 073252, except

those helicopters that have incorporated MOD 074602.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

14 D after

Final AD

issue date.

110FH =>

660FH/13M

Only

applicable for

autopilot

05.00.64

67.00.61110FH

63 Y AD 2015-0094 2015-05-29

Main Rotor Drive - Cross-Bar - Inspection


and AS 355 E, F, F1, F2, N and NP helicopters, and EC130 B4

and T2 helicopters, all serial numbers.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2015-06-12

Next

scheduled

MGB

removal

Perf 2015-11-

21 by PHAB

iaw WO

17220006.

Next insp:

9770,2FH /

94216TC.

05.00.84

4500F

H/

60000

TC

33 N AD 2013-0281R1 2015-01-30

Lights - Position Strobe Light - Inspection / Deactivation /

Modification

SUPERSEDES AD 2011-0244-E


350 B2, AS 350 B3 and AS 350 D helicopters, all s/n, if modified

in production with (optional) modification OP0811 and

equipped with a Grimes-Honeywell power supply unit, Part

Number (P/N) 60-1431-3, in the baggage compartment as

part of that optional modification, except helicopters that have

embodied at least one of the modifications as listed in

Appendix1 of this AD.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2015-02-13 See AD

2015-04-10

N/A. MOD

OP0811 not

embodied.Ho

neywell pwr

suppl unit not

installed.

33.00.33R

1

25 N AD 2014-0279 2014-12-19

Equipment / Furnishing - Restraint System Rotary Buckle Sub-

Assembly - Identification / Replacement

Applicability: Romtex Anjou Aeronautique model 358 torso

restraint systems.

These restraint systems are known to be installed on, but not

limited to, Airbus Helicopters EC130 T2, AS 350 B2 and B3

helicopters.

ROMTEX ANJOU

AERONAUTIQUE

Torso Restraint

Systems

2015-01-022015-02-02

see AD

2015-04-10

N/A.

Equipment

not installed.

Another

brand

installed.

63 N AD 2014-0233 2014-10-23

Rotor Drive - Hydraulic Pump Bearing - Inspection /

Replacement

SUPERSEDES AD 2013-0284R1


350 B2, AS 350 B3 and AS 350 D helicopters, all serial

numbers,

* if equipped with single hydraulic system (PRE MOD OP3346

or OP3082) and incorporating Airbus Helicopters, modification

079566 (hydraulic pump drive assembly part number (P/N)

350A35-0132-00 equipped with bearing P/N 704A33651243),

or

* modified in service by Airbus Helicopter Alert Service Bulletin

(ASB) No. 05.00.72 Rev.04 when the pump drive assembly is

equipped with bearing P/N 704A33651243,

except helicopters which embody modification 079568

(hydraulic pump drive assembly P/N 350A35-0132-01 fitted

with bearing P/N 704A33651269).

AIRBUS HELICOPTERS

AS 350 / EC 1302014-10-31 See AD

2015-04-10

N/A. Bearing

not installed.

H/C too old

63.00.24

20 N AD CF-2014-26 2014-08-25

Standard Practices - Helicopter External Transport System

(HETS) - Unapproved Parts, Inadequate Service Life Limits and

Maintenance Requirements

Applicability: Airbus Helicopters (formerly Eurocopter France)

model AS350 B, AS350 B1, AS350 B2, AS350 B3, AS350 BA and

AS350 D.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

BELL HELICOPTER

TEXTRON CANADA

(BHTC)

206

407

BELLIS INVESTMENTS

LTD

STC SH98-35

MD HELICOPTERS INC

(MDHI)

369

500N

2014-08-28

120D/12M/4

Y

see AD

2015-04-10

N/A. No

Canadian

parts

63 N AD 2013-0284R1 2014-07-25

SUPERSEDED BY EASA AD 2014-0233




numbers,

- if equipped with single hydraulic system (PRE MOD OP3346

or OP3082) and incorporating Airbus Helicopters modification

079566 (hydraulic pump drive assembly part number (P/N)

350A35-0132-00),

- except pumps with a pump support P/N followed by the

letter "V", and

- except helicopters which embody modification 079568

(hydraulic pump drive assembly P/N 350A35-0132-01 fitted

with bearing P/N 704A33651269).

AIRBUS HELICOPTERS

AS 350 / EC 1302014-08-08 See AD N

05.00.72R

4

62 N AD2014-0132R1

FAA 2015-17-112014-06-02

Main Rotor - Rotating Star Swashplate - Inspection /

Replacement


all serial numbers, if equipped with a swashplate assembly

comprising a rotating star with Part Number (P/N)

350A371003-04, P/N 350A371003-05, P/N 350A371003-06,

P/N 350A371003-07 , or P/N 350A371003-08.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2014-06-092014-07-09

see AD

2015-04-10

P/N affected,

but repair not

performed =

AD N/A. Test

iaw ASB

performed

2015-11-21

iaw PHAB

WO17220006

to confirm.

62.00.34

53 N/A EAD 2014-0076-E 2014-03-25

Fuselage - Rear Structure Junction Frame Reinforcement

Angles - Inspection


all serial numbers,

- if incorporating modification (MOD) 07 3215, or

- if equipped with at least one reinforcement angle, Part

Number (P/N) 350A08.2493.21 or P/N 350A08.2493.23,

following the repair carried out in accordance with MRM Work

Card 53.10.22.772 or AMM Task 53-31-00, 8-5.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2014-03-2710FH ->

Every 165FH

N/A due to

PRE MOD

073215. See

ASB 05.00.43

05.00.70 165FH

23 Y IN 2670-I-23 2013-12-19VHF-AM Systems: European requirement concerning VHF 8.33

kHz channel spacing

AIRBUS HELICOPTERS

AS 350

AS 355

EC 120

EC 130

AS 365

EC 155

SA 330

AS 332

EC 225

2013-12-19 2018-01-01To be

performed.

- N/A AD 2013-0287 2013-12-05

Rotorcraft Flight Manual - Engine Digital Electronic Control

Unit Emergency Procedure - Amendment

Applicability: AS 350 B3 and EC 130 T2 helicopters, all serial

numbers, if equipped with ARRIEL 2D engine and THALES

FADEC Part Number (P/N) C13165DA00 or P/N C13165FA00.

AIRBUS HELICOPTERS

AS 350 / EC 1302013-12-12 See AD N 01.00.67

76 N/A EAD 2013-0191-E 2013-08-22

Engine controls - Switches 53Ka, 53Kb and 65K - Inspection /

Modification



equipped with an ARRIEL 2B1 engine incorporating the two-

channel FADEC (MOD 073254), and embodying modification

MOD 073261 (new twist grip).

AIRBUS HELICOPTERS

AS 350 / EC 1302013-08-23 See AD

2015-04-08

N/A. AS350 B3

model only.

80.00.09R

1

64 Y AD 2013-0133 2013-06-28

Tail Rotor - Tail Rotor Hub Pitch Horn - Inspection /

Replacement

Applicability: (B, BA, BB, B1, B2, B3, D) AS350/AS355

helicopters, all serial numbers, equipped with Tail Rotor Hub

(TRH) pitch horn assemblies P/N 350A121368.01, P/N

350A121368.02, P/N 350A121368.03, or P/N 350A121368.04,

incorporating TRH pitch horn P/N 350A121368.XX (where XX

stands for two digit dash number excluding 01, 02, 03, and 04

which are reserved for assemblies).

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2013-07-0310FH ->

Every 165FH

Perf 2015-12-

03 by PHAB,

WO17220006

at A/CTT

5270,2. Next

insp: A/CTT

5435,2.

05.00.74 165FH

67 N EAD 2013-0095-E 2013-04-16

Rotor Flight Controls - Main/Tail Rotor Servo-Control Bearings -

Inspection / Replacement


350 B2, AS 350 B3 and AS 350 D, all serial numbers, equipped

with single hydraulic main and tail servo-controls

manufactured by “SAMM”, “TRW”, “GOODRICH”, or “UTAS”.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2013-04-18 10FH/7D

2015-11-12

N/A. Installed

Servo S/N

(6030, 6137,

3175) not

affected.

.05 N AD 2013-0088 2013-04-10

SUPERSEDED BY PAD 15-070


Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 D, AS

350 B1, AS 350 B2, AS 350 B3 and EC 130 B4 helicopters, all

serial numbers.

AIRBUS HELICOPTERS

AS 350 / EC 1302013-04-24 2013-04-24 N/A

76 N/A AD 2013-0061 2013-03-11

SUPERSEDED BY EASA EMERGENCY AD 2013-0191-E



equipped with an ARRIEL 2B1 engine incorporating the two-

channel FADEC (MOD 073254), and embodying modification

MOD 073261 (new twist grip), except helicopters that embody

modification 074263.

AIRBUS HELICOPTERS

AS 350 / EC 1302013-03-25 See AD N

05.00.61R

1

80.00.09

63 N EAD 2013-0044-E 2013-02-27

SUPERSEDED BY EASA EAD 2013-0284-E



numbers, if equipped with single hydraulic system (PRE MOD

OP3346 or OP3082) and incorporating Eurocopter

modification 079566 (new hydraulic pump drive).

AIRBUS HELICOPTERS

AS 350 / EC 1302013-03-01 See AD N 05.00.72

64 N/A AD 2013-0029 2013-02-08

Rotorcraft Flight Manual - Section Limitations - Amendment

Tail Rotor - Laminated Half-Bearings - Inspection /

Replacement / Modification



modified in production by incorporating Eurocopter

modification (MOD) 07 5601, except those helicopters that

have been modified by incorporating Eurocopter MOD 07 5606

in production.

AIRBUS HELICOPTERS

AS 350 / EC 1302013-03-01 See AD

2015-04-08

N/A. AS350 B3

model only.

01.00.65R

1

01.00.66

64 Y EAD 2012-0257-E 2012-12-05

Tail Rotor - Laminated Half-Bearings - Inspection /

Replacement


350 B2 and AS 350 D helicopters, all serial numbers (s/n).

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2012-12-07Every day

(ALF)

Perf 2015-12-

03 by PHAB,

WO17220006

at A/CTT

5270,2. Next

insp: A/CTT

5280,2

05.00.71

R1

ALF /

10FH

67 N/A AD 2012-0252 2012-11-28

Rotor Flight Controls - Twist Grip Assembly - Adjustment /

Functional Check / Replacement / Modification



equipped with the ARRIEL 2B engines.

AIRBUS HELICOPTERS

AS 350 / EC 1302012-12-12 See AD

2015-04-07

N/A. B3

model only

05.00.49R

3

64 N/A EAD 2012-0217-E 2012-10-19





modification (MOD) 07 5601.

AIRBUS HELICOPTERS

AS 350 / EC 1302012-10-19 See AD N 01.00.65

64 N/A EAD 2012-0207-E 2012-10-05




modification (MOD) 07 5601.

AIRBUS HELICOPTERS

AS 350 / EC 1302012-10-05 See AD N 01.00.65

52 N AD 2012-0205 2012-10-01

Doors - Sliding Door Lower Ball-joint - Modification



(s/n), if equipped with sliding doors, except those that embody

modification AL. 4262.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2012-10-15 165FH/13M

2015-04-10

N/A. No

sliding doors

52.00.34

26 N/A AD 2012-0033R1 2012-02-27

Fire Protection - Fire Detection System - Modification


equipped with a Turbomeca ARRIEL 1D1 engine and

incorporating Eurocopter modification (mod) 73273, except

helicopters that incorporate mod 074346.

AIRBUS HELICOPTERS

AS 350 / EC 1302012-02-27 40FH/75D

MOD 073273

not

incorporated

26.00.02

33 N EAD 2011-0244-E 2011-12-22




(s/n), if modified in production with (optional) modification

OP0811 and equipped with a Grimes-Honeywell power supply

unit, Part Number (P/N) 60-1431-3, in the baggage

compartment as part of that optional modification.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2011-12-23 See AD

2011-12-22

N/A to

configuration

05.00.66

34 N AD 2011-0239 2011-12-15

Navigation- Radio Altimeter Indicator- Modification

Applicability: Radio altimeter indicator IND201, Part Number

(P/N) 102-2100, all serial numbers. The affected radio

altimeter indicators are known to be installed on, but not

limited to, Eurocopter (formerly Eurocopter France,

Aerospatiale) EC 120 B, AS 350 B2, AS 350 B3 and AS 355 NP

helicopters .

SMS (trading as

Cobham Avionics)

IND201 Radio

Altimeter Indicators

2011-12-292012-06-29

see AD

2015-04-10

N/A.

Equipment

not installed

76 N/A AD 2011-0237 2011-12-14




equipped with the ARRIEL 2B engine.

AIRBUS HELICOPTERS

AS 350 / EC 1302011-12-28 See AD N 05.00.49

67 N AD 2011-0164 2011-08-31

Rotors Flight Control - Tail Rotor Control Stop Screws -

Inspection



(s/n), if equipped with an Autopilot (AP).

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2011-09-14110FH ->

Every 110FH

2011-08-31

N/A. No

autopilot

installed

05.00.64

25 Y AD 2011-0103 2011-05-27

Equipment / Furnishings - Emergency Locator Transmitter

(ELT) Antenna - Modification / Replacement


Applicability: Tri-Band ELT antennas, Part Number (P/N) 21-41

( ) series, all serial numbers (s/n) up to 12999 inclusive, which

are used in combination with a large variety of ELT units; see

also Note below.

Chelton P/N 21-41 ( ) series antennas installed in combination

with the following ELT units are not affected by this AD:

*Chelton Avionics, Inc DBA Wulsberg Electronics (formerly

ARTEX) ELT model C406-N HM, P/N 453-5061,

*Chelton Avionics, INC DBA Wulsberg Electronics (formerly

ARTEX) ELT model C406-N, P/N 453-5060, and

*ELTA ELT model ADT406²AF/AP-H, P/N 01N65901 rev. (x)

The affected antennas are known to be installed on, but not


Aerospatiale) AS 350, EC 155 and AS 332 series helicopters.

CHELTON LTD

(COBHAM ANTENNA

SYSTEMS)

Tri-Band ELT

Antennas

2011-06-03 See AD

2015-04-09

Verified

performed

Chelton

Limited

(trading

as

Cobham

Antenna

Systems)

SB

02/2011

Issue 1

65 N AD 2011-0104 2011-05-27

Tail Rotor Drive - Tail Gearbox (TGB) Casing Assembly -


Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters

and AS 355 E, F, F1, F2, N and NP helicopters, all serial

numbers.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2011-06-10 110FH/13M

2011-05-27

N/A to casing

P/N and S/N

(2015-04-08

N/A. P/N

350A33-1090-

01 installed)

65.00.46

25 N AD 2011-0093 2011-05-20


Applicability: Tri-Band ELT antennas, Part Number (P/N) 21-41

( ) series, all serial numbers (s/n) up to 12999 inclusive, which

are used in combination with a large variety of ELT units

without electro-static discharge (ESD) protection. ESD

protection is identified by a declaration of category A of

section 25 of RTCA, Inc. DO160 version D change 3 (or later

version) or EUROCAE ED-14D (or later version); see also Note

below.

Chelton P/N 21-41 ( ) series antennas installed in combination

with the following ELT units are not affected by this AD:

*Chelton Avionics, Inc DBA Wulsberg Electronics (formerly

ARTEX) ELT model C406-N HM, P/N 453-5061,

*Chelton Avionics, INC DBA Wulsberg Electronics (formerly

ARTEX) ELT model C406-N, P/N 453-5060, and

*ELTA ELT model ADT406²AF/AP-H, P/N 01N65901 rev. (x)

The affected antennas are known to be installed on, but not


Aerospatiale) AS 350, EC 155 and AS 332 series helicopters.

CHELTON LTD

(COBHAM ANTENNA

SYSTEMS)

Tri-Band ELT

Antennas

2011-06-03 See AD N

Chelton

Limited

(trading

as

Cobham

Antenna

Systems)

SB

02/2011

Issue 1

25 N AD 2011-0072 2011-04-20

Equipment & Furnishings - Emergency Flotation Gear

Attachment Brackets - Inspection / Replacement



numbers, if equipped with fixed parts of the emergency

flotation gear.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2011-05-04 See AD

2011-05-27

N/A. Not

installed

05.00.63

- N AD US-2011-08-06 2011-04-13 Power Turbine Rotors - Identification / Replacement

HONEYWELL

INTERNATIONAL INC

LTP101

LTS101

2011-05-17 See AD

2015-04-08

N/A. Engine

type not

installed

N/A

65 N EAD 2011-0038-E 2011-03-04

[Correction] Tail Rotor Drive - Tail Gearbox (TGB) Control Lever

- Inspection / Rework / Replacement


Applicability: AS 350 B, BA, BB, B1, B2, and D helicopters, all

serial numbers, all serial numbers, if equipped with TGB

control lever Part Number (P/N) 350A33-1058-00, P/N 350A33-

1058-01, P/N 350A33-1058-02, or P/N 350A33-1058-03.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2011-03-08 See AD

2010-06-17

N/A to

350A33-1526

Lever

05.00.62R

1

29 Y AD 2011-0033 2011-03-01

Hydraulic Power - Forward Hydraulic Servo Control Hoses /

Protection Installation

Applicability: AS 350 B, BA, BB, D, B1, B2, and B3 helicopters,

all serial numbers, with a single hydraulic power system and

the following forward (pitch) servo-control hydraulic hoses

installed:

- P/N 704A34-412-033 (other reference MP/N 675-102-05-

01);

- P/N 704A34-412-035 (other reference MP/N 675-102-06-

01).

AIRBUS HELICOPTERS

AS 350 / EC 1302011-03-15 2011-04-15

2011-04-04

Sleeves

installed

A/CTT 4658,3

29.00.13

25 N AD 2009-0122R1 2010-10-27

Equipment / Furnishings -Load Release Units - Inspection /

Modification / Limitation

Applicability: Eurocopter helicopter models:

EC 120 B, AS 350 B, BA, B1, B2, B3, BB and D, EC 130 B4, AS

355 E, F, F1, F2 and N, AS 365 N, N1, N2 and N3, EC 155 B and

B1, SA 330 F, G and J, AS 332 C, C1, L, L1 and L2, EC 225 LP, all

serial numbers, if equipped with any type of SIREN Load

Release Units.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

EC 120 B

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

2010-11-10 See AD

2009-06-15

N/A.

Equipment

not installed

01.00.49

65 N EAD 2010-0082-E 2010-04-28


Applicability: AS 350 B, BA, BB, B1, B2, and D helicopters, all

serial numbers, and AS 355 E, F, F1, F2 and N helicopters, all

serial numbers, if equipped with TGB control lever Part

Number (P/N) 350A33-1058-00, P/N 350A33-1058-01, P/N

350A33-1058-02, or P/N 350A33-1058-03, except those

marked with an “X”.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2010-04-29 See AD

2010-06-17

N/A to

350A33-1526

Lever

05.00.62R

1

25 N AD 2010-0014 2010-02-26

Equipment and Furnishings - Hoist Operator's Belt Snap Hook -



Applicability: EUROCOPTER helicopters:

- AS 350 B, BA, BB, B1, B2, B3 and D, before embodiment of

MOD 073299. All serial numbers (S/N) if equipped with an

operator’s belt (called "hoist operator’s belt") part number

(P/N) 330A87-0730-00, 330A87-2371-00, 341A84-1120-00,

350A84-0047-00, 360A84-0040-00, 360A84-0040-01 or

360A84-0040-02, fitted with a snap hook P/N GA343-95, and,

All S/N if equipped with a hoist operator’s belt P/N 3160S73-

08-200-1 fitted with a snap hook P/N 4100-80AT28.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 315/316/319

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

2010-02-09 See AD

2010-04-28

N/A. Hoist not

installed

25.00.89

25.00.93

25 N AD 2009-0183-CN 2010-02-11

CANCELLATION NOTICE - Equipment / Furnishings - D-Lok

Hook of the Rescue Hoist - Inspection / Removal from Service /

Replacement


Applicability: Eurocopter model AS332, AS350, AS355, SA365,

AS365 and EC155 series and EC225 LP helicopters, all serial

numbers, if equipped with Lifesaving Systems D-Lok Hooks

with part numbers (P/N) 410-A or 410-F and identified as part

of lot number 208 or 1108.

AGUSTAWESTLAND

A109

AB 139

AW 139

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

AIRBUS HELICOPTERS

DEUTSCHLAND

EC135/635

MBB-BK 117

SIKORSKY

S-61

S-76

S-92

2010-02-11 2010-02-11

Ref.

Publicatio

ns: FAA

AD US-

2010-03-

02

26 N AD 2009-0277R1 2010-02-05

Fire Protection - Portable Halon 1211 Fire Extinguishers -

Identification / Replacement

Applicability: Eurocopter helicopter models:

EC 120 B, AS 350 B, BA, B1, B2, B3, BB and D, and EC 130 B4,

AS 355 E, F, F1, F2, N and NP, SA 341 G and SA 342 J if

equipped with P/N 863520-00 portable fire extinguishers,

serial numbers (s/n) as listed in L’Hotellier Service Bulletin (SB)

863520-26-001.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

EC 120 B

SA 341/342

2010-02-05 2010-08-05

2010-03-12

N/A to

General S/N

0640211

L’Hotellie

r SB

863520-

26-001

.05 Y AD 2010-0006 2010-01-07

Time Limits / Maintenance Checks - Tail Rotor (TR) Pitch-

Change Links - Inspection

Applicability: Models AS 350 B, AS 350 BA, AS 350 BB, AS 350

B1, AS 350 B2, AS 350 B3 and AS 350 D helicopters, all serial

numbers, if equipped with TR pitch-change links having Part

Number (P/N) 350A33-2100-00, 350A33-2100-01, 350A33-

2100-02, 350A33-2100-03, 350A33-2100-04, 350A33-2121-

00, 350A33-2121-01, 350A33-2121-02, 350A33-2143-00,

350A33-2145-00 or 350A33-2145-01 .

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2010-01-2130FH ->

Every 30FH

Performed

2015-11-30

iaw PHAB WO

17220006.

Next insp:

A/CTT 5300,2.

05.00.60 30FH

N AD US-2009-24-12 2009-12-03 Gas Generator Turbine Disc - Reduced Life Limit - Replacement

HONEYWELL

INTERNATIONAL INC

LTP101

LTS101

2010-01-04 See AD

2015-04-08

N/A. Engine

type not

installed

N/A

76 N AD 2009-0256 2009-12-02


Applicability: AS350 B3 and EC130 B4 helicopters, all serial

numbers, if equipped with the ARRIEL 2B1 engine associated

with the two-channel FADEC, and embodying modification

(MOD) 073254 (AS 350 B3) or MOD 073773 (EC 130 B4) (new

twist grip).

AIRBUS HELICOPTERS

AS 350 / EC 1302009-12-16 See AD N 05.00.61

25 N EAD 2009-0179-E 2009-08-11

SUPERSEDED BY EASA AD 2009-0183-E



AS365 and EC155 series and EC225 LP helicopters, all serial

numbers, if equipped with Lifesaving Systems D-Lok Hooks

with part numbers (P/N) 410-A or 410-F and identified as part

of lot number 208 or 1108.

AGUSTAWESTLAND

A109

AB 139

AW 139

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

AIRBUS HELICOPTERS

DEUTSCHLAND

EC135/635

MBB-BK 117

SIKORSKY

S-61

2009-08-12 See AD N

Goodrich

Service

Bulletin

42315-

489-01R1

25 N EAD 2009-0148-E 2009-07-09




SA365, AS365 and EC155 series, EC225 LP and SA360 C

helicopters, all serial numbers, if equipped with Lifesaving

Systems D-Lok Hooks with part numbers (P/N) 410-A or 410-F

and identified as part of lot number 208 or 1108.

AGUSTAWESTLAND

A109

AB 139

AW 139

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

AIRBUS HELICOPTERS

DEUTSCHLAND

BO 105

EC135/635

MBB-BK 117

SIKORSKY

S-61

2009-07-11 See AD N

Goodrich

Service

Bulletin

42315-

489-01R1

25 N AD 2009-0124 2009-06-12


Applicability: Eurocopter model AS332, AS365, AS350, AS355,

EC225, SA330, SA360 and EC155 series helicopters fitted with

Goodrich hook kit or rescue hoist assemblies as identified in

table 1 of Goodrich Service Bulletin 42315-489-01 revision 1,

dated 05 June 2009.

AGUSTAWESTLAND

A109

AB 139

AW 139

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

AIRBUS HELICOPTERS

DEUTSCHLAND

EC135/635

MBB-BK 117

2009-06-26 10FH

2009-06-18

N/A. Not

installed

Goodrich

Service

Bulletin

42315-

48901R1

64 N AD 2009-0039 2009-02-19

Tail Rotor - Tail Rotor Blades Skin - Inspection / Repair


Applicability: EUROCOPTER helicopter models:

- AS 350 B, BA, BB, B1, B2, B3 and D

all serial numbers, if equipped with tail rotor blades, P/N:

- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/

-12/ -13/ -14.

- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.

- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2009-03-05

2015-09-24:

T/R Blades

P/N 355A12-

0040-14

installed.

2009-12-09

Perf A/CTT

4274,8

05.00.40R

3

Daily/A

LF

80 Y AD 2009-0027 2009-02-18

Engine Starting - Starter-Generator Damping Assembly -

Adjustment


Applicability: AS 350 B, BA, BB, B1, B2, B3 and EC 130 B4

helicopters, all serial numbers, if equipped with ARRIEL

engines where Aircraft Parts Corporation (APC) starter-

generators with Part Number (P/N) 150SG122Q or P/N

200SGL130Q without “004” marking on their name plates are

installed.

