-~-AIRCRAFT · CNJ AD72-22-01 Landing Gear Uplock Rollers by inspection and lubrication. AD90-08-14 Wing Spar Structures due@ 1075.2. AD84-26-02 Paper Induction Air Filters next due@

?:5i£2 The Standard

-~-AIRCRAFT LOG

ASA-SA-2

- _----~~ --. . -

N63JL BEECH E55 s/n TE-839

Aircraft Record General Information

Manufacturer __,./3e~~=6(=(t~H~Jl~1fi.~ee~&~~r..~r~Lh~R~t:J~- Model -~£~5~5~----------'

rial re 839 Registration Number -~N~'6..,_._1~~~L~-----D to of Manufacture ____ f'---~---'-·-7'----'--/ _________________________ _

n ne(s) currently installed:

M nuf cturer _ ________ Model ___________ Serial __________ _

nuf cturer _ ___ _____ Model ___________ serial __________ _

"'' II r( ) currently installed:

-----------~ Model __________________ _

_____ Serial _________ _ _ Serial-----------

.... ____ Serial ______ Serial ______ Serial _____ _

•t1I I __ Serial ______ Serial ______ Serial _____ _

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Test s, Repairs and A lt e rations TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE

Palm Beach Aircraft Services, Inc. 2633 Lantana Road,~ar 408

I Lantana, FL

I Reg#: N63Jl Model: E55 S/N: TE-839 Date: 01-10-2001 Hobbs: 683.0

Installed new left fuel boost pump P/N#4150-00-1, S/N#2952 overhauled by Dukes, Inc. , WO#R34196. Installed left fuel boost pump switch with new P I /N#35-380053-3. Installed left elevator trim tab hinge pin with new P/N#95 -610006-27. Installed new elevator trim tab push pull rod bolts with new P /N#NAS1004-6D & P/N#NAS464P4-8 Installed new elevator trim tab bushings with new P/N#105740X-AM0290. Adjust right engine vacuum pressure. Service shimmy dampner in accordance with service instructions. Ops checked good. This aircraft engine and/or component identified above was repaired /installed in accordance with current FAA regulations and is approved for return to service. - END -

l e_~ i-----f-----

L. ~th2159990A&P r

YEAR:

DATE

RECORDING YACH TIME

TODAYS FLIGHT

TOTAL TIMEIN SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

Palm Beach Aircraft Services, Inc. 2633 Lantana Road, Hangar 408

Lantana, FL 33462

Reg#: N63JL Model: E55 SIN: TE-839 Date: 07-19-2001 Hobbs: 767.0

Removed and replaced (2) each angle engine cowl braces with new P /N#96-910012-47 and (2) each P/N#96-910012-48. Removed and replaced (2) each angle baffle upper cowl braces with new P/N#96 -910012-49 and (2) each P/N#96-910012-50. Removed left engine vacuum pump P/N#242CW, S/N#60624 and replaced with new P /N#2.42CW, S/N#4AU36. Installed all new main brake linings with new P /N#RA66-44, bled brakes ops checked good. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is approved for return to service with respect to the work performed. - END -

~~~~- ---

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE Palm Beach Aircraft Services, Inc.

2633 Lantana Road, Han~ar 408 Lantana, FL 3346 t

I

Reg: N63JL Model: E55 SIN: TE-839 l Date: 09-18-2001 Hobbs: 773.0 Installed right engine model I0-520-CB7B, S/N#299424-R overhauled

~ byTeledyneContinental Motors. Installed J.P. Instruments twin engine temperature system EDM-760 with fuel flow IAW STC#SA00729SE, Generated FAA Form 337. Installed Gamijectors Kit P/N#GAD13M, S/N#9228 IAW STC#SE09217SC, Generated FAA Form 337. Remo\/00 and replaced alternate air duct with new P/N#111716AX6XX30 and air scoop to manifold induction duct with new P/N#96-919111. Remo\/00 and replaced vacuum regulator filter with new P/N#B3-5-1. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is appro\/00 for return to service with respect to the work performed. - END -

f~~ I

Robert A Kindig 111338~ I-

YEAR:

DATE

RECORDING TODAYS TOTAL TIMEIN SERVICE


YACH FLIGHT TIME


Lantana, FL 33462

Reg: N63JL Model: E55 SIN: TE-839 Date: 10-05-2001 Hobbs: 786.6

Removed and replaced nose gear door actuator shaft assembly with new P/N#96-820034. Removed and replaced nose gear pin assembly with new P/N#002-820016-39. Peformed functional test and gear swing, ops checked good. This maintenance was performed in accordance with the manufacturer's instructions ,,----------and procedures, and the aircraft is approved for return to service with respect to the work performed. - END -


Lantana, FL 33462

Reg: N63JL Model:E55 S/N:TE839 Date: 12-11-2001 Hobbs: 806.5 ACTT: 5306.6

Performed Annual Inspection in accordance with FAR Part 43, Appendix D. Complied with all applicable AD's thru BNJ 2001-21 . CNJ AD72-22-01 Landing Gear Uplock Rollers by inspection and lubrication. AD90-08-14 Wing Spar Structures due@ 1075.2. AD84-26-02 Paper Induction Air Filters next due@ 988.4 or 5488.5TT. CNJ AD98-25-10R1 Seat Restraint System by inspection. Pitot/StaticfTransponder FAR 91 .411 & 91.413 next due October 2002. Performed Annual EL T Test IAW FAR 91.207(d). EL T battery next due 8/2002. 02 Bottle next due for hydrostatic test August 2005. Replaced & serviced aircraft batteries with new (2) each P/N#G-25. S/N#G01984086 & G01984117. Serviced brake reservoir. Replaced left & right vacuum regulator filters with new P/N#B3-5-1 . Removed and replaced right propeller P/N#2AF34C55-NO, S/N#704141 after reseal by Palm Beach Aircraft Propeller W0#10108. I certify that this Aircraft has been inspected/repaired in accordance with an Annual Inspection and has been determined to be in an airworthy condition and that work described above was accomplished and inspected in accordance with current FAA regulations and is approved for return to service. - END -

_llu~ David A. JOtison 291A

"'l'I -I .- Cl - Cl ~:I> = -< -i en

YEAR: RECORDING TODAYS TOTAL Description of'1ltsP2(:tions, Tests, Repairs and Alterations YACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facil ity. (See back pages for other specific entries.)

DATE

Palm Beach Aircraft Services, Inc. 2633 Lantana Rd, St#41

Lantana, FL 33462 5619638111

Reg: N63JL Model: E55 SIN: TE839 Date: 03-28-2002 Hobbs: 862.5

Removed and replaced main gear tires with new 650X8 8 ply. Removed and replaced all main gear brake linings with new P /N#RA66-44. Removed and replaced red gear up light with new P L /N#GE327. This maintenance was performed in accordance with l the manufacturer's instructions and procedures, and the aircraft 1

is approved for return to service with respect to the work ~

performed. - END -

f L I

f Jeff Kamerer 210521646 A&P

,, '

I. ll h 141 . 1.

H K'I' HJ 1M ·>~4-J~9-0088

( '0111pl I d 1) I il 11 Altun t 1 I . t por FAR 4 Appendix E. 111 f>/N ....-.q, /(/ _. '/NJlf?I Alt.2o ~u. 11 l PIN SIN Alt. -----Completed 91.413 Transponder test per FAR 43 Appendix F. # l P/N /= 7 7, IJ-- SIN Z g ( 9 ( #2P/N - SIN -Completed 91. 411 Encoder test per FAR 43 Appendix E. #1 PIN /l-#!2() SIN 2182-3 #2 PIN .---- SIN --Completed 91. 411 Static system test per FAR 43 Appendix E.

Work order # ? "'f<J 2 Date /- l-9 -<I' 2-Sign /,,kl~ AJC# jVtJ.:J'-

Serial n: IY;:llS-Altimdi!r RMds

~ Rlxi!Jl T llys. Temp. l lehlp. 1 . J -IOOO 0 c\

0 t:.J

12-000 -w ' ± 14000 . l -tr1

500 + /(.) 16000 - ~CJ

1000 +11) 18000 -~,.,

1500 I-+- tu 20000 - :L__o ;

' 2000 +1(.) 25000

2500 -f-tu 30000 3000 +10 35000

4000 +ID 40000

6000 6 45000

3{)00 -1.:J 0 50000 t 100'00 -/I) ~/O Work Order #: J CJ'1 o /

=~~~~~~~ FAA#K~==~~4-~ifil38

LYNCH AVIONICS

750 S.W. 34th St. Ft. Lauderdale, FL 33315

FAA Cert. KT 4fl322M ~ f r.v 71;· VII

OOVH

DESC.

0 REP fiacK

/f c.- f ( Yh-- n-cx...,._ .

MFG. tfit.--,rc~ 0r:-MoD ~<J Jy /l SIN I Y? ;J'' CUST. C;fA-AICNo. ~ ~ f :f l POSITION ti" I

?Eifv 1c8 LE

LYNCH AVIONICS


FAA Cert. KT 4R322M t /;) 91.lf IJ

0 OVH

DESC.

0 REP ~BCK •'

f7? 14-J f1,,._, p n-- . MFG. J:;~..._..i

MOD j:_T?t-Tf- sitQJ!ZZ ·' CUST. /j(/J-AICNo. I\./ ('Jul.

POSITION :II I DATE

TECH.

LYNCH AVIONICS


FAA Cert. KT 4R322~ ..

OOVH

DESC

0 REP ;gacK

MOD J:k°3 () SIN '().r i ,;2- 3°1

CUST. !;fl!-

POSITION ..:Ft I DATE Q- 2-'J- (}Z,_

TECH. /~~

Thia elrcreft end/or component identified on the reverH aide w• repelred end lnapected' In eccorde..- with current Reguletiona of the Feclefel Aviation Agency end ia epproved for return to Hrvke. Pertinent detella of the repair ere on file at thia repair station under

Work Order No __ _.7L:,t>:_1L.::,.t1...,.J'-------------

Signed~:::..~;__.....:::....:~--

(Slgneture of euthoriz

-,/fl:;y

Thia elrcraft and I or component identified on the reverH aide w• repeired end lnapected' In .c:corda..- with current Reguletiona of the Feclefal Aviation Agency end ia approved for return to Hrvice. Pertinent detella of the repair ere on file at this repair station under

Work Order No __ _.3~4_.jc...:O:c.....:..2 ____________ _

Signed ~ ~ (Slgna?r'e of euthorized ~idual)

lnapector

Thia aircraft end/ or component identified on the reverH aide wn repeired end lnapected ' in eccorda..- with current Reguletiona of the Feclefel Aviation Agency end ia epproved for return to Hrvlce. Pertinent detella of the repeir ere on file at thia repeir station under

?o'767 ' Work Order No-----------------------

7-J.-',.- 6 ').--Detr._-"-__ ;.._ ______ ~

YEAR:

DAl

RECORDING TODAYS TOTAL TACH FLIGHT TIME IN TIMS: ~ERVICE

mobarak. aircraft

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of T ...... hni ... i<>n "' Qorv::iir ~<>f"ilit" f _q"'"' h<1rl< n<1ne>!': fnr nthPr !':nPr.ifir. Pntries.)

PAli'rrti'lG a INTERIOR 3804 ST. LUCIE BLVD ST . LUCIE CTY. INT AIRPORT

FORT PIERCE, FLORIDA 34946 PHONE (772) 465-7711 FAX: (772) 465-2507

LOG BOOK SUPPLEMENT A/C MAKE: Beechcraft I MODEL: Baron E55 AC REGISTRATION # N63JL

Serial # TE-839 l DATE: 10-15-02 PRIMARY: G8003 Matterhorn White (AWL) SECONDARY: 24160 Blue (IM) TRIM: 44469 Medium Gold Met (IM) TRIM: Ml 152 Dark Cherry Met (IM)

CUSTOM PAINTED BY: Mobarak Aircraft LLC. (772) 465-7711 "The aircraft was stripped and painted with the above following colors. The primary and secondary flight control were removed, the primary flight controls were checked for balance and reinstalled back on aircraft. All work was performed to manufactures manuals and specifications END.


DATE

SUPPLEMENTAL LOG BOOK ENTRY

Reg: N63JL Model: E55 S/N: TE-839 Date: 12-31-2002 Hobbs: 941.9 ACTT: 5442.0

Performed Annual Inspection in accordance with FAR Part 43, Appendix D. Complied with all applicable AD's thru B/W 2002-21 . AD72-22-01 Landing Gear Uplock Rollers by inspection and lube IAW 81#0448-211 next due 1041.9. C/W AD98-25-10-R1 Seat Restraint System NIA by seat belt mfg. AD01-23-10 Flap Flex Shaft Assemblies and Actuators N/A by no record of replacment of UH or R/H flap flex shaft assemblies or flap actuators. C/W AD02-11-07 Electroluminescent Panel Retaining Screw IAW MSB33-3452. Pitot/Static!Transponder Test next due 7/2004. Performed ELT Annual Test IAW 91 .207(d), removed and replaced ELT battery with new P/N#BP1010, due for replacement l

. ~r;;e~ {t/Jx~

-f.


DATE 12/2004. Removed and replaced left horizontal skin-stabilizer with new P/N#96-6200005-122. Removed and replaced heater hose with new P/N#111716-AX3XX42. Removed and replaced main landing gear brake discs with (2) each new P/N#164-02706 and (8) each brake linings with new P/N#066-02200. Replaced all main landing gear bearings with (4) each P/N#13889 and (4) each races P/N#13836. Removed and replaced tail NAV lamp with new lamp P/N#1683. I certify that this Aircraft has been inspected/repaired in accordance with an Annual Inspection and has been determined to be in an airworthy condition and that work described above was accomplished and inspected in accordance with current FAA regulations and is approved for return to service. - END -

~ -

I

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations YACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE


Reg: N63JL Model: E55 S/N: TE-839 Date: 02-28-2003 Hobbs: 989.8

Removed and replaced axial fan assembly/heater blower motor P /N#500702-5081, S/N#AA-69568 repaired/tested by Pifer's Airmotive, Inc., W0#16321. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is approved for return to service with respect to the work performed. - END -

L I

Jeff~~erer 210521646 A&P

-

~ I. h..pproving ~ational Aviation 2. 3. Fonn Tracking Number:

Authority/Country: AUTHORIZED RELEASE CERTIFICATE FAA/United States 16321

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

4 . Organization Name and Pifer 's Airmotive, Inc. (248) 674-0909 5. Work Order/Contract/Invoice

Address: 1660 Airport Rd. Fax# (248) 674-3538 Number:w/o 1 6321 Waterford, Ml 48327 Repair Station# TA 2R I80L L

6. Item 7. Description: 8. Part Number: 9. E~bili!.l:;* I 0. Quantity: 11. Serial/Batch Number: 12. S1atus/Work:

1. Axial Fa90~s ~ y/500702-508 T B V / Installe ( 1) S#AA-69568 R epaired/ Tes

13. Remarks:

I ~ I

14. Certifies the items identified above were manufacrured in conformity to: I](M 14 CFR 43.9 Return to Service 0 Other regulation specified in Black 13

0 Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of

0 Non-approved design dara specified in Block 13. FederaJ Regulations, part 43 and in respect to that work, the items are approved for return to service.

15. Au1horized Signa1urc: 16. Approval/Authorization No.: 20a:d-Signature: 0~ 21. Approval/Certificate No.:

QJ..o V'I\ • TA2Rl80L

17. Name (Typed or Printed): 18. Date (m/d/y): 22. Name (Typed or Printed): u 23. Date (m/d/y):

Lois M. P i fer 2/2 0 / 03

User/Installer Responsibilities

It is imponanl 10 und_erstand that the ex istence of this doc11men1 alone does nm automatically constitute authority lO install the part/component/assembly

Where the user/installer perfonns work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block I, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority c f the country specified in Block I.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Fonm; 8130-3 (6-0 1) *Installer must cross-check eligibility with applicable 1cchnical darn. NSN: 0052-00-012-9005


- ---DATE

Reg:N63JL Model: E55 SIN: TE-839 Date: 07 -30-2003 Hobbs: 1056.6 Removed and replaced main landing gear tires with new Goodyear Flight Special l II 6.50X8-8 ply, repacked wheel bearings. Removed and replaced left propeller resealed by Palm Beach Aircraft Propeller W0#11383. Removed and replaced LH aileron trim tab plate assembly with new (1) each P/N#45-135032-25, arm linkage P/N#45-135039-3 and hardware. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is ~v~rn zith. respe~to the work performed. - END -

.· ~Id_, ·r I Robert A. Kindig Ill 338580935 A~

r

---I

-

. -


DATE


Reg:N63JL Model: E55 S/N: TE-839 Date: 12-01-2003 Hobbs: 1096.8 ACTT: 5596.9 Performed Annual Inspection in accordance with FAR Part 43, Appendix D. Complied with all applicable AD's thru B/W 2003-23. C/W AD72-22-01 Landing Gear Uplock Rollers by inspection and lube IAW 51#0448-211 next due 5696.9. C/W AD84-26-02 Paper Induction Air Filters by replacment of (2) each new filters P/N#AM101120FP. C/W AD90-08-14 Wing Spar Structure IAW SB#2269 & 2360 by inspection next due 1596.8. PitoUStatic/Transponder Test next due 7/2004. Performed EL T Annual Test IAW 91 .207(d), EL T battery due for replacement 12/2004. Removed and replaced taxi light bracket with new P/N#58-360027-3 and lamp with new P/N#4626. Removed and replaced LH uplock springs with (2) each P/N#100942C0020-31. Removed and replaced nose gear upper torque knee pin with new P

- ~ued--

YEAR:

DATE

RECORDING YACH TIME

TODAYS FLIGHT


Description of Inspections, Tests, Repairs am • . Entries must be endorsed with Name, Rating and Certificate Nu, . Technician or Repair Facility. (See back pages for other specific e 1111,

- ----+---- +--------tt1N#58-820010. Removed and replaced LH unfeathering propeller ccumulator with P/N#95-380026A(203}, S/N#13996 overhauled by

-----+-----1----~"ccessories, Inc., WO# 44826R. Removed and replaced vacuum relief 1lters with (2) each new P/N#B3-5-1. Removed and replaced nose tire

- ---+----- -1-- - --fwith new Goodyear Flight Custom Ill 5.00X5 6 ply, repacked wheel _ _ _ __, ___ _ _,_ __ __,bearings. I certify that this Aircraft has been inspected/repaired in

accordance with an Annual Inspection and has been determined to be _ __ __, ____ _,_ _ _ __,in an airworthy condition and that work described above was

accomplished and inspected in accordance with current FAA --- -+------+---___, egula ·ons an is approved for return to service. - END-

~ ~'a---//?~~


Reg: N63JL Model: E55 S/N: TE-839

Date: 03-10-2004 Hobbs: 1160.9 Replaced rudder trim cover with new P/N#96-630000-127 & rudder trim door . with new P/N#96-630000-131. Replaced left & right main gear uplock boots with (1) each P/N#060. Replaced RH landing lamp with new FE P/N#4596. Resealed nose gear strut with rebuild kit P/N#NGK-15, serviced with nitrogen ?606. 1:h1s maintenance was performed in accordance with the manufact~rer's 1nstruct1ons and procedures, and the aircraft is approved for return to service with respect to

the work performed. - END -~

"' T YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations

f YACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE

- SUPPLEMENTAL LOG BOOK ENTRY

Reg: N63JL Model: E55 S/N: TE-839 Date: 03-22-2004 Hobbs: 1163.7

Removed aircraft windshield and replaced with new P/N#LP -269.500 SG, sealed with P/N#SP-6611 seal kit IAW STC#SA993NE, updated equipment list and weight & balance data. Generated FAA Form 337. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is approved for return to service with

. respect to the work performed. - END -

/(d~~A_;@_ Robert A. Kindig Ill 338~35 A&P

- -


DATE


Reg: N63JL Model: E55 S/N: TE-839 Date: 04-27 -2004 Hobbs: 1222.5

Removed and replaced left & right main landing gear tires with new Goodyear Flight Custom Ill 6.50X8 8 ply, repacked wheel bearings. Removed and replaced left main brake linings with new (8) each P/N#RA66-22. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is approved for return to service with respect to

. 1 the work performed. - END -

~~ Michael S. Arato 2764597 A&P


DATE


Reg: N63JL Model: E55 SIN: TE-839

Date: 06-08-2004 Hobbs: 1247.4

Installed new repalcement Vortex generator kit with P/N#1001, P /N#1002 P/N#1003 & P/N#1004. This maintenance was perform~d in accordance with the manufacturer's instruct~ons and procedures, and the aircraft is approved for return to service with ~o the work ~erfom~ed . - END -

