ii log the standard - aest-sales.com · i&j via (ion inc. date 3-19-2002 bra total time...

P*7-1 The Standard

II 4_4-AIRCRAFT LOG

ASA-SA-2

0 G

set

Aircraft Record General Information

Manufacturer PI 14 , CF) Model P,A-J-S-c)(7.,,‹_1..,1)

Serial • Registration Humber r) ($0 (.3 p

.91 Date of Manufacture

Engine(s) currently installed:

Manufacturer 1-4.-4g)S Model TX0 - "S-41 0 IA Serial

Manufacturer Model Serial

Model F8 2/1C-Z, - R

Propeller(s) currently installed:

Manufacturer /9011±,b0

r- HUB Model

L Blade Model 14_ iS9 LI

R Blade Model

MINK H •;f• " I " -

Serial Serial

Serial H Serial#W J O Serial

Serial cg-/cA-s- Serial C-$-S**7 LS' Serial

id Alterations

TAM v illein 111111r / ate Number of

TIME I SERVICE Technician or Repair FaCinty. specific entries.)

DATE

Total Time Airframe 4.23148 :LH: _ Date 10-04-01 _ 14/Aviation inc.

2900 Dammeyer Road N600MP

_ ilemikon. Ohio 45015 Piper PA23-250 SN: 27-7554035

Replaced left engine exhaust tail pipe With serviceable PIN 32779-00 see attached work order and maintenance release for detail Torqued and —

saftyed all bolts and clamps. Ran engine ops cheek good end.

James W Thompson A&P277607049 —

TAM "'MORT TIME IN Pritc

TIME SERVICE Entries must be endorsed witn Name, Haling ana INUI IL.Pci

Technician or Repair Facility. (See back pages for other specific entries.)

DATE

10/15/01 Hobbs 1826.9 N600MP S/N 27-7554035

—

—Removed Edo-Aire Mitchell Turn and Bank indicator P/N 52D75-10, S/N 6870 C, Installed Factory new Mid-Continent Instruments Turn Coordinator P/N 1394T100 -7Z. S/N /109-367. Removed Bonzer, Inc. Radar altimeter indicator from copilots instrument

-panel, installed factory new condition Sigma-Tek Attitude Gyro P/N 5000B-36, S/N

-T78133N. Further details of this installation are on file under WO# 396 dated 10/10/01.

Weight and Balance change is negligible.

Scott Wallen Hamilton Avionics

CRS H04R608Y

_•

- -

wap0

elf' .01 00, a-

I 7 111■111I

,• YEW =UMW ,

TAM FLIGHT TIME IN . _ _ - wimerazions

Entries must be endorsed with Name, Rating and Certificate Number of

TIME tCX7/

SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE

- 10/15/01 Hobbs 1826.9 N600MP SN 27-7554035

—Removed Edo-Aire Mitchell Turn and Bank indicator P/N 52D75-10, S/N 6870 C, Installed Factory new Mid-Continent Instruments Turn Coordinator P/N 1394T100-7Z, S/N 2109-367. Removed Bonzer, Inc. Radar altimeter indicator from copilots instrument

-panel, installed factory new condition Sigma-Tek Attitude Gyro P/N 5000B-36, S/N

—T78133N. Further details of this installation are on file under WO# 396 dated 10/10/01.

- Weight and Balance change is negligible.

Scott Wallen Hamilton Avionics

CRS H04R608Y

iJ_

lbw Fl 4i?1,,TI;t _

I

3 0 0

—n CD CD O.

/ 1,11

CD CD

1124 3

YEAR: RECORDING TACH TIME

CRS#: ECFR4590 Date:11/13/01 S.0.#: LAV01-259 DATE AEROGENESIS I, LLC Reci#N600MP T_ype: Piper

CAPITAL CITY AIRPORT Model PA-23-250 S/N: 27-7554035 LANSING, MI 48906 Hcbbs: 1853.4

- 10/15/01

Remched KNS-80 RNAV PN 066-4008-00 SN 8092 for repair. Installed KNS-80 S/N: 8092 into aircraft. Replaced Post Light Bulbs. Repaired Post Light wnng. All work done IAW manufacturer's installaicn manuals aid •F:2_,“.. C43.13-1B 8,2A. The arcraft was repaired and inspectej ir_l_xecrctar}:e yifent . ons d the FM aid is approved for return to service. — Removed Edo-A

Installed Factory Name: - Dae:

SIN 2109-367. 13 panel installed factory new uI1uwm e,

— T78133N. Further details of this installation are on file under WO# 396 dated 10/10/ui.