AIRBUS HELICOPTERS

AS 350 / EC 1302009-03-04 110FH/3M

2009-05-10

Performed

A/CTT 4001,0

80.00.07R

1

55 Y AD 2009-0030 2009-02-12

Stabilizers - Upper and Lower Fin Attachment Fitting -

Inspection / Modification / Replacement


Applicability: AS 350 B, B1, B2, B3, BA, BB and D helicopters,

all serial numbers if fitted with the following upper and lower

fins on which modification (MOD) 073330 has not been

embodied:

Upper fin assembly part number (P/N): 350A14-0020-00XX,

350A14-0020-01XX, 350A14-0020-02XX, 350A14-0020-03XX,

350A14-0020-08XX, 350A14-0020-09XX, 350A14-0020-10XX,

350A14-0020-17XX, 350A14-0020-18XX, 350A14-0020-19XX,

350A64-1144-00XX

Lower fin assembly P/N: 350A14-0021-00XX, 350A14-0021-

01XX, 350A14-0021-02XX, 350A14-0021-03XX, 350A14-0021-

04XX

AIRBUS HELICOPTERS

AS 350 / EC 1302009-02-26 See AD

2009-04-09

A/CTT 3914,4

55.00.13R

2

55.00.16R

1

MOD

073330

67 Y AD 2009-0019 2009-02-03

Rotors Flight Control - Collective Pitch Lever Locking Stud -

Inspection / Repair


Applicability: All AS350 B, BA, BB, B1, B2, B3, D helicopters,

• Delivered before embodiment of modification 073175; or

• Helicopters on which the locking studs or the collective pitch

levers or the locking strips have been reworked or modified in

service; or

• Helicopters having accomplished Revision 0 or Revision 1 of

EUROCOPTER SB No. 67.00.37, corresponding to modification

073237; or

• Helicopters with a serial number equal to: 3972, 3973, 3982,

3987, 4003, 4023, 4046, 4050, 4086, 4120, 4122, 4132, 4143,

4152, 4172, 4194, 4259, 4314, 4324, 4378, 4392, 4447, 4452,

4477, 4489, 4490, 4501, 4523, 4546, 4560, 4589, 4594, 4599,

4632, 4659, 4666, 4671.

AIRBUS HELICOPTERS

AS 350 / EC 1302009-02-17 See AD

Perf 2015-11-

21 iaw PHAB

WO

17220006.

MOD 073237

implemented

iaw SB 67-00-

37. Next insp:

A/CTT 5930,2

/ 2017-11-21

EASB

05.00.58

660FH

/2Y

64 N AD 2007-0138R2 2009-02-03



Applicability: EUROCOPTER helicopters models:

- AS 350 B, BA, BB, B1, B2, B3 and D - all serial numbers, if

equipped with tail rotor blades, Part Number (P/N) :

- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/

-12/ -13/ -14.

- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.

- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2007-05-18 See AD N05.00.40R

2

.05 N AD 2009-0011 2009-01-28


Applicability: AS 350B, BA, BB, B1, B2, B3 and EC 130B4

helicopters, all serial numbers.

AIRBUS HELICOPTERS

AS 350 / EC 1302009-02-11 See AD N N/A

80 N AD 2009-0004 2009-01-12


Applicability: AS 350 B, BA, BB, B1, B2, B3 and EC 130 B4

helicopters, all serial numbers if equipped with Aircraft Parts

Corporation (APC) 150SG and 200SGL-type starter-generators.

AIRBUS HELICOPTERS

AS 350 / EC 1302009-01-26 See AD N 80.00.07

25 N EAD 2008-0214-E 2008-12-08

Equipment & Furnishing - Emergency Flotation Gear -

Inspection / Limitation / Replacement


Applicability: AS350 B, BA and D helicopters, all serial numbers

equipped with the emergency flotation gear installation.

AIRBUS HELICOPTERS

AS 350 / EC 1302008-12-10 See AD

2009-03-27

N/A to 350B201.00.59

67 N EAD 2008-0205-E 2008-12-02


Applicability: All AS350 B, BA, BB, B1, B2, B3, D helicopters,

• Delivered before embodiment of modification 073175; or

• Helicopters on which the locking studs or the collective pitch

levers or the locking strips have been reworked or modified in

service; or

• Helicopters having accomplished Revision 0 or Revision 1 of

EUROCOPTER SB No. 67.00.37, corresponding to modification

073237; or

• Helicopters with a serial number equal to: 3972, 3973, 3982,

3987, 4003, 4023, 4046, 4050, 4086, 4120, 4122, 4132, 4143,

4152, 4172, 4194, 4259, 4314, 4324, 4378, 4392, 4447, 4452,

4477, 4489, 4490, 4501, 4523, 4546, 4560, 4589, 4594, 4599,

4632, 4659, 4666, 4671.

AIRBUS HELICOPTERS

AS 350 / EC 1302008-12-04 See AD N 05.00.58

25 N AD 2008-0189 2008-10-10

Equipment and Furnishings - Emergency Flotation Gear -

Replacement

Applicability: All AS350 BA helicopters, all serial numbers fitted

with emergency flotation gear including the container

assemblies listed below and for which an operating time limit

extension has not been already granted by the equipment

manufacturer AERAZUR:

- Left hand (LH) container assembly P/N 158170 or P/N

158210-1 and

- Right hand (RH) container assembly P/N 158171 or P/N

158215-1.

AIRBUS HELICOPTERS

AS 350 / EC 1302008-10-24 2008-11-24

2015-04-08

N/A. AS350

BA only.

Emergency

Flotation Gear

not installed.

25.01.02

55 N AD 2008-0121 2008-06-27


SUPERSEDES AD 2006-0095 and AD 2006-0060-E

Applicability: AS 350 B, B1, B2, B3, BA, BB and D helicopters,

all serial numbers, fitted with the following upper and lower

fins to which modification (MOD) 073330 has not been

embodied:

- Upper fin assembly P/N: 350A14-0020 – 00XX; Upper fin

assembly P/N: 350A14-0020 – 01XX; Upper fin assembly P/N:

350A14-0020 – 02XX; Upper fin assembly P/N: 350A14-0020 –

03XX; Upper fin assembly P/N: 350A14-0020 – 08XX; Upper fin

assembly P/N: 350A14-0020 – 10XX; Upper fin assembly P/N:

350A14-0020 – 18XX; Upper fin assembly P/N: 350A14-0020 –

19XX.

- Lower fin assembly P/N: 350A14-0021 – 00XX; Lower fin

assembly P/N: 350A14-0021 – 01XX; Lower fin assembly P/N:

350A14-0021 – 02XX; Lower fin assembly P/N: 350A14-0021 –

04XX.

AIRBUS HELICOPTERS

AS 350 / EC 1302008-07-11 See AD N

55.00.16

55.00.13

25 Y AD 2008-0044 2008-02-27

Equipment / Furnishings - Rear Bench Seat and Sliding Doors -

Limitation / Removal / Modification.

Applicability: AS 350 helicopters models B, BA, BB, B1, B2, B3,

D and AS 355 helicopters models E, F, F1, F2, N, equipped with

rear bench seat, unless modified in

accordance with Modification (MOD) 073166 [AS 350 Service

Bulletin No.25.00.70 or AS 355 Service Bulletin No.25.00.66].

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2008-03-12 2001-03-21 25.00.70

67 N AD 2007-0289 2007-11-19

Rotor flight controls - Collective lever recess - Modification.

Applicability: EUROCOPTER helicopters models AS 350 B, AS

350 B1, AS 350 D, AS 355 E, AS 355 F, AS 355 F1 and AS 355

F2, all pre MOD 071995.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2007-12-03 See AD2008-02-25

N/A to B2

67.00.16R

2

25 N AD 2007-0256 2007-09-19

Equipment and Furnishing - Seat Restraint System Plastic

Rotary Buckle Handle - Inspection/Replacement

Applicability: All the Pacific Scientific rotary buckles p/n’s

1111430-XX and 1111475-XX used on restraint systems p/n’s:

2000029-01, 2000067-01, 2000115-101, 2000029-03,

2000115-121, 2000029-101, 2000029-121 manufactured from

November 2004 through May 2007 inclusive. These p/n’s are

known to be installed on, but not limited to, Eurocopter a/c

models AS 350, AS 355, EC120, EC 130, EC 155.

PACIFIC SCIENTIFIC

COMPANY

Seat Restraint System

2007-10-03 See AD

2008-03-05

N/A.

Equipment

not installed

05.00.55R

2

52 N AD 2007-0236 2007-08-31

Doors - Sliding Door Rear Roller Support Shaft and Rear Fitting -



Applicability: Models AS 350 B, AS 350 BA, AS 350 BB, AS 350

B1, AS 350 B2, AS 350 B3 and AS 350 D, all serial numbers, if

fitted with sliding door(s) pre-MOD 073298 and/or pre-MOD

073308.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2007-09-14 2007-09-30

2008-03-05

N/A.

Equipment

not installed

05.00.47R

1

52.00.30R

1

.05

52N AD 2006-0251R2 2007-06-29


SUPERSEDES AD F-2005-136

Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,

fitted with sliding door(s) before embodiment of MOD 073298

and/or MOD 073308.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-09-01 See AD N

67 N EAD 2007-0141-E 2007-05-21

Rotor Flight Controls - Main & Tail Rotors Servo-Controls -

Inspection / Replacement.

Applicability: EUROCOPTER helicopters models: - AS 350 B, BA,

BB, B1, B2, B3 and D all serial numbers, and equipped with

GOODRICH main rotor servo-controls and tail rotor servo-

controls with no letter “C” marked in the inspection box of the

servo-control identification plate, and with the following Part

Numbers (P/N) and Serial Numbers (S/N):

- Main rotor servo-controls P/N SC5083 with S/N 270M, 272M,

409M, 423M, 452M or 1573, P/N SC5083-1 with S/N from

2902 to 2921 inclusive P/N SC5084 with S/N 30, 84, 104, 186,

438, 575 or 695, P/N SC5084-1 with S/N from 1462 to 1481

inclusive.

- Tail rotor servo-controls: P/N SC5072 with serial number

222M, 306M or 309 .

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2007-05-23 See AD

2015-11-12

N/A. Installed

Servo S/N

(6030, 6137,

3175) not

affected.

01.00.58R

1

53 N EAD 2007-0139-E 2007-05-15

[CORRECTED] Fuselage - Center cross-member under the cabin

floor - Inspection / Modification

Applicability: EUROCOPTER AS350 B, BA, BB, B1, B2, B3 and D,

all serial numbers delivered before January 1st, 2007 and

equipped with a collective-to-yaw control coupling with or

without an Automatic Flight Control System.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2007-05-18 10FH/1M

2008-03-05

N/A.

Equipment

not installed

53.00.37

67 N AD 2007-0099 2007-04-11

Rotors Flight Control - Main & Tail Rotors Servo-Controls -

Inspection / Modification

Applicability: - EC 130 B4, AS 350 B3

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

2007-04-25 See AD

2008-09-30

N/A. B3

model only

67.00.40

35 N AD 2006-0286R1 2007-03-22

Oxygen Reserve Cylinders- Removal/Emptying


Applicability: Oxygen Reserve Cylinders having Part Number

(P/N) GLF(XXX)-(X), GLD(XXX)-(X), PC2300 and SLF300, which

are known to be installed on, but not limited to Airbus A300

series aircraft; Dassault Aviation (AMD-BA) Mystère-Falcon

20, Mystère-Falcon 50, Falcon 200 and Falcon 900 aircraft;

Pilatus aircraft; Eurocopter SA 315 B and AS 350 B3

helicopters; and Hindustan Aeronautics Limited helicopters.

ZODIAC AEROTECHNICS

Oxygen Cylinders2006-09-25 See AD

2008-03-05

N/A.

Equipment

not installed

05.00.54

67 N EAD 2006-0363-E 2006-12-01

Rotor Flight Controls - Load Compensator Lever - Check

Applicability: AS 350 B1 and AS 350 B2 helicopters, all serial

numbers

AIRBUS HELICOPTERS

AS 350 / EC 1302006-12-04 2006-12-04

2008-03-05

Affected P/N

not installed.

67.00.39R

1

24

80N AD 2006-0337 2006-11-07

Electrical Power - Starting - Starter Generator Limitation

Applicability: AS 350 B3 and EC 130 B4 helicopters fitted with

APC 200 A starter generators (P/N 200SGL130Q) before

embodiment of MOD 073345.

AIRBUS HELICOPTERS

AS 350 / EC 1302006-11-17 See AD

2008-03-05

N/A due to

A/C type

01.00.57

53 N AD 2006-0273 2006-09-04

Fuselage - RH Cabin Vibration Damper & Blade - Inspection /


SUPERSEDES AD F-2005-102R1

Applicability: All Model AS 350 B, BA, BB, B1, B2, B3 and D

helicopters, all serial numbers; and All Model AS 355 E, F, F1,

F2 and N helicopters, all serial numbers, if equipped with RH

(right hand) cabin vibrator damper blades, all part numbers,

and with an automatic flight control system, all design

standards.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-09-14 See AD

2008-03-05

N/A.

Equipment

not installed

05.00.48R

1

? N AD US-2006-11-17 2006-09-04

Rotor Flight Controls - Cyclic Control Stick / Receptacle -


Applicability: Model AS350B, BA, B1, B2, B3, C, D, and D1

helicopters, with a Geneva Aviation, Inc. (Geneva) P132

Console installed in accordance with Supplemental Type

Certificate No. SH4747NM, certificated in any category.

AIRBUS HELICOPTERS

AS 350 / EC 130

GENEVA AVIATION INC.

STC SH4747NM

2006-07-07 2006-09-07

2015-04-09.

N/A.

Equipment

not installed.

25 N AD 2006-0098 2006-08-31[Corrected] Equipment / Furnishings - Hoist Hooks


AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 315/316/319

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

SE 313 / SA 318

2006-05-05 2004-05-31

2008-09-30

N/A. Hoist not

installed.

01.00.54

34 Y

AD

SIB

LVD

2006-0265

2011-15R2

2-3368R1

2006-08-30

2013-07-19

2013-04-24

Navigation Systems – Mode S and C Transponders – Check

Applicability: Mode ‘C’ and Mode ‘S’ transponders, all types

and models utilising Gilham code altitude input.

ACSS

Transponders

BECKER

FLUGFUNKWERK GMBH

Transponders

FUNKWERK AVIONICS

GmbH

Transponders

GARMIN

INTERNATIONAL INC

Transponders

GARRECHT AVIONIK

GMBH

Transponders

HONEYWELL

INTERNATIONAL INC

Transponders

ROCKWELL COLLINS

Transponders

TRIG AVIONICS LTD

Transponders

2013-04-17 See AD

2015-12-08

perf by PHAB

iaw

WO17220006

at A/CTT

5270,2. Next

test: 2017-12

2Y

(recom

mende

d)

35 N EAD 2006-0261-E 2006-08-25


Applicability: AS 350 B3 and SA 315 B helicopters, all serial

numbers, if equipped with Oxygen Cylinders having Part

Number (PN) GLF311-1, GLF312, GLF313, GLF316, GLF514 or

GLD511.

AIRBUS HELICOPTERS

AS 350 / EC 130

SA 315/316/319

2006-08-28 See AD N 05.00.54

.05

52N AD 2006-0249 2006-08-22

Doors- Sliding Door- Wear on Rollers and Rails

SUPERSEDES AD F-2002-344-093R1

Applicability: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,

B2, B3 and D equipped with sliding door(s) not modified per

MOD 073287 and/or MOD 073290 or in compliance with

EUROCOPTERService Bulletin No. 52. 00.29 or No. 52.00.22 .

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-09-01 See AD

2008-03-05

N/A.

Equipment

not installed

05.00.41R

2

25

.01N AD 2006-0248 2006-08-22



Applicability: AS 350 BA helicopters equipped with an

AERAZUR emergency flotation gear comprising:

- LH side container assembly 158170 or 158210-1,

- RH side container assembly 158171 or 158215-1.

The containers referenced above are comprised in the

emergency flotation gear removable parts, P/N 350A82-8040-

00 or 350A82-8040-01.

AIRBUS HELICOPTERS

AS 350 / EC 1302006-09-01 See AD N

01.00.55R

1

67 N AD 2006-0247 2006-08-22

Rotor Flight Controls- Tail Servo-Control


Applicability: EUROCOPTER AS 350 B3 helicopters fitted with a

GOODRICH tail servo-control P/No. SC5071-XX or SC5072,

except:

- tail servo-controls P/No. SC5072 with a serial number equal

to or above 1372,

- tail servo-controls overhauled or repaired in compliance with

GOODRICH Service Bulletin No. SC507X-67-39-01-3,

- tail servo-controls having never been removed since the

delivery of a new aircraft.

AIRBUS HELICOPTERS

AS 350 / EC 1302006-09-01 See AD

2008-09-30

N/A. B3

model only

67.00.30

25 N AD 2006-0252 2006-08-22



Applicability: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,

B2, B3 and D, before embodiment of MOD 073299. Equipped

with an operator’s belt (called "hoist operator’s belt") PN

330A87-0730-00, 330A87-2371-00, 341A84-1120-00, 350A84-

0047-00, 360A84-0040-00, 360A84-0040-01 or 360A84-0040-

02, fitted with a snap hook PN GA343-95, or, equipped with an

operator’s belt (called "hoist operator’s belt") PN 3160S73-08-

200-1 fitted with a snap hook PN 4100-80AT28.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 315/316/319

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

2006-09-01 See AD N25.00.89

25.00.93

64 N EAD 2006-0235-E 2006-08-09


Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D

equipped, according to the permitted assemblies, with tail

rotor blades, P/Ns.:

- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/

-12/ -13/ -14.

- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.

- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-08-10 See AD N05.00.40R

1

76 N EAD 2006-0183-E 2006-06-29

Engine Controls - Twist Grip Assembly -



Applicability: AS 350 B3 helicopters equipped with twist grips

post-MOD 073084 and not modified per MOD 073222 (new

solenoid).

AIRBUS HELICOPTERS

AS 350 / EC 1302006-06-30 See AD

2008-09-30

N/A. B3

model only

05.00.44

25 N AD 2006-0164 2006-06-09

Equipment/Furnishings- Untimely Firing of Squibs on

GOODRICH Electric Hoists

Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,

Equipped with - GOODRICH electric hoists, PN 76370-XXX, (all

types of motors), and not modified per MOD 073318 (or per

Eurocopter AS 350 Alert Service Bulletin (ASB) No. 25.00.95 or

Eurocopter AS 355 Alert Service Bulletin No. 25.00.85) or, -

GOODRICH electric hoists, PN 76370–XXX, not equipped with

the AUXILEC motor.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-06-23 See AD

2008-09-30

N/A. Hoist not

installed.

25.00.94

55 N AD 2006-0095 2006-04-24



Applicability: AS 350 B3 helicopters before application of

EUROCOPTER Alert Service Bulletin (ASB) 350 No. 55.00.13.

AIRBUS HELICOPTERS

AS 350 / EC 1302006-05-02 See AD N 05.00.46

76 N AD 2006-0094 2006-04-21


Applicability: AS 350 B3 helicopters, equipped with twist grips

before embodiment of MOD 073261 (new twist grip assembly

compatible with the ARRIEL 2B1 engine installation).

AIRBUS HELICOPTERS

AS 350 / EC 1302006-05-05 2006-04-12 N

05.00.49R

1

55 N EAD 2006-0060-E 2006-03-07


Applicability: 1 -AS 350 B, B1, B2, BA, BB and D helicopters,

equipped with: upper and lower fins pre-MOD 073288.

AIRBUS HELICOPTERS

AS 350 / EC 1302006-03-07 See AD

2010-07-20

perf A/CTT

4466,2

55.00.13

2.B.3

67 Y EAD 2006-0055-E 2006-03-01

Rotor Flight Controls - Main Servo-Controls

Applicability: AS 350 B, BA, BB, B1, B2, B3 and D, and AS 355 E

helicopters, equipped with main servo-controls, all part

numbers, not modified per MOD 073343, and on which the

tightening torque of the nut that secures the upper ball-end

has been increased following: - embodiment of MOD 073191,

Or, - compliance with MET Work Card 67.30.00.402 since MET

Revision 04-06 for AS 350 helicopters and Revision 04-08 for

AS 355 helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2006-03-01 See AD

2006-04-24

perf A/CTT

2230,6

05.00.51

65 N AD F-2005-158 2005-12-21

[Corrected] Tail Rotor Drive - Tail Rotor Drive Shaft

Maintenance

EFFECTIVITY: AS 350 B3 and EC 130 B4 helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 1302005-10-01 See AD

2008-09-30

N/A. B3

model only

25 N AD F-2002-027-088R1 2005-09-14

Equipment/Furnishings - BREEZE 450-lb Electric Hoist Damper

Assembly

EFFECTIVITY: This Airworthiness Directive applies to AS 350 B3

helicopters equipped with BREEZE 450-lb electric hoist PN BL

29700-23.

AIRBUS HELICOPTERS

AS 350 / EC 1302005-09-24 See AD

2008-09-30

N/A. Hoist not

installed.

25.00.73

53 N AD F-2005-102R1 2005-08-03


EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,

fitted with blades, all part numbers, of RH cabin vibration

dampers, and an automatic flight control system, all design

standards.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2005-08-13 See AD N05.00.48R

1

.05

52N AD F-2005-136 2005-08-03



EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,

fitted with sliding door(s).

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2005-08-03 See AD N

25 N AD F-2005-087 2005-06-22


EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3, and

D, equipped with GOODRICH electric hoist 76370-XXX fitted

with any types of motor except AUXILEC motors.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2005-05-30 See AD N 25.00.94

.01

25

45

N AD F-2004-170R1 2005-03-16

Equipments/Furnishings - Hoist Hook - Operational

Procedures/Restriction

EFFECTIVITY: Helicopters: - AS 350 B, BA, B1, B2, B3, BB and D,

equipped with BREEZE hoists fitted with hook assembly PN BL-

7520-01, with hook PN BL-7520.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 341/342

2005-03-26 See AD

2008-09-30

N/A. Hoist not

installed.

01.00.56

67 Y AD F-2005-042 2005-03-16

Rotor Flight Controls - Ball-type Yaw Controls - Replacement

EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2 and

D, fitted with stainless steel-caged ball-type controls, PNos.:

- 704A 34-130-068 with automatic flight control system (pre-

MOD 072771),

- 704A 34-130-058 without automatic flight control system

(pre-MOD 072771).

AIRBUS HELICOPTERS

AS 350 / EC 1302005-03-26 See AD

2005-08-26

perf A/CTT

2184,7

67.00.26R

1

.05

52N AD F-2005-032 2005-02-16

SUPERSEDED BY DGAC FRANCE AD F-2005-136

EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3

and D, fitted with sliding door(s).

AIRBUS HELICOPTERS

AS 350 / EC 1302005-02-16 See AD N

67 N AD F-2004-196 2005-01-19


EFFECTIVITY: EUROCOPTER AS 350 B3 helicopters fitted with a

GOODRICH tail servo-control PN SC5071-XX or SC5072.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-12-28 See AD N 67.00.30

.05

55N AD F-2005-010 2005-01-05


EFFECTIVITY: AS 350 B3 helicopters, all serial numbers.

AIRBUS HELICOPTERS

AS 350 / EC 1302005-01-05 See AD N 05.00.46

05

67N AD F-2001-580R2 2004-12-08

Rotor Flight Controls - Tail Servocontrols Eye End Fitting

Locking - Check

Effectivity: AS350 B, BA, B1, B2, B3, BB and D helicopters,

equipped with tail servocontrols, all part numbers and all

types, that have not been modified per MOD 073139 or per

EUROCOPTER AS350 Service Bulletin No. 67.00.22.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-12-18

50FH ->

Every 550FH

2007-08-30

Verified A/CTT

3096,6

2015-04-07 SB

67.00.22

verified

performed

05.00.37R

1

29 Y AD F-2004-174 2004-11-10

Hydraulic Power - Rotorcraft Flight Manual - Hydraulic Power

Loss Procedure

EFFECTIVITY: AS 350 helicopter versions B, BA, B1, B2, B3, BB

and D.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-11-20 See AD

Perf 2006-05-

03 A/CTT

2230,6

64 N AD F-2004-178 2004-11-10

Tail Rotor - Tail Rotor Blade Trailing Edge Tab - Modification

EFFECTIVITY: AS 350 helicopters, versions B, BA, BB, B1, B2, B3

and D, fitted with tail rotor blades PN 355A 12.0040 all dash

numbers and PN 355A 12.0050.04, with serial numbers from

8400 to 9224 inclusive, before embodiment of Repair Sheet FR

No. 238 or of Work Card 64.10.00.872 [refer to the equipment

log card (FME)].

AIRBUS HELICOPTERS

AS 350 / EC 1302004-11-20 See AD

2015-04-07

N/A to blades

S/N 18525

64.00.05R

2

.05

52N AD F-2002-344-093R1 2004-11-10


EFFECTIVITY: AS 350 helicopters, versions B, BA, BB, B1, B2, B3

and D fitted with sliding doors.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-11-20 See AD N

05.00.41R

1

.05

64Y AD F-2000-222-079R1 2004-09-15

Tail Rotor Head Pitch Change Plate Bearing Spacer

EFFECTIVITY: AS 350 helicopters, versions B, B1, B2, B3, BA, BB

and D, fitted with tail rotor pitch change rotating plates all

part numbers, on which EUROCOPTER modification (MOD) 07

6554 has not been embodied.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-09-25 See AD

Perf on Spider

S/N M1815

2001-11-19

05.00.33R

1

25 N AD G-2004-0019 2004-07-27

Equipment & Furnishings - Camera System Installation Floor-

mounted Platform Panel Hold-down Hook - Replacement

Applicability: Eurocopter Model AS350 and AS355 helicopters,

certificated in any category that have beenmodified in

accordance with MAG(E) modification 350-1521, 350-1680 or

350-1707. Installation of Cameraplatform.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

MANN AVIATION

GROUP

CAMERA SYSTEM

INSTALLATION

2004-08-05 2004-11-05

2015-04-09.

N/A.

Equipment

not installed.

25 N AD F-2004-096 2004-06-23


EFFECTIVITY: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,

B2, B3 and D, equipped with an operator's belt (called "hoist

operator's belt") PNs: 330A87-0730-00, 330A87-2371-00,

341A84-1120-00, 350A84-0047-00, 360A84-0040-00, 360A84-

0040-01 and 360A84-0040-02, fitted with a snap hook PN

GA343-95, or equipped with an operator's belt (called "hoist

operator's belt") PN 3160S73-08-200-1, fitted with a snap

hook PN 4100-80AT28.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

2004-07-03 See AD N 25.00.89

25

.01N AD F-2004-085 2004-06-23


EFFECTIVITY: AS 350 BA helicopters equipped with an

AERAZUR emergency flotation gear comprising:

- LH side container assembly 158170 or 158210-1,

- RH side container assembly 158171 or 158215-1.