~~~ Robert A. Kindig Ill 3if%80935 A&P

-- ~ ·

I


DATE

t3~ ;Vb 3 ;;-,..-L... /for3dS I ;ll/4 • C)_ LOGBOOK ENTRY: - -

THE STATIC PRESSURE SYSTEM,TRANSPONDER WITH ALTITUDE REPORTING WAS IDENTIFIED

~ TESTED AND INSPECTED I/A/W FAR43 APPENDlX E, PAR A & C, APPENDIX F (FAR9l.413) AND IS APPROVED FOR RETURN TO SERVICE. PERTINENT Dtr,~~ OF THlS TEST IS ON FILE I ATTHISREPAIRSTATIONUNDER W.O. (o/C(J DATE J ,/~/ r.;;2] i ;;..,oot

SIGNATURE /}11ai,!c, ~. ~~ 17INSP~~~dJ c TROPIC RADIOlNC.2695 N.W. 56th ST. HANGER 53-D

I FT.LAUDE DAL FL.33309 FAA APPROVED REPAIR STATION## RZ4R510M ,---------

FT.LAUDERDALE EXECUTIVE AIRPORT* ARCHER RAMP* TELEPHO"l'IJ ## 95 776-4030 ~ ~T7fcl9 ~IU d-81C/7 /j t<__ 500 ,5/A ;) ; Gd-3 ~

---1 2-zv~ r-

CERTIFICATION EXPIRES ON d i ~(['O{p --L ~ -1

ALTIMETER SCALE ERROR DATE ., TESTED AT TROPIC RADIO INC. FM APPROVED REPAIR STA.•4RZ4RS10M PART NO .

• l. lf {J -Teet ERROR

,.... ERROR ~

- 1000 f-2-() 10000 w 0.:

00 12000 500 +10 14000

45000 Q..

< 50000 Pl 1000 f-JU 16000 1500 f-2.o 18000 2000 +- 0 20000 3000 +-20 22000 4000 0 25000

51000 • a:: 52000 ~ 53000

~ ~ -

6000 -/0 30000

8000 .-/._ 35000

TROPIC RADIO INC . .2695.N. W. ~JJJ ST. BANGER ~D

Fr.LAUDERDALE , FL 33309

•I

:FAA APPROVED REPAIR STATION #RZAR!ilOM fl.LAUDERDALE EXEClJl."IVE AlRPORT *ARCHER RAMP*

PHONE: 954-776-4030

/ "/ //J/t /f I (

YEAR:

DATE

RECORilllilG f1ilo4-~ TOTAL Description of Inspections, Tests, Repairs and Alterations TACH TIME

FLIGHT

N63JL

TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

RavtheOD Aircraft Services ITT FAA CRS ERYR682D 3992 Aviation Circle Atlanta Georgia 30336

404-699-9200

S/N TE-839 Date: 8/3/04

1. Repaired wire on the LH squat switch. Op landing gear retraction checked good IAW Baron

Shop Manual Section 5.

I certify that with respect to the work perfor eel this Airframe was repaired and inspected in accordance with current FAA regulations. ly those items specified in the Work Order have been inspected and found to be Airwo nd etu · d to Service. No other representations concerning Airworthiness are expressed o imp _ed. e ii are on file under work order number: 11-04-37440T.

CRS: ERYR682D


DATE


Reg: N63JL Model: E55 S/N: TE-839 Date: 08-17-2004 Hobbs: 0.0 ACTT: 5789.6

Removed Hobbs hour meter at 1289.5 and replaced with new model #873 at 0.0. This maintenance was performed in accordance with the manufacturer's instructions and procedures, and the aircraft is approved for return to service with respect to the work performed. - END -

·~~~~ VRobertA. Kindig Ill ~§A&P

YEAR: RECORDING TACH TIME

TODAYS FLIGHT


Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.\

WINDWARD AVIATION 2615 Lantana Road, Ste K!Hangar 805

Lantana, FL 33462 561-966·8668

N63JL SIN: TE-839 1971 BEECH E55 BARON HOBBS: 48.9 HOURS ACTT: 5839.5 HOURS 7 FEBRUARY 2005 NOTE: HOBBS METER CIRCUITRY CHANGED TO RECORD FLIGHT TIME INSTEAD OF ENGINE OPERATION TIME.

TIIlS AIRCRAFT WAS INSPECTED IN ACCORDANCE WITH A BEECHCRAFT/RA YTHEON 100 HOUR/ANNUAL INSPECTION MANUAL.

ENGINE NACELLES: REPLACED ENGINE SILICONE BAFFLING AS REQUIRED. REPAIRED RIGHT ENGINE BAFFLE SUPPORT FORWARD OF #6 CYLINDER. REPAIRED LEFT ENGINE BAFFLE FORWARD OF #5 CYLINDER. REMOVED AND REINSTALLED LEFT ALTERNATOR TO ACCESS REPAIR. REPLACED BOTH VACUUM PUMP INLET FILTER ASSEMBLIES. REPOSillONED LEFT ENGINE PROPELLER CONTROL CABLE. REPLACED LEFT ENGINE INTAKE MANIFOLD DRAIN HOSE. REPLACED ENGINE DRAIN HOSES AND CLAMPS AS REQUIRED. REPLACED LEFT FUEL DISTRIBUTION VALVE-TO-FUEL PUMP HOSE COOLING DUCT. REPLACED LEFT VACUUM PUMP, SEE FORM 8130-3 FROM RAPCO. REFURBISHED LEFT LOWER ENGINE COWLING BY REPLACING SKINS AND FORMERS AS REQUIRED. REPAIRED RIGHT ENGINE COWLING BY REPLACING FORMERS.

FUSELAGE: REPLACED TAXI LAMP. REPLACED FORWARD CABIN FLOORBOARD. REPLACED FORWARD BAGGAGE DOOR SEAL. REMOVED AND REINSTALLED HEATER IRIS VAL VE TO FREE UP AND LUBRICATE. LUBRICATED IRIS VAL VE ACTUATOR CABLE. REPLACED LEFT AFT HEADSET JACK MOUNT. THRUST DETECTOR LABELLED INOP. CLEARED STATIC DRAIN LINE. REPLACED PILOT AND CO-PILOT YOKE MAP LAMPS. REPLACED TAILNAVLAMP. REPLACEDELTBATTERY AND TESTED TRANSMITTER, BATTERY NEXT DUE FEBRUARY 2007. REPAIRED RIGHT COWL FLP POSillON LIGHT CIRCUITRY AND REPLACED TWO LAMPS. PLACARDED ALCOHOL ANTI-ItE SYSTEM INOP. REPLACED CONTROL COLUMN RETENTION PIN.

- ----------"'----------------------------------------------CONTINUED ON NEXT PAGE---------------------------------------------------------

\

YEAR: RECORDING TODAYS TACH FLIGHT

TOTAL TIME IN

WINDWARD AVIATION 2615 Lantana Road, Ste K/Hangar 805

Lantana, FL 33462 561-966-8668

N63JL SIN: TE-839 1971 BEECH E55 BARON HOBBS: 48.9 HOURS ACTT: 5839.5 HOURS 7 FEBRUARY 2005 NOTE: HOBBS METER CIRCUTIRY CHANGED TO RECORD FLIGHT TIME INSTEAD OF ENGINE OPERATION TIME. ---------------------------------------CONTINUED FROM PREVIOUS PAGE-----------------------------------------------WINGS: FLUSHED DEBRIS FROM RIGHT FUEL TANK AND DRAIN VAL VE. TIGHTENED RIGHT AFT NACELLE FUEL CELL TRANSMITTER ATTACHMENT SCREWS. REPLACED BOTH INSTRUMENT AIR FILTERS AND ATTACHMENT CLAMPS IN AFT NACELLE. REPLACED INNER AND OUTER FUEL CAP 0-RINGS. REPLACED LEFT FORWARD AND AFT WING BOLT COVER CLIPS. CLEANED WING BOLT TUB DRAIN HOLES AND LUBRICATED TUBS. CLEANED PITOT TUBE WIRING CONNECTIONS. REPOSillON FLAP ROLLERS AND LUBRICATE. REPAIR FLAP DOWN LIMIT SWITCH ROLLER AND LUBRICATE ALL FLAP SWITCH ROLLERS.