- Weight and Balance change is negligible.

_ ,---15/t/s"-----

_ >-

Scott Wallen C _ Hamilton Avionics P. — CRS H04R608Y — _ = _ ; CD

i ' s - -

Fl n C.% gr, •

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E" I I ia I CO g >

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN 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

I&J via (ion Inc. Date 3-19-2002 Total Time Airframe 4223.1 Bra 2910111ohnimer Road N600MP Hobbs 1898.1 Hrs Hamilton. Ohio 45015 Piper PA23-250 SNI 27-7554035 Completed an Annual Inspection of this aircraft airframe on this date. Complied with AD81-04-05R1. amendment 39-4040, flap control inspection. No defects found in flap spar after inspection in accordance with paragraph (aX1). AD81-04-05R1 is nest due by 4323.1 Ins total time airframe. Complied with AD80-18-10, amendment 39-3903. fuel control cable inspection. All components are okay in accordance with paragraph (bX1), and (bX2).(i)and(ii). A1380-18-10 is next due by 4323.1 hrs total time airframe. Complied with AD88-21-07R1, amendment 39-6272. fuel well drain inspection. Drains are okay by inspection. AD88-21-07R1 is next due by 4- 1 -2003. Complied with FAR 91.207 pars (d), ELT inspection. All ELT components are okay by inspection. Replaced 2ea B3-5-1 Vacuum Filters. Replaced 2ea 13889-20629 Bearings and 2ea 13836-20629 Races on the nose wheel. Removed the left engine inboard e:ihaust pipes and sent to Aerospace Welding Minneapolis Inc. for repairs. See attached work order and maintenance release for details. Replaced the right engine starter with lea MHB-4061R Starter. See FAA Form 8130-3 and work order for details. Replaced both main tires with 2ea 7.00-6 8Ply Flight Custom II Tires with 2ea 092-318-0 Tubes. Replaced both right aileron rod ends and the left aft rod end with 3ea 452-860 Bearings. Replaced the rear baggage door switch and light with lea 688-390 Switch and lea 470-620 Light. Replaced the fuel filler panel studs with 4ea S3275-5W Studs with 4ea 494-060 Retainers. Replaced the nose and aft baggage door locks with lea 30426-004 Lock. Re-sealed the co-pilots master cylinder with lea '.i.IS28775- 012 0-Ring, lea MS28775-1I3 0-Ring and lea M528775-115 0-Ring. Replaced the lower rudder trim tab hinge half on the trim tab with lea 16914-000 Hinge. hatalled the trim tab with 3ca 21510-002 Hinge pins. Replaced the rudder trim tab control rod with lea 16515-000 Rod and attached it with lee 402-261 Bolt on the fwd end. Replaced the stabilator trim tab horn bolt and bearing with lea 691-349 Bolt and lea 14976-063 Bearing, Replaced the right nose gear door upper rod end with lea 452-335 Rod end. Re-sealed the nose gear door actuator with lea .AN6227-6 0-Ring, lea AN6227-9 0-Ring lea 755-902 Back-up Ring, and 2ea 755-904 Bach-up Rings. Replaced the nose gear drag link attach bolt and bushing with 2ea400-758 Bushings and 2ea 751- 417 Bushings. Replaced the nose gear steering collar linings with 2ea 31788-002 Linings. Removed the hydraulic pump and sag it to Professional Aircraft Accessories for overhaul. See FAA Form 8130-3 and work order for details. Replaced the left engine vacuum pump with lea Aero Accessories 441CC-7 Pump, SN06A19956 Pump. Serviced and charged battery. Lobed all control surface hinge points. Cleaned fuel strainers and sealed each with lea 753-205 Gasket and 1 ea 751-882 Gasket. Cleaned and greased all wheel bearings. Cleaned and greased all landing gear. Filled brake and hydraulic reservoirs. Run up check okay. No leaks noted. I certify that this aircraft airframe has been inspected in accordance with an Annual Inspection and was