The containers are comprised in emergency flotation gear,

removable parts, PN 350A82-8040-00 or PN 350A82-8040-01.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-06-11 See AD N 01.00.55

29 Y AD F-2004-089 2004-06-23

Hydraulic System - Hydraulic Cut-Off Function - Modification

EFFECTIVITY: AS 350 helicopter versions B, B1, B2, B3, BA, BB

and D, pre-MOD 073263.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-07-03 See AD

2005-01-05

Verified A/CTT

1860,5

29.00.07

24 Y AD F-2003-260R1 2004-06-09

Electrical Power - Battery Lug Connection


and D, pre-MOD 073226 (subject of EUROCOPTER AS 350

Service Bulletin No. 24.00.11).

AIRBUS HELICOPTERS

AS 350 / EC 1302004-06-19 See AD

2004-06-03

Verified A/CTT

1597,1

24.00.10

67 Y AD F-2003-322R1 2004-05-26

Rotor Flight Controls - Double Locking of Stop Screws

Effectivity: before embodiment of MOD 073206 or MOD

073102.

Components affected: Roll, pitch and collective flight control

stops.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

EC 120 B

SA 365/366 / AS 365

/ EC 155

2004-06-05

1. 100FH

2.

500FH/12M

2004-10-14

Verified A/CTT

1860,5

67.00.25

2.B.1

.05

29Y AD F-2004-055 2004-04-28

Time Limits / Maintenance Checks - Replacement of Hydraulic

Fluid in Cold Weather


and D that operate in a flight envelope where the outside air

temperature (OAT) is below minus 15° Celsius (or below plus

5° Fahrenheit).

AIRBUS HELICOPTERS

AS 350 / EC 1302004-05-08 See AD

2012-07-02

Perf A/C TT

5070,6

05.00.45R

1

110FH

/1M

(only if

OAT is

below

15°

Celsius

)

25

.01

.04

N AD F-2004-046 2004-03-31


EFFECTIVITY: Helicopter versions: AS 350 B, BA, B1, B2, B3, BB

and D, equipped with GOODRICH (LUCAS – AIR EQUIPEMENT)

hoists, part numbers: 76300-xxx, 6340-xxx, 76360-xxx, 76360-

xxx-xx, 76363-xxx, 76365-xxx, 76368-xxx, 76370-xxx, 76375-

xxx, 76378-xxx, fitted with hooks, part numbers: 704160,

708223, 708931, 709866, 710177.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 315/316/319

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

SE 313 / SA 318

2004-03-31 See AD

76

.05N AD F-2004-045 2004-03-31


EFFECTIVITY: AS 350 B3 helicopters fitted with twist grip post-

MOD 073084.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-03-31 See AD

34 N AD F-2002-281R1 2004-03-17

Navigation - Horizontal Situation Indicator KI 525A - Wiring

Change


and D, equipped with HSI KI 525A.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-03-27 See AD

2008-03-05

N/A.

Equipment

not installed

34.00.13

53 Y AD F-2004-035 2004-03-17

Fuselage - Rear Structure Junction Frame - Inspection /

Replacement


and D

- pre-MOD 073215, or

- not equipped with the four reinforcement angles, P/Nos.

350A08.2493.20 / .21 / .22 / .23, following the repair carried

out in accordance with MRM Work Card 53.10.22.772.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-03-27 See AD

Perf 2015-11-

21 by PHAB

iaw WO

17220006.

Next insp:

A/CTT 5820,2.

05.00.43R

1550FH

28 Y AD F-2004-033 2004-03-17

Fuel - Fuel Bleed Lever - Modification


and D, pre-MOD 073239.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-03-17 See AD

2004-10-14

Verified A/CTT

1860,5

28.00.16

67 Y AD F-2003-002R1 2004-02-18

Rotor Flight Controls - Cyclic Stick Bowl Lower Friction Cup -



and D, modified per MOD 070682 (this MOD forms the subject

of EUROCOPTER AS 350 Service Bulletin No. 67.09), and before

embodiment of MOD 073179.

The component affected is the lower friction cup P/N 350A27-

1612-20 of the cyclic stick.

AIRBUS HELICOPTERS

AS 350 / EC 1302004-02-28 See AD

Rev A perf

2001-12-10

A/CTT 1330,3

MOD 073179

67.00.24

67 N AD F-2002-314-092R1 2003-12-10

Rotor Flight Controls - "TRW-SAMM" Main Servo Controls -

Check

EFFECTIVITY: AS 350 B3 helicopters equipped with "TRW –

SAMM" main servocontrols, part numbers SC 8042 or SC 8043

that underwent their last complete overhaul or repair since

complete overhaul at "HAWKER PACIFIC AEROSPACE", USA,

before March 1, 2002.

AIRBUS HELICOPTERS

AS 350 / EC 1302003-12-20 See AD

2015-11-12

N/A. B3

model only.

67.00.23R

1

67 Y AD F-2003-406 2003-10-29

Rotor flight controls - Collective lever lock

EFFECTIVITY AS 350 helicopter versions B, BA, BB, B1, B2, B3

and D fitted with the pilot collective lever locking system:

Locks PN 350A77.1309.xx and 350A27.3155.20.

AIRBUS HELICOPTERS

AS 350 / EC 1302003-11-08 See AD

2004-10-14

§2.B.2 o 2.B.3

verified A/C

TT 1860,5

67.00.27

25 N AD G-2003-0008 2003-09-17

Equipment / Furnishings - Tail Rotor and Cyclic Control Cut-

Outs of Floor Mounted Camera System Installation Platform

Panel - Rework

Applicability: Eurocopter Model AS350 and AS355 helicopters,

certificated in any category that have been modified in

accordance with MAG(E) modification 350-1521 or 350-1680.

Installation of Camera platform.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

MANN AVIATION

GROUP

CAMERA SYSTEM

INSTALLATION

2003-09-18 2003-10-18

2015-04-09.

N/A.

Equipment

not installed.

71 N AD F-2003-208 2003-05-28

Power plant - Interference between the bleed valve air

exhaust duct and the engine fuel line

EFFECTIVITY AS 350 B3 helicopters equipped with optional

engine flushing system and modified per MOD 073098.

AIRBUS HELICOPTERS

AS 350 / EC 1302003-06-07 See AD

2008-09-30

N/A. System

not installed

71.00.16

62

63

64

65

N/A AD F-2002-452R1 2003-04-30

Main rotor and tail rotor dynamic component - Correction of

operating hours

EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D

equipped with dynamic components following overhaul (RG)

or repair (RE) at the EUROCOPTER helicopter maintenance and

overhaul facility (D.E.R.H.), listed in Tables 1 and 2 (as

applicable) in paragraph 4 "Appendix" of the Alert Service

Bulletins (ASBs) referenced below.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 330 / AS 332 / EC

225

SA 341/342

SA 365/366 / AS 365

/ EC 155

2003-05-10 See AD

2015-04-10

N/A. P/N and

S/N not

affected

.01

67N AD F-2003-099 2003-03-05

Mail and Tail TRW SAMM servocontrols

EFFECTIVITY: AS 350 helicopters, versions B, BA, B1, B2, B3, BB

and D equipped with the following main and tail TRW SAMM

servocontrols: SEE AD

AIRBUS HELICOPTERS

AS 350 / EC 1302003-03-05 See AD

2015-11-12

N/A. Installed

Servo S/N

(6030, 6137,

3175) not

affected.

25 N AD F-2002-585 2002-11-27

BREEZE or TRW (or LUCAS or AIR EQUIPEMENT)

EFFECTIVITY: The following helicopters: - AS 350 helicopters

versions B, BA, BB, B1, B2, B3 and D, equipped with the

optional BREEZE or TRW (or LUCAS or AIR EQUIPEMENT) 300

lb. electric hoist and hoist box 26 M part number 350A63-1136-

00 (AS 350) or 350A63-1136-01 (AS 355), not modified per

MOD 073190, and delivered before October 1st, 2002 .

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

2002-12-07 See AD

2008-09-30

N/A. Hoist not

installed.

25.00.79

.05

62N AD F-2001-557-086R3 2002-05-15

Main rotor - STARFLEX star

EFFECTIVITY: AS 350 version B, BA, B1, B2, B3, BB and D

helicopters equipped with STARFLEX stars P/N

350A31.1916.00, mounted on Main Rotor Hubs (MRH) prior to

the embodiment of MOD 076221.

AIRBUS HELICOPTERS

AS 350 / EC 1302002-05-15 See AD

2008-09-30

N/A to

Starflex P/N

62.00.24

MOD

076221

24 N AD F-2002-187-090 2002-04-03

Electrical power

EFFECTIVITY: AS 350 version B3 helicopters before

embodiment of MOD 073146, with the following serial

numbers: 3461, 3463, 3464, 3467, 3469, 3471, 3472, 3473,

3475, 3477, 3478, 3479, 3484, 3485, 3486, 3493, 3494, 3511

and 3522.

AIRBUS HELICOPTERS

AS 350 / EC 1302002-04-13 See AD

2008-09-30

N/A. B3

model only

24.00.09

.05

53N AD F-2000-340-080R2 2002-02-20

Tail rotor drive shaft forward fairing

EFFECTIVITY: AS 350 B3 helicopters equipped with tail rotor

drive shaft forward fairing P/Nos.: - 350A23.0032.09 pre MOD

073097 - 350A23.1075.00 post MOD 073097.

AIRBUS HELICOPTERS

AS 350 / EC 1302002-03-02 See AD

2010-08-23

N/A. 350B3

only

05.00.35R

2

.05

65N AD F-1999-085-076R3 2002-02-20

Tail rotor hub pitch-change plate bearing

EFFECTIVITY: AS 350 helicopters, versions: B, BA, B1, B2, B3,

BB and D fitted with tail rotor hub pitch change plate, P/Nos.

350A33-2004-00/-01/-02/-03/-05 or 350A33-2009-00/-01,

and which do not incorporate MOD 076551 [new generation

bearing P/No. 6010F234M16 (704A33.651.190) introduced by

EUROCOPTER AS 350 Service Bulletin No. 65.00.38 R1].

AIRBUS HELICOPTERS

AS 350 / EC 1302002-03-02 See AD

2008-09-30

N/A to

6010F234M16

bearings

05.00.29R

3

.05 N AD F-2002-044 2002-01-23

SIREN cargo hooks

EFFECTIVITY: This Airworthiness Directive applies to the

following helicopter models: - AS 350 B3, fitted with SIREN

cargo hooks P/N AS-21-5-7.

AIRBUS HELICOPTERS

AS 350 / EC 130

SA 365/366 / AS 365

/ EC 155

2002-01-23 See AD

2008-09-30

N/A. B3

model only

05.00.39

53 Y AD F-1997-147-072R1 2002-01-23

Tail boom-to-aircraft structure junction attachment screws

EFFECTIVITY: This Airworthiness Directive (AD) applies to AS

350 helicopters, versions B, BA, BB, B1, B2 and D equipped

with attachment screws P/N 22201BC060008L

(N5103337287), which ensure the tail boom-to-aircraft

structure junction attachment.

AIRBUS HELICOPTERS

AS 350 / EC 1302002-02-02 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.46

76 N AD F-2001-548-084 2001-11-14

Engine controls - Switching unit

EFFECTIVITY: This Airworthiness Directive applies to AS 350 B3

helicopters delivered new before October 15, 2001 and

equipped with switching unit P/N 200192.

AIRBUS HELICOPTERS

AS 350 / EC 1302001-11-14 See AD

2008-09-30

N/A. B3

model only

76.00.16

77 N AD F-2001-319-083 2001-07-25

Engine indicating - ASU PCB

EFFECTIVITY: AS 350 B3 helicopters equipped with printed

circuit boards P/Nos. SE 03022 (704A47720110) (ASU No. 2

board) delivered before May 1st, 1999 and AS 350 B3

helicopters delivered new before May 1st, 1999.

AIRBUS HELICOPTERS

AS 350 / EC 1302001-08-04 See AD

2008-09-30

N/A. B3

model only

77.00.07

N AD CF-2000-06R1 2000-08-23

Left-Side Pilot Configuration - Modification

Applies to all Eurocopter Canada Limited (ECL) Left-Side Pilot

Configuration kits, Transport Canada Supplemental Type

Certificate (STC) SH96-32, Issues 1 through 5, installed in

Eurocopter France (Aerospatiale) AS 350 BA and B2

helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 130

EUROCOPTER CANADA

LTD

STC SH96-32

2000-04-17 See AD

2015-04-10

N/A.

Equipment

not installed

28 N AD F-2000-302 2000-07-12

Ferry fuel tanks

APPLICABILITY: Helicopters of following models: - AS 350 B,

BA, B1, B2, B3, BB and D, equipped with metal ferry fuel tanks,

part number 330A 871310 .00, .01, .02, .03 and .04, - SA 316 B

and C, SA 3160 and SA 319 B, equipped with metal ferry fuel

tanks, part number 3160S 7375020 and 3160S 7375020-1.

AIRBUS HELICOPTERS

AS 350 / EC 130

AS 355

SA 315/316/319

SA 330 / AS 332 / EC

225

SA 365/366 / AS 365

/ EC 155

2000-07-12 See AD

2008-03-05

N/A.

Equipment

not installed

28.00.14

79 Y AD F-2000-268-078 2000-06-28

Engine oil pipe - Fire proofing

EFFECTIVITY: AS 350 helicopters, versions: B, B1, B2, BA, BB

and D on which MOD 07 2793 has not been embodied.

AIRBUS HELICOPTERS

AS 350 / EC 1302000-07-08 See AD

Perf 2001-10-

29 A/CTT

1330,3

79.00.11R

1

33 N AD F-1999-512-077 1999-12-29

"NR" indicator lighting

EFFECTIVITY: AS 350 B3 version helicopters, which do not

incorporate MOD 072810 or any other approved modification,

enabling full "NR" indicator lighting in normal mode and

emergency mode.

AIRBUS HELICOPTERS

AS 350 / EC 1302000-01-08 See AD

2008-09-30

N/A. B3

model only

33.00.17

- N AD F-1999-017-075 1999-01-13Climbing Speeds

EFFECTIVITY : AS 350 B3 helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 1301999-01-13 See AD

2008-09-30

N/A. B3

model only

.01 N AD F-1998-511-074 1998-12-16

Single-pole circuit breakers

EFFECTIVITY: AS 350 helicopters, versions : B, BA, BB, B1, B2,

B3 and D equipped with single-pole CROUZET circuit breakers,

part numbers : SEE AD

AIRBUS HELICOPTERS

AS 350 / EC 1301998-12-16 See AD

2008-03-05

N/A.

Equipment

not installed

01.00.47

.05 N AD F-1998-173-073 1998-04-22


Tail Rotor Drive Shaft Bearings

AIRCRAFT CONCERNED: AS 350 helicopters, versions B, B1, B2,

D, BA, BB and B3 with tail rotor drive shaft rear section

bearing mountings, equipped with : non-regreasable bearings

P/N SKF 6007.2RS 1 MT 47CA (AS 704A33.651.010) or

regreasable bearings P/N KOYO 83A 85 1C3 (AS

704A33.651.143), FAFNIR P9107NPP7 (AS 704A33.651.111),

FAG 593404 (AS 704A33.651.181)

AIRBUS HELICOPTERS

AS 350 / EC 1301998-05-02 See AD

Perf 2012-07-

02 A/CTT

5070,6

05.00.08R

5

100FH

(VC)

.05 N AD F-1996-156-071R1 1997-04-06

MGB suspension bi-directional cross beam

This Airworthiness Directive applies to AS 350 helicopters,

versions B, BA, B1, B2 and D fitted with a MGB suspension bi-

directional cross beam P/N 350A38.1018 - all dash numbers,

installed on the complete cross beam assemblies P/No

350A38.0210 - all dash numbers (which are not modified per

MOD. 072720).

AIRBUS HELICOPTERS

AS 350 / EC 1301997-06-14 See AD

2008-03-05

N/A.

Equipment

not installed

05.00.28

.01 N AD F-1994-279-070R1 1995-01-18

Main rotor shaft


versions B, BA, B1, B2 and D, equipped with a "TIMKEN" main

rotor shaft P/N 350A37-0003- all dash numbers, that have

logged less than 100 operating hours since new or overhaul.

AIRBUS HELICOPTERS

AS 350 / EC 1301995-01-18 See AD

2008-03-05

N/A.

Equipment

not installed

01.00.44

.01 Y AD F-1994-180-069 1994-08-03

Cycle pitch change control rod

This Airworthiness Directive covers AS 350 helicopters,

versions B, BA, D, B1 and B2, fitted with cyclic pitch change

control rod P/N 704A34-113-279.

AIRBUS HELICOPTERS

AS 350 / EC 1301994-08-03 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.42

.01 Y AD F-1994-087-068 1994-04-13

MGB oil pressure switch

The present Airworthiness Directive applies to AS 350 B, BA, D,

B1 and B2 helicopters fitted with MGB oil pressure switch P/N

704A37.721.082 (S 1130.021.082).

AIRBUS HELICOPTERS

AS 350 / EC 1301994-04-13 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.43

.05 Y AD F-1984-064-037R3 1994-02-02

Tail rotor blade spars

The present AD applies to AS 350 helicopters, all versions fitted

with tail rotor blades assemblies P/N: -350A08.1011 all

dashnumbers, -350A12.0020 all dashnumbers, -350A12.0030

all dashnumbers, -350A12.0031 all dashnumbers, -

350A12.0040 all dashnumbers

AIRBUS HELICOPTERS

AS 350 / EC 1301994-02-12 See AD

Perf 2001-10-

29 A/CTT

1330,3

05.00.11R

5

.05 Y AD F-1993-090-067R1 1993-12-22

Door "clear vision" window

The present Airworthiness Directive applies to AS 350

helicopters, versions B, BA, B1, B2 and D fitted with "clear

vision" windows : Part Numbers : see AD

AIRBUS HELICOPTERS

AS 350 / EC 1301994-01-02 See AD

Perf 2015-12-

03 by PHAB

iaw

WO17220006

at A/CTT

5270,2. Next

insp: A/CTT

5370,2.

05.00.25R

1100FH

.01 N/A AD F-1988-184-052R1 1993-07-21

DUNLOP Servocontrols

This AD covers AS 350 B, B1, D helicopters fitted with the

following DUNLOP main and tail servocontrols: P/N: see AD

AIRBUS HELICOPTERS

AS 350 / EC 1301993-07-31 See AD

Perf 2001-10-

29 A/CTT

1330,3

2015-11-12

Goodrich M/R

servos

installed.

01.00.21R

1

- N AD F-1993-067-066 1993-05-12

Flight in falling snow


helicopters, versions B, B1, B2 and BA.

AIRBUS HELICOPTERS

AS 350 / EC 1301993-05-22 See AD

2008-03-05

N/A. RFM

revised

62 Y AD F-1992-179-064R1 1993-03-31

Main rotor pitch change horn bushes


helicopters, versions B, D, B1, B2 and BA on which the pitch

change horns P/N 350A31-1877-02 are not marked with an

"X" and have a serial number less than 100-000.

AIRBUS HELICOPTERS

AS 350 / EC 1301993-04-10 See AD

Perf 2001-10-

29 A/CTT

1330,3

62.00.21R

1

.01 Y AD F-1993-030-065 1993-03-03

Main rotor mast assembly

IThe present Airworthiness Directive applies to EUROCOPTER

AS 350 helicopters, versions B, BA, B1, B2 and D fitted with

rotor mast assembly Part Numbers : 350A37.0004.02,

350A37.0004.03, 355A37.0005.01

AIRBUS HELICOPTERS

AS 350 / EC 1301993-03-03 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.41

.01

26N AD F-1992-159-063R2 1992-11-25

Engine bay fire detection

The present Airworthiness Directive applies to all

EUROCOPTER AS 350 helicopters, versions B1 and B2.

AIRBUS HELICOPTERS

AS 350 / EC 1301992-12-05 See AD

2006-05-03

N/A. MOD

072598

performed at

A/CTT 2230,6

01.00.38

26.00.01

25 N AD F-1992-144-061 1992-07-08

"JOLLIET" Emergency Locator Transmitter Antenna


versions B, BA, B1, B2 and D, fitted with the "JOLLIET"

emergency locator transmitter system, not modified per AMS

350A.07.2492.

AIRBUS HELICOPTERS

AS 350 / EC 1301992-07-18 See AD

2008-09-30

N/A. Jolliet

not installed.

25.00.45

.01 Y AD F-1992-145-062 1992-07-08

Hydraulic system


versions B, BA, B1, B2 and D, fitted with the hydraulic reservoir

P/N 350A75-1030-00.

AIRBUS HELICOPTERS

AS 350 / EC 1301992-07-18 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.36

.01 Y AD F-1990-198-056R1 1991-11-27

Battery temperature probe

This AD is applicable to AEROSPATIALE helicopters AS 350 D,

B, B1 and B2 equipped with one or two SAFT 1606-1

battery(ies) not modified by amendment E.

AIRBUS HELICOPTERS

AS 350 / EC 1301991-12-07 See AD

Perf 2001-10-

29 A/CTT

1330,3

01.00.29R

1

25 N AD F-1991-165-058R1 1991-11-27

Electric hoist installation

The present AD applies to AEROSPATIALE AS 350 helicopters,

versions B, B1, B2, D, fitted with an AIR EQUIPMENT hoist P/N

76370.010, 76370.011 or 76370.030.

AIRBUS HELICOPTERS

AS 350 / EC 1301991-12-07 See AD

2008-09-30

N/A. Hoist not

installed.

25.00.42R

1

62 Y AD F-1989-155-054R4 1991-10-02

Swashplate

The present AD applies to AEROSPATIALE AS 350 helicopters

all S/N of versions B, B1, B2, D on which the swashplate is

fitted with bearings P/Ns: see AD.

AIRBUS HELICOPTERS

AS 350 / EC 1301991-10-12 See AD

Rev B perf

2001-10-29

A/CTT 1330,3

62.00.12R

2

.01 Y AD F-1991-159-060 1991-07-31

Tail rotor drive shaft bearings


versions B, D, B1,B2, L1 and AVEX equipped with FAFNIR tail

rotor drive shaft bearings P/N P.9107.NPP7 not marked with

"X" on sealing flanges and installed on those helicopters which

were acceptance tested by AEROSPATIALE Marignane, when

see AD.

AIRBUS HELICOPTERS

AS 350 / EC 1301991-07-31 See AD

Rev B perf

2001-10-29

A/CTT 1330,3

01.00.34

.01 Y AD F-1991-137-059 1991-07-01

Pitch control lever expansion pin - Tail rotor

This AD is applicable to AEROSPATIALE helicopters AS 350 D,

B, B1 AND B2.

AIRBUS HELICOPTERS

AS 350 / EC 1301991-07-01 See AD

Rev B perf

2001-10-29

A/CTT 1330,3

01.00.33

.01 N AD F-1989-081-053 1989-05-17

Spherical thrust bearings P/N 704A 33-633-1

This AD covers AEROSPATIALE AS 350 helicopters, versions B,

B1 and D.

AIRBUS HELICOPTERS

AS 350 / EC 1301989-05-27 See AD

2008-09-30

N/A to

bearings P/N

01.00.23

. 05 N AD F-1981-094-018R2 1988-07-20 Main gear boxAIRBUS HELICOPTERS

AS 350 / EC 1301988-07-20 See AD

2008-09-30

N/A to

helicopter S/N

05.00.06

.01 Y AD F-1987-161-051 1987-11-25 Spherical thrust bearing bolts - Service life limit reductionAIRBUS HELICOPTERS

AS 350 / EC 1301987-12-05 See AD

2001-10-29

Accomplished

A/CTT 1330,3

01.00.20

.01 Y AD F-1987-115-050 1987-08-19

Flight cycle calculation

This AD concerns AEROSPATIALE AS 350 helicopters, versions

B, B1 and D.

AIRBUS HELICOPTERS

AS 350 / EC 1301987-08-29 See AD

2001-10-29

Accomplished

A/CTT 1330,3

01.00.19

52 N/A AD F-1987-088-049 1987-06-24

Sliding doors


all versions, equipped with LH and/or RH sliding door(s).

AIRBUS HELICOPTERS

AS 350 / EC 1301987-06-24 See AD

2001-10-29

Accomplished

A/CTT 1330,3

52.00.18

28 Y AD F-1986-077-046R2 1986-12-10

Fuel filter

The AD is applicable to AEROSPATIALE AS 350 (ECUREUIL and

ASTAR) Helicopters fitted with a LEBOZEC and GAUTHIER fuel

filter P/N 432B12.3, .sC, .3D or a GUIOT fuel filter P/N

704A34620002, prior to compliance with modification 350A

071671.

AIRBUS HELICOPTERS

AS 350 / EC 1301986-12-10 See AD

2001-10-29

Accomplished

A/CTT 1330,3

28.00.07R

1

.01 Y AD F-1986-125-048R1 1986-10-15

Behaviour of the helicopter on the ground with rotor turning

Present AD applies to AEROSPATIALE AS 350 B, B1, C, D and

D1 helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 1301986-10-15 See AD

2001-10-29

Accomplished

A/CTT 1330,3

01.00.17A

.05 Y AD F-1978-193-001R1 1986-10-01

Tail rotor

The AD applies to AEROSPATIALE AS 350B, C, D and D1

helicopters.

AIRBUS HELICOPTERS

AS 350 / EC 1301986-10-01 See AD

2001-10-29

Accomplished

A/CTT 1330,3

05.00.02

- N AD F-1986-057-044R1 1986-07-09

Main rotor head roving sleeve beams


models B and D, fitted with roving sleeve upper and lower

beams P/Ns 350A31-1830-00 and -01, 350A31-1831-00 and -

01, -04, -05, -06, -07, and AEROSPATIALE AS 350 helicopters

model B1, fitted with roving sleeve uper and lower beams

P/Ns 350A31-1831-04, -05, -06, -07.

AIRBUS HELICOPTERS

AS 350 / EC 1301986-07-16 See AD

2015-04-15

N/A. P/Ns not

installed

N/A

28 Y AD F-1986-097-047 1986-06-25

Fuel filter

The AD is applicable to AEROSPATIALE AS 350 (ECUREUIL and

ASTAR) Helicopters fitted with a LEBOZEC and GAUTHIER fuel

filter P/N 432B12.3, .sC, .3D or P/N 350A52-1070-00 (after

modification 350A 071671).