AILERONS: PATCHES NOTED ON LEFT AILERON. REMOVED AND REINSTALLED LEFT AILERON TO CHECK BALANCE IN ACCORDANCE WITH BEECHCRAFT/RA YTHEON SHOP MANUAL USING THE COUNTERBALANCE METHOD: 0.8 IN-LB NOSE HEA VY(MANUAL LIMITS: 0.2 - 1.2 IN-LB NOSE HEAVY). AL THOUGH BEECH TECHNICAL SUPPORT AND SHOP MANUAL DO NOT RECOMMEND SURF ACE PATCHES, THEY WOULD ACCEPT THE REPAIR SINCE 11ffi AILERON BALANCED.

LANDING GEAR AND WHEELS AND BRAKES: ADJUSTED RIGHT AND LEFT MAIN BRAKE LINE AT CALIPER CLAMP AND REPLACED B-NUT ON LEFT LINE. REPLACED OUTER GEAR DOOR ROD ENDS AND ATTACHMENT HARDWARE. ADJUSTED OUTER LANDING GEAR DOOR CLOSED POSillON. FREE-UP AND LUBRICATED NOSE GEAR LEFT TURN STOP. INSTALL INNER MAIN GEAR DOOR FABRIC PATCHES. ADJUSTED LEFT AND RIGHT UPLOCK CLEARANCES. REPLACED LARGE AND SMALL UPLOCK SPRINGS. RESEALED AND SERVICED SHIMMY ------------------------------------------CONTINUED ON NEXT PAGE----------------------------------------------------------------

YEAR: RECORDING TODAYS TACH FLIGHT TIME

-- ~----

----~~




Lantana, FL 33462 561-966-8668

N63JL SIN: TE-839 1971 BEECH E55 BARON HOBBS: 48.9 HOURS ACTT: 5839.5 HOURS 7 FEBRUARY 2005 NOTE: HOBBS METER ClRCUI1RY CHANGED TO RECORD FLIGHT TIME INSTEAD OF ENGINE OPERATION TIME. -----------------------------------------CONTINUED FROM PREVIOUS PAGE----------------------------------------------DAMPENER. REPLACED NOSE GEAR UPPER DRAG LINK BUSHING. REPLACED LEFT WHEEL WELL CLAMP FOR WEIGHT ON WHEELS ClRCUI1RY. REPLACED ALL BRAKE LININGS.

ELEVATORS: ADWSTED RIGHT AND LEFT ELEVATOR 1RIM TAB BOLTS. REPLACED ELEVATOR BELLCRANK WASHERS. INSTALLED ELEVATOR BELLCRANK CENTER PIVOT BUSHING KIT 002-524029-1. REPLACED HEATER FRESH AlR DUCT IN NOSE CONE. REPAlR NOTED ON LEFT ELEVATOR 1RAILING EDGE. LEFT ELEVATOR BALANCED IN ACCORDANCE WITH BEECHCRAFTIRA YTHEON SHOP MANUAL USING THE COUNTER-BALANCE METHOD: LEFT 12. l IN-LB TAIL HEAVY, RIGHT: 5.3 IN-LB TAIL HEAVY. MANUAL LIMITS: LESS THAN 12.4 IN-LB TAIL HEAVY). AL THOUGH BEECH TECHNICAL SUPPORT AND SHOP MANUAL DO NOT RECOMMEND SURF ACE PATCHES, THEY WOULD ACCEPT THE REPAlR SINCE THE ELEVATOR BALANCED. NOTE: WEIGHT ADDED TO ACHIEVE BALANCE.

AIRWORTHINESS DIRECTIVE COMPLIANCE:

VERIFIED COMPLIANCE WITH: AD 71-24-IORl CON1ROL WHEEL INTEGRITY - KIT# 58-524038-6603 INSTALLED IN 1985 TO COMPLY WITH AD; AD 72-01-02 OIL DRAIN TUBE INSPECTION - PCW; AD 72-11-02 FUEL SELECTOR ---------------------------------------------CONTINUED ON NEXT PAGE------------------------------------------------


DATi::




Lantana, FL 33462 561-966-8668

N63.JL SIN: TE-839 1971 BEECH E55 BARON HOBBS: 48.9 HOURS ACTT: 5839.5 HOURS 7 FEBRUARY 2005 NOTE: HOBBS METER CIRCUITRY CHANGED TO RECORD FLIGHT TIME INSTEAD OF ENGINE OPERATION TIME. ----------------------------------CONTINUED FROM PREVIOUS PAGE--------------------------------------------INSPECTION - PCW; AD 73-21-02 FUEL/OlL HOSE INSPECTION- PCW; AD 74-24-03 STROBE LIGHT SYSTEM INSPECTION - PCW; AD 84-09-01 EMERGENCY EGRESS WINDOW LATCH INSPECTION AND SAFETY WIRE - PCW; AD 90-08-14 WING SPAR DYE PENTRANT INSPECTION - NOT DUE AT THIS TIME, DUE AT ACTT: 6097.9; AD 91-17-01 ELEVATOR TRIM TAB ACTUATOR INSPECTION AND REIDENTIFICATION - PCW; AD 97-14-15 CABIN DOOR HANDLE OPERATIONS CHECK-PCW; AD 2000-18-02 ELEVATOR SKIN RECALL - NIA; AD 96-20-071AD 2001-08-01//AD 2001-17-131AD 2004-21-05 JANITROL HEATER INSPECTION - NIA BY PIN; AD 2002-11-07 ELECTROLUMINESCENT PANEL SCREW INSPECTION - CORRECT LENGTH INSTALLED ..

COMPLIED WITH :AD 76-07-12Rl BENDIX IGNITION SWITCH OPERATIONS CHECK; AD 72-22-01 UPLOCK ROLLER LUBRICATION AND INSPECTION; AD 91-15-20 ENGINE MOUNT DYE PENTRANT INSPECTION - NO CRACKS FOUND; AD 98-04-24 SEVERE ICING CONDITIONS SUPPLEMENT IN POH - INSERTED SUPPLEMENT IN POH.

ALL AD'S COMPLIED WITH, SEE AD LOGBOOK. GROUND RUN GOOD. THIS AIRCRAFT WAS INSPECTED TN ACCORDANCE WITH A BEECHCRAFT/RA YTHEON 100 HOUR/ANNUAL INSPECTION MANUAL AND DETERMINED TO

BE IN AIRWORTHY CONDillON AS OF THIS~DATE.

0~~ ___________ DONAL J NULIS AP 123300572 IA ___________ _

YEAR:

\

ID

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RECORDING TACH TIME

' ( I

TODAYS FLIGHT


1.Approvlng National Aviation Authority/Country:


WO:J"SJ.J-O:JdE!.J"MMM

99 ~ L-L9£ (<me:) :xe:J • Z6ZZ-L9£ (zgz) :4d

3. Form Tracking Nurii6ir.

AUTHORIZED RELEASE CERTIFICATE FAA/UNITED STATES FM FORM 8130-3, AIRWORTHINESS APPROVAL TAG I j

4. OrganlzatlonNameandAddress. 5. Work Order, Contract, or Invoice Number:

RAPCO, Inc. 445 Cardinal Lane, Hartland, WI 53029

6. Item:

7 .Description: 8.

Vacuum Pump

Part Number:

._ ( t

9. Ellgibility:•

TBVBY INSTALLER

11. Serial/Batch Number: 12. Status/We>Oc:

Overhauled

Overhauled In accordance with Process Specification# 203-6~1009

14. Certifies the items identified above were manufactured In conformity to: 19. 0 14 CFR 43.9 Return to Service 0 Other regulation specified In Block 13

D Approved design data and are In a condition for safe operation.

0 Non-approved design data specified in Block 13 ·" ~ ~=~~~~:i~t ~~~:s1 ~t':ar:::m~l:f;!~ni~l~o~~::'c~ ~~ ~C::;t~:d~~~~fk F~=~~ ~:re:~1ons, part 43 and in respect to that work, the items are approved for return to

15. Authorized Signature: 16. Approval Authorization No; 20. Authorized Signature: 21. Approval/Certificate No:

NE5R064N 17 Name (Typed or Printed): 18. Date (mldly): 22. Name (Typed or Printed): 23. Date (m/dly):

~I .. ' FAA Form 8130-3 (06-01) NSN:0052-0<H>12-9005 --· ·~-,_,. __ . .._... -- ........ --

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November 22, 2005 N63JL

The A TC transponder was tested and inspected as required by FAR 91.413 and found to meet the performance specification of FAR 43, Appendix F.

Transponder: King KT-76A sin 92091

The aircraft and/or component identified above was inspected in accordance with current FAA Regulations and was found airworthy and approved for the return to service.

P•lm B~ch A,;onk<, Inc. FAA CRS Ml4RJ63M k Work Order: 2467 1 --------


DATE ---

--

SUPPLEMENTAL LOG BOOK ENTRY --

-'°'eg: N63JL Model: E55 S/N: TE-839 --

Date: 12-20-2005 Hobbs: 108.2 - --

--Removed and replaced Nose gear trunnion brace with new P/N 96-820029-5. Replaced all bushings on nose gear trunnion brace --

with new P/N 08DU10, 105740X-YD500, 60-820039, 105740X -YN400, performed gear retraction and extension test and -' -

emergency retarction/extension test. Removed and replaced --nose main landing gear tire with new Goodyear Flight Custom Ill _'i .50X5 6 ply, Removed and replaced nose landing gear beraing --cone with new P/N 08125, removed and replaced nose landing r-gear bearing cup with new P/N 08231 . This maintenance was performed in accordance with the manufacturer's instructi_ons ~nd procedures, and the aircraft is approved for return to service with --

respect to the work performed. - END - --«~M- --

Robert A. Kindig 338~ A&P ,---_L

-- ~

YEAR: RECORDING TODAYS TOTAL Dt YACH FLIGHT TIMEIN En

, TIME SERVICE Te

DATE

-

-..