determined to be in airworthy condition. -END- L/Z. - - Jeffre r j( Whyle I.A.297760788 I

wirsi• gl

YEAR: RECORDING TODAYS TOTAL Description of inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN 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

irs irs 135 No

cay

Inc xd Ply the

MAYDAY AVIONICS, 1INI.,./W9C.X7rt y DATE: --/0-"c349, REPAIR STA: IT5R947M

Certified Altiinf lttf Transponder, Static System & En-coder I.A.W. 91.411 & 91.413. System complies with paragraph (c), appendix E, of Part 43. Certified to 30

J GOO feet.

aw / ' -

Ar." 4ralilllille S. 3 3/ / /

(x) L_

311t Elite Aviation 2820 Bobmeyer Road I larnilton, Ohio 45015 N6OOMP Piper PA23-250 SN: 27-7554035 nnie 4-19-20112

ea llobbs: 1914.2 Total Tune Airtrame: 4z4v.4iirs _ _

;1. aft Replaced

the pilots control yoke universal joint, shall, and shaft bearings with lea 12734-000 Universal Joint. I .a 1 520-004 Sha , and 2ea 452-340

Beiwings.-END-

D5 0•••3

ATI Jeffrey /'h 'e A&P297760788

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A.; 7,41. 1 A 7 I li r.1 c TrAr.r, 1•141 4-111001110 TESTED A$

UfWrINFO 11,/ FAI 6,1,1' 4NJ TO4T Atticturt IAS , , Itr21 /IF' 11/11" 0 Stit.VICT

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%AMA' Avt i S

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p DATE .7 3-

_ A

'actions, Tests, Repairs and Alterations

d with Name, Rating and Certificate Number of

(See back pages for other specific entries.)

It rc) HOBBS /451.7

yo35-solt 3773 0 A-cr //id g-e(-4-%,(

cON THIS SYSTEM AND GROUND TESTED AS

HE AIRCRAFT HAS

DAY AVIQtIC INC

)ATE

LOGBOOK ENTRY

DATE 6 -4,2 -G. a MFG p.zolart_ MODEL PA-AA 3 -,2 SD A/C REG /s/ZpontiP SiN A 7- 75-51jo 35- so 37,ç7 HOBBS

, • , _._, ... • -•. :, , j alp , A MP.FIFF—/ ,A2_2 .R 1 • A o • g 3.

Ait,d---"P.P, • Proz6.12 6--...wcp, 541 x:973 11

AFTER SERVICE WAS PERFORMED, THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN RETURNED TO SERVICE.

dr_ Y • A IONICS NC

CRS# IT5R947M

IFG y,re MDL PA -0,3 --,Dso HOBBS r, 5'1.7 A/C REG 00004 s/N 7-7.5-5-zp>3.5 so# L.7 7 3Q 1 54-411ecQ mi.: .("" g'o

AFTER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN RE RNED 0 SERVICE.

' I R9 7 MAYDAY AVI/NI/S INC DATE 7//O- o-

YE DATE-/-O, MPC

ispections, Tests, Repairs and Alterations

..,.... — ,..,dorsed with Name, Rating and Certificate Number of

SERVICE I Technician or Repair Facility. (See back pages for other specific entries.)

DATE

LOGBOOK ENTRY

MFG P.Per MDL PA -..3 - .-,ST7 HOBBSI13 -9.7

A/C REGKacomP S/N -7- 7c-s-(035-S011,37750

Re, we a 40 co-.1150-x, 1(4- , (-(Q.4.-ee.ck ALT Hoick Ite lA4 _

RQ . wtStAliect G iQ t). 4 Co- A-4 4 oDg2 AFTER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS

REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN RETURNED 0 SERVICE. RETURNED

--

CT94 M MAYDAY AVI IC INC ,i4----t

1 1

LOGBOOK ENTRY

1.FG F,P,m"--- MDLPft-3 -3-Q50 HOBBS ii

A/C REG0 (Doomp S/N „Q -7_75 45-(12,35". SOW 7 7 3 0 In .. 1.-1 ItecQ / m4, ,e-r- ick1S- V.3 6,A) 8 V- .) c.nere...