AIRBUS HELICOPTERS

AS 350 / EC 1301986-06-25 See AD

2001-10-29

Accomplished

A/CTT 1330,3

28.00.08

.01 Y AD F-1985-135-042 1985-07-31 Fuel filter and main gear box oil filterAIRBUS HELICOPTERS

AS 350 / EC 1301985-07-31 See AD

2001-10-29

Accomplished

A/CTT 1330,3

01.00.14A

.05 Y AD F-1985-095-040 1985-06-19

Main rotor shaft

Applicability: AEROSPATIALE helicopters AS 350 all versions

(ECUREUIL and ASTAR) - Main Rotor Shaft P/N 350A37-1076-

00 through -06.

AIRBUS HELICOPTERS

AS 350 / EC 1301985-06-26 See AD

2001-10-29

Accomplished

A/CTT 1330,3

05.00.15

.05 Y AD F-1985-068-038 1985-05-22Inspection of the bolted junction : bevel ring gear / Vertical

shaft of the bevel reduction gear module on the MGB

AIRBUS HELICOPTERS

AS 350 / EC 1301985-05-29 See AD

2001-10-29

Accomplished

A/CTT 1330,3

05.00.10R

1

.05 Y AD F-1983-173-036 1983-11-09 Main rotor mast shaft - Checking for cracksAIRBUS HELICOPTERS

AS 350 / EC 1301983-11-16 See AD

2001-10-29

Accomplished

A/CTT 1330,3

05.00.13R

1

.01 Y AD F-1983-075-033 1983-05-04

Tail rotor - Retiring from operation and replacing stainless

steel leading edges

The present AD applies to T/R assemblies P/N 350A12-0030-

01 to -05 from S/N 979 (inc) to 1150 (inc) excepting S/N 997 to

999, 1004, 1010, 1014, 1016, 1021 to 1026, 1028, 1029, 1033,

1044, 1136 which have been already reconditioned.

AIRBUS HELICOPTERS

AS 350 / EC 1301983-05-11 See AD

2001-10-29

Accomplished

A/CTT 1330,3

01.00.10

.05 Y AD F-1982-098-026 1982-07-28 Upper fin attachment fittingAIRBUS HELICOPTERS

AS 350 / EC 1301982-08-05 See AD

2001-10-29

Accomplished

A/CTT 1330,3

05.00.09

65 Y AD F-1982-175-029 1982-12-15 Main gear box - Oil monitoringAIRBUS HELICOPTERS

AS 350 / EC 1301982-12-22 See AD

2001-10-29

Accomplished

A/CTT 1330,3

65.00.20

55 Y AD F-1981-203-021 1981-12-02 Inproved installation of upper and lower finsAIRBUS HELICOPTERS

AS 350 / EC 1301981-12-09 See AD

1990-07-31

C/W by

factory A/CTT

0,0

55.00.02

ATA Appl ASB SB Rev. Issue date Subject Notes Ass. RequirmentsAD Due PerfEmbodiment

of MODRec.

33 Y - 33.00.40 0 2015-11-26

LIGHTING - Outer lighting - Improvement of wiring

protection in the stabilizer

EFFECTIVITY: (B2, B3) Helicopters PRE MOD 074720

Recommende

dN/A .074720

31 N/A - 31.00.64 0 2015-11-24

INDICATING AND RECORDING SYSTEMS - Modification to

the NR indicator electrical power supply

EFFECTIVITY: (B2, B3) Helicopters POST MOD 074222

and PRE MOD 074700.

Recommende

dN/A

N/A. PRE

MOD 074222.074700

67 N/A 67.00.57 1 2015-11-18

ROTOR FLIGHT CONTROLS - Optimization of the yaw

sheath routing

EFFECTIVITY: (B3)

Recommende

d

Applicable to

AS350 B3

.073422

AL 4738

67 N/A - 67.00.66 1 2015-10-22

ROTOR FLIGHT CONTROLS - Functional check procedure

for the tail rotor load compensator

EFFECTIVITY: (B3)

Recommende

d

Applicable to

AS350 B3

52 OPT - 52.00.25 1 2015-10-13

DOORS - Improved Closing System for the Side Baggage

Compartment Doors

Effectivity: (B, BA, BB, B1, B2, B3, D, L1)

OPTIONAL N/A 350A073016

31 N/A - 31.00.52 2 2015-10-06

INDICATING AND RECORDING SYSTEMS - VEMD version

2005

EFFECTIVITY: (B3) Helicopters equipped with VEMDs

"Vehicle & Engine Multifunction Display" listed in

paragraph 1.A.2. and with Global Positioning System

(GPS), compatible with ARINC 429 High Speed, and pre-

MOD 073195.

Recommende

d31.00.54

Applicable to

AS350 B3.073195

25 OPT - 25.02.60 0 2015-10-05

EQUIPMENT AND FURNISHINGS - Change of JAR

OPS3.745 first aid kit

Effectivity: (B, BA, BB, B1, B2, B3, D, L1) Helicopters -

with first aid kit P/N 7052A4256019 and POST MOD

OP3110 (Type 159 pilot and copilot crashworthy seats),

or - POST MOD 074338 (Sicma 198 seats with SRP210

for pilot and co-pilot), and PRE MOD 074687 (Change of

JAR OPS 3.745 first aid kit).

OPTIONAL N/A .074687

65 Y 01.00.70 - 1 2015-09-21

LIMITATIONS - Tail rotor drive - Tail rotor drive shaft

bearings

EFFECTIVITY: (B,BA,BB,B1,B2,B3,D) a) Helicopters

equipped with tail rotor drive shaft bearings with Part

Numbers (MP/Nos.):

- 6007-2RSMT47CA (P/N 704A33-651-010, non-

regreasable) manufactured by SKF,

- P9107NPP7 (P/N 704A33-651-111, regreasable)

manufactured by FAFNIR,

- 83A851BC3 and 83A851B-1C3 (P/N 704A33-651-143,

regreasable) manufactured by KOYO.

b) Helicopters equipped with tail rotor drive shaft

bearing with Part Number (MP/N):

- 593404 (P/N 704A33-651-181 , regreasable)

manufactured by FAG.

ASB 05.00.08 N/A 2015-0195 165FH

New

driveshaft

bearings

installed

2015-11-03.

Next insp:

A/CTT

5435,2.

- 165FH

34 N/A - 34.00.20 0 2015-09-16

NAVIGATION - Check of the altimeter

EFFECTIVITY: (B3) Helicopters POST MOD 07-3368 and

PRE MOD AL 4236 whose S/N:s are listed in SB

Recommende

dN/A

Applicable to

AS350 B3AL-4236

23 OPT - 23.00.06 0 2015-09-10

COMMUNICATION - VHF antenna sealing

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopters

PRE MOD 074715 (VHF antenna tightness), POST MOD

OP4657 (New Garmin radio line - GNC255 VOR/VHF) or

OP0154 (COLLINS 251E VHF) or OP0625 (KING KY196

VHF) or 071979 (KY196A COPILOT VHF)


67 N/A - 67.00.66 0 2015-08-26

ROTOR FLIGHT CONTROLS - Functional check procedure

for the tail rotor load compensator

EFFECTIVITY: (B3)

Recommende

d

Applicable to

AS350 B3

71 OPT - 71.00.18 2 2015-07-30

POWER PLANT - Firewall reinforcement

EFFECTIVITY: (B, BA, B1, B2, B3, L1) Helicopters pre-

MOD 073219


63 y 01.00.69 - 1 2015-07-28

LIMITATIONS - Main Gearbox (MGB) Casings -

Limitations and follow-up of casings in torque cycles (TC)

EFFECTIVITY: (B1, B2) Helicopters equipped with a MGB

sump with a Part Number specified in paragraph 4.A.

MGB bottom

casing P/N

350A32-3119-

03 installed.

N/A PAD 15-105

165FH/6M

from 2015-06-

02

2015-12-04:

The recorded

TC on MGB

sump is

34216 /FH is

5270,2. No

further

action is

required until

TC has

reached

93700 (PHAB

WO

17220006).

63 N/A 01.00.68 - 1 2015-07-28

LIMITATIONS - Main Gearbox (MGB) Casings -

Limitations and follow-up of casings in torque cycles (TC)

EFFECTIVITY: (B3) Helicopters equipped with MGB

casings (main casing assembly and MGB sump) with Part

Numbers specified in paragraph 4.A.

Applicable to

AS350 B3N/A PAD 15-104

65 y - 65.00.43 1 2015-07-15

TAIL ROTOR DRIVE - Tail rotor pich change plate - four

contact bearing

EFFECTIVITY: (B, BA, BB, B1, B2, D, L1) Helicopters PRE

MOD 076550

Recommende

dN/A

Rev 0

performed

2009-02-19

.076550 NO

65 N/A - 65.00.41 3 2015-07-15

TAIL ROTOR DRIVE - Tail rotor pich change plate - four

contact bearing

EFFECTIVITY: (B3) Helicopters PRE MOD 076550

Recommende

dN/A

Applicable to

AS350 B3.076550

63 OPT - 63.00.23 0 2015-07-15

MAIN ROTOR DRIVE - Modification of material and

position of MGB intake O-ring

EFFECTIVITY: (B, B1, B2, B3, BA, BB, D, L1) Helicopters

PRE MOD 077240


32 OPT - 32.00.11 3 2015-06-24

LANDING GEAR - L/G skids - Reinforced wear plates for

skid L/G

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopter(s)

equipped with L/G skids P/N 350A41-1016-XX or 350A41-

1079-XX PRE MOD 072610 or POST MOD 072610 (anti-

gravel paint on landings), PRE MOD 072111 or post

MOD 072111 (skids equipped with long wear plates),

with reinforced wear plates PRE MOD OP 3376

OPTIONAL N/A OP3376

- -159-036-

002015-06-22

Load Cell Torsional Fatigue Failure

Applicability: Helicopter models AS350, AS355, EC130,

Bell 206L and Bell 407 with an Onboard Systems

superseded load cell installed per Table 1 in Onboard

Systems SB 159-036-00.

Recommende

dN/A

N/A. STC

SR01164SE,

SR01393SE,

SH1262NW,

SR01812SE

not installed.

100FH

55 Y - 55.00.18 0 2015-06-22

STABILIZER - Horizontal stabilizer - Improvement of the

Stabilizer / Tail Boom Fittings interface

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopters

PRE MOD 074643

Recommende

dN/A .074643

28 N/A - 28.00.21 0 2015-06-22

FUEL - DISTRIBUTION - Integration of a relay in the fuel

pump control circuit

EFFECTIVITY: (B2, B3) Helicopters POST MOD 073273

and PRE MOD 074280 and 350A084578.00

Recommende

dN/A

MOD 073273

not

embodied.

350A084578.00

25 N/A - 25.02.40 0 2015-06-18

EQUIPMENT AND FURNISHINGS - External load carrying -

Improved locking system of the LISI AS21-5-7 cargo hook

EFFECTIVITY: (B2, B3) Helicopters equipped with the

fixed parts of cargo hook assembly P/N 704A418110.29

(MP/N AS21-5-7)

Recommende

dN/A

No cargo

hook

installed.

67 N/A 05.00.64 - 1 2015-06-18

TIME LIMITS - MAINTENANCE CHECKS - Tail rotor control

- Checking the locking of the stop screws of the yaw

flight controls

EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) AS350

helicopters equipped with adjustable primary yaw stop

in the luggage compartment. Which embody one of the

following modifications: 071908, 071912, 073252. But

do not embody modification 074602.

Compliance

with ASB

67.00.61

cancels the

inspections

issued by this

ASB.

N/A PAD 15-087 110FH - 110FH

67 N/A 67.00.61 - 0 2015-06-18

ROTOR FLIGHT CONTROLS - Installation of dual

mechanical safetying on primary yaw stops

EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) AS350

helicopters equipped with adjustable primary yaw stop

in the luggage compartment. Which embody one of the

following modifications: 071908, 071912, 073252. But

do not embody modification 074602.

Compliance

with this ASB

cancels the

mandatory

scheduled

inspection

introduced by

ASB 05.00.64.

N/A PAD 15-087

660FH/13M

from 2015-06-

18

.074602

63 N/A - 63.00.22 0 2015-06-16

MAIN ROTOR DRIVE - Engine-to-MGB coupling - New

drive bearing of the hydraulic pump on dual hydraulic

helicopters

EFFECTIVITY: (B3) . Dual hydraulic helicopters (POST

MOD OP3346 or OP3082) POST MOD 079566 and PRE

MOD 079568

Recommended N/A 2016-07-16Applicable to

AS350 B3.079568 NO

76 N/A 05.00.77 - 1 2015-06-15

TIME LIMITS - MAINTENANCE CHECKS - Twist grip -

Checking and ensuring water-tightness of connectors on

microswitches 53Ka, 53Kb and 65K (IDLE/FLIGHT modes)

EFFECTIVITY: (B3) ARRIEL 2D engine (MOD 07-4302).

Applicable to

AS350 B3N/A 10FH/7D - .074699

76 N/A 05.00.61 - 3 2015-06-15

ENGINE CONTROLS- Twist grip - Functional check and

installation of a protection for microswitches 53Ka and

53Kb and 65K (IDLE/FLIGHT mode)

EFFECTIVITY: (B3) ARRIEL 2B1 engine associated with

the two-channel FADEC POST MOD 073261 (new twist

grip).

Applicable to

AS350 B3N/A 10FH/7D - .074699

25 N/ASIN 2829-

S-25- 2 2015-06-15

EQUIPMENT AND FURNISHINGS - REMINDER: Rupture of

the restraint system buckle cover

EFFECTIVITY: Type 198 & 284 ZODIAC seats

No Zodiac

Seats

installed.

2014-0127 2015-07-02

63 N/A 01.00.68 - 0 2015-06-02

LIMITATIONS - Main Gearbox (MGB) Casings - Limitation

and follow-up of casings in torque cycles (TC)

EFFECTIVITY: (B3) Helicopters equipped with a MGB

sump with a Part Number: 350A32-3156-21, 350A32-

3156-22, 350A32-3121-04, 350A32-3121-06 or 350A32-

3119-05

Applicable to

AS350 B3N/A -

63 N/A 01.00.69 - 0 2015-06-02

LIMITATIONS - Main Gearbox (MGB) Casings - Limitation

and follow-up of casings in torque cycles (TC)

SUPERSEDED BY REV 1

EFFECTIVITY: Helicopters equipped with a MGB sump

with a Part Number: 350A32-3119-03 or 350A32-3119-

05

MGB bottom

casing P/N

350A32-3119-

03 installed.

N/A -20000FH/

93700TC-

20000FH/

93700TC

63 Y 05.00.84 - 0 2015-05-21

TIME LIMITS - MAINTENANCE CHECKS - Main rotor drive -

Periodic inspection of bi-directional suspension cross-bar

P/Nos. 350A381040.20 and 350A381040.00

EFFECTIVITY: Helicopters equipped with a bi-directional

suspension cross-bar with one of the following Part

Numbers: 350A38-1040-20 or 350A38-1040-00.

MGB

suspension

cross bar P/N

350A38-1040-

20 installed.

N/A 2015-0094

Next MGB

removal ->

every

4500FH/

60000TC

Perf 2015-11-

21 by PHAB

iaw WO

17220006.

Next insp:

9770,2FH /

94216TC.

-4500FH/

60000TC

29 Y - 29.00.18 0 2015-05-11

HYDRAULIC POWER GENERATION - Collective Lever -

Installation or replacement of relay 47D.

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Single

hydraulic helicopters PRE MOD 074688

Recommende

dN/A .074688

25 N/A - 25.02.38 0 2015-05-11

EQUIPMENT AND FURNISHINGS - Front Seats - Restoring

conformity of ZODIAC AEROSPACE 198-series seat

buckets

EFFECTIVITY: (B2, B3)

Recommende

dN/A

150FH/ 3M

from 2015-04-

14

No Zodiac

Seats

installed.

- NO

33 N/A 33.00.33 - 1 2014-11-17

LIGHTS - Position lights - Protection of the power supply

unit of the optional equipment "position strobe lights" -

Corresponds to modification 074611

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters: -

which embody modification OP0811 (installation of

position strobe lights on the horizontal stabilizer) and -

equipped with GRIMES - HONEYWELL power supply unit

Part Number (MP/N) 60-1431-3 of the optional position

strobe light equipment and - which do not embody at

least one of the following modifications: - 074611

(installation of a protector assembly on the wires and

power supply unit of the optional position strobe light

equipment), - 350P085326 (installation and protection

of a Wulfsberg RT5000 AM/FM multi-band tactical wide

band radio), - 073274 (replacement of fuses with circuit-

breakers), - OP1882 (installation of air conditioning), -

OP2698 (replacement of Freon R12).

ASB

05.00.662013-0281R1

660FH/13M

from 2013-11-

20

2015-04-10

N/A. MOD

OP0811 not

embodied.Ho

neywell pwr

suppl unit

not installed.

.074611

63 N/A 63.00.24 - 0 2014-10-21

MAIN ROTOR DRIVE - Engine-to-MGB coupling - New

hydraulic pump drive bearing - Corresponds to

modification 079568

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters

equipped with a single hydraulic system and a hydraulic

pump drive assembly P/N 350A35-0132-00 (POST MOD

079566 and PRE MOD 079568).

N/A 2014-0233 2015-06-30

2015-04-10

N/A. Bearing

not installed.

H/C too old

.079568

25 N/A 25.00.79 - 1 2014-05-21

EQUIPMENT AND FURNISHINGS - BREEZE 300 lb. (136

kg) ELECTRIC HOIST INSTALLATION Failure of the

Pyrotechnic Squib Control to Operate - Corresponds to

MOD 07 3190

EFFECTIVITY: (B,BA,BB,B1,B2,B3,D) . Aircraft equipped

with optional BREEZE or TRW (or LUCAS or Air

Equipement) 300 lb. electric hoist and hoist operator's

control unit 26M, P/N 350A63-1136-00.

Aircraft

equipped

with

BREEZE or

TRW (or

LUCAS or

Air

Equipeme

nt) 300 lb.

electric

hoist fixed

parts pre

modificati

on 07

3190.

100FH/2M

550FH/12M

from 2014-05-

22

Hoist not

installed..073190

62 Y 62.00.34 - 0 2014-04-28

MAIN ROTOR - Swashplates - Check of the rotating star

EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . On helicopters

equipped with a swashplate assembly comprising a

rotating star with Part Number (MP/N) 350A371003-04, -

05, -06, -07 or -08.

N/A 2014-0132R1

165FH eller

senast 2014-

12-31

2015-04-10

P/N affected,

but repair

not

performed =

AD N/A. Test

iaw ASB

performed

2015-11-21

iaw PHAB

WO1722000

6 to confirm.

N/A

52 N/A 52.00.35 - 0 2014-04-03

DOORS - Crew doors - Check of the installation of the

crew door actuators

EFFECTIVITY: On crew door actuators on helicopters

equipped with the emergency flotation gear.

Emergency

flotation gearN/A

53 N/AEASB

05.00.70- 0 2014-03-24

TIME LIMITS - MAINTENANCE CHECKS - Rear structure -

Check of the rear frame reinforcement angles

EFFECTIVITY: Helicopters fitted with a rear structure /

tail boom junction frame, repaired or reinforced with at

least one reinforcement angle on the RH side as per

MRM Work Card 53.10.22.772 or AMM Task 53-31-00, 8-

5 or which embody MOD 073215.

PRE MOD

073215.N/A 2014-0076-E 165FH

73 N/A 01.00.67 - 2 2014-02-17

LIMITATION - FUEL SYSTEM AND CHECK - FADEC - Flight

manual procedure

EFFECTIVITY: AS350 B3 helicopters equipped with an

ARRIEL 2D engine and THALES FADEC P/N C13165DA00

or C13165DA00PC00 or C13165FA00, including all

amendments.

AS350 B3 N/A

71 N/A 71.00.36 - 0 2014-01-15

POWER PLANT - Air intake - Air intake draining on

helicopters equipped with the ARRIEL 1 engine -

Corresponds to modification 350A081080

EFFECTIVITY: Helicopters equipped with engine air

intakes with the following part numbers (MP/N): -

350A54-1080-00 (AS350 B), - 350A54-1080-01 (AS350 B,

B1 and L1), and which do not embody modification

071537 .

071537

embodied.N/A

67 N/A 67.00.43 - 2 2013-11-28

ROTOR FLIGHT CONTROLS - Modification to the electrical

operation of the twist grip for ARRIEL 2B engines -


EFFECTIVITY: Helicopters equipped with the Arriel 2B

engine and modification configuration combination in

accordance with table hereafter: see ASB

ARRIEL 1D1

installed.

H/Cs pre-

MOD

072817

shall

embody SB

33.00.19

previously.

33 N/A 33.00.33 - 0 2013-11-20

LIGHTS - Position lights - Protection of the power supply

unit of the optional equipment "position strobe lights" -


EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters: -

embodying modification OP0811 and equipped with the

GRIMES - HONEYWELL power supply unit MP/N 60-1431-

3 of the optional equipment “position strobe lights”, and -

embodying neither modification 074611 nor

modification 350P085326 (installation and protection of

a Wulfsberg RT5000 multi-band AM/FM hyper-

broadband tactical radio, located in the baggage

compartment).

SUPERSEDED

BY REV 1

ASB

05.00.66

2015-04-10

N/A. MOD

OP0811 not

embodied.Ho

neywell pwr

suppl unit

not installed.

.074611

80 N/A 80.00.09 - 1 2013-08-13

ENGINE STARTING - Improving twist grip operational

logic - Corresponds to MOD 074263

EFFECTIVITY: (B3) . Helicopters equipped with ARRIEL

2B1 engine (MOD 073254), post-MOD 073261 and pre-

MOD 074263.

ARRIEL 1D1

installed.N/A

80

24Y - 05.00.75 0 2013-04-11

ENGINE STARTING - Starter control - Periodic adjustment

and check of the tensioning of the SKURKA (ex APC)

starter-generator damper system

EFFECTIVITY: Helicopters equipped with SKURKA (ex

APC) starter-generator part number (MP/N) 150SG122Q

or 200SGL130Q

N/A 600FH

Perf 2015-11-

30 iaw PHAB

WO1722000

6. Next insp:

A/CTT 5870,2

600FH

52 N/A 52.00.34 - 0 2012-07-09

DOORS - Sliding Door - Double locking of the sliding door

lower ball-joint bolt - Corresponds to modification AL.

4262

EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) . Helicopters

equipped with sliding doors which do not embody

modification AL. 4262 .

N/A 2012-0205

165FH/13M

from 2012-07-

09

Sliding doors

not installed.AL. 4262

67 YEASB

05.00.58- 0 2008-12-01

Time Limits – Maintenance Checks - Collective pitch lever

locking stud

EFFECTIVITY: Helicopters delivered before modification

073175, or - helicopters on which work has been carried

out in service on the locking studs or on the collective

pitch levers or on the locking strips, or - helicopters

having been subject to compliance with Revision 0 or

Revision 1 of Service Bulletins No. 67.00.37 (AS350) or

No. 67.00.19 (AS550), corresponding to modification

073237, or - helicopters with a serial number equal to:

3972-3973-3982-3987-4003-4023-4046-4050-4086-

4120-4122-4132-4143-4152-4172-4194-4259-4314-

4324-4378-4392-4447-4452-4477-4489-4490-4501-

4523-4546-4560-4589-4594-4599-4632-4659-4666-

4671

SB 67.00.37

embodied by

PHAB

WO17220006

2015-11-21.

N/A

Performed

2015-11-21

iaw PHAB

WO

17220006.

Next insp:

A/CTT 5930,2

/ 2017-11-21

660FH /

2Y

53

55Y - 05.00.53 0 2007-05-25

TIME LIMITS - Maintenance Checks - Check of the upper

and lower fin spar attachment frame and screws

assembly

EFFECTIVITY: Upper and lower fin spar attachment

frame and screws assembly.

N/ANext T

inspection

Perf 2015-11-

30 iaw PHAB

WO1722000

6 at A/CTT

5270,2.

Every T

insp

67 YEASB

67.00.3967.00.39 1 2007-03-26

ROTOR FLIGHT CONTROLS - Load Compensator Lever

EFFECTIVITY: (B1, B2, BB) Helicopters equipped with a

load compensator fitted with a lever that was replaced

after delivery.

N/A

2015-12-03:

PHAB

WO1722000

6: Load

compensator

lever verfied

to be correct

during

inspection of

checking the

yaw control

travel.

-

53 y 05.00.43 - 0 2004-02-03

TIME LIMITS - MAINTENANCE CHECKS - REAR

STRUCTURE - Check of the Rear Frame

EFFECTIVITY: Rear structure / tail boom junction frame: -

pre-MOD 073215, or - not equipped with the four

reinforcement angles, P/Nos. 350A08.2493.20 /.21 /.22

/.23, following the repair carried out in accordance with

MRM Work Card 53.10.22.772.

PRE MOD

073215.N/A F-2004-035

Performed

2015-11-21

iaw PHAB

WO

17220006.

Next insp:

A/CTT 5820,2

550FH

29 Y29.00.04

R1- 1 2004-01-27

HYDRAULIC POWER - Lubrification of the Splines on the

Hydraulic Pump Drive Shaft (§ 2.B.3. Lubrication of the

drive shaft splines = recurrent)

Effectivity: (B,BA,BB,B1,B2,B3,D) Hydraulic pump drive

shaft.

N/A -Every

110FH/6M

Perf 2015-11-

21 iaw PHAB

WO1722000

6. Next insp:

A/CTT 5380,2

/ 2016-05-21

.079547 110FH/6M

.05 Y - 05.00.32 2000-08-01

TIME LIMITS - Corrosion check and corrosion prevention

at the lower bearing and on the splines of the main rotor

shaft.

EFFECTIVITY: Main rotor shafts P/N: 350A37-1076-00 to

12 pre and post MOD 076202, 350A37-1290-00 to 05

pre and post MOD 076201.

Shaft P/N

350A37-1290-

03 installed.

N/ANext planet

gear removal

Performed

2015-11-21

PHAB WO

17220006.