Reg: N63JL Model: E55 S/N: TE-839 Date: 08-09-2006 Hobbs : 150.3 ACTT: 5940.9

Performed Annual Inspection in accordance with FAR P Appendix D. Complied with all applicable AD's thru B/W

art 43, 2006-13. -rollers, AD 72-22-01, C/W by inspection of landing gear uplock

next due 6040.9. AD84-26-02, P/C/W by replacement o f2 new 2/01/03, del#

PIN AM101120FP paper induction air filters @ 5596.9 1 next due 6096.9 ACTI. AD-96-20-07 N/A by Heater Mo D83A28, SN#7700747. AD90-08-14, C/W by inspectio spar structure on 12/01/03@ 5596.9, next due 6096.9 A

n of wing en. battery due 07

Performed Annual ELT inspection IAW FAR 91 .207 (d), expiration Feb. 2007. Pitot/Static Transponder test next 106. Removed and replaced left main landing gear brak es with (4) new P/N RA66-22. Removed and replaced right win g auxiliary tank with new P/N 2F1-6-31627-18, S/N 05-051 87.

auled P on

Removed and replaced right fuel boost pump with overh IN 4150-00-1 , S/N 3880. Performed landing gear retracti /extension and emergency extension test. Landing gear operated normally at this time.I certify that this Aircraft h as been

tion and that

inspected/repaired in accordance with an Annual lnspec has been determined to be in an airworthy condition and work described above was accomplished and inspected in accordance with current FAA regulations and is approve d for return to service. - END -

lli.v10 A - h'-A '.X'lf'l ,3Lii.f)?;lfl;if=\

----- - - ~---=-=-------

YEAR: RECORDING TODAYS TOTAL TACH FLIGHT TIME IN

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of

- LOGBOOK ENTRY: .fx,vf'IOIJ N &--3f L t/O!l;(jS / (p 3~ Cf ~pecific entries.) - THE STA TIC PRESSURE SYSTEM, TRANSPONDER WITH ALTITUDE REPORTING WAS IDENTIFIED

TESTED AND INSPECTED I/A/W FAR43 APPENDIX E, PAR A&C, APPENDIX F (FAR914l3) - AND rs APPROVED FOR RETURN TO SERVICE. PERTINENT DE~THTS TEST IS ON FILE

ATTHISREPAIRSTATIONUNDER WO. 7370 DATE ~ 1000

= SIGNATURE df!1t}llk "3 · ~Lo-' INSP. l!Yii> TROPIC D 1'i 69~ S GER 53 D

- FT.LAUDERDALE FL. 33309 FAA APPRO D REPAIRS FT.LALDERD LE XECUTIVE AIRPO * CHER RA

(

- f-l.t 1~ A .S1/N ,!J.f}/</7 /{£ 950 .5/N ~t B:J.3

CERTIFICATION EXPIRES ON ~ .301 :J__{)O 8

N # RZ4RSJOM

-I ~

TROPIC RADIO INC. lft'5 N. W. 5'TI:I ST. BANG.ER SJ.-D

FT.LAUDERDALE, FL33389 FAA APPROVED REPAIR STATION #RZ4RSIOM

FT.LAUDERDALE EXEaTl"IVE AIRPORT *AR.CHER. RAMP*

PHONE: 954-776-4030

MakeandM<>Qd,........,..~U_/U,..,._/~te;..{).--~~~~-=--:-:~~-=-:--:-;~~=--~ Part No: - -=d=.-. (~_,_.. _ _._-.,..--___,r---~ Customer:_---'~~~~~4""~~-.L...L..!...:_~~:::...L--==--.,..--=--,,-Inspected By:

~~~~~~~

ALTIMETER SCALE ERROR DAT TESTED AT TROPIC RADIO INC.

~ f.c> I 200(:;, FM APPROVED REPAIR STA.·•RZ•Rl10M

PART ~'l_3 lff' - / 'SERIAL NO. I '-I 7 I 5 Teat , ERROR Teat ERROR Teat ERROR etlttl PT..illl. .fI.1lli_

-1000 .:t::_IO 10000 .-l -b .. 0000 :s: L 00 0 12000 -~o .. 5000 :s: L

500 +--;:s 14000 -~ 50000 ~ L 1000 +10 16000 - 't..S 51000 ~ z 1500 +-5 18000 - 'ft) 52000 :;z_ 2000 + !:$_ 20000 - 50 53000 D 3000 -l-1$ 22000 :::s: L 54000 z ~ .. ooo +-5 25000 "7 55000 z ~ 6000 5 30000 /~ 60000 L ::sJ 8000 ·-10 35000 L ~ 70000 _L ~ ...

Reg: N63JL Date: 8/22/2006

Supplemental Log Book Entry Airframe

Model: ESS Hobbs: 169.7

SIN: TE-839 -' -

- -~-- - - -. - ------ ···~


- Reg: 63JL Model: E-55 SIN: TE-839 Date: 09-06-2006 Hobbs: 169.7

- Removed and replaced right auxiliary fuel sender with overhauled auxiliary fuel sender P/N#7740-11, S/N#062790.

- installed with new fuel sender gasket P/N#755-049. Performed R _ /H fuel quanity calibration and R/H fuel transmitter operated

normally. This maintenance was performed in accordance with - the manufacturer's instructions and procedures, and the aircraft

is approved for return to service with respect to the work - performed. - END -

~£~\ -KristoperStadler 594502494 A&P

~ctions, Tests, Repairs and Alterations d with Name, Rating and Certificate Number of . :ility. (See back pages for other specific entries.)


Reg: N63JL Model: E55 S/N: TE-839 Date: 08-09-2006 Hobbs : 150.3 ACTT: 5940.9

Performed Annual Inspection in accordance with FAR Part 43, Appendix D. Complied with all applicable AD's thru B/W 2006-1~ . AD 72-22-01 , C/W by inspection "of landing gear uplock rollers, next due 6040.9. AD84-26-02, P/C/W by replacement of 2 new P/N AM101120FP paper induction air filters@ 5596.9 12/01/03, next due 6096.9 ACTT. AD-96-20-07 N/A by Heater Model# D83A28, SN#7700747. AD90-08-14, C/W by inspection of wing spar structure on 12/01/03@ 5596.9, next due 6096.9 ACTT. Performed Annual EL T inspection IAW FAR 91 .207 (d), battery expiration Feb. 2007. Pitot/Static Transponder test next due 07 106. Removed and replaced left main landing gear brakes with (4) new P/N RA66-22. Removed and replaced right wing auxiliary tank with new P/N 2F1-6-31627-18, S/N 05-05187.

Removed and replaced right fuel boost pump with overhauled P /N 4150-00-1 , SIN 3880. Performed landing gear retraction /extension and emergency extension test. Landing gear operated normally at this time.I certify that this Aircraft has been inspected/repaired in accordance with an Annual Inspection and , has been determined to be in an aiMiorthy condition and that work described above was accomplished and inspected in accordance with current FAA regulations and is approved for return to service. - END -

David A. Johnson 34480929 IA

1 . Approving National

Avi a t i o n Autho~i t y/Country :

2. 3 . Form Tracki ng Numbe r

AUTHORIZED RELEASE CERTIFICATE R57 4 25

4 . Organization Name a nd Addres s : 5 . Work Order/Contract / I nvoice Number •

DUKES INC . 9060 WINNETKA AVENUE NORTHRIDGE, CA 91324 Phone : 47717

8 . 9 . 1 0 . 11 . 12.

1 FUEL BOOST PUMP 415 0 - 00-1 N/A 1 3880 OVERHAULED

13. REMARKS : UNIT FUNCT I ONS PER ATP 4140-04 REV . "C " THE TEARDOWN REPORT # R57425 DESCRIBING THE ACTUAL WORK PERFORMED IS ATTACHED . THE PRESCRIBED WORK WAS PERFORMED IN ACCORDANCE WITH FAA APPROVED DATA . DUKES INC . CERTIFIES THAT THE WORK SPECIFI ED IN BLOCK 12 & 1 3 WAS PERFORMED IN ACCORDANCE WI TH EASA IMPLEMENATION RULE PART 14 5 APPROVAL ,AND WITH RESPECT TO THAT WORK, THE AI RCRAFT COMPONENT IS CONSI DERED READY FOR RELEASE TO SERVI CE UNDER EASA APPROVAL l'fi.JMBER EASA . 14 5 . 4 3 91

14. Certi fies the i tems i dent ified 43 . 9 Return to service . [~er regu l at ion s pecified i n Block 1 3 .

Approved d esign d ata and

Non -approved d e s i gn data speci fied

15. 16 . Appr oval/ Authorization No .

17. 18 . Date : (m/d/y )

tha t unless otherwise spec i f i ed in Block 1 3 , t he work identif i e d in Block 12

and described in Block 13 was accomp l i shed in accordance with Title 1 4 , Code o f

Federal{1Regulations , part 43 and in r e spect to t hat work, the items are approved for

return to service

20 . Authori zed Si~: ' 21 . Approva l I

Certificate No .·

\1--J~ WU2R279L

22 . or Prin ted ) : 23 . Date : (m/ d / y l

PRODUCT SUPPORT 03/1 5 /0 5

It is importa n t t o understand that the existence Jf this documen t does not automat icall y const itu v clU Lhori t y to install the part / component / assemb l y .

Where the user/installer pe rforms wo rk in acco 1~dance with the national 1c gulations of an airworth iness au4!101it y di. t fe ren t than the a irworthiness autho rity of the cou nt r y specified in

Block 1, it i s essen tial that the user/installer ensures that llis/her airworthiness accepts parts / compone;?ts / a sf;cutb l les f r om the airworthiness a uthority of t h e country specified in Block 1 .

Statements in Bl ock 1 4 and 19 do not constitute installat ion certifica tion . In all cases, aircraft mainteqance 1. eco i.d s mu s t contain an insta l l a tion certif i cat i on i ssue d in accordance wi th t he

na tional regula t ions by t he user/ins ta l l er before the a ircraft may be flown.

FAA Form 8130-3 ( 6 - 01) * Installer must cross - c heck eligibility with applicable t echn ical data . NSN • 0 0 52 -00 -0 12 -9005

~;;(/C/7 Sr:RVICE BULLETINS

AD's ____ _ O/H MANUAL#

OF OKLAHOMA, INC. FAA APPROVED REPAIR STATION

CRS # RV3R829L 2740 N. SHERIDAN - TULSA, OK 74115

800-255-9924 -. fH.918-835-9924- FAX 918-835-3681

MAINTENANCE TRAVELER

P.0.11 &,3J,!_ SHIP VIA_L/~.£:4'.'EO_:_~=

.£,.. U:::-,.--'

~ REPAIR SALE

CUSTOMER '4 h ~~£ dL~'-'h"-"')=cJ=...-____.°ZLC"""'""',_,,·o....:.· _WORK ORDER #

TACH GENERATOR

P/N, ___________________ MFG. _______________ S/N ________ _

Bearing.· ____ Gasket ___ Rotor ___ .Shaft. ___ ,Pin, ___ Coil ___ .Seal. ___ Plug ____ .Assemble ___ Test_ ___ _

" FUEL BOOST PUMP

P/N -)I/So -oo ·_ / MFG. An!::£~ uc. S/N 3?Jb Armature Valve Assy . Fuel Seal Impeller Coupling Harness Housing

Bearing Spring Field Brush O'Ring Rotor Blade Volts

Amps PPH@ PSI PSI 0 Flow With/Without Fittings Assemble Test

PART# & NAME P.O.# QUANTITY COST

LABOR'-----'---------

PARTS. _________ _

SUBTOTAL. _______ _

TAX _______________ _

FREIGHT~------------

TOTAL. ____________ _

INSPECTOR

\ _& \ MECHANIC

Aircraft Beech E-55 S/N TE-839

N-number 63JL Date 03/ 15/07

Tach: N/A Hobbs: 199.5

A/C Total T ime 5990.1

rations ber of

entries.)

COMPLETED THE FOLLOWING MAINTENANCE: I. Performed l 00 Hour Airframe Inspection II AIW Beech Service Manual 2. Complied With 100 Hour Lubrication Requ irement 3. Complied With EL T lnsp. 91.207 Battery Exp.03/09 4. C/W AD's ,72-11-02 Uplock roller lubrication, 76-07-12 bendix ign ition switch check, 84-26-02 paper air filter inspection, replacement due 6096.9 ACTT. Repaired magneto leads and grounds. Adjusted inner gear doors. Replaced EL T battery P/N BP I 0 I 0

I certify that this airframe was inspected in accordance with Beechcraft service manual found to be in an airworthy condition and is approved for return to service

A/P# 3 150777 /) d__· v~., /117t~

Date 3/15/07 Don Manzella

Hobbs indicates 199 .5 Hours. Date03/15/07 Aircraft S/NTE-839 Total airframe time5990. l I certify that this Airframe has been inspected In accordance with a Annual inspection and was determined to be in an airworthy condition