AFTER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS

REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN RE RNED 0 SERVICE. C I R9 7 MAYDAY AVI I S INC

.) DATE 7 ..3 a-

Mons, Tests, Repairs and Alterations Nith Name, Rating and Certificate Number of Its. (See back pages for other specific entries.)

Piper PA23-250 Sbli 27-7554(135

rn Date 7-16-2002

iy Approved Aircraft Accessories. Inc. See serviceable tag and

noted.-END-

Jeffrey W yle A& .297760788

N# 600MP SN: 27

YEAR: RE TA TII

DATE

LOG BC f••

Hobbs

Installec This wo

The v and wa W/O# DATEE NORT1

LOGBOOK ENTRY 0 2

MFG P, MODEL f, 23 - 2 50 A/C REG A.1 S/N .27 5 3- Lit../ 3 5-

sot 3 7 7 3 o HOBBS I cl y P4,rte0 Alt Fr rowtr,..ttrx. grisr;f•r?

+VP • 403.1T Tr, ell

reit ASS fr•I/541. RPAACiO 191r0i

At Re P•i ir ACT 11 or T r

ch , c1C ,e'ca

AFTER SERVICE WAS PERFORMED, THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN APPROVED FOR RETURN TO SERVICE. CMnnnlit ct-QQQAAA TYDAY ON‘7./IIICV INC . 1iir CRS I IT5R947M

wit791S iOJ a4e)dwal asfl

Checked the cable tensions for the elevator, rudder, and the aileron systems. No defects were noted.

This work was done per the Piper PA-23-250 maintenance manual.

The work identified above was performed in accordance with the current Federal Aviation Regulation

and was found lobe airworthy for return to service. Pertine• r. , tai s are on file at t is .gency under

. W/0# 36821 Signed:

DATED: 06/26/02 for .---.. -...

NORTHERN AIR INC., CRS# N81R812N, GE- • D -, FORD I 'L AIRPORT, GRR, MI. 49512

1-..;

012 LiThi

TOTAL TIME IN k SERVICE -

-11111 YEAR:

DATE

RECORDING TACH TIME

TODAYS FLIGHT

LOG

- Installed This

and

— W/O4t

Hobbs

The

DATED:

BOOK ENTRY Make: PIPER

time: 2002.9

a new cabin work was done

work identified

was found to

AIR

37017 08/20/02

IN 0

door lock per the

above be airworthy

INC., CRS#

Ft -Ir 1-1 E FL IN A I 12

Dated: 08/20/02 N#: 600MP

Model: PA-23-250 SN1 27-7554035

t 4-

0

i g- C r. E r .. 1 2 i c4 , ; .::. . 0 e O. 4

r.. is. . .

and weather seal. Piper PA-23-250 maintenance manual.

was peormed in d nce with the current Federal Aviation Regulations

Is re on fi at this for return to service. pertinent

- ency under;

Signed: -_-_-.3----- ,------

for .------r----‘----

N81R812N, GER . . R ORD IN R"• GRR, MI. 49512

res

'554035 16-2002 tag and

mit

DATE

_Au _._

LOGBOOK DA T r

_ . ENTRY

MODEL PA 2 3 - 2 C ° RECORDING TACH TIME

TODAYS FLIGHT

TOTAL TIME IN SERVICE

MFG P feit

A/C REG A- 60ori P S/N 2 - 7 5S- 9 03 S°11 3 S' 2 ) 7 HOBBS 2 0 3 Y 1 Regc 4c < C...yeKo 5 2 /2 cy

1-4 <=, Ft 1-41 12, C.r 1...-/ -tc4 _

Pecs; r. t4ck c io ock

LOG BOOK ENTRY Date

Make: PIPER Mod.