Next insp:

2021-11-21

6Y / Every

planet

gear

carrier

removal

62 Y 62.00.22 - 0 1994-03-18

MAIN ROTOR - Spring type vibration damper

Effectivity: AS 350 Helicopters, versions: B, BA, B1, B2, L1

PRE MOD 350A07-6199

N/A - 500FH

1995-03-16

perf on

Antivibration

damper S/N

M715. 2001-

10-29

Accomplishe

d A/CTT

1330,3

350A08-0720 NO

62 Y 62.00.21 - 1 1993-03-09

MAIN ROTOR - Pitch-change lever bushes

EFFECTIVITY: (B, BA, D, B1, B2, L1) PItch-change lever

P/N 350A31-1877-02 not marked wIth an X, and S/N

lower than 100.000.

N/A -

Perf 2015-12-

03 by PHAB,

WO1722000

2 at A/CTT

5270,2.

- NO

MOD A/CTT SB AD DATE Note

AL-4236 5270,2 34.00.20 2015-10-09 N/A. B3 model only.

AL.4262 5270,2 52.00.34 2015-10-09 N/A. Equipment not installed.

OP0124 0 1990-07-31

OP0136 0 1990-07-31

OP0177 0 1990-07-31

OP0223 0 1990-07-31

OP0235 0 1990-07-31

OP0237 0 1990-07-31

OP0303 0 1990-07-31

OP0370 0 1990-07-31

OP0403 0 1990-07-31

OP0419 0 1990-07-31

OP0464 0 1990-07-31

OP0471 0 1990-07-31

OP0472 0 1990-07-31

OP0544 0 1990-07-31

OP0626 0 1990-07-31

OP0649 0 1990-07-31

OP0650 0 1990-07-31

OP0651 0 1990-07-31

OP0664 0 1990-07-31

OP0699 0 1990-07-31

OP0710 0 1990-07-31

OP07200

2230,601.00.51

1990-07-31

2006-05-03

OP0910 0 1990-07-31

OP1045 0 1990-07-31

OP1751 0 1990-07-31

OP3376 32.00.11 2015-10-09 OPTIONAL. Not embodied.

350PO84960 2230,6 ASB25.00.80 2006-05-03

070001 0 1990-07-31

070002 0 1990-07-31

070003 0 1990-07-31

070004 0 1990-07-31

070007 0 1990-07-31

070009 0 1990-07-31

070010 0 1990-07-31

070011 0 1990-07-31

070012 0 1990-07-31

070013 0 1990-07-31

070014 0 1990-07-31

070015 0 1990-07-31

070016 0 1990-07-31

070017 0 1990-07-31

070018 0 1990-07-31

070019 0 1990-07-31

070020 0 1990-07-31

070021 0 1990-07-31

070022 0 1990-07-31

070023 0 1990-07-31

070024 0 1990-07-31

070025 0 1990-07-31

070027 0 1990-07-31

070028 0 1990-07-31

070029 0 1990-07-31

070030 0 1990-07-31

070031 0 1990-07-31

070032 0 1990-07-31

070033 0 1990-07-31

070034 0 1990-07-31

070035 0 1990-07-31

070036 0 1990-07-31

070037 0 1990-07-31

070038 0 1990-07-31

070039 0 1990-07-31

070040 0 1990-07-31

070042 0 1990-07-31

070043 0 1990-07-31

070044 0 1990-07-31

070045 0 1990-07-31

070047 0 1990-07-31

070048 0 1990-07-31

070049 0 1990-07-31

070050 0 1990-07-31

070051 0 1990-07-31

070052 0 1990-07-31

070053 0 1990-07-31

070054 0 1990-07-31

070055 0 1990-07-31

070056 0 1990-07-31

070057 0 1990-07-31

070058 0 1990-07-31

070059 0 1990-07-31

070060 0 1990-07-31

070061 0 1990-07-31

070064 0 1990-07-31

070065 0 1990-07-31

070066 0 1990-07-31

070068 0 1990-07-31

070070 0 1990-07-31

070071 0 1990-07-31

070072 0 1990-07-31

070073 0 1990-07-31

070075 0 1990-07-31

070076 0 1990-07-31

070078 0 1990-07-31

070079 0 1990-07-31

070080 0 1990-07-31

070081 0 1990-07-31

070083 0 1990-07-31

070084 0 1990-07-31

070085 0 1990-07-31

070086 0 1990-07-31

070088 0 1990-07-31

070090 0 1990-07-31

070092 0 1990-07-31

070093 0 1990-07-31

070094 0 1990-07-31

070100 0 1990-07-31

070101 0 1990-07-31

070102 0 1990-07-31

070103 0 1990-07-31

070104 0 1990-07-31

070107 0 1990-07-31

070109 0 1990-07-31

070110 0 1990-07-31

070112 0 1990-07-31

070113 0 1990-07-31

070114 0 1990-07-31

070115 0 1990-07-31

070117 0 1990-07-31

070119 0 1990-07-31

070120 0 1990-07-31

070121 0 1990-07-31

070123 0 1990-07-31

070125 0 1990-07-31

070126 0 1990-07-31

070129 0 1990-07-31

070130 0 1990-07-31

070131 0 1990-07-31

070133 0 1990-07-31

070135 0 1990-07-31

070138 0 1990-07-31

070141 0 1990-07-31

070142 0 1990-07-31

070147 0 1990-07-31

070148 0 1990-07-31

070156 0 1990-07-31

070158 0 1990-07-31

070160 0 1990-07-31

070161 0 1990-07-31

070162 0 1990-07-31

070164 0 1990-07-31

070165 0 1990-07-31

070181 0 1990-07-31

070183 0 1990-07-31

070184 0 1990-07-31

070185 0 1990-07-31

070186 0 1990-07-31

070187 0 1990-07-31

070188 0 1990-07-31

070189 0 1990-07-31

070193 0 1990-07-31

070194 0 1990-07-31

070197 0 1990-07-31

070198 0 1990-07-31

070199 0 1990-07-31

070200 0 1990-07-31

070201 0 1990-07-31

070207 0 1990-07-31

070208 0 1990-07-31

070212 0 1990-07-31

070213 0 1990-07-31

070214 0 1990-07-31

070215 0 1990-07-31

070230 0 1990-07-31

070232 0 1990-07-31

070241 0 1990-07-31

070260 0 1990-07-31

070262 0 1990-07-31

070265 0 1990-07-31

070267 0 1990-07-31

070269 0 1990-07-31

070273 0 1990-07-31

070277 0 1990-07-31

070279 0 1990-07-31

070280 0 1990-07-31

070281 0 1990-07-31

070285 0 1990-07-31

070286 0 1990-07-31

0702890

2230,601.00.51

1990-07-31

2006-05-03

070290 0 1990-07-31

070291 0 1990-07-31

070292 0 1990-07-31

070293 0 1990-07-31

070294 0 1990-07-31

070298 0 1990-07-31

070299 0 1990-07-31

070300 0 1990-07-31

070301 0 1990-07-31

070302 0 1990-07-31

070306 0 1990-07-31

070309 0 1990-07-31

070314 0 1990-07-31

070316 0 1990-07-31

070318 0 1990-07-31

070320 0 1990-07-31

070323 0 1990-07-31

070324 0 1990-07-31

070325 0 1990-07-31

070326 0 1990-07-31

070327 0 1990-07-31

070332 0 1990-07-31

070333 0 1990-07-31

070334 0 1990-07-31

070335 0 1990-07-31

070336 0 1990-07-31

070337 0 1990-07-31

070338 0 1990-07-31

070342 0 1990-07-31

070343 0 1990-07-31

070344 0 1990-07-31

070345 0 1990-07-31

070346 0 1990-07-31

070348 0 1990-07-31

070349 0 1990-07-31

070351 0 1990-07-31

070352 0 1990-07-31

070357 0 1990-07-31

070358 0 1990-07-31

070362 0 1990-07-31

070363 0 1990-07-31

070364 0 1990-07-31

070365 0 1990-07-31

070367 0 1990-07-31

070368 0 1990-07-31

070376 0 1990-07-31

070377 0 1990-07-31

070378 0 1990-07-31

070379 0 1990-07-31

070380 0 1990-07-31

070381 0 1990-07-31

070382 0 1990-07-31

070383 0 1990-07-31

070388 0 1990-07-31

070390 0 1990-07-31

070392 0 1990-07-31

070394 0 1990-07-31

070398 0 1990-07-31

070399 0 1990-07-31

070400 0 1990-07-31

070401 0 1990-07-31

070404 0 1990-07-31

070405 0 1990-07-31

070406 0 1990-07-31

070407 0 1990-07-31

070408 0 1990-07-31

070409 0 1990-07-31

070410 0 1990-07-31

070411 0 1990-07-31

070412 0 1990-07-31

070413 0 1990-07-31

070414 0 1990-07-31

070415 0 1990-07-31

070417 0 1990-07-31

070420 0 1990-07-31

070421 0 1990-07-31

070422 0 1990-07-31

070423 0 1990-07-31

070427 0 1990-07-31

070428 0 1990-07-31

070429 0 1990-07-31

070430 0 1990-07-31

070433 0 1990-07-31

070434 0 1990-07-31

070438 0 1990-07-31

070440 0 1990-07-31

070441 0 1990-07-31

070442 0 1990-07-31

070443 0 1990-07-31

070444 0 1990-07-31

070446 0 1990-07-31

070447 0 1990-07-31

070449 0 1990-07-31

070451 0 1990-07-31

0704520

2230,601.00.51

1990-07-31

2006-05-03

070455 0 1990-07-31

070456 0 1990-07-31

070457 0 1990-07-31

070458 0 1990-07-31

070459 0 1990-07-31

070460 0 1990-07-31

070461 0 1990-07-31

070469 0 1990-07-31

070470 0 1990-07-31

070473 0 1990-07-31

070474 0 1990-07-31

070475 0 1990-07-31

070476 0 1990-07-31

070477 0 1990-07-31

070479 0 1990-07-31

070482 0 1990-07-31

070483 0 1990-07-31

070484 0 1990-07-31

070485 0 1990-07-31

070486 0 1990-07-31

070488 0 1990-07-31

070489 0 1990-07-31

070490 0 1990-07-31

070491 0 1990-07-31

070494 0 1990-07-31

0704980

2230,601.00.51

1990-07-31

2006-05-03

070499 0 1990-07-31

070500 0 1990-07-31

070503 0 1990-07-31

070504 0 1990-07-31

070509 0 1990-07-31

070511 0 1990-07-31

070515 0 1990-07-31

070516 0 1990-07-31

070518 0 1990-07-31

070522 0 1990-07-31

070523 0 1990-07-31

070524 0 1990-07-31

070525 0 1990-07-31

070527 0 1990-07-31

070530 0 1990-07-31

070531 0 1990-07-31

070532 0 1990-07-31

070533 0 1990-07-31

070534 0 1990-07-31

070535 0 1990-07-31

070538 0 1990-07-31

070541 0 1990-07-31

070542 0 1990-07-31

070549 0 1990-07-31

070550 0 1990-07-31

070551 0 1990-07-31

070557 0 1990-07-31

070558 0 1990-07-31

070559 0 1990-07-31

070564 0 1990-07-31

070566 0 1990-07-31

070569 0 1990-07-31

070572 0 1990-07-31

070582 0 1990-07-31

070583 0 1990-07-31

070584 0 1990-07-31

070585 0 1990-07-31

070586 0 1990-07-31

070590 0 1990-07-31

070591 0 1990-07-31

070592 0 1990-07-31

070600 0 1990-07-31

070601 0 1990-07-31

070602 0 1990-07-31

070608 0 1990-07-31

070609 0 1990-07-31

070611 0 1990-07-31

070612 0 1990-07-31

070613 0 1990-07-31

0706150

2230,601.00.51

1990-07-31

2006-05-03

070616 0 1990-07-31

070620 0 1990-07-31

070621 0 1990-07-31

070622 0 1990-07-31

070667 0 1990-07-31

070669 0 1990-07-31

070675 0 1990-07-31

070677 0 1990-07-31

070679 0 1990-07-31

070682 0 1990-07-31

070683 0 1990-07-31

070689 0 1990-07-31

070695 0 1990-07-31

070697 0 1990-07-31

070698 0 1990-07-31

070700 0 1990-07-31

070706 0 1990-07-31

070708 0 1990-07-31

070709 0 1990-07-31

070717 0 1990-07-31

070719 0 1990-07-31

070721 0 1990-07-31

070732 0 1990-07-31

0707330

2230,601.00.51

1990-07-31

2006-05-03

070744 0 1990-07-31

070745 0 1990-07-31

070747 0 1990-07-31

070748 0 1990-07-31

070750 0 1990-07-31

070756 0 1990-07-31

070762 0 1990-07-31

070766 0 1990-07-31

070773 0 1990-07-31

070780 0 1990-07-31

070781 0 1990-07-31

070782 0 1990-07-31

070787 0 1990-07-31

070792 0 1990-07-31

070795 0 1990-07-31

070796 0 1990-07-31

070799 0 1990-07-31

070802 0 1990-07-31

0708040

2230,601.00.51

1990-07-31

2006-05-03

070805 0 1990-07-31

070810 0 1990-07-31

070812 0 1990-07-31

070815 0 1990-07-31

070817 0 1990-07-31

070818 0 1990-07-31

070821 0 1990-07-31

070823 0 1990-07-31

070826 0 1990-07-31

070832 0 1990-07-31Partial installation of SBR type SARMA rod. - Drawing

embodied. 350P08336922. - Aft transmission flange installed

flange AU4G1T6. 350A34102320. Called out by AMS 079029.

070838 0 1990-07-31

070854 0 1990-07-31

070858 0 1990-07-31

070859 0 1990-07-31

070862 0 1990-07-31

070863 0 1990-07-31

070866 0 1990-07-31

070868 0 1990-07-31

070887 0 1990-07-31

070893 0 1990-07-31

070895 0 1990-07-31

0709000

2230,601.00.51

1990-07-31

2006-05-03

070918 0 1990-07-31

070921 0 1990-07-31

070922 0 1990-07-31

070923 0 1990-07-31

070927 0 1990-07-31

070929 0 1990-07-31

070944 0 1990-07-31

070948 0 1990-07-31

070949 0 1990-07-31

070952 0 1990-07-31

070955 0 1990-07-31

070959 0 1990-07-31

070963 0 1990-07-31

070971 0 1990-07-31

070979 0 1990-07-31

071000 0 1990-07-31

071007 0 1990-07-31

071008 0 1990-07-31

071011 0 1990-07-31

071017 0 1990-07-31

071025 0 1990-07-31

0710460

2230,601.00.51

1990-07-31

2006-05-03

0710470

2230,601.00.51

1990-07-31

2006-05-03

0710500

2230,601.00.51

1990-07-31

2006-05-03

071051 0 1990-07-31

071058 0 1990-07-31

071063 0 1990-07-31

071065 0 1990-07-31

071068 0 1990-07-31

071073 0 1990-07-31

071083 0 1990-07-31

071093 0 1990-07-31

071096 0 1990-07-31

071098 0 1990-07-31

071103 0 1990-07-31

071113 0 1990-07-31

071115 0 1990-07-31

071138 0 1990-07-31

0711560

2230,601.00.51

1990-07-31

2006-05-03

071175 0 1990-07-31

071182 0 1990-07-31

071209 0 1990-07-31

071210 0 1990-07-31

0712110

2230,601.00.51

1990-07-31

2006-05-03

Bevel reduction gear M1624 1990-04-27

TGB M907 2008-10-06

071222 0 1990-07-31 Main Rotor Mast M456 1990-04-27

071243 0 1990-07-31

071244 0 1990-07-31

071269 0 1990-07-31

071270 0 1990-07-31

071278 0 1990-07-31

071286 0 1990-07-31

071295 0 1990-07-31

071306 0 1990-07-31

0713180

2230,601.00.51

1990-07-31

2006-05-03

0713230

2230,601.00.51

1990-07-31

2006-05-03

071324 0 1990-07-31

071344 0 1990-07-31

071348 0 1990-07-31

071354 0 1990-07-31

071357 0 1990-07-31

071364 0 1990-07-31

071365 0 1990-07-31

071392 0 1990-07-31

071393 0 1990-07-31

071395 0 1990-07-31

071398 0 1990-07-31

071412 0 1990-07-31

071413 0 1990-07-31

071414 0 1990-07-31

071417 0 1990-07-31

071429 0 1990-07-31

071437 0 1990-07-31

071438 0 1990-07-31

0714470

2230,601.00.51

1990-07-31

2006-05-03

071474 0 1990-07-31

071502 0 1990-07-31

071504 0 1990-07-31

071506 0 1990-07-31

071520 0 1990-07-31

071534 0 1990-07-31

0715370

2230,601.00.51

1990-07-31

2006-05-03

071539 0 1990-07-31

071549 0 1990-07-31

071570 0 1990-07-31

071580 2230,601.00.51

01.00.502006-05-03

071581 0 1990-07-31

071583 0 1990-07-31

0715910

2230,601.00.51

1990-07-31

2006-05-03

071602 0 1990-07-31

071609 0 1990-07-31

0716160

2230,601.00.51

1990-07-31

2006-05-03

071624 0 1990-07-31

0716270

2230,601.00.51

1990-07-31

2006-05-03

071629 0 1990-07-31

071651 0 1990-07-31

071659 0 1990-07-31

071660 0 1990-07-31

071665 2230,601.00.51

01.00.502006-05-03

0716670

2230,601.00.51

1990-07-31

2006-05-03

071671

0

1330,3

2230,6

.

28.00.07R1

01.00.51

1990-07-31

2001-10-29

2006-05-03

071674 0 1990-07-31

0716780

2230,601.00.51

1990-07-31

2006-05-03

0716860

2230,601.00.51

1990-07-31

2006-05-03

071688 0 1990-07-31

071691 0 1990-07-31

071699 2230,6 01.00.51 2006-05-03

0717010

2230,601.00.51

1990-07-31

2006-05-03

071703 2230,6

01.00.35

53.00.18

01.00.51

2006-05-03

071704 0 1990-07-31

071705 0 1990-07-31

071709 2230,601.00.35

01.00.512006-05-03

0717130

2230,601.00.51

1990-07-31

2006-05-03

071719 0 1990-07-31

0717210

2230,601.00.51

1990-07-31

2006-05-03

071726 0 1990-07-31

071727 0 1990-07-31

071733 0 1990-07-31

071735 0 1990-07-31

071736 0 1990-07-31

071737 0 1990-07-31

0717400

2230,601.00.51

1990-07-31

2006-05-03

071753 2230,601.00.51

01.00.502006-05-03

0717550

2230,601.00.51

1990-07-31

2006-05-03

071773 0 1990-07-31

071778 0 1990-07-31

071781 0 1990-07-31

071782 0 1990-07-31

0717980

2230,601.00.50

1990-07-31

2006-05-03

071806 0 1990-07-31

0718130

2230,601.00.51

1990-07-31

2006-05-03

071814 0 1990-07-31

071815 0 1990-07-31

071818 0 1990-07-31

071820 0 1990-07-31

071822 0 1990-07-31

0718260

2230,601.00.51

1990-07-31

2006-05-03

071830 0 1990-07-31

071834 0 1990-07-31

071835 0 1990-07-31

071841 0 1990-07-31

071842 2230,628.00.10

01.00.512006-05-03

071848 0 1990-07-31

071852 0 1990-07-31

071855 0 1990-07-31

071865 0 1990-07-31

071883 0 1990-07-31

071884 0 1990-07-31

071891 0 1990-07-31

071894 0 1990-07-31

071900 0 1990-07-31

071902 0 1990-07-31

071907 0 1990-07-31

071922 0 1990-07-31

071923 0 1990-07-31

071927 0 1990-07-31

0719340

2230,601.00.51

1990-07-31

2006-05-06

071941 0 1990-07-31

071942 0 1990-07-31

071952 0 1990-07-31

0719530

2230,601.00.51

1990-07-31

2006-05-06

071954 0 1990-07-31

071955 2230,6 01.00.51 2006-05-03

071966 2230,639.00.04

01.00.512006-05-03

071967 0 1990-07-31

071969 0 1990-07-31

071971 0 1990-07-31

071973 0 1990-07-31

071978 0 1990-07-31

071980 0 1990-07-31

071981 0 1990-07-31

071982 0 1990-07-31

071986 2230,601.00.51

52.00.212006-05-03

071988 0 1990-07-31

071989 0 1990-07-31

0719950

.

.

67.00.16R2

.

2007-0289

1990-07-31

2008-02-25

.

N/A to B2

072016 0 1990-07-31

072056 2230,6 01.00.51 2006-05-03

072058 2230,6 01.00.50 2006-05-03

072201 2230,6 01.00.51 2006-05-03

072204 2230,601.00.51

52.00.212006-05-03

072205 0 1990-07-31

072208 2230,601.00.51

01.00.502006-05-03

072213 0 1990-07-31

072214 2230,601.00.51

01.00.502006-05-03

072225 0 1990-07-31

072226 0 1990-07-31

072230 2230,601.00.51

01.00.502006-05-03

072239 2230,639.00.04

01.00.512006-05-03

072243 0 1990-07-31

072246 2230,601.00.50

01.00.512006-05-03

072248 0 1990-07-31

072255 0 1990-07-31

072259 0 1990-07-31

072270 0 1990-07-31

072276 0 1990-07-31

072279 0 1990-07-31

072385 2230,6 39.00.04 2006-05-03

072407 2230,601.00.51

01.00.502006-05-03

072460 2230,652.00.21

01.00.512006-05-03 SBT 52.00.21 NOTE: Upper striking plates removed

072475 2230,601.00.51

39.00.062006-05-03

072490 2230,6 01.00.35 2006-05-03

0725982230,6

2230,6

01.00.51

26.00.01

2006-05-03

2006-05-03

072660 2230,6 01.00.35 2006-05-03

072717 JAPAN Belt and Harness strip

072720 0 63.00.07 1990-07-31 FCW 2015-11-20 by PHAB.

072793 79.00.11 JAPAN

072840 33.00.17 2008-09-30 N/A. B3 model only.

073012 1330,3 05.00.31R1 2001-10-29 Accomplished.

073029 1729,1 05.00.36 2004-08-07 Verified.

0731183164

.

2008-01-28

2008-10-06


Oil Pump M1653 2008-01-28

TGB M907 2008-10-06

073139 1520,7 67.00.222003-04-23

2015-04-07

Verified.

SB performed. Verified by PHAB (JA)

073161 1520,7 53.00.31 2003-05-09 Verified.

073179 1330,3 67.00.24 F-2003-002(A) 2001-12-10 Accomplished.

073190 25.00.79 2015-10-09 N/A. Equipment not installed.

073195.

5270,2

31.00.52R1

31.00.52R2

2008-09-30

2015-10-09

N/A. B3 model only.

N/A. B3 model only.

073215 2015-11-30 Applicable. Not incorporated.

073219 71.00.18 2015-10-09 OPTIONAL. Not embodied.

073222 67.00.33 2008-09-30 N/A. B3 model only.

073226 24.00.11R1 2008-09-30 N/A to 1606-1 battery.

073237 5270,205.00.58

67.00.372015-11-21 Implemented by PHAB WO17220006.

073273 2012-02-27 Not incorporated.

073287 52.00.29 2008-08-22 N/A. Not installed.

073288 2420 55.00.12 2006-07-17

073290 52.00.29 2008-08-22 N/A. Not installed.

073298 52.00.30R1 2008-03-05 N/A. Equipment not installed.

073308 52.00.30R1 2008-03-05 N/A. Equipment not installed.

073325 53.00.34 2008-03-05 N/A. Equipment not installed.

073354 31.00.54 2008-09-30 N/A. B3 model only.

073370 24.00.13 2008-09-30 N/A. VEMD not installed.

073380 25.01.01 2008-09-30 N/A. Not installed.

073330 3914,4 55.00.16R1 2009-0030 2009-04-09

074346 26.00.02 2012-02-27 N/A. Mod 073273 not incorporated.

074602 67.00.61 2015-10-09 N/A

074611 33.00.33 2015-10-09 N/A

074643 55.00.18 2015-10-09 Applicable. Not incorporated.

074688 29.00.18 2015-10-09 Applicable. Not incorporated.

07469905.00.77

05.00.612015-10-09 N/A. B3 model only.


075001 0 1990-07-31

075002 0 1990-07-31

075004 0 1990-07-31

075005 0 1990-07-31

075007 0 1990-07-31

075008 0 1990-07-31

075009 0 1990-07-31

075010 0 1990-07-31

075012 0 1990-07-31

075013 0 1990-07-31

075014 0 1990-07-31

075015 0 1990-07-31

075016 0 1990-07-31

075020 0 1990-07-31

075027 0 1990-07-31

075028 0 1990-07-31

075032 0 1990-07-31

075043 0 1990-07-31

075045 0 1990-07-31

075046 2230,6 01.00.51 2006-05-03

075051 0 1990-07-31

075500 0 1990-07-31

075501 0 1990-07-31

075502 0 1990-07-31

075503 0 1990-07-31

075504 0 1990-07-31

075505 0 1990-07-31

075506 0 1990-07-31

075507 0 1990-07-31

075508 0 1990-07-31

075509 0 1990-07-31

075512 0 1990-07-31

075513 0 1990-07-31

075515 0 1990-07-31

075516 0 1990-07-31

075519 0 1990-07-31

075521 0 1990-07-31

075522 0 1990-07-31

0755240

2230,601.00.51

1990-07-31

2006-05-03

075525 0 1990-07-31

075526 0 1990-07-31

075527 0 1990-07-31

075532 0 1990-07-31

075535 0 1990-07-31

075536 0 1990-07-31

075537 0 1990-07-31

0755380

2230,601.00.51

1990-07-31

2006-05-03

075540 0 1990-07-31

075541 0 1990-07-31

075544 0 1990-07-31

075547 0 1990-07-31

0755480

2230,601.00.51

1990-07-31

2006-05-03

075549 0 1990-07-31

075551 0 1990-07-31

075552 0 1990-07-31

075555 2230,6 01.00.51 2006-05-03

075557 0 1990-07-31

075563 0 1990-07-31

075564 0 1990-07-31

075577 0 1990-07-31

075578 0 1990-07-31

075580 5270,2 2015-10-01 Due to inst of TR Blades with P/N 355A12-0040-14

075587 ?