~~~ 2vi3}Cf)G l .[A

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YEAR:

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RECORDING TODAYS YACH FLIGHT TIME


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RECORDING TODAYS TACH FLIGHT TIME



't)

YEAR:

DATE

RECORDING TODAYS JACH FLIGHT TIME

TOTAL TIME IN SERVICE


11/25/08 N63JL Beech E-55 SIN TE-839 Hobbs 284.4 "AIRCRAFT LOG ENTRY''

Removal and replacement of pilot PTT switch. Ops check goo nd.

3 l l 7379IA

e

cc

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I

YEAR:

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YEAR: RECORDING TODAYS YACH FLIGHT TIME



1.

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in I

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations YACH FLIGHT TIMEIN

')..(X;'' TIME SERVICE

Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

/) DATE

1AYn- 2-7fJ 1~?.f;

FRONT EN it' Y DOOM SEAL '

MatD-7, ADS 1200-11, ADltD-15 I

~ I

F AA-PMA PQ1008SW '

Replacement Seal for Beechcraft I f

For Models 19A, B 19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R, 3S-33, 3SA33, 3S-B33, 3S-C33, 3S-C33A, E33, E33A, E33C, F33 , F33A, F33C, G33, H3S, G36, BS, K3S, M3S, N3S, P3S, S3S, V3S , V3SA, V3SB, 36, I A36, A36TC, B36TC, 3S, A3S, B35, C3S, D3S, E3S, F3S, G3S, 3SR, SO (L23A), I BSO (L23B), CSO, DSO (L-23E), DSOA, DSOB, DSOC, DSOE, DSOE-S990, ESQ (L23D, RL23D), FSO, GSO, HSO, JSO, B9SA, D9SA, E9S, 9S-SS, 9S-ASS, 9S-BSS, I 9S-BSSA, 9S-BSSB (T-42A), 9S-CSS, 95-CSSA, GS8, DSS, DSSA, ESS, ESSA, S6TC,

AS6TC, 58, SSA, 95, 895, S8TC, S8TCA, 76, 77 I

~ l

Aircraft Door Seals LLC. . I

MAR o & 2009 7100 N.W., 63'• Street, Hangar 1002

111 l

Bethany, Oklahoma 73008 405-470-3636, Fax 405-470-3637

I

-4 MECHANIC

"

YEAR:

DATE




02102109 N63JL Beech E-55 SIN TE-839 Hobbs 284.4 "AIRCRAFT LOG ENTRY'

Replacement ofloose rivets on both engine nacelles. Removal and replacement of right wing aux fuel tank. Fuel tank was filled with no leaks observed. Removal and replacement of tail cone top plate. Removal and replacement of pilot window including inner and outer frames. Replacement of O~ T Probe. Removal and installation of aircraft battery to service and charge. Installation of several mspect1on panels after owner

had pa;nted. Replacement ofm;";ng h"dwarn and cam-loo on a;cframe-~------

~I 173791A

WINDWARD A VIA TI ON 2615 Lantana Road, Ste K/Hangar 805

Lantana, FL 33462 561-966-8668

N63JL SIN: TE-839 BEECH 58 BARON 5 AUGUST 2009

COMPLIED WITH AD 2008-13-17 TOGGLE SWITCH CIRCUIT BREAKER REPLACEMENT IN ACCORDANCE WITH ALTERNATIVE METHOD OF COMPUANCE(AMOC) FOR AIRWORTHINESS DIRECTIVE AD 2008-13-17 PARAGRAPH 3.B. CIRCUIT BREAKERS FOR THIS AIRCRAFT HA VE BEEN PLACED ON ORDER AND A LETTER TO THAT EFFECT HAS BEEN SENT TO THE FORT LAUDERDALE FLIGHT STANDARDS DISTRICT OFFICE. THE INVOICE FOR THE CIRCUIT BREAKERbN FILE AT1W~ AVIATION.

··-----------------------------MARISA SMITH LEACH AP 308217~&-~-----------------------

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DATE

FLIGHT LINE AVIONICS, INC. SUPPLEMENTAL LOG BOOK ENTRY

Aircraft Registration: N63JL SIN: TE839 Model: E55 Performed altimeter static system test and automatic pressure altitude reporting system and the following listed are found to comply with the requirements of FAR 91.411 IAW Appendix E of Part 43. Tested to 20 thousand feet.

Altimeter PIN: 5934 SIN: 84715 Cal. Date: 6/19/2009 ...........................................................................................................................

Performed transponder test and the following listed are found to comply with requirements of FAR 91.413 !AW Appendix F of Part 43.

Transponder Model: KT76A SIN: 92091 Cal. Date: 6/19/2009 Details on file at this Repa tation under Work Order: # 1!005

.-. s ::'.:)_ -=\ Signed: DUE NEXT: 6/2011

North County Airport 11550 Aviation Blvd. Suite 3 West Palm Beach, FL 33412

(772) 528-4881 I-

CRS Fl8R921V

\ p ~ \ M H/\NIG

I.

MECHANIC

Piiot

ALTITUDE

-1,000 (20') 0 (+/-20') 500 (20') 1,000 (20') 1,500 (25') 2,000 (30') 3,000 (30') 4,000 (35') 5,000 6,000 (40') 8,000 (60') 10,000 (80') 12,000 (90') 14,000 (100') 15,000 16,000 (110') 18,000 (120') 20,000 ( 130') 22,000 (140') 25,000 (155') 30,000 (180') 35,000 (205') 40,000 (230') 45,000 (255') 50,000 280' 53,000 55,000

ription of Inspections, Tests, Repairs and All must be endorsed with Name, Rating and Certiflco l< N

ician or Repair Facility. (See back pages for other p< <.111

S INC. KENTRY

Model: E55 c pressure altitude reporting y with the requirements

to 20 thousand feet.

Cal. Date: 6/19/2009

are found to comply of Part 43.

Cal. Date: 6/19/2009 der: # 11005

UE NEXT: 6/2011 ort

Suite 3 33412

DATE I

08/20/09 N63JL Beech E-55 S/N Tl ·:-xv> "AIRCRAFT LOG ENTRY"

ZZ6l£ :JaqwnN

3:>!0AUJ/PllJlUO:J/J3pJQ >tJOM "S

77P.. LC'

I lohhs .. 5 ..