Hobbs time: 2002.9

—Installed a new cabin door lock and weather se; This work was done per the Piper PA-23-250 n

The work identified above was performed in and was found to be airworthy for return to se'

— W10# 37017 Sigr

DATED: 08/20/02 for

—NORTHERN AIR INC., CRS# N81R812N, GI

3 I !

AFTER SERVICE WAS PERFORMED, THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43_13 AND THE AIRCRAFTAS BEEN APPROVED FOR RETURN TO SEE (J

AVIONICS INC_ CRS it IT5R947M

„1791.S aleldwal asn

• — YEAR: RECORDING TODAYS TOTAL 7:•••-, TACH

TIME FLIGHT TIME IN

SERVICE

DATE

Elite Aviation. inc. 2820 Bobmeyer Road • Hobbs: 2112.6 Hrs

Date 4-23-20(13 — Completed an Annual Inspection of this aircraft airframe on this date. Complied with AD814)4-05R I. amendment 39-4040. flap control inspection No defects found in flap spar or flap arm after inspection in accordance with paragraph (all I) and (b)(2). AD81-04-05R1 is next due by 4537.6 hrs total time airframe. Complied with A080-18-10, amendment 39-3903, fuel control cable inspection. All components are okay in accordance with paragraph (bit It and (b)(21,(i)and(ii). AD80-18-10 is next due by 4537.6 hrs total time airframe. Complied with AD88-21-07R1, amendment 39-6272, fuel well drain inspection. Drains are okay by inspection. AD88-21-07RI is next due by 5-1-2004. Replaced the ELT battery with lea BS2I66 Battery. ELT batten

expires April, 2005. Complied with FAR 91.207 para (d), ELT inspection. All ELT components are okay by inspection. Replaced 2ea 133-5-1 Vacuum

. Filters. Replaced lea 13889-20629 Bearing and lea 13836-20629 Race on the nose wheel. Replaced the central vacuum filter and both vacuum regulator

filters with lea RAD9-18-I and 2ea RAB3-5-1 Filters. Replaced the right brake linings with (lea 066-06200 Linings. Serviced and charged battery. lobed all control surface hinge points. Cleaned fuel strainers and sealed each with lea 753-205 Gasket and lea 751-882 Gasket Cleaned and greased all wheel

bearings. Cleaned and greased all landing gear. Filled brake and hydraulic reservoirs. Run up cheek okay. No leaks noted. 1 certify that this aircraft airframe has been inspected in accordance with an Annual Inspection and was determined lobe in airworthy conditii . - -.ND-

/ /././....../ . .

cffrey 1 ' ' le I.A.297760788

I 1 I I Elite Aviation. Inc. 2820 Bobmeyer Road Hamilton, Ohio 45015 N600MP Piper PA23-250 SN: 27-7554035 Hobbs: 2118.2 Hrs Total Time Airframe: 4443.2 Hrs Da - 4-28-2003 Replaced the aircraft battery with lea G246 Battery serviced with electrolyte. -END-

../ ..,_,-../.... ,,,,....

ile Jeffrey Whyte LA.297760788

_I_ 1 I

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.)

Hamilton, Ohio 45015 N600MP Piper PA23-250 SN: 27-7554035 Total Time Airframe: 4437.6 Ilrs

YEAR

DATE

1111.1111111111.11 111111....111. Mons YEAR: RECORDING TODAYS

terations

or of TACH FLIGHT iiiyit in Entries must be endorsed with Name, Rating and Certificate Number of

itries.) TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

. 27-7354(,;5

1,4-23-20(13 pection \,,,

hrs total tirth:' (graph (ha 1 ,. iel Sail draw

L1.1 hallo, :■ - I Vacuum

urn regulah(r ite ■-■ l_ubed sed all ■«heel Ah,wremil

...

DATE 1 I I

— — – -

LOGBOOK ENTRY MAYDAY AVIONICS INC. _

MFG p; pac— moLPADr-D5-0 HOBBS ,.ltpct - cl

A/C RE 61..)tpOorIP S /N 7-7.S5(1035- SO SC31(901 Q .7b) 11-A■04 kali if,

r4?,t4to,Na AP CarSole ://c CP-AO PC 11

Iie■ LkshAl ( eS, , &I.3_0 CrOCC2 I.

AFTER SERVICE WAS PEgFORMED THIS SYSTEM AND —

ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT

EEN A RO D FOR RETURN TO SE VIC .