076000 0 1990-07-31

076001 0 1990-07-31

076002 0 1990-07-31

076003 0 1990-07-31

076004 0 1990-07-31

076005 0 1990-07-31

076006 0 1990-07-31

076008 0 1990-07-31

076010 0 1990-07-31

076012 0 1990-07-31

076013 0 1990-07-31

076014 0 1990-07-31

076015 0 1990-07-31

076017 0 1990-07-31

076018 0 1990-07-31

076019 0 1990-07-31

076021 0 1990-07-31

076022 0 1990-07-31

076025 0 1990-07-31

076026 0 1990-07-31

076027 0 1990-07-31

076029 0 1990-07-31

076030 0 1990-07-31

076032 0 1990-07-31

076034 0 1990-07-31

076035 0 1990-07-31

076036 0 1990-07-31

076037 0 1990-07-31

076038 0 1990-07-31

076039 0 1990-07-31

076040 0 1990-07-31

076041 0 1990-07-31

076042 0 1990-07-31

076043 0 1990-07-31

076044 0 1990-07-31

076045 0 1990-07-31

076046 0 1990-07-31

076047 0 1990-07-31

076048 0 1990-07-31

076049 0 1990-07-31

076050 0 1990-07-31

076051 0 1990-07-31

076052 0 1990-07-31

076053 0 1990-07-31

076055 0 1990-07-31

076056 0 1990-07-31

076057 0 1990-07-31

076058 0 1990-07-31

076059 0 1990-07-31

076060 0 1990-07-31

076061 0 1990-07-31

0760630

2230,601.00.51

1990-07-31

2006-05-03

076064 0 1990-07-31

076065 0 1990-07-31

076068 0 1990-07-31

076069 0 1990-07-31

076070 0 1990-07-31

076072 0 1990-07-31

076074 0 1990-07-31

076076 0 1990-07-31

0760780

2230,601.00.51

1990-07-31

2006-05-03

076080 0 1990-07-31

076085 0 1990-07-31

076087

0

1330,3

2230,6

.

65.00.26R1

01.00.51

1990-07-31

2001-10-29

2006-05-03

0760880

2230,601.00.51

1990-07-31

2006-05-03

076089 0 1990-07-31

076090 0 1990-07-31

076095 0 1990-07-31

076098 0 1990-07-31

076100 0 1990-07-31

076103 0 1990-07-31

076105 0 1990-07-31

076107 0 1990-07-31

076108 0 1990-07-31

076109 0 1990-07-31

076110 0 1990-07-31

076112 0 1990-07-31

076113 0 1990-07-31

076114 0 1990-07-31

0761170

2230,601.00.51

1990-07-31

2006-05-03

076120 0 1990-07-31

076124 0 1990-07-31

076125 0 1990-07-31

076129 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076132 0 1990-07-31

076138 0 1990-07-31 MRH M807 1990-11-15

076142 0 1990-07-31

076143 0 1990-07-31 Vibration damper M715 1990-04-27

0761440

2230,601.00.51

1990-07-31

2006-05-03

076145 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076148 0 1990-07-31 Vibration damper M715 1990-04-27

076150 0 1990-07-31

MRH M807 1990-11-15

Vibration damper M715 1990-04-27

Main Rotor Mast M456 1990-04-27

076152 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076156 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076159 0 1990-07-31

076163 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076167 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076169 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076172 2230,601.00.35

01.00.512006-05-03

076174 2230,601.00.51

62.00.132006-05-03

0761750

2230,601.00.51

1990-07-31

2006-05-03MRH M807 1990-11-15

076176 0 1990-07-31 Main Rotor Mast M456 1990-04-27

076187 5070,6 2012-07-02 Mast S/N M456 (new type of swashplate bearing)

076188 5070,6 2012-07-02 Mast S/N M456 (new type of swashplate bearing)

076221 62.00.24 F-2001-557-086(A)R3 2008-09-30 N/A to Starflex P/N

076227 62.00.26 2008-09-30 N/A to M/R Hub P/N

076306 5270,2 2015-10-30 O-ring installed = MOD performed.

076500 0 1990-07-31

076502 0 1990-07-31

076504 0 1990-07-31

076505 0 1990-07-31

076506 0 1990-07-31

076507 0 1990-07-31

076508 0 1990-07-31

0765100

2230,601.00.51

1990-07-31

2006-05-03

076511 0 1990-07-31

0765130

2230,601.00.51

1990-07-31

2006-05-03

076514 0 1990-07-31

076515 0 1990-07-31

076516 0 1990-07-31

076517 0 1990-07-31

0765190

2230,601.00.51

1990-07-31

2006-05-03

0765210

2230,601.00.51

1990-07-31

2006-05-03

076522 0 1990-07-31

0765230

2230,601.00.51

1990-07-31

2006-05-03

076525 0 1990-07-31

076526 0 1990-07-31

076527 0 1990-07-31

076528 0 1990-07-31

0765290

2230,601.00.51

1990-07-31

2006-05-03

0765350

2230,601.00.51

1990-07-31

2006-05-03

0765360

2230,601.00.51

1990-07-31

2006-05-03

076543 2015-11-03 TRH. Found performed.

076544 1330,3 65.00.35 2001-10-29

076550

.

5270,2

3739,1

65.00.41R2

65.00.41R3

65.00.43R0

2008-09-30

2015-10-09

2009-02-19

N/A. B3 model only.

N/A. B3 model only.

Perf. 704A33651210 NR3931

076551 1330,3 65.00.38R1 2001-10-29

076554 05.00.33R1 F-2000-222-079(A) 2001-11-19 Performed on Spider M1815

077000 0 1990-07-31

077001 0 1990-07-31

077002 0 1990-07-31

077003 0 1990-07-31

077004 0 1990-07-31

077005 0 1990-07-31

077008 0 1990-07-31

077009 0 1990-07-31

077011 0 1990-07-31

077012 0 1990-07-31

077014 0 1990-07-31

077016 0 1990-07-31

077017 0 1990-07-31

077018 0 1990-07-31

077019 0 1990-07-31

077020 0 1990-07-31

077021 0 1990-07-31

077022 0 1990-07-31

077023 0 1990-07-31

077024 0 1990-07-31

077026 0 1990-07-31 Bevel reduction gear M1624 1990-04-27

0770270

2230,601.00.51

1990-07-31

2006-05-03

077028 0 1990-07-31

077029 0 1990-07-31

077034 0 1990-07-31


077042 2230,6 01.00.51 2006-05-03

077043 0 1990-07-31


077057 0 1990-07-31


077070 0 1990-07-31

077072 0 1990-07-31 Epicyclic reduction gear M594 1990-04-27

077083 0 1990-07-31

077092 0 1990-07-31

077096 0 1990-07-31

0770980

2230,601.00.51

1990-07-31

2006-05-03 Bevel reduction gear M1624 1990-04-27


077108 0 1990-07-31

077109 0 1990-07-31

0771110

2230,601.00.51

1990-07-31

2006-05-03

077114 2230,6 01.00.51 206-05-03

077117 0 1990-07-31 Epicyclic reduction gear M594 1990-04-27

077118 0 1990-07-31


Oil Pump M1653 1990-04-27

Epicyclic reduction gear M594 1990-04-27


077121 2230,601.00.51

63.00.122006-05-03 MGB spin-on filter

077125 0 1990-07-31

077133 3164 2008-01-28 Bevel reduction gear M1624


077162

63.00.12

63.00.18

63.00.09

Not implemented. Oil Filter P/N CH48108 installed.

077174Not implemented. Old Oil Filter P/N CH48108 installed. P/N

FA01315A AFTER MOD 077174.

077175 63.00.09R1 2001-11-30

Bevel reduction gear M1624

Oil Pump M1653 2001-11-30

Epicyclic reduction gear M594



0772043164

.

.

63.00.13 2.B3

2008-01-28

2008-09-30

Bevel reduction gear M1624

N/A. B3 model only.

077207 5270,2 2015-10-01 Reduction gear bevel S/N M1624. Performed by PHAB.


078500 0 1990-07-31

078501 0 1990-07-31

078502 0 1990-07-31

078503 0 1990-07-31

078504 0 1990-07-31

078505 0 1990-07-31

078507 0 1990-07-31

078508 0 1990-07-31

078509 0 1990-07-31

078510 0 1990-07-31

078511 0 1990-07-31

078512 0 1990-07-31

078513 0 1990-07-31

078514 0 1990-07-31

0785150

2230,601.00.51

1990-07-31

2006-05-03

078517 0 1990-07-31

0785190

2230,601.00.51

1990-07-31

2006-05-03

078520 0 1990-07-31

078521 0 1990-07-31

0785220

2230,601.00.51

1990-07-31

2006-05-03

0785230

2230,601.00.51

1990-07-31

2006-05-03

0785240

2230,601.00.51

1990-07-31

2006-05-03TGB M907 2008-10-06

078525 0 1990-07-31

078526 0 1990-07-31 TGB M907 2008-10-06

078527 0 1990-07-31

078528 0 1990-07-31 TGB M907 2008-10-06

078532 0 1990-07-31 TGB M907 2008-10-06

078533 0 1990-07-31 TGB M907 2008-10-06

078534 0 1990-07-31 TGB M907 2008-10-06

0785350

2230,601.00.51

1990-07-31

2006-05-03TGB M907 2008-10-06

078536 0 1990-07-31 TGB M907 2008-10-06

078537 5270,2 2015-11-03 Aft T/R drive shaft PPT01299

078538 2008-10-06 TGB M907 2008-10-06

078543 1330,3 65.00.36 2001-10-29 TGB M907 2008-10-06

078547 2008-10-06 TGB M907 2008-10-06

078552 5270,2 2014-06-03 TGB M907 2014-06-03

079000 0 1990-07-31

079002 0 1990-07-31

079003 0 1990-07-31

079005 0 1990-07-31

079006 0 1990-07-31

079008 0 1990-07-31

079011 0 1990-07-31

0790170

2230,601.00.51

1990-07-31

2006-05-03

079020 0 1990-07-31

079023 0 1990-07-31

0790250

2230,601.00.51

1990-07-31

2006-05-03

0790290

2230,601.00.51

1990-07-31

2006-05-03

079057 5270,2 2015-11-03 Aft T/R drive shaft PPT01299 (partially perf)

079059 5270,2 2015-11-03 Aft T/R drive shaft PPT01299

079501 0 1990-07-31

079504 0 1990-07-31

079505 0 1990-07-31

079506 0 1990-07-31

079507 0 1990-07-31

0795080

2230,601.00.51

1990-07-31

2006-05-03

079510 0 1990-07-31

079512 0 1990-07-31

079514 0 1990-07-31

079522 0 1990-07-31

079524 0 1990-07-31

079526 0 1990-07-31

079533 0 1990-07-31

0795370

2230,601.00.51

1990-07-31

2006-05-03

079539 0 1990-07-31

079541 0 1990-07-31

079547 1860,5 29.00.04R1 2004-10-14 Verified.

079552 5270,2 2015-11-06 Shaft P/N 350A35-1100-21 installed.

079558Hydraulic pump - drive bearing, inst 2015-10 iaw PHAB

WO17220002

079563 63.00.14 2008-09-30 N/A. Poly V not installed.

079566 2015-04-10 Not implemented.

07956863.00.22

63.00.24

2015-10-09

2015-10-09

N/A. B3 model only.

N/A. Equipment not installed.

080720.

1330,362.00.22

1995-03-16

2001-10-29Vibration damper M715

350A084578.00 5270,2 28.00.21 2015-10-09 N/A (MOD 073273 not embodied.)

350A08-0720 1330,3 62.00.22 1995-03-16 Verified.

ATA Name P/N S/N SLL (04-10/05-12) TBO (05-10) CHK (04-20) Inst A/CTT Inst CTT Inst. DateCurrent

timeTime left Maintenance

Helicopter AS350 B2 2364 - - - - - 1990-07-315271,3FH/

34227TC-

24.31 Battery (SAFT) 1606-1 H03093 OC 24M VC 5270,2 UNK 2015-11-20 1,1FH (TSO)2017-11-20

(24M OH)

VC before installation (04-

20). Periodical: DI every

12M (05-21-02/CMM CHK

2.B), OH (RS FT) every

24M (05-22-02/CMM CHK

3). Specific periodical: DI

every 6M. (05-25-

00/CMM CHK 2.A).

Component Overhauled

2015-11-20.

25.00 First Aid Kit 70028 692/70028 N/A 12M N/A 5270,2 0 2015-11-27 1,1FH aug-1612M insp (JAR-OPS) NEW

2015-08.

25.00Belt crew

Amsafe/AUTOFLUG704A41123012 - OC N/A N/A

Manu.date:

belt 2002-02

/ harness

2011-04

25.00Belt crew

Amsafe/AUTOFLUG704A41123012 - OC N/A N/A

Manu.date:

belt 2002-04

/ harness

2011-04

25.00 Belt pass ANJOU 3491107-12-070 - OC N/A N/AManu.date:


2004-06


2010-05


2011-02


2011-05

25.66 ELT Kannad ELT406AF S1821502-02 P1273-0028 N/A N/A N/A 2234 0 2006-05-04 3037,32016-01-16

(1M insp)

600FH/24M (05-22-00),

1M (05-25-00), MM

KANNAD Periodical (6Y)

25.66 ELT Battery S1820506-01 1105016 6Y N/A N/A 4721,7 0 2011-09-01 549,6

Exp date:

2017-09-01.

WO JFL-48

26.22 Cabin fire extinguisher 704A32810008 640211 N/A 120M (OTL) 2886,4 0 2007-06-28 2384,9 2017-06-28

28.20 Fuel Pump P94B12-209 (704A44510042) B65524 OC N/A N/A 2230,6 0 2006-05-03 3040,7

2398,9FH

(MSM 05-25-

00)

DI every 2400FH (05-25-

00) Perf 2015-11-05 A/CTT

5270,2

62.10Unequipped blade pin

(Yellow)350A31-1771-21 M48086 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2


(Yellow)350A31-1771-21 M48169 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2


(Red)350A31-1771-21 M48333 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2


(Red)350A31-1771-21 M48353 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2


(Blue)350A31-1771-21 M48343 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2


(Blue)350A31-1771-21 M48288 INF N/A N/A 0 0 1990-04-01 5271,3 INF

LUB 600FH/6M (05-25-00)

Perf 2015-11 A/CTT

5270,2

62.10 Main Rotor Blade (R ) 355A11-0030-04 27926 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH

(SLL)

62.10 Main Rotor Blade (Y) 355A11-0030-04 27914 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH

(SLL)

62.10 Main Rotor Blade (B) 355A11-0030-04 27862 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH

(SLL)

62.20 MRH 355A31-0001-06 M807 OC N/A GVI 4378,1 5925,3 2010-06-24 6818,5 OC

GVI when removed (04-

20). GVI every 30FH (05-

25-00, PRE MOD 076153).

TCK when installed 2FH

(05-26-00). All tasks

performed 2015-11 A/CTT

5270,2.

62.20 *Blade horn 350A31-1877-02 M8973 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH

(SLL)

VC (04-20). Perf 2015-11

A/CTT 5270,2


(SLL)

VC (04-20). Perf 2015-11

A/CTT 5270,2

62.20 *Blade horn 350A31-1877-02 M9065 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH VC (04-20). Perf 2015-11


(SLL)

VC (04-20). Perf 2015-11

A/CTT 5270,2

62.20 *Star, Starflex 350A31-1917-01 M3243 2400FH N/A 10FH (Other H/C) 0 2007-08-24 1529 871FH (SLL)GVI 10FH (04-20). Perf

2015-11 A/CTT 5270,2

62.20*Pin, Spherical Thrust

Bearing (Y)350A31-1854-21 23841 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)


Bearing (Y)350A31-1854-21 24155 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)


Bearing (R )350A31-1854-21 24137 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)


Bearing (R )350A31-1854-21 24129 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)


Bearing (B)350A31-1854-21 23301 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)


Bearing (B)350A31-1854-21 24146 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

600,2FH

(SLL)

62.20 *Spherical thrust bearing 579107-00 J (704A33633211) N20461 6400FH N/A 10FH 4598,9 0 2011-02-03 672,45727,6FH

(SLL)

GVI 10FH (04-20) Perf

2015-11 A/C TT 5270,2


(SLL)


2015-11 A/C TT 5270,2


(SLL)


2015-11 A/C TT 5270,2

62.20*Upper sleeve flange

(Straight)350A31-1850-03 M10767 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8

4200,2FH

(SLL)



4200,2FH

(SLL)



4200,2FH

(SLL)

62.20*Lower sleeve flange


4200,2FH

(SLL)



4200,2FH

(SLL)



4200,2FH

(SLL)

62.20*Frequency adapter

YellowE4165F01 (704A33640088) .0277 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/A


2015-11 A/C TT 5270,2

62.20 *Frequency adapter Red E4165F01 (704A33640088) .0264 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/AGVI 10FH (04-20) Perf

2015-11 A/C TT 5270,2

62.20 *Frequency adapter Blue E4165F01 (704A33640088) .0267 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/AGVI 10FH (04-20) Perf

2015-11 A/C TT 5270,2

62.20Vibration damper, spring

type350A31-0033-03 M715 OC N/A N/A 0 0 1990-06-01 5271,3 OC

62.30 Main rotor mast 350A37-0004-02 M456 OC N/A N/A 0 0 1990-06-01 5271,3 OC

62.30 *Non-rotating swashplate 350A37-1002-05 M1799 INF N/A 100FH 0 0 1990-04-01 5271,3 INF

LUB 100FH (04-20) POST

MOD 076188. Perf 2015-

11 A/CTT 5270,2

62.30 *Rotating swashplate 350A37-1003-07 M1340 INF N/A 100FH 0 0 1990-04-01 5271,3 INF

LUB 100FH (04-20) POST

MOD 076188. Perf 2015-

11 A/CTT 5270,2

62.30 *Scissor drive adapter 350A37-1119-21 M1819 INF N/A N/A 0 0 1990-04-01 5271,3 INF62.30 *Scissor drive adapter 350A37-1119-21 M1819 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Scissor link, upper 350A37-1126-01 PMA107 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Scissor link, upper 350A37-1126-01 PMA195 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Scissor link, lower 350A37-1127-01 PMA770 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Scissor link, lower 350A37-1127-01 PMA825 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *MRH attachment bolt 350A37-1244-20 84035 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)












62.30 *Main rotor shaft 350A37-1290-03 M3642 160000TC N/A N/A 0 0 1990-04-015271,3FH

/34227TC125773TC

SB 05.00.32 6Y corr check.

Performed 2015-11-21

A/CTT 5270,2

62.30 *Rotor shaft upper casing 350A37-1291-00 PMA523 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Rotor shaft lower casing 350A37-1292-00 PMA496 INF N/A N/A 0 0 1990-04-01 5271,3 INF

62.30 *Swashplate bearing 704A33651158 NR10004 OTL 6300FH N/A 10FH 5070,6 0 2012-07-02 200,7 6099,3FHGVI 10FH (04-20) DI

600FH (05-22-01). Perf

2015-11 A/CTT 5270,2

63.10 Hydraulic pump - Belt FILONTYPEFO (704A33690004) - OTL 1200FH N/A N/A 4663,4 0 2011-05-16 607,9592,1FH

(OTL)

63.10Hydraulic pump - Drive

bearing593733 (704A33651206) R/NA10785 OTL 3600FH/72M N/A N/A 5270,2 0 2015-11-02 1,1

3598,9FH/20

21-11-02

63.20 Bevel reduction gear 350A32-0300-05 M1624 N/A 3500FH/288M N/A 0 0 1990-06-012107,3

(TSO)

1392,7FH/20

32-01-28

63.20 *Main casing 350A32-3121-04 MA15620 INF N/A N/A 0 0 1990-06-01 5271,3 INF

63.20 *MGB bottom casing 350A32-3119-03 M3540 20000FH / 93700TC N/A N/A 3164 0 2008-01-28 2107,3

17892,7FH /

59473TC

(SLL)

63.20 *Bevel gear 350A32-3173-20 L979 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH

(SLL)

63.20 *Bevel wheel 350A32-3165-20 M791 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH

63.20 *Bevel wheel 350A32-3165-20 M791 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH

(SLL)

63.20 Epicyclic reduction gear 350A32-0110-00 M594 N/A 3500FH/288M N/A 0 0 1990-06-012107,3

(TSO)

1392,7FH/20

32-01-28

63.20 *Sun gear 350A32-1075-20 ZF4466 INF N/A N/A 0 0 1990-06-01 5271,3 INF

63.20 *Fixed ring gear 350A32-1051-20 ZF1987 N/A N/A N/A 0 0 1990-06-01 5271,3 N/ANO SLL, enligt mail Airbus

2015-10-29

63.20 *Planet gear 350A32-1082-03 ZF7523 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH

(SLL)


(SLL)


(SLL)


(SLL)


(SLL)

63.20 *Planet gear cage 350A32-1089-21 ZF635 68700TC N/A N/A 3164 18984TC 2008-01-28 34227TC34473TC

(SLL)

63.20 Oil pump 350A32-0400-00 M1653 N/A 3500FH/288M N/A 0 0 1990-06-01 2107,3 TSO1392,7FH/20

32-01-28

63.30 MGB suspension cross bar 350A38-1040-20 AF238598 INF N/A N/A 0 0 1990-06-01 5271,3 INF

64.10 Tail Rotor Blades 355A12-0040-14 18525 4000FH N/A 30FH 5270,2 0 2015-11-05 1,1 3998,9FH

GVI 30FH (04-20).

Component new 2015-11-

05.

64.10 *Tail rotor blade horn 350A12-1368-04 SND1402 INF N/A N/A 5270,2 0 2015-11-05 1,1 INF

64.10 *Tail rotor blade horn 350A12-1368-04 SND1403 INF N/A N/A 5270,2 0 2015-11-05 1,1 INF

65.10Front Shaft Assy (short

shaft)350A34-0150-03 M3909 N/A N/A N/A 4569,3 2337,8 2010-11-19 3039,8 N/A

65.10Rear Section, Rear

Transm.350A34-0210-06 PPT01299 OC N/A N/A 5270,2 0 2015-11-05 1,1 OC

Ny komponent, levererad

PHAB 2015-11-03

65.10 *Aft shaft (long shaft) 350A34-1012-05 PPT01299 10500FH N/A N/A 5270,2 0 2015-11-05 1,1 10498,9FHNy komponent, levererad

PHAB 2015-11-03

65.10T/R drive shaft - lub

bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1

3598,9FH/

2020-10

DI every 600FH (04-20-

00). 150FH GVI (05-21-

01). LUB 600FH/24M (05-

22-00). New inst 2015-11-

05, A/CTT 5270,2.



3598,9FH/

2020-10


00). 150FH GVI (05-21-

01). LUB 600FH/24M (05-

22-00). New inst 2015-11-

05, A/CTT 5270,2.



3598,9FH/

2020-10


00). 150FH GVI (05-21-

01). LUB 600FH/24M (05-

22-00). New inst 2015-11-

05, A/CTT 5270,2.

T/R drive shaft - lub 3598,9FH/


00). 150FH GVI (05-21-



3598,9FH/

2020-10

00). 150FH GVI (05-21-

01). LUB 600FH/24M (05-

22-00). New inst 2015-11-

05, A/CTT 5270,2.



3598,9FH/

2020-10


00). 150FH GVI (05-21-

01). LUB 600FH/24M (05-

22-00). New inst 2015-11-

05, A/CTT 5270,2.

65.20 Tail Gear Box 350A33-0200-05 M907 N/A 3000FH/288M N/A 5270,2 1880,2 2015-11-06 4265,71118,7FH

/2032-10-06

65.20 *Casing 350A33-1090-01 MA0047 20000FH N/A 1200FH/24M (Other H/C) 0 2008-10-06 1881,318118,7FH

(SLL)

GVI 1200FH/24M (05-25-

00) Perf 2015-11-06 at

CTT 1880,0, A/CTT 5270,2.

65.20 *Tail rotor shaft 350A33-1092-01 MA2318 20000FH N/A N/A 5270,2 3286,5 2014-06-03 3287,616712,4FH

(SLL)

65.20 *Bevel gear 350A33-1000-21 L10803 7500FH N/A N/A (Other H/C) 0 2008-10-06 1881,35618,7FH

(SLL)

65.20 *Bevel wheel 350A33-1001-21 L8972 20000FH N/A N/A (Other H/C) 0 2008-10-06 1881,318118,7FH

(SLL)

65.20 *Control lever 350A33-1526-00 MA84921 20000FH N/A N/A 5270,2 0 2015-11-06 1,119998,9FH

(SLL)

DI every 1200FH/24M (05-

25-00). Component new

2015-11-06.

65.20 Pitch Change Rod 350A33-2145-01 S25983 N/A N/A 30FH 5270,2 0 2015-11-10 1,1 N/A

DI every 30FH (04-20-00)

Component NEW 2015-11

A/CTT 5270,2

65.20 Pitch Change Rod 350A33-2145-01 S25425 N/A N/A 30FH 5270,2 0 2015-11-10 1,1 N/A

DI every 30FH (04-20-00)

Component NEW 2015-11

A/CTT 5270,2

65.20 Spider Assy, Pitch Change 350A33-2030-00 M1815 OC N/A N/A 1330,5 1333,2 2001-11-30 5274 OCDI 150FH (05-21-01) Perf

2015-11 A/CTT 5270,2

65.20*TRH pitch change

bearing704A33-651-210 4050 OTL 3000FH N/A N/A 4828,3 353,4 2011-12-31 796,4

2203,6FH

(OTL)

67.30 Main servocontrol SC5083-1 (704A44831161) 6130 N/A 3000FH/240M N/A 5270,2 0 2015-11-01 1,12998,9FH/20

35-11-01 New 2015-11


35-11-01 New 2015-11


35-11-01 New 2015-11

67.30 Tail rotor servo control AC67032 (704A44831115) BY448 INF 1800FH/240M N/A 3835,9 0 2009-03-18 1435,4364,6FH/202

8-07-26

(GVI 500FH (04-20)PRE

MOD 073139) N/A: MOD

embodied.