Removal and installation of left boost pump P/N 4150-00-1 NV S/N 082708 for ov ·rhnul. S ' · W\11'" \lrd ·r 19622 dated 08/10/09 from Aviation Group, Inc. Remove both fue l screens for i11sp ·c1io11 . R ·p l;i · ·111 ·111 of' a ll gaskets for fuel bowls. Removal of Thrust Detector System previously installed and Iii ' ]7. Replocem'"t of in,trnmeot nu1' "' coquiced. Rcpoic bmken wice oo com~

~3 11 73791A

10/12/09 N63JL E55 SIN TE839 Hobbs 341 .1 "AIRCRAFT LOG ENTRY"

Replaced left outboard flap track. Replaced lower rudder attach bracket and bearing.Replaced left main gear door. Jacked aircraft and cycled gear to check gear door. Cycled gear three times and no faults noted. Removed control yoke for painting. Installed control yoke as per maintenance

manual ~~ A&P595248401A

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YEAR: RECDRDINI TACH TIME

DATE

LOOMIS ~tcUTlVb JET REFINISHING LOG BOOK SUPPLEMENT

Make: Beechcraft Model: Baron E55 SIN: TE839 Registration No.N63JL Hobbs Time: 341.1 Strip and paint with the following Colors: Overall A WLGRIP G8003 Matterhorn White, Stripe Colors: DuPont MS600 N0328 DK. Concord Met., G8070 Gold Met.,N4397 Red Met.

Flight controls removed prior to paint, balance checked, And reinstalled after painting was completed per manufacture's Maintenance manual. 1. L/H Nav light cover replaced.

A&P: 595248430 Date: 7 /18/2008

Signature:~~

'

terations umber of c entries.)

l I

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y 11/20/09 N63JL Beech E-55 SIN TE-839 Hobbs 349.7

"AIRCRAFT LOG ENTRY'' Replacement ofright main tire with Good Year Flight Custom Ill. Repl aced 0-:_1'5S on right main and left aux fuel caps. ~ ~

3260835A&P

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HE FEDE

.'ITH RE~

1 block I J , 1ed in 111·1·0

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YEAR:

DATE

~t1>~S :SS~ 6 Serial# Tachometer

"SUPPLEMENTAL LOG ENTRY"

(7.;;;f> LA-<::.c,,-f:> t.c.-P-r 1.--z...o-cri IL,c,. ·~Jr

;e1,,;n-1 .1.-'.;....,,..v -~,~ fu .y{' ' ocn. ,.J'-- ft

11/04/10 N63JL Beech E-55 SIN TE-839 "AIRCRAFT LOG ENTRY'

S.·'1.v·4'-'..t/ C'A'.J'X{J"'

(.i..<.>.u J . r (l CJ ,,,_J)

Hobbs 385.2

Replacement of voltage regulator selector switch. Replacement of right engine # probe. Service aircraft batteries. Ops check good.

robe and #6 cht

I_ I I_

YEAR:

-DATE

RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations YACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

.'5/N IE- 8 ~ 9 -r~ 373.

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{!J.e-H!Ve/J off" eo 12-~s/ol{) ; I./ .Lr. aJ/JeeL wa-/ /1

--rizc;-11-TliiJ ?i/16 eJfRom19 7£)) i- -lo1.1 '--'~ed u/ wh; k -Ptt-!NI. '9~/;,rr ,I/ t/' ;Jot,/Ul- -

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Descrip.1ion of Inspections, Tests, Repai,rs.aw..1-Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

Date 1pe // -. 02.d I~ Date ./be I/ . & /Ol..-. J certify that th altimeter, altitude reporting and 1 certiffthe below transponders(s) have been

static system test and inspection required by FAR inspected and found to comply with the re-91.411 has been performeq. The LH __L RH__ quirements ofF AR Part 91 413 on Work Order altimeter, Model/PN tA.1K.::J 51' ](/f)-3 No / Ol/t/5 date<l/9P,e // .. ~/~

-· SIN l!)> l/3 q CL certified to FAk Part 43, #1 Transponder: Make ~<J;~hC/v6 _ Appx. E. by~~RECMY?e(CRS# >< 5(?126fi'K Model Kr?~& SIN '9« otJI

on W.O.#/~JL!L5was tested to Olo, ooe> ft. #2 Transponder: Make -C!!1- Th I· d rt. J Model ~~AIN_-__ _ - on date A:>e // . C7CJ/0- . e at. ttu e repo mg. . . . _ _

.er ft D ·1 Signed~ for _ system was tested to / ~"oo<:J . . . eta1 s . ... . . . In · parkchasers Aircraft Services, c. On file un<le~ ~0.# /01 19:5 date~ic·Obl. r FAA Repair Station No. XSPR699K

- Signedd~ for ~----------~ - " Sparkchasers Aircraft Services, Inc.

_ Repair Station No. XSPR699K

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.l.1111

"''' 11.

YEAR: Spa1Xcha$8ra A!rCl'Bft Service8, Inc.

FM CRS# XSPR699K . Al.T)~~TlON RfCORO

DATE J: ALTITUDE

3000 4000

. 5000

6000 8000

0 10000 12000

I cc stat 91. al ti snAp on on sys On

w 1---140--00--~'""""'-

In · 15000 16000

s. 18000 I g .. ._.,.:::::; 1---200-00-.i-_.;a-

22000 25000 30000 35000 40000 45000 50000

Iterations umber of

fie entries.)

for s, Inc. 699K


- -DATE

N63JL Hobbs 431.7 AIRCRAFT MAINT. LOG ENTRY

Replaced defective internally lighted Pilot's altimeter United Instruments 5934P sn 84715 with new exchange United Instruments 5924P-3 sn 494392 and FAA/PMA Nulight ring. Adjusted Narco AR500 altitude Encoder. Tested static system/ altitude reporting system. Tested new altimeter IAW FAR 43 appx E. Tested KY 76A sn 92091 transponder IAW FAR 43 appx F. Details on file wo# 101195. CRS XSPR699K Sparkchasers Aircraft Services.

Signed i<./A>.d Date4£ //·~/;}_, ~ FMCRSXSPR699K L_

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YEAR: RECORDING TACH TIME

TODAYS FLIGHT



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Description of Inspections, Tests, Repairs and terations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)



Description of Inspections, Tests, Repairs and Altera ons Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

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YEAR:

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P~t 5/05/2014 N63JL Beechcraft E-55 Serial# TE-839 Hobbs 585.0 6375.3 TIAF Annual Inspection Installed new ELT battery (expires 3/2016). This ELT has been tested and inspected in accordance with FAR 91.207 par d and found to comply at this time. Installed new tires and tubes on main wheels. Installed new nose gear tire. Cleaned and packed wheel bearings. Removed paint from right elevator. Primed with epoxy primer and painted to match airframe. Installed new seals in brake calipers, installed new brake pads, and bled brake system. Installed new 5NBC713YJ uplock bearings, 1309098176 uplock bearing bolts, 35-815115 uplock springs, 100942C0020-31 Tension springs, 134553-4M rod ends, 35-815056-4 Rod ends, 35-815124 bushings, and NAS4645-33 bolts in main landing gear system. Greased system and ran normal and emergency. Installed new taxi light bulb. Serviced propeller accumulators with nitrogen. Lubed all hinges, pulleys and rod ends. Removed Continental I0-520-CB7B serial# 2~8591-R from left hand position. Installed Continental I0-520-C7B serial# 810876-R with McCauley 2AF34C55-NO serial ti 753993 in left hand position. Removed Continental I0-520-CB7B serial # 288424-R from right hand position. Installed Continental 10-520-C serial# 126383-8-C with Mccaul y

2AF34C55-NO serial # 720938 in right hand position. (Cont)

11! -

-

' -;

YEAR:

- -DATE



Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating arm Ctmificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

~.A. Complied with AD 76-07-12 Rl Bendix magneto switches by operational test. No defects

noted. Due in 100 hours. Complied with AD 90-08-14 To prevent cracks in the wing forward spar carry-through web structure by inspection. One stop drilled crack has not

progressed. Due in 200 hours. Complied with AD 2007-08-08 To decrease the possibility

of gear-up landings caused by seizure of the uplock rollers by installing and greasing new

rollers. Due in 100 hours. AD 2013-16-01 To require an inspection of the elevator

balance weights does not apply due to weights not changed during time period. Tested -combustion heater burner can for leaks with no defects noted. Removed original

rotating beacon and installed Whelen 01-0790088-14 LED beacon assembly. I certify

that this airframe has been inspected in accordance with an Annual inspection and found to be airworthy at this time.

Richard C. Pahnke "' )j\ '.ti453613 {~~cifJ~

I I I I

F I

YEAI

TIME SERVICE

p ct on , T t , Repairs and Alterations - ·····-- ···--· __ - ·· • . a <J with N 1rn • Rating nd Certificate Number of 1 chnlcian or Rep Ir acilily. (See back pages for other specific entries.)

DATE

Reg#: N63JL Model: Beech E-55 Serial#: TE-839 Work Order#: 80448

f .AIR <JRE INC Aviation Services

I certify the ATC Transponder System Test and Inspections required by FAR 91.413 were performed this date and found to comply with FAR 43, Appendix F. #I Make Bendix King Model KT76A SIN 92091 #2 Make NIA Model NIA SIN NIA Details of this inspection are on file at this repair station under WO# B 0448 .

Operational checks normal. See work order for detail.