DATE 67 a0

– —

CRS # IT5R947M

!7-75$4105

(4-28-2003

t 4.

i YEAR: RECORDING 1 TODAYS I TOTAL TACH FLIGHT TIME IN TIME SERVICE

Description of Inspections, Tests, Repairs and Alteration Entries must be endorsed with Name, Rating and Certificate Number cA Technician or Repair Facility, (See back pages for other specific entrio,

_ LOGBOOK ENTRY

DATE 4-X5-03 MFG PiiNea-- MODEL PA - z.3 - zso A/C RE.G Nl.POCHAr SiN -7 sZ.-10.35 SO# acIS- • HOBBS al 76

Ne.t0 Rsor a 1 3 0 -ts.18 ftv-sfee4,SM .I. CL,v0r.e&_ 4. LaAt..

s3 For- leals. rs%..htf-Nitek trIa• C..tts•1 he Yx. OverLJe4 a...3108R)(2-

AFTER SERVICE WAS PERFORMED, THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN APPROVED FOR RETURN TO SERVICE.

27DT:20N CS CRS I IT5R947M

■ -__

!-

..,

.4 R-

YEAR: RECORDING TACH TIME

TOUTS 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.)

DATE

MEG A/C sof

DATE LOGBOOK ENTRY

i , ,eit MODEL FA 2 3 - 2 S- 6

REG /1/ 00 Ai P S/N 27 - 7 5 c Le r) -) _5--

39 c c 5- HOBBS 2 ) R 0 . '3

e A 77-17- 4,n , £y/(O.

c 4 e ric 4 0 pi, , S-20 E.-7 S/A' i C 9 /I '

1

AFTER SERVICE WAS PERFORMED, THIS SYSTEM , AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13 AND THE AIRCRAFT HAS BEEN APPROVED FOR RETURN TO

7,4.77 C.

....i

Ai Y -A-ZIONIC IN CRS It IT5R947 '7 0 ..

.... 70

I r 1, •1 i N m t91 t Z ..›. = _ _

YEAR: RECORDING TOMS mit Description of Inspections, 'rests, Repa i rs and Alterations

TACH FLIGHT TIME IN 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

'

<=. 12 -r 11-1 IE 1 12

Airframe log book entry Dated: 7/18/2003 N 600MP Make: Piper Model: PA23-250 SN: 27-7554035 Total Time: 2185.7

Removed panels and copilot seat. Jacked aircraft. Ran gear and flaps with hand pump. Found cross

fitting leaking. Disconnected and removed all three cross fittings. Installed fittings into new cross fittings and torqued. Pressure tested cross fittings, no leaks noted. Installed cross fittings in aircraft and connected lines. Serviced reservoir and ran gear and flaps through several cycles using aircraft hand pump. Ops checked normal, no leaks noted at this time. Installed panels and copilots seat and stops. Removed aircraft from jacks.

The work identified above was performed in accordance with the current Federal Aviation Regulations and was found to be airworthy for return to service. Pertinent stalls are on file at this togency under; W/O# 38850 Signed:

GesA \-o• DATED: 07/18/03 for

CialDP'4' e NORTHERN AIR INC., CRS# N81R812N, GERALD R, F INT'L AIRPORT, GRR. mi. 49512

'ations TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations YEAR: RECORDING Der of TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of

ntnes.) TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

DATE

LOGBOOK ENTRY MAYDAY AVIONICS INC. — MFG pecl— MDL -- ) HOBBS 2190. - A/C REG.06;00i4P S/N 07- 7S-S-405- sots 35 7.2

1<€010a4 LT ca.-beater— GIP ) -Fat tep4-, r- - a95cA q4.L.c cp4 gelier

AFT'ER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED

-- AS REPUIRED,BY FAR 43.13 AND THE AIRCRAFT qF A VED FOR RETURN TO SE VI E. DATE 7 3

— CRS 4 IT5R947M

LOGBOOK ENTRY MAYDAY AVIONICS INC.

MFG F,PeA-- MDLPAQ3-35D HOBBS Q191L4 A/C REG 1.)60>41) , S/N 75-Wa6- SO# 31727

ge.Ta-,04 0/4 1,2T Oniotter 4CLAp- AN) tit) gealf AFTER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS RED IRED BY FAR 43.13 AND THE AIRCRAFT HA • IN 17AVN FOR RETURN TO Rvick, DATE_ 3 1 I.) CRS # 5R947M

ITP 2 P I 41

r

=MI YEAlk I Tairdirl, AIteratjons

of . . Specific entries.) .

NAV!

Elite Aviation, Inc. 2820 liobinever Road Hamilton, Ohio 45015 N6OOMP Piper PA23-250 SN 27-7554o Is — Hobbs: 2202.3 Firs Total Time Airframe: 4527.3 firs D e 8-12-2003 Resealed the left gear door actuator with 3ea MS28775-113 0-Rings. Ops check good. No leaks noted. -1:N13- /

_...e...r....." .. a ...

' Jeffrey J yle LA.297760788 I

1

I I - ----.........__-- 7.-

Ir--1 0 R -I- I—I E Ft IV A. I R N 600MP

Airframe log book entry Date: 9/91/2003 Total Time: 2217.8 Make: Piper Model: PA23-250 Serial No: 27-7554035

Removed and replaced stabilator trim cable from cockpit crank to turnbuckle in empanage per Piper Aztec

Service Manual. Chapter 5. Operational and travel check within limits per Table V-1 and Figure 5-7 of Service Manual.

woirhkeorwdoerrkoicle3n9t2ifi3ei d above was pesrilgonremded inaczlance witiVurrent Federal Aviatiotanr RcegRsulNa stioRnes io2nNd — -

Northern Air Inc., P.O. Box 888380. Gerald R.Xoird

Intl Airp7, Grand Rapids, MI. 49588-8380 — • '

Elite Aviation Inc. 2820 Bobmeyer Road I [amnion, Ohio 45015 N600MP Lycoming TIO-540-CIA SN: L-3577-61A — Hobbs: 22683 Hrs Total Time Engine: 45933 Hrs SMOFI: 1197.5 Hrs Left Engine Date 12-3-2003 Removed the exhaust pipes from the cylinders to the turbo and the waste gate and sent them to Dawley Aviation for repairs. See Serviceable tag and work — order for details. Installed the exhaust pipes with 6e,a 77611 Gaskets, lea 75845 Gasket, 3ea 78246 Gaskets, lea ST 932 EG ' Pro. Ai :pier Fitting - END-

, / /

/ ....4‘....v . • ... . . . 41 . -

C - ey Whylc A& ' 97760788

_


DATE __..

Elite Aviation. Inc. 2820 Bobmeyer Road Hamilton, Ohio 45015 N600111P Piper PA23-250 SN: 27-7554035

Hobbs:2301.6 Hun Total Time Airframe: 4626.6 Bra Date 2-5-2004

Roofed both right brake calipers with 4ea MS28775-222 0-Rings and replaced 3ca 082-02000 piston rings Rey, the right enpne alternator with lea ALU8421R Alternator, SN: 8M000130. Ops check good. No leaks noted. -END- i.... .,./ .001

(/' JeffieS, I Whyte -A&P297760788

4 4 4 _4_

Elite Aviation. Inc. 2820 Bobrneyer Road Hamilton, Ohio 45015 H600MP Piper PA23-250 SN: 27-7554035

Hobbs: 23092 Bra Total Time Airframe . 4634.8 Bra Date 5-14-2004

Completed an Annual Inspection of this aircraft airframe on this date. Complied with A080-18-10, amendment 39-3903, fuel control cable inspection All

components are okay in accordance with paragraph (b)( I). and (bX2),(ftandfifi. AD80-18-10 is next due by 4734.8 hrs total time airframe. Complied with

AD81-04-05R1, amendment 39-4312, flap control inspection. No defects found in flap spar or flap arm after inspection in accordance with paragraph (aXIt

and 0)(2), AD81-04-05R1 is next due by 4734.8 hrs total time airframe. Complied with A088-21-07R1, amendment 39-6272, fuel well drain inspection_

Drains are okay by inspection. AD88-21-07R1 is next due by 6-1-2005. Complied with AD2003-09-13. amendment 39-13142, flap torque tube inspection.

Inspected flap torque tube in accordance with Piper Service Bulletin 10518. No cracks or defects found. AD2003-09-13 is next due by 5134.8 hours total

time airframe. Installed the flap torque tube with 2ea 17629-000 Bearings. Complied with FAR 91.207 para (d), ELT inspection. All ELT components are

okay by inspection. Removed the hydraulic power pack and sent it to Pifer's Airmotive for overhaul. See FAA Form 8130-3 for details. Installed hydraulic

power pack. Resealed both parking brake valves with 2ea MS28775-006 0-Rings, 2ea MS28775-113 0-Rings, and 2ea 752-844 0-Rings. Replaced the left

engine oil pressure hose to the firewall with lea MS28741-3-0120 Hose. Replaced the hydraulic filter with lea 751-759 Filter. Removed the right main

gear actuator and resealed it with I ea MS28775-12I 0-Ring, lea MS28774-121 Back-Up Ring, lea 756-098 Seal, lea 756-099 Seal, and replaced lea

MS20822-4D Fitting and lea AN8I6-4D Fitting. Replaced the left gear aft door hinge and rod with Ica 31443-006 Hinge Half, lea 31443-007 Hinge Half,

lea 21510-002 Hinge Pin, and lea 31475-000 Rod. Replaced both main gear forward door rod ends with 4ea 452-335 Rod Ends. Replaced tno gear ith se

door belcntrik bearing blocks with 2ea 17544-002 Bearing Blocks. Replaced the nose gear door lower rod ends with 2ca 452-335 Rod Ends, sealed the

nose gear actuator with lea MS28775-121 0-Ring, lea MS28774-121 Back-Up Ring, lea 756-098 Seal, lea 756-099 Seal and replaced the rod d with Ica

762-685 Rod End. Replaced the tail nay light with lea 6E305 Bulb. Removed both prop de-ice slip rings and resurfaced them in accordance th Chapter

14-48 of the Piper Aztec Service Manual. Replaced the prop deice brushes with Sea 753-427 Brushes, and 6ea 2E1207 Springs. Replaced the rod ends

on the right engine inboard cowl flap rod. Removed the right engine exhaust and sent it to Dawley Aviation for repair. See serviceable tag and work order

for details. Reinstalled the exhaust with 3ca 78246 Gaskets, 2ea 75845 Gaskets, and Sea RA77611 Gaskets. Replaced the right engine lord mounts with 4ca

19613-12 Lord Mounts. Replaced the left aileron inboard hinge bearing with Ica 25704-000 Bearing. Replaced the left aileron forward rod end with lea

452-860 Rod End. Replaced the inboard and center hinge bearings on both flaps with 2ea 452-808 Bearings and 2ea 758-123 Bearings. -Continued-

it

I LT I Pt I P


DATE .

-Continued- Replaced the flap control rods with 2ea 18316-000 Rod Ends. Replaced loose rivets in the left flap with CR3243 Rivets. Removed the patch

under the right wing and tabricated a new, larger patch, using existing holes and extending to the spar rivets, and installed with CR3243 Rivets. Replaced

the stabilator trim tab rod bearing with lea 14976-063 Bearing. Replaced the stabilator left trim tab hinges with 6ea 16914-000 Hinge Halves and 3ca

21510-002 Hinge Pins. Removed the oxygen bottle and had a hydrostatic test performed on it. Resealed the pilot master cylinders with 2ea MS28775-012

0-Rings, 2ea MS28775-1I3 0-Rings, and 2ea MS28775-115 0-Rings. Replaced the manifold pressure filters with 2ea 754817 Filters. Resealed the fuel

crossfeed valve with lea MS28775-113 0-Ring and 3ea MS28775-010 0-Rings. Replaced the right brake disc with lea 164-03206 Disc. Replaced the left

brake disc with lea RAI64-03206 Disc. Resealed the nose strut with lea MS28775-328 0-Ring and lea MS28775-228 0-Ring. Replaced 2ea 03-5-1

Vacuum Filters. Serviced and charged battery. Lobed all control surface hinge points. Cleaned fuel strainers and sealed each with lea 753-205 Gasket and