80.00 Starter-Generator 150SG122Q 6464 N/A 900FH N/A 4948,4 462,8 2012-04-10 785,7 114,3FH


00), 600FH (SB 05.00.75)

Perf 2015-11 A/CTT

5270,2

MGB Oil Mobil 254

Eng Oil Mobil 254

Hyd Oil Fluid 31Hyd Oil Fluid 31

Fett Grease 7

ENGINE INSP REF TOL Note Last perf. ENG TT Remaining time

ENG SLL (various) (05-10-01-200-801) N/A See Binder tab No.6 -

ENG DAILY (05-10-10-200-801) - DAILY DAILY

ENG TBO/OC (various) (05-15-00-201-801) - See Binder tab No.6 -

ENG Use-Limited Parts (05-15-00-201-802) - See Binder tab No.6 -

ENG 15FH/7D insp (05-20-10-201-810) - DAILY DAILY

ENG 30FH insp (05-20-10-201-815) 3

Performed together

with AS350B2 MSM Ch

05-20-02

5270,2FH 5300,2FH

ENG 50FH insp (05-20-10-201-817) 5 Not to be performed - -

ENG 100FH insp (05-20-10-201-820) 10 7527,5 98,90FH

ENG 150FH insp (05-20-10-201-825) 15 7464,65 86,05FH

ENG 200FH insp (05-20-10-201-830) 20 7464,65 136,05FH

ENG 300FH insp (/12M) (05-20-10-201-835) 30H/1M 7492,35263,75FH/2016-

02-17

Scheduled Engine Inspections

ENG 300FH insp (/12M) (05-20-10-201-835) 30H/1M 7492,3502-17


ENG 500FH insp (05-20-10-201-846) 50 7362,6 334,00FH

ENG 600FH insp (05-20-10-201-850) 50 7068,85 140,25FH

ENG 750FH insp (/2Y) (05-20-10-201-852) 50H/2M 7362,6584,00FH/ 2016-

06-20

ENG 800FH insp (05-20-10-201-855) - Not to be performed - -

ENG 1000FH insp (05-20-10-201-860) 50 6967,7 439,10FH

ENG 1500FH insp (05-20-10-201-870) 50 7464,65 1436,05FH


ENG 3600FH insp (05-20-10-201-886) 50 5995,8 2067,20FH

ENGOil Change,

750FH/24MMobil 254 7464,65

686,05FH /2016-

10-02

ATA Appl.AD

classAD nr FAA AD

Issue

DateSubject

Approval

Holder /

Type

Designation

Effective

date

Expire

datePerformed SB Repetetive

77 N/A AD 2015-0175 2015-08-24Engine Indicating - Tachometer Boxes - Replacement

Applicability: ARRIEL 1E2 engines, all serial numbers.

TURBOMECA

ARRIEL 12015-09-07 1600FH

N/A to Arriel

1D1

MSB 292 77

0844

72 N/A AD 2015-0064R1 2015-07-29

Engine – Front Support Pins – Inspection / Replacement

Applicability: ARRIEL 1E2 turbo-shaft engines, all serial

numbers.

TURBOMECA

ARRIEL 12015-07-29 15FH

N/A to Arriel

1D1

MSB 292 72

0842

72 Y AD 2014-0036 2015-13-04 2014-02-11

Engine - Accessory Gear Box (M01) - 41/23 Tooth Bevel Gear

Assembly - Check / Replacement

Applicability: ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,

1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial

numbers.

TURBOMECA

ARRIEL 1

ARRIEL 2

2014-02-25 2016-10-25MSB 292 72

0839

During every

qualifying shop

visit

72 N/A AD 2013-0120 2013-06-04

Engine - Free Turbine Bearing Plug - Inspection / Rework


1E2, 1K, 1K1, 1S, 1S1, all serial numbers.

TURBOMECA

ARRIEL 12013-06-18 50FH

M04 S/N

10274 not

affected.

A292.72.083

8

72 N/A AD 2012-0187R2 2012-12-06

Engine - Airworthiness Limitation Section - Cycle Counting Aid

System - Modification/Amendment



numbers.

TURBOMECA

ARRIEL 12012-12-13 See AD

Engine not

affected. Cycl

count aid

system not

used.

ALF

72 Y AD 2010-0101R32010-19-06

DCA/TUR/70D2012-09-05

Engine - Module M03 (Gas Generator) - Post-TU347 Second

Stage Turbine Disc - Reduced Life Limit

Applicability: Arriel 1A, 1A1, 1B, 1C, 1C1, 1C2, 1D, 1D1 and

1S1 turbo-shaft engines, all serial numbers, if modified by

Turboméca TU347, except those with Gas Generator 2nd

stage Turbine Discs modified by Turboméca Modification

TU365 in production, or modified by Turboméca Service

Bulletin (SB) 292 72 0365 in-service.

TURBOMECA

ARRIEL 12012-09-19 6500 Ng Cycl

Complied With

2010-09-21

A.292.72.083

1

6500 Ng Cycl

(MM 05-10-01-

200-801-A01 )

72 N/A AD 2012-0143 2012-08-01

Engine - Gas Generator Second Stage Turbine - Inspection /

Replacement

Applicability: All ARRIEL 1B post-mod TU 148, ARRIEL 1D,

ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, all serial

numbers, except those with Gas Generator 2nd stage turbine

wheels installed that have incorporated Turbomeca

modification TU347 in production, or have been modified by

Turbomeca Service Bulletin (SB) 292 72 0347 in-service.

TURBOMECA


N/A. TU 347

incorporated

A292.72.080

7

72 Y AD 2012-0117 2012-07-03

Engine - Gas Generator Rotating Assembly and Rear Bearing -

Check / Replacement



numbers.

TURBOMECA

ARRIEL 12012-07-17

Whenever

M03 is

removed

MM X 292 G2

452 2 Issue

14

Yes

72N/A

(S)AD 2009-0236R1 2010-10-09 2012-06-22


Applicability: All ARRIEL 1B post-mod TU 148, ARRIEL 1D,

ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, with gas

generator second stage turbine wheels Part Numbers (P/N)

listed in Appendix 2 of this AD.

TURBOMECA

ARRIEL 12012-06-29 See AD N/A

A292.72.080

7

72 Y AD 2012-00712003-12-14

DCA/TUR/822012-04-26

Engine - Axial Compressor, Gas Generator Hollow Shaft and

Rear Bearing - Identification / Inspection / Cleaning /

Replacement

Applicability: ARRIEL 1A, 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,


numbers, except those incorporating Turboméca TU360

modification.

TURBOMECA

ARRIEL 12012-05-10

Engine

history

checked: not

op in dusty

environment

= not

repetetive

2012-08-23A292.72.023

0Not repetetive

73 N/A AD 2012-0063 2012-04-17

Engine Fuel & Control - Fuel Control Unit (FCU) 3-way Union

Plug - Inspection

Applicability: ARRIEL 1E2, 1S and 1S1 turboshaft engines, all

serial numbers.

TURBOMECA


N/A to 1D1

engines292.73.0817

72 N/A AD 2010-0273R1 2011-02-16

Engine - Module M03 (Gas Generator) - Second Stage

Turbine Nozzle Guide Vane - Inspection/Replacement

Applicability: Arriel 1B turboshaft engines, if modified by

TU76 or TU202, and not modified by TU148, and fitted with

repaired second stage Nozzle Guide Vane.

TURBOMECA


N/A to 1D1

engines

A292.72.082

9

73 N/A EAD 2011-0023-E 2011-02-10

[Correction] Engine Fuel & Control - Low Pressure Fuel

System / Ejector Assembly - Inspection / Replacement

Applicability: Arriel 1E2, 1S and 1S1 turboshaft engines, all

serial numbers, on which Turbomeca Internal Consign (IC)

No. 298468 or Turbomeca Service Bulletin (SB) No. 292 73

0826 version A has been accomplished.

TURBOMECA


N/A to 1D1

engines

A292.73.083

4

292.73.0826

72 N/A AD 2010-0118 2010-06-18


Applicability: Arriel 1B turboshaft engines, if modified by

TU76 and not modified by TU148 and fitted with repaired

second stage Nozzle Guide Vane.

TURBOMECA


N/A to 1D1

engines

A292.72.082

9

72 N/A EAD 2009-0245-E 2009-26-07 2009-11-10

Engine - Module M05 (Reduction Gear Box) Lubrication Duct -

Inspection / Repair

Applicability: Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2,

1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial numbers if

modified by TU332 and fitted with Modules M05 (Reduction

Gear Box) as identified in figure 1 of Turboméca Mandatory

Service Bulletin (MSB) A292 72 0825 version B.

TURBOMECA

ARRIEL 12009-11-12 2010-02-12 N/A 292.72.0825

72 N/A AD 2009-0112R1 2009-08-08 2009-07-30

Engine - Module M04 (Power Turbine) Power Turbine Blades -

Life Limit / Replacement

Applicability: Variant Arriel 1B, 1D and 1D1 turboshaft

engines, fitted with Modules M04 (Power Turbine) as

identified in figure 1 of Turboméca Mandatory Service

Bulletin (MSB) A292 72 0827 version C, and Variant Arriel 2B,

2B1 and 2B1A turboshaft engines, fitted with Modules M04

as identified in figure 1 of Turboméca MSB A292 72 2833

version C.

TURBOMECA

ARRIEL 1

ARRIEL 2

2009-06-01 See ADN/A to MO4

S/N 10274

A292.72.082

7

72N/A

(S)EAD 2009-0117-E 2009-26-07 2009-06-02


Applicability: Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2,

1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial numbers if

modified by TU332 and fitted with Modules M05 (Reduction

Gear Box) as identified in figure 1 of Turboméca Mandatory

Service Bulletin (MSB) A292 72 0825.

TURBOMECA

ARRIEL 12009-06-04 2010-02-04 N/A 292.72.0825

72N/A

(S)EAD 2009-0068-E 2009-08-08 2009-03-25


Applicability: Variant Arriel 1B, 1D and 1D1 turboshaft

engines, fitted with Modules M04 (Power Turbine) as

identified in fig 1 of Turboméca Mandatory Service Bulletin

(MSB) A292 72 0827 version A.

TURBOMECA

ARRIEL 1

ARRIEL 2

2009-03-27 See AD N/AA292.72.082

7

72 N/A AD 2009-0002 2010-02-01 2009-01-07

Engine - Reduction Gear Box Intermediate Pinion -

Modification

Applicability: Arriel 1B, 1D and 1D1 turboshaft engines, all

serial numbers.

TURBOMECA

ARRIEL 12009-01-21 2011-02-28 N/A

292.72.0276

B

73 S AD 2008-0014 2008-01-17


Applicability: Arriel 1E2, 1S and 1S1 turboshaft engines, all

serial numbers.

TURBOMECA


N/A to 1D1

engines292.73.0817

72N/A

(S)AD 2007-0018R1 2010-10-09 2007-08-14

SUPERSEDED BY EASA AD 2009-0236 DATED 29 OCTOBER

2009

Applicability: all ARRIEL 1B post-mod TU 148, ARRIEL 1D,

ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, not modified

with Turbomeca modification TU347 or Service Bulletin (SB)

292 72 0347 [Installation of turbine Part Number (P/N) 0 292

25 039 0].

TURBOMECA


A292 72

0807 E

72 N/A AD 2007-0045 2007-02-21

Return to Service for Civil Use from an Operator Not

Controlled by a Civil Authority

Applicability: ARRIEL 1A,1A1,1A2,1B, 1C, 1C1, 1C2, 1D, 1D1,

1E2, 1K, 1K1, 1S, 1S1 turboshaft engines originally assembled

by TURBOMECA and having previously been used by an

operator who is not under the control of a civil Authority

(Military, Paramilitary…).

TURBOMECA

ARRIEL 12007-03-08 2007-03-08

N/A to this

engine.292.72.0806

72 Y AD 2007-0002 2006-06-17 2007-01-05

Engine - 2nd Stage Nozzle Guide Vane (NGV2) - Inspection

Applicability: TURBOMECA ARRIEL 1B, 1D and 1D1 models

turboshaft engines, modified TU 202, except to those having

2nd stage nozzle guide vanes of which serial numbers or

specific marks are identified in Service Bulletin No. 292 72

0231 update No 5.

TURBOMECA


Found

Embodied

2010-09-21

A292.72.023

1Not repetetive

72 Y AD 2006-0068 2007-02-17 2006-03-24Engine - Fuel Leaks on the Start Electro Valve - Inspection

Applicability: Arriel 1 Series

TURBOMECA


Complied With

2010-09-21

A292.72.025

1Not repetetive

72N/A

(S)AD

F-2004-

047R12010-10-09 2005-10-26


EFFECTIVITY: This Airworthiness Directive (AD) applies to the

following turboshaft engine variants: ARRIEL 1B which have

been modified per TU 148, ARRIEL 1D, ARRIEL 1D1 and

ARRIEL 1S1 (not incorporating TU347).

TURBOMECA


A292 72

0807 E

72 S ADF-2004-

088R12006-06-17 2004-08-04


EFFECTIVITY: This Airworthiness Directive (AD) applies to

TURBOMECA ARRIEL 1B, 1D and 1D1 models turboshaft

engines, modified TU 202, except to those having 2nd stage

nozzle guide vanes of which serial numbers or specific marks

are identified in Service Bulletin No. 292 72 0231 Revision 5.

TURBOMECA


Found

Embodied

2010-09-21

292 72 0231

R5

72 N/A AD 2003-16-03 2003-09-18

Second Stage Turbine Disk - Inspection of gas generator 2nd

Stage NGV

Applicability: Arriel 1 A, 1 A1, 1 A2, 1 B, 1 C, 1 C1, 1 C2, 1 D, 1

D1, 1 E2, 1 K, 1 K1, 1 S, and 1 S1 that have not incorporated

modification TU 202

TURBOMECA


A292 72

0181 R3 and

A292 72

0212 R5

72 N/A AD 2003-11-08 2003-07-03

2nd stage gas generator - Replacement of 2nd stage turbine

blades (post TU204)

Applicability: Arriel -1B, -1D, and -1D1

TURBOMECA


72 Y AD 2003-03-12 2003-03-07

Bleed Valve - Centrifugal impeller blade rupture. Bleed valve

boss sleeve (TU300 and 316)

Applicability: Arriel 1 A2, 1 C, 1 C1, 1 C2, 1 D, 1 D1, 1 E2, 1 K,

1 K1, 1 S, 1 S1 and Arriel 2 B, 2 B1, 2 C, 2 C1, 2 S1

TURBOMECA


Complied With

2010-09-21Not repetetive

72 Y AD 2002-14-26 2002-08-06

Containment Shield Rings - Installation of containment shield

(TU215 or 254 or 255) and supports (TU259)

Applicability: Arriel Models 1A, 1A1, 1B, 1D, and 1D1

TURBOMECA

ARRIEL 12002-08-06 2002-09-20

Found

Embodied

2010-09-21

Not repetetive

72 S ADF-1990-

064R12003-12-14 2001-03-21


APPLICABILITY: ARRIEL 1 turboshaft engines all variants

installed on single or twin-engine helicopters.

TURBOMECA


Complied With

2008-10-07

A292 72

0230

72 Y AD 2000-20-01 2000-10-17

Rear Bearing Oil Return System - Electrical mag plug for gas

generator rear bearing

Applicability: Arriel 1 A, -1 A1, -1 A2, -1 B, -1 C, -1 C1, -1 C2, -

1 D, -1 D1, -1 K, -1 K1, -1 S, and -1 S1

TURBOMECA


Found

Embodied

2010-09-21292 72 0163

R1 (TU208)

Not repetetive

72 N/A AD 94-25-08 1995-01-17

Gearboxes - Inspection of reduction gearbox chip plug every

8H not modified TU232

Applicability: Arriel Model 1B, 1D, 1D1, 1A with TU13, and

1A1 with TU13 Engines

TURBOMECA


72 N/A AD 91-24-02 1992-02-21

Main Rotor Drive Shaft - Free Wheel Shaft with S/N 793 or

higher not modified TU211 or TU212

Applicability: Arriel 1B, 1D, Arriel 1D, and Arriel 1D1 Engines

TURBOMECA


AD SB TU Description Compliance Date Eng hrs Perf by Rec Module

1 Fitting of a power output shaft made of a tube (3 mm thick) Included in the definition package 2002-06-27 0 Turbomeca

2 Compressor casing. Fitting of cast stators .. Included in the definition package 2002-06-27 0 Turbomeca

4 Combustion chamber. Addition of a positioning dowel device Included in the definition package 2002-06-27 0 Turbomeca

5 Fitting of removable gas generator rear bearing Included in the definition package 2002-06-27 0 Turbomeca

6 Free turbine bearing support fitted with enlarged sealing ring Included in the definition package 2002-06-27 0 Turbomeca

7 1st and 2nd stage diffuser assemblies of centrifugal compressor. Included in the definition package 2002-06-27 0 Turbomeca

8 Free turbine nozzle guide vane. Included in the definition package 2002-06-27 0 Turbomeca

9 Front and rear bearings of axial compressor. Included in the definition package 2002-06-27 0 Turbomeca

11 Injectors supply electric cock. Included in the definition package 2002-06-27 0 Turbomeca

12 Accessory box. Addition of a support for the anticipator control Included in the definition package 2002-06-27 0 Turbomeca

13 Suppression of the free turbine overspeed device Included in the definition package 2002-06-27 0 Turbomeca

14 Axial compressor wheel. Thicking of blades profile on their root Included in the definition package 2002-06-27 0 Turbomeca

15 FCU. Installation of a strainer .. Previously Embodied 2010-09-09 FCU S/N C500B

16

Single engine output for helicopter tail rotor drive.

Previously Embodied 2010-09-21 Free Wheel Shaft

Assy S/N 3182B

19 Power shaft. Suppression of the blanker stop shoulder .. Included in the definition package 2002-06-27 0 Turbomeca

20 Inst of fire detector on the front face of reduction gear box.. Included in the definition package 2002-06-27 0 Turbomeca

21 Lubricating system. Addition of a strainer .. Included in the definition package 2002-06-27 0 Turbomeca

23 FCU. Principal cock of Fuel control unit. Previously Embodied 2010-09-09 FCU S/N C500B

24 Oil pump inlet union and swivel union hollow bolt Included in the definition package 2002-06-27 0 Turbomeca

25 Common oil tapping on the accessory box .. Included in the definition package 2002-06-27 0 Turbomeca

26 Detection of min oil press in gas gen bearings supply circuit Included in the definition package 2002-06-27 0 Turbomeca

27 Free turbine nozzle guide vane. Inserted turbine ring .. Included in the definition package 2002-06-27 0 Turbomeca

28 FCU. Suppression of the tin plating .. Previously Embodied 2010-09-09 FCU S/N C500B

29 Accessory box. Included in the definition package 2002-06-27 0 Turbomeca

30 FCU. Fine adjustment of max Ng stop .. Included in the definition package 2002-06-27 0 Turbomeca

31 Free turbine sealing ring diameter Included in the definition package 2002-06-27 0 Turbomeca

33 Installation of module identification plates Included in the definition package 2002-06-27 0 Turbomeca

37 Combustion chamber outer part. Included in the definition package 2002-06-27 0 Turbomeca

38 Free turbine nozzle guide vane .. Included in the definition package 2002-06-27 0 Turbomeca

92.078(B)R2 39M05. Turbine reduction gear.

N/A to this engine 2010-11-18MO5 S/N 9975

40 Turbine reduction gear. Included in the definition package 2002-06-27 0 Turbomeca

41 Axial compressor. Inst of a wheel shrink fitted on its shaft Included in the definition package 2002-06-27 0 Turbomeca

42 1st and 2nd stage diffusers. Included in the definition package 2002-06-27 0 Turbomeca

43 Turbine reduction gear. Included in the definition package 2002-06-27 0 Turbomeca

44 Accessory drive. Installation of a tail type pinion .. Included in the definition package 2002-06-27 0 Turbomeca

45 Inst of check valve at connection of oil return pipe to oil cooler Included in the definition package 2002-06-27 0 Turbomeca

46 Main output drive. Addition of ducts … Included in the definition package 2002-06-27 0 Turbomeca

47 Engine front support. Addition of a drain Included in the definition package 2002-06-27 0 Turbomeca

48 Electro-valve support. Mounting of a reinforced support Included in the definition package 2002-06-27 0 Turbomeca

49 Installation of a magnetic plug with indication on the panel Included in the definition package 2002-06-27 0 Turbomeca

51 FCU. Pump pressure relief valve .. Previously Embodied 2010-09-09 FCU S/N C500B

52 Integral injection wheel Included in the definition package 2002-06-27 0 Turbomeca


56

Improvement of the starting bleed valve sealing

Previously Embodied 2010-08-19 Starting Drain

Valve S/N 1165M

58 FCU. Installation of "D.U." rings in the pump unit bearings Previously Embodied 2010-09-09 FCU S/N C500B

60 Reduction gear. Roller bearings inner races.. Included in the definition package 2002-06-27 0 Turbomeca

61

Rear drive. Installation of magnetic seal


Assy S/N 3182B

62 Torquemeter. Inst of the transmitter on accessory box casing Included in the definition package 2002-06-27 0 Turbomeca

63 Suppression of the alternator drive in the module MO5 Included in the definition package 2002-06-27 0 Turbomeca

64 Assembly of the compressor casing and of the accessory box. Included in the definition package 2002-06-27 0 Turbomeca

65 Torquemeter. Installation of an oblique double contact bearing.. Included in the definition package 2002-06-27 0 Turbomeca

67 "Le Bozec & Gautier" bleed valve. Addition of a close limit .. Included in the definition package 2002-06-27 0 Turbomeca

68 Fuel injection union. Installation of two "o'rings .. Included in the definition package 2002-06-27 0 Turbomeca

69 Bearings of the reduction gear drive pinion. Included in the definition package 2002-06-27 0 Turbomeca

70 Free turbine rear bearing. Addition of an axial load device Included in the definition package 2002-06-27 0 Turbomeca

71 Free turbine bearing. Inst of a bearing support.. Included in the definition package 2002-06-27 0 Turbomeca

72 Starter generator drive. Installation of MRC 1905 S bearings Included in the definition package 2002-06-27 0 Turbomeca

73 Installation of an intermediate casing made of INCONEL 625 Included in the definition package 2002-06-27 0 Turbomeca


75 Installation of an injection wheel made from a forging blank Included in the definition package 2002-06-27 0 Turbomeca

76 Installation of a 2nd stage nozzle guide vane with a flexible hub Included in the definition package 2002-06-27 0 Turbomeca

77 Reduction gear. Toothing ratio 30/98 becomes 29/99 Included in the definition package 2002-06-27 0 Turbomeca

79 Cover of the centrifugal compressor. Included in the definition package 2002-06-27 0 Turbomeca

80 Drain valve of the fuel injection system. Included in the definition package 2002-06-27 0 Turbomeca

82 2nd stage gas generator turbine. Included in the definition package 2002-06-27 0 Turbomeca

85 FCU. Fuel pump bearings with Teflon flanks Included in the definition package 2002-06-27 0 Turbomeca

86 Reduction gear casing. Front part reinforced Included in the definition package 2002-06-27 0 Turbomeca

87 Fuel injection manifold. Included in the definition package 2002-06-27 0 Turbomeca


89 External section of combustion chamber. Included in the definition package 2002-06-27 0 Turbomeca

92 FCU. New adjustment of the deceleration unit Included in the definition package 2002-06-27 0 Turbomeca

95 FCU. Change of material of Ng and Ntl springs .. Previously Embodied 2010-09-09 FCU S/N C500B

99 Replaced by TU215 Included in the definition package 2002-06-27 0 Turbomeca

100 Installation of a 2nd stage turbine nozzle guide vane .. Included in the definition package 2002-06-27 0 Turbomeca

101 Addition of a ring for curviccoupling sealing .. Included in the definition package 2002-06-27 0 Turbomeca

102 Fuel distributor of the main injection system. Included in the definition package 2002-06-27 0 Turbomeca

105 Free turbine rear bearing. Included in the definition package 2002-06-27 0 Turbomeca

292.72.0069 106 M05. Reduction gear rear casing. Embodied 2010-11-18 MO5 S/N 9975

107 Fuel injection distributor. Fuel pipe and sleeve .. Included in the definition package 2002-06-27 0 Turbomeca

108 Combustion chamber inner part. Included in the definition package 2002-06-27 0 Turbomeca

109 1st and 2nd stage turbine nozzle guide vane.. Included in the definition package 2002-06-27 0 Turbomeca

110 Injector electro-valve. Suppression of emergency manual ctrl Included in the definition package 2002-06-27 0 Turbomeca

111 FCU. Inst of reinforced spring to hold metering valve diaphragm Previously Embodied 2010-09-09 FCU S/N C500B

112 Free turbine front bearing. Installation of a labyrinth .. Included in the definition package 2002-06-27 0 Turbomeca

113 Installation of "Le Bozec" compressor bleed valve with axial outlet Included in the definition package 2002-06-27 0 Turbomeca

116 Engine control and indicating harness. Installation of a plug.. Included in the definition package 2002-06-27 0 Turbomeca

117 1 st stage gas generator turbine wheel. Addition of "chamfer".. Included in the definition package 2002-06-27 0 Turbomeca

118 2nd stage gas generator turbine wheel. Addition of "chamfer".. Included in the definition package 2002-06-27 0 Turbomeca

119 Rotating assembly. Fitting of turbine bolt in INCO 718 material Included in the definition package 2002-06-27 0 Turbomeca

120 Gas generator rear bearing oil return pipe of 0.8 mm thickness Included in the definition package 2002-06-27 0 Turbomeca

121 FCU. Installation of a reinforced spring Previously Embodied 2010-09-09 FCU S/N C500B

125 FCU. Addition of a 0.5 mm jet on the metering valve .. Previously Embodied 2010-09-09 FCU S/N C500B

292.72.0209 126 Axial compressor. Installation of NC19FeNb axial bolt Included in the definition package 2002-06-27 0 Turbomeca

129 Free turbine bearing. Improvement of the lubrication .. Included in the definition package 2002-06-27 0 Turbomeca

130 1st stage turbine nozzle guide vane. Vanes made of KCN 22 W Included in the definition package 2002-06-27 0 Turbomeca

132 Turbine casing. Plate sheets and bosses made of NC 22 CNb. Included in the definition package 2002-06-27 0 Turbomeca

134 Free turbine bearing pressurisation. Inst of P2 pipe (pre TU 59) Included in the definition package 2002-06-27 0 Turbomeca

135 Module M05 (reduction gear). Improvement .. Included in the definition package 2002-06-27 0 Turbomeca

140 Oil filter. Addition of a stop in front of the by-pass plug Included in the definition package 2002-06-27 0 Turbomeca

142 Introduction of retainers on the oil transfer tubes .. Included in the definition package 2002-06-27 0 Turbomeca

143 Accessory gear box. Installation of 2 SNFA bearings .. Included in the definition package 2002-06-27 0 Turbomeca

144 Gas generator rear bearing lubricating oil pipe. Included in the definition package 2002-06-27 0 Turbomeca

145 Min oil pressure switch supply pipe. Installation of a clamp .. Included in the definition package 2002-06-27 0 Turbomeca

146 Oil return pipe of the gas generator rear bearing. New routing Included in the definition package 2002-06-27 0 Turbomeca

147 Front bearing lubricating pipe. Addition of a clamp .. Included in the definition package 2002-06-27 0 Turbomeca

292.72.0108 149 M02. Inst of generator 1st & 2nd stage turbine with sealed roots Embodied 2010-11-18 MO2 S/N 3741

292.72.0094 150 Identification plate of module M03 Included in the definition package 2002-06-27 0 Turbomeca

151

Free Wheel Shaft Assy


Assy S/N 3182B

292.72.0109 152 M03. Intro of sealing segment between 1st & 2nd stage gas gen.. Embodied 2010-11-18 MO3 S/N 9936

153

Free Wheel Shaft Assy


Assy S/N 3182B

154 Heat shield securing. Repl of 2 mounting tabs by securing strap Included in the definition package 2002-06-27 0 Turbomeca

155 Gas generator rear bearing. Inst of bearing with reduced.. Included in the definition package 2002-06-27 0 Turbomeca

158 FCU. Constant AP device equipped with matched valve & guide Embodied on non-modular elements 2002-06-27 0 Turbomeca

158 FCU. Constant AP device equipped with matched valve & guide Embodied on complete engine 2002-06-27 0 Turbomeca

162 Increase of the clearance on the free turbine bearing support Included in the definition package 2002-06-27 0 Turbomeca

163 M03. 2nd stage generator nozzle guide vane. Embodied 2010-11-18 MO3 S/N 9936

164 Accessory gearbox. Fitting of a magnetic plug Included in the definition package 2002-06-27 0 Turbomeca

165 Replaced by TU259 Included in the definition package 2002-06-27 0 Turbomeca

166 Free turbine/reduction gear coupling sleeve.. Included in the definition package 2002-06-27 0 Turbomeca

292.72.0122 167 Power shaft. Press fitting of the 52 tooth-pinion Included in the definition package 2002-06-27 0 Turbomeca

168 Gas generator 1st stage turbine blades. Included in the definition package 2002-06-27 0 Turbomeca

170 M05. Reduction gearbox. Replacement of a normal screw.. Included in the definition package 2002-06-27 0 Turbomeca

171 Compressor bleed valve. Addition of a 3 way union.. Included in the definition package 2002-06-27 0 Turbomeca

292.72.0130 173 Protection of 1st stage turbine blades Embodied 2010-11-18 MO3 S/N 9936

292.72.0127 174 M03. Injection manifold Embodied 2010-11-18 MO3 S/N 9936

292.72.0124 175M02. M03. Rotating assy. Addition of a curvic-coupling sealing ring..

Embodied 2010-11-18MO2 S/N 3741,

MO3 S/N 9936

292.72.0124 175 M03. Rotating assy. Addition of a curvic-coupling sealing ring.. Embodied 2010-11-18 MO3 S/N 9936

292.73.0121 176 FCU flyweight assembly. Replacement of bearing Previously Embodied 2010-09-09 FCU S/N C500B

292.73.0133 183 FCU. Replacement of the thermal compensating capsule Previously Embodied 2010-09-09 FCU S/N C500B

292.75.0132 184 M03. Unions of the clean P2 air tapping points for the FCU.. Embodied 2010-11-18 MO3 S/N 9936

292.72.0135 188 Compressor bleed valve. Opening threshold at Ng = 93% Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.72.0135 188 Compressor bleed valve. Opening threshold at Ng = 93% Embodied on complete engine 2002-06-27 0 Turbomeca

292.72.0136 189 Accessory gearbox. 23 tooth bevel gear Embodied 2010-11-18 MO1 S/N 9845

292.72.0139 195 Gas Generator rear bearing Embodied 2010-11-18 MO3 S/N 9936

A292.72.0212 197 Inspection of 2nd stage turbine NGV2 mod to TU197 standard Engine not concerned 2010-09-21 MO3 S/N 9936

292.73.0147 198 FCU. Conic section of the constant delta P valve Previously Embodied 2010-09-09 FCU S/N C500B

292.73.0160 199

Fuel system. Improvement of the start drain valve

Previously Embodied 2010-08-19 Starting Drain

Valve S/N 1165M

292.73.0148 200 FCU. Staked housing sleeve Previously Embodied 2010-09-09 FCU S/N C500B

292.72.0149 201 New routing of pipe Embodied 2010-11-18 MO1 S/N 9845

A292.72.0150 202 2nd stage NGV of the gas generator Previously Embodied 2010-11-18 MO3 S/N 9936

F-2002-

258(A)292.72.0265 204 Cancellation of incorporation of TU204 Engine not concerned 2010-11-18

MO3 S/N 9936

98.394(A) 292.72.0163 208 Installation of a chip detector with electric warning Embodied 2010-11-18 MO1 S/N 9845

90.105(B)R1 292.72.0140 211Free wheel shaft assy - inst of a free wheel flange..

Cancelled by TU 221

90.105(B)R1 292.72.0141 212

Freewheel Shaft Assy. New manufacture


Assy S/N 3182B

292.77.0154 214A Indicating and control harness Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.77.0154 214A Indicating and control harness Embodied on complete engine 2002-06-27 0 Turbomeca

1995.069

(A)R3292.72.0175 215

M04. U-shaped INCO 625 containment shieldEmbodied 2010-11-18

MO4 S/N 10274

292.71.0155 216A Permanent installation of the vibration pick up Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.71.0155 216A Permanent installation of the vibration pick up Embodied on complete engine 2002-06-27 0 Turbomeca

292.73.0176 217 FCU. Addition of a second sealing ring Previously Embodied 2010-09-09 FCU S/N C500B

91.156(B)R1 292.72.0146 221

Freewheel shaft assy. Limitation of dynamic deflection


Assy S/N 3182B

292.75.0171 231 Installation of a strainer union for P2 air tapping Embodied 2010-11-18 MO3 S/N 9936

2009-0002 292.72.0276 232 Reduction gearbox intermediate pinion Embodied 2010-11-18 MO5 S/N 9975

292.72.0172 234A Intermediate pinion. Increase of the minimum value Embodied 2010-11-18 MO5 S/N 9975

NO SB 240A M05. Reduction gearbox front casing. Inst. magn. plug Embodied 2010-11-18 MO5 S/N 9975

292.77.0164 241A Accessory gearbox. Installation of torquemeter pickup Embodied 2010-11-18 MO1 S/N 9845

292.72.0167 244 Combustion chamber outer part Embodied 2010-11-18 MO3 S/N 9936

292.72.0196 245 Power shaft provided with an oil collector Embodied 2010-11-18 MO1 S/N 9845

292.75.0193 247A Installation of an attachment bracket for the reinforced.. Embodied 2010-11-18 MO5 S/N 9975

292.72.0191 250 2nd stage turbine. Diameter increase of turbine housing Embodied 2010-11-18 MO3 S/N 9936

A292.72.0207 255 M04. Incorporation of mod TU255 Engine not concerned 2010-09-21

292.72.0204 257A Washer assembly. Increase of outer diameter Embodied 2010-11-18 MO3 S/N 9936

1995.069

(A)R3292.72.0208 259

Reduction gear. Installation of double supportEmbodied 2010-11-18

MO5 S/N 9975

292.72.0189 262 Injection system drain. Return to tank Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.72.0189 262 Injection system drain. Return to tank Embodied on complete engine 2002-06-27 0 Turbomeca

292.73.0205 266A FCU. Improvement of sealing Previously Embodied 2010-09-09 FCU S/N C500B

292.72.0214 267 M03. Rear bearing. Installation of bearing Embodied 2010-11-18 MO3 S/N 9936

292.72.0219 268A M05. Angular off setting of anti torque washers Embodied 2010-11-18 MO5 S/N 9975

292.74.0203 271A Igniters with separated cables Embodied 2010-11-18 MO3 S/N 9936

292.73.0220 272 NTL bearing of the FCU. Increased lubrication Previously Embodied 2010-09-09 FCU S/N C500B

292.74.0221 273 Installation of HE generator of thyristor type Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.74.0221 273 Installation of HE generator of thyristor type Embodied on complete engine 2002-06-27 0 Turbomeca

292.72.0215 274 Gas generator rear bearing. Installation of deflector Embodied 2010-11-18 MO3 S/N 9936

292.72.0217 275 M02. Tighter fit between cover and casing Embodied 2010-11-18 MO2 S/N 3741

292.72.0211 276 Axial compressor nut with a long base Embodied 2010-11-18 MO3 S/N 9936

292.72.0222 277A M03. 1st and 2nd stage diffuser Embodied 2010-11-18 MO3 S/N 9936

292.72.0223 278 M03. Injection manifold Embodied 2010-11-18 MO3 S/N 9936

292.77.0216 280 Control and indicating harness. Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.77.0216 280 Control and indicating harness. Embodied on complete engine 2002-06-27 0 Turbomeca

292.72.0215 281 Transfer of lubricating jet Embodied 2010-11-18 MO3 S/N 9936

292.72.0227 282 Cancellation of TU282. Modif of manifold and injection wheel

292.72.0215 283 Internal diameter of oil scavange tube Embodied 2010-11-18 MO3 S/N 9936

292.72.0215 284 Gas generator rear bearing. Increased area Embodied 2010-11-18 MO3 S/N 9936

292.72.0228 286 M03. Injection wheel designed from Arriel 2 part Embodied 2010-11-18 MO3 S/N 9936

292.73.0240 289 Installation of protection box Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.73.0240 289 Installation of protection box Embodied on complete engine 2002-06-27 0 Turbomeca

292.72.0241 290A Start and electrovalve bracket Embodied 2010-11-18 MO3 S/N 9936

292.72.0239 291A 1st stage gas generator turbine Embodied 2010-11-18 MO3 S/N 9936

292.74.0242 292A Igniters with separated cables Embodied 2010-11-18 MO3 S/N 9936

292.72.0243 293A Indicating magnetic plug Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.72.0243 293A Indicating magnetic plug Embodied on complete engine 2002-06-27 0 Turbomeca

292.73.0250 299A Optimisation of starting drain valve sealing Previously Embodied 2010-08-19 Starting Drain

Valve S/N 1165M

F-2002-

126(A)292.72.0261 300 Compressor module. Installation of sleeve Embodied 2010-11-18

MO2 S/N 3741

292.72.0267 302A M01. Installation backlash of bevel gear Embodied 2010-11-18 MO1 S/N 9845

292.72.0199 306A Gas generator module. 1st and 2nd stage diffuser Embodied 2010-11-18 MO3 S/N 9936

292.73.0271 307 Fuel system. Ignition solenoid valve Embodied on non-modular elements 2002-06-27 0 Turbomeca

292.73.0271 307 Fuel system. Ignition solenoid valve Embodied on complete engine 2002-06-27 0 Turbomeca

292.72.0272 308A M01. Installation of one INFLEX mechanical magnetic plug Embodied 2010-11-18 MO1 S/N 9845

292.72.0279 314A M05. Installation of one INFLEX mechanical magnetic plug Embodied 2010-11-18 MO5 S/N 9975

F-2002-

126(A)292.72.0275 316A M02 compressor module. Bonding of sleeve Embodied 2010-11-18

MO2 S/N 3741

292.75.0326 326 Integration of an anti-contamination device at bleed valve inlet Konstaterat ej genomförd. 2015-09-03 SE.MG.0107

292.73.0327 327A FCU. Shoe of acceleration control unit Previously Embodied 2010-09-09 FCU S/N C500B

292.73.0329 329A FCU. Plasma coating on NTL flyweight support shaft Previously Embodied 2010-09-09 FCU S/N C500B

292.77.0331 331A Equipment/accessory. Thermocouple harness Embodied on non-modular elements 2007-05-15 Turbomeca

292.72.0332 332B M05. Replacement of the TRIPLEX ball bearing Embodied 2010-11-18 MO5 S/N 9975

292.73.0337 337 FCU. To ensure proper installation of constant delta P … Previously Embodied 2010-09-09 FCU S/N C500B

292.73.0344 344 FCU. Pressure reducing valve with improved sealing Embodied 2010-09-09 FCU S/N C500B

292.72.0347 347 M03. Modified 2nd stage turbine Embodied 2010-11-18 MO3 S/N 9936

292.72.0355 355 M03. Shortening of power turbine NGV lip Embodied 2010-11-18 MO3 S/N 9936

292.72.1357 357 M03. Small labyrinth with increased clearance Rev A embodied 2010-11-18 MO3 S/N 9936

292.72.0359 359 M01. Fastening of two spring strips Embodied 2010-11-18 MO1 S/N 9845

292.05.0103 Recording of operating hours/cycles N/A to 1D1 engines

292.72.0157 a) M05. Inspection of the magnetic plug N/A to POST TU 232

292.72.0157 b) Incorporating of TU39 N/A to POST TU 232

1990.064

(A)R1A292.72.0230

Checking of axial compressor erosion and cleaningEmbodied. Superseeded by AD 2012-0071 2008-10-07

MO3 S/N 9936

2012-0071 A292.72.0230Checking of axial compressor erosion and cleaning

Embodied (DCA/TUR/82) 2012-08-23MO2 S/N 3741,

MO3 S/N 9936

2007-0002 A292.72.0231 Position inspection of secondary air ducts - NGV2 Embodied 2010-11-18 MO3 S/N 9936

292.72.0237 Check and possible replacement of coupling sleeve Embodied 2010-11-18 MO5 S/N 9975

292.72.0246 Ultrasonic frequency inspection of centrifugal compressorEmbodied. Rev E: Integrated in Overhaul

Manual 2015-07-012010-11-18

MO3 S/N 9936

2006-0068 A292.73.0251 Check of the installation of the fuel unions Embodied 2010-09-21

2007-0045 292.75.0806 Military/paramilitary engines N/A to this engine

2009-0236 A292.72.0807 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. Superseded by 2012-0143 2010-11-18 MO3 S/N 9936

2012-0143 A292.72.0807 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. 2015-09-01 SE.MG.0107 MO3 S/N 9936

2007-

0018R1A292.72.0809

Relative position check of 2nd stage turbine bladesSuperseeded by 72.A292.0807

2009-0236 A292.72.0810 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. Superseded by 2012-0143 2010-11-18 MO3 S/N 9936

2008-0014 292.73.0817 FCU 3-way uniion plug N/A to 1D1 engines

292.73.0818 FCU. Check and replacement of the constant delta P … N/A to POST TU 337 engine

2009-0117-E 292.72.0825M05. Insp/repair of post TU332 lubrication ducts

Superseded by 2009-0245-E 2010-11-18MO5 S/N 9975

2009-0245-E 292.72.0825M05. Securement of post TU332 lubrication ducts

Embodied 2010-11-18MO5 S/N 9975

2009-

0112R1A292.72.0827

M04. Restricted use limit of the FT bladesN/A to M04 S/N 10274 2010-11-18

MO4 S/N 10274

2010-

0101R1A292.72.0831 M03. POST TU347 2nd Stg Turbine Disc - Reduced Life Limit

Embodied. Re-inforced Eddy Current Insp -

CFR applied2010-11-18 MO3 S/N 9936

2010-




2010-




2012-0117M03. High Ng Rating Vib Check after M03 deep maintenance

To be performed after M03 deep

maintenanceYes

2012-

0187R1 Cycle counting aid system - Modification/AmendmentFound embodied 2013-03-27

292.72.0836POST TU 360 engines. Operation in a dusty atmosphere. Determination of the limit

for first cleaning of the gas generator rotating assembly. Determination of the

optimal cleaning frequency for the gas generator rotating assy

TU 360 not embodied.

292.73.0837 FCU. Updated log card reflecting the TBO extension to 3,600 hrs Embodied 2014-06-20 FCU S/N C500B

2013-0120 A292.72.0838Module M04 (Free Turbine). Check of the presence, positioning and bonding of the

free turbine bearing plugM04 S/N 10274 not affected. MO4 S/N 10274

2014-0036 292.72.0839 41/23 bevel gear of accessory gearbox (Moduel M01) During every qualifying shop visit MO1 S/N 9845

292.72.0841Fuel injection manifold chemical cleaning. Method 2: Injection with a special tool

inserted through the start injectors and igniter plugsNot performed.

292.71.0843 Creation of a configuration applicable to ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D,

1D1, 1E2, 1K, 1K1, 1S and 1S1 turboshaft engines during overhaul

Not performed.

292.72.0845 Visual check of power turbine (PT) blades Not performed.

ENG Engine Arriel 1D1 9835 5270,2 7527,5 7528,6

Engine Starts: 8609, Ng

Cycl: 9052,70, Np Cycl:

9607,60

ENG*MO1 (Accessory

Gearbox)70BM015420 9845 - 15Y 5270,2 2010-11-29 1532,80 2025-11-25

ENG *MO2 (Axial Compressor) 70BM025020 3741 - 7200FH/15Y 5270,2 1531,70 2010-11-29 1532,805667,2 /

2025-11-25

Intermediate insp 3600FH

(Task 05-20-10-201-886)

2068,30FH remaining (Se

rad 184)

ENG **Axial Comp Wheel 2292152810 3777FB 14,000 Ng Cycl - 5270,2 9041,95C 9052,70C 4947,30C

ENG **FWD Ball Bearing 9609000166 18520 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **AFT Ball Bearing 9609000166 18702 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Tail Gear Bearing 9606490202 23707 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG*MO3 (Gas Generator)

Ng70BMO35420 9936 - 3600FH/15Y 5270,2 1531,70 2010-11-29 1532,80

2067,2 /

2025-11-25

ENG **Centrifugal Impeller .0292252930 2329FT 14,000 Ng Cycl - 5270,2 9041,95C 9052,70C 4947,30C

ENG **Injection Wheel .0292254010 962AD 10,000 Ng Cycl - 5270,2 9041,95C 9052,70C 947,30C

ENG **1st Stage Disk .0292253240 ADH3973AD 10,000 Ng Cycl - 5270,2 9041,95C 9052,70C 947,30C

ENG **2nd Stage Disk .0292250400 J902AD 6,500 Ng Cycl - 5270,2 3563,15C 3573,90C 2926,10C AD 2010-0101R3

ENG**2nd Stage NGV FWD

Hub2292401800 10961PR 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG **2nd Stage NGV AFT Hub 2500019278 10744PR 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG **Bearing 9609000562 3273 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG**1st Stage Turbine

Blades229225A1L0 CC7/1 6000FH/12000 Ng Cycl - 5270,2

1531,70/

3563,15C

1532,80/

3573,90C

4467,20/

8426,10C

**2nd Stage Turbine 1531,70/ 1532,80/ 5667,20/ ENG

**2nd Stage Turbine

Blades.029225A2S0 XL5 7200FH/10000 Ng Cycl - 5270,2

1531,70/

3563,15C

1532,80/

3573,90C

5667,20/

6426,10C

ENG *MO4 (Free Turbine) Nf 70BMO45410 10274 - 7200FH/15Y 5270,2 1531,70 2010-11-29 1532,805667,2 /

2025-11-25

Intermediate insp 3600FH

(72.50.10) 2068,30FH

remaining.

ENG **Free Turbine Disk 2292802500 ADH4674AD 10,000 Np Cycl - 5270,2 9590,60C 9607,60C 392,40C

ENG **FWD Ball Bearing 9609000166 18661 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **AFT Ball Bearing 9609000166 18652 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Roller Bearing 9606080705 5526 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG **Free Turbine Blades 029280A1N0 G22/1 7200FH/12000 Np Cycl - 5270,21531,70/

5328,90C

1532,80/

5345,90C

5667,20/

6654,10C

ENG*MO5 (Reduction

Gearbox)70BMO55420 9975 - 3600FH/15Y 5270,2 1531,70 2010-11-29 1532,80

2067,2 /

2025-11-25

ENG **FWD Drive Bearing 9609000397 149 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **AFT Drive Bearing 9609000397 195 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **FWD Int. Bearing 9609000247 8227 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **AFT Int. Bearing 9609000247 8380 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Torquemeter Bearing 9609000631 2608 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Output Ball Bearing 9609000139 5184 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Output Roller Bearing 9609000266 5481 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Coupling Sleeve .0292708020 3764SET 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG **Left-Hand Nut .0292701370 83 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG *FCU Assy .0164540200 C500B - 3600FH/10Y 5270,2 1531,70 2010-12-01 1532,802067,20 /

2020-09-09Overhauled 2010-09-09

ENG **FCU Filter - - 3,000FH - 5270,2 1531,70 1532,80 1467,20

ENG *Free Wheel Shaft Assy .0292907680 3182B - 3600FH 5270,2 1531,70 1532,80 2067,20Overhauled 2010-09-21

ENG **Free Wheel 9560157860 6959 3,600FH - 5270,2 1531,70 1532,80 2067,20

ENG **Bearing 9608650901 7525SN 7,200FH - 5270,2 1531,70 1532,80 5667,20

ENG **Free Wheel Shaft .0292907740 426 12,000FH - 5270,2 1531,70 1532,80 10467,20

ENG *Starting Drain Valve .0174078030 1165M - 10Y 2010-09-16 2020-09-13

ENG *Drain Valve .0174126090 D032B - 10Y 2010-09-16 2020-09-13Overhauled 2009-03-16

77.10 *Tachometer 64550-007-1 (704A37611002) 21446 N/A N/A Moved from Eng 19047 to

new Eng 9835

77.20 *Oil Pressure Transmitter 64279-004-1 (704A37642060) 5194 N/A N/A Moved from Eng 19047 to

new Eng 9835

STC Subject Note!

FAA SR01452LA / EASA.IM.R.S.00292 Installation of an AKV, Inc. (formerly AKV Partners) Ng cycle counter, p/n 350NGTEC, in accordance with

Master Drawing List no NCC-001, Rev. B, dated January 10, 2004, or later FAA-approved revisions. The

present STC is the validation of the FAA STC SR01452LA whose FAA date of reissuance and amendment is

February 18, 2004.

Inst. but deaktivated.

Provision still installed

JCAB 97-109 / LFV 142/01 Sliding Window. JCAB 97-109 approved 1997-07-11. LFV approved 2001-11-29. LFV Flight Manual

Supplement Nr. S 46/01

Inst.

JCAB 97-107 / LFV 142/01 Floor Camera Hole. JCAB 97-107 approved 1997-07-11. LFV approved 2001-11-29. Inst.

TCCA SH91-20 / FAA SH856NE / LFV

139/01 / EASA.IM.R.S.01492

D350-561 Cargo Mirror Installation. TCCA approved 1991-04-10, FAA approved 2000-02-15, LFV approved

2001-11-18, EASA approved 2010-09-03. Installation of Dart Aero Accessories Inc. Cargo mirror in

accordance with Dart Aero Accessories Inc. Drawing D350-561, Revision B, dated March 29, 1991.

STC removed

TCCA SH92-18 / DGAC 44/96 / FAA

SH989NE / LFV 110/97 /

EASA.IM.R.S.01560

DGAC approved 1996-11-15, FAA approved 2009-06-30, EASA approved 2009-07-17. Installation of D350-

567 Vertical Reference (Floor) Window in accordance with Dart Aerospace Ltd. Installation Instructions

D350-567, Revision D, dated July 8, 2008 or later Transport Canada revision.

Inst.

Interval Action Reference Performed Due Notes

600FH Vertical Refefens Window Dart ICA-D350-567-R2 5270,2FH 5870,2FH STC

600FH Starter-Generator damper system Airbus SB 05.00.75 5270,2FH 5870,2FH

600FH Upper/Lower fin spar attachment Airbus SB 05.00.53 5270,2FH 5870,2FH

100FH/6M Hydraulic Pump Drive Shaft Splines Airbus ASB 29.00.045270,2FH /

2015-11-21

5370,2FH /

2016-05-21

6Y ELT Testing Kannad CMM 25-63-05 2015-11-06 2021-11-06

Batt exp date or

transmitting >1hELT Battery Kannad CMM 25-63-05 - 2017-09-01

6Y Corrosion lower bearing/splines M/R shaft Airbus SB 05.00.32 2015-11-21 2021-11-21

2Y Altimeter Indicator Check LFS 1980:5 (BCL-M 4.3) § 6 2015-10-13 2017-10-13

2Y Airspeed Indicator Check LFS 1980:5 (BCL-M 4.3) § 7 2015-10-13 2017-10-13

2Y Compass Deviation Check LFS 1980:5 (BCL-M 4.3) § 8 2012-08-08 2014-08-08

On the deferred

maintenance list

from PHAB

WO17220006.

165FH T/R Drive Shaft Bearings EASA AD 2015-0195 5270,2FH 5435,2FH

Repetitive (National) Requirements

4500FH/60000TC M/R Drive Cross Bar EASA AD 2015-00945270,2FH /

34216TC

9770,2FH /

94216TC

30FH T/R Pitch-Change Links EASA AD 2010-0006 5270,2FH 5300,2FH

660FH/2Y Coll. Pitch Lever Locking Stud EASA AD 2009-00195270,2FH /

2015-11-21

5930,2FH /

2017-11-21

2Y Mode S/C Transponders LVD 2-3368R1 2015-12-08 2017-12-08

550FH Rear Structure Junction Frame EASA AD F-2004-035 5270,2FH 5820,2FH

100FH Door ”Clear Vision” Window EASA AD F-1993-090-067R1 5270,2FH 5370,2FH

6500 Ng Cycl Second Stage Turbine Disc EASA AD 2010-0101R3 2010-09-212926,10 Ng Cycl

left

ALF/10FH Tail Rotor–Laminated Half-bearings – Inspection / Replacement EASA AD 2012-0257 5270,2FH 5280,2FH / ALF

165FH Tail Rotor Hub Pitch Horn – Inspection / Replacement EASA AD 2013-0133 5270,2FH 5435,2FH

Documents

AS350B2 s/n 2364 SE-JFL - cdn-3.thejameslist.com s/n 2364 SE-JFL 1. ... AS355F1, AS355F2, AS355N, AS355NP, EC130B4, ... Rotorcraft Flight Manual - Chapter Normal Procedures