For: Air Care, Inc. FAA Repair Station

ACOR030C

Hobbs: 593 Ta ch: Total Time: Date: 5/22/2014

I certify that the Altimeter, each automatic pressure altitude reporting system and static system has been inspected and tested as required by FAR 9 l.41 l. The Altimeter has been tested to 20 000 feet. Encoding Altimeter tested to 20 000 feet. ADC SIN NI A . Details are on file under WO# B 0448

i_I _

L

f~

YIAR: RECORDING TODAYS YACH FLIGHT TIME

TOTAL TIME IN SERVICE


llAfE::__J-___ +----1-----1------------------------

9/05/2015 N63JL Beechcraft E-55 Serial# TE-839 Hobbs 638.0 6448.3 TTAF Annual Inspection Installed new ELT battery. (expires 8/2017). This ELT has been tested and inspected in accordance with FAR 91.207 par d and found to comply at this time. Cleaned and packed wheel bearings. Lubed all hinges, pulleys, and rod ends. Complied with AD 76-07-12 Rl Bendix magneto switches by operational test. No defects noted. Due in 100 hours. Complied with AD 2007-08-08 To decrease the possibility of a Gear-up landing by greasing landing gear uplock rollers and running landing gear normal and emergency. No defects noted. Due in 100 hours. Installed new Cl 121 com antenna on rear upper fuselage. Repaired fresh air vent in rear dorsal fin. AD 90-08-14 To prevent cracks in the wing spar carry-through structure is due at 6575.3 TIAF. Installed new D9-14-5 instrument filters .Installed new G25 batteries. I certify that this airframe has been inspected in accordance with an Annual inspection and found to be airworthy at this time.

Richard C. Pahnke IA 3453613

I I

~=1.L .,Y~3JL /3Q"<J Date NII M;1kL'

.. 'UJ'l'l HMF 1' ll LUG F l'l<l "

fa/, 7 ' I ~ 1\).1111 l l\tc't

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- - " 1. Approving National Aviation 2. 3. Form Tracking Number:

Authqrity/Country:

AUTHORIZED RELEASE CERTIFIC~\TE ~NITED STATES 31922 FAAFonn 8130-3, AIRWORTIIINESSAPPROV AL TAG 1

4. Organization Name and Address:

\

5. Work Order/Contract/Invoice

THE AVIATION GROUP, INC. 211 PROSPECT PARK, PEACHTREE CITY, GA 30269 Number: 31922

6. Item: . 7. Description: 8 . Part Number: 9. El!g_ibility: * 10. Quanti!r: 11. S~rial/Batch Number: 12. Status/Work:

1 PUMP 4150-00-1 NV VARIOUS 1 082708 I OVERHAULED

13. Remarks: THE ABOVE APPLIANCE WAS OVERHAULED AND, INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMNISTRATION AND IS APPROVED FOR RETURN TO SERVICE. Manual: 4140 Revision#:S Revision Date:G/2005 Full details held on W.O. 31922 .) Comments:

' CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 12/13 WAS CARRIED OUT IN ACCORDANCE WITH EASA PART 145, AND WITH RESPECT TO THAT WORK, THE COMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE UNDER EASA APPROVAL NUMBER: EASA.145. 4208. (*INSTALLER MUST CROSS CHECK ELIGIBILITY WITH APPLICABLE TECHNICAL DATA.)

LIFE LIMIT PARTS MUST BE ACCOMPANIED BY MAINTENANCE HJ STORY INCLUDING TOTAL TIME/TOTAL CYCLES

14. Certifies the items identified above were manufactured in conformity to: 19. IZJ 14 CFR 43.9 Return to Service IZJ Other regulation specified in Block 13

D Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in block 13, the work identified in Block 12

D Non-approved design data specified in Block 13. and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and in respe~t to that work, the items are approved for return to service.

15. Authorized Signature: 16. Approval/Authorization No.: 20. Authorized Signature: 21. Approval/Certificate No.:

;;.::? 12 . ./-..£,~~+ VGOR728L

17. Name (Typed or Printed): 18. Date (m/d/y): 22. Name (Typed or Printed): 23. Date (mmm/dd/yyyy):

Lawrence R. Hunt AUG/10/2009

User/Installer Res_E_onsibilities It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Blockl.

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

THE FAA form 8130-3 and JAA Form One are ~uivalent. Other countries such as Canada also have e_!tuivalent acce_l!.table documents. FAA Form 8130-3 (6-01) . *Installer must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005

~~AIR01RE INC. P.O. Bmr. 7668, Rocky Mount, NC 27804 Phone 252-977-1717

:ALTIMETER I REPORTING SYSTEM TEST lNFORMATION

Tested in compliance with Appendix E, Part 43, FAA Hegulations. Paragraph {A), (B), and {C) as Applicable.

7 i7irViJV Altitude Tested to Maximum of l.-U. Feet.

ALTITUDE SCALE SCALE FRICTHiJ,N FRICTION ENCOOING a!ROR ERROR TOLERENGE PULSE TCLERAHCE

·1000

0

500

1000

11'00

1300

1500 0 Tolerance 1800

2000 D 75 H. Oltf.

260(} <--.-/ 7511. Dill.

2700 . ._./

2800 Barometric Scale Tr.st 3000 'Baro. Altllude Altl!ude + 4000 Settln Scale Reads Difference Tolerance - ft.

5000 28.10 ,_rt c -1727 25 6000

6800 2a.so -(3tf-O -1340 25

8000 29.00 D ~ ·~ -860 25 --- .-. l'i ·(; I , ,

10000

12000 W.50 oo -392 25

14000

14801]

15000

29.92 -t ( () 0 25

30.50 ~;3o +531 25

16000 -· 30.90 + f Of) +1393 25 18000

20000 fO.Lir, 30.99 - - 76 ' +974 25

22000

25000

30000 Blind Encoder Mode 30800 ·I - - Date Tested 35000

40000 230 Altimeter Test Inspector

45000 255 ·----- Encoding TtJst Inspector

50000 . ...-.....__

280 -----· Work Order No .

J ENCODING ALTIMmR TEST POINTS BLIND ENCODER MUST BE TESTED AT ALL POINTS

1. Approving National Aviat ion Authority/Country

2. 3. Form Track ing Number.

63296

AUTHORIZED RELEASE CERTIFICATE FAA/UNITED STATES FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG

4. Organization Name and Address. Accessories, Inc

4123 MAY ST.

6. Item: 7. Description:

ACCUMULATOR

13. REMARKS

FAA# TM2R192L WICHITA, KS 67209 Ph: 316-946-0701, Fax: 316-946-5801

8. Part Number:

95-380026A (203-1 )

9. Eligibility: * 10. Quantity

NIA

5. Work Order, Contract or Invoice Number:

67924R

11. Serial/Batch Number: 12. Status/Work:

15315 Overhauled

his part was OVERHAULED. Work order, (ref. block 5) , prescribing actual work performed is on file . Prescribed work was performed in accordance with FAA approved data.

rescribed work was perfomed in accordance with 'fS38t::cZUJ4 R/!11· 8 C/-lc/-1'1?3 Certifies that the work pecified in block 12/13 was carried out in accordance with EASA part-145 and in respect to that work the component is considered ready for release to service nder EASA Part-145 Approval Number: EASA 145.5969

19. 00 14 CFR 43.9 Return to Service 00 Other regulation specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations , part 43 and in respect to that work , the items are approved for return to service .

20. Authorized Signature:

22 . Name (Typed or rinted):

Wayne Toman User/Installer Responsibilities

21 . Approval/Certifcate No:

TM2R192L 23. Date (m/d/y)

Jul21 , 2011

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly .

Where the user/installer work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statement in Blocks 14 and 19 do not constitute installation certification . In all cases aircraft maintenance records must contain an installation certificat ion issued in accordance with the national regulations by the user/installer before the aircraft may be flown .

FAA Form 8130-3 (6-01 ) • Installer must cross check eligibility with applicable technical data NSN 0052-00-012-90005

r

1. Approving National Aviation Authority/Country:

FAA/UNITED STATES

2 . 3 Form Tracking Number.

/f/03 J'l. ~296 ) AUTHORIZED RELEASE CERTIFICATE

FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG 4. Organization Name and Address. Accessories, Inc

4123 MAY ST. 5. Work Order, Contract or Invoice

Number:

6. Item: 7. Description:

2 ACCUMULATOR

13. REMARKS

FAA# TM2R192L WICHITA, KS 67209 Ph: 316-946-0701, Fax: 316-946-5801

8. Part Number:

95-380026A (203-1)

9. Eligibility: *

NIA

. r· 67925R

10. Quantity 11 . ~erial/Batch Number: 12. Status/Work:

15319 Overhauled

his part was OVERHAULED. Work order, (ref. block 5) , prescribing actual work performed is on file. Prescribed work was performed in accordance with FAA approved data.

rescribed work was perfomed in accordance with q53~,i1 Rell· '8 q-Jt./~/q73 Certifies that the work pecified in block 12/13 was carried out in accordance with EASA part-145 and in respect to that work the component is considered ready for release to service nder EASA Part-145 Approval Number: EASA.145.5969

19. 00 14 CFR 43.9 Return to Service 00 Other regulation specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations , part 43 and in respect to that work, the items are approved for return to service.

21. Approval/Certifcate No

TM2R192L Name (Typed o 23. Date (m/d/y):

Wayne Toman Jul21, 2011

User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute authority to install the part/component/assembly.

Where the user/installer work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statement in Blocks 14 and 19 do not constitute installation certification . In all cases aircraft maintenance records must contain an installation l::ertification issued in accordance with the national regulations by the user/installer before the aircraft may be flown.

FAA Form 8130-3 (6-01 ) * Installer must cross check eligibil ity with applicable technica l data NSN 0052-00-012-90005

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Documents

-~-AIRCRAFT · CNJ AD72-22-01 Landing Gear Uplock Rollers by inspection and lubrication. AD90-08-14 Wing Spar Structures due@ 1075.2. AD84-26-02 Paper Induction Air Filters next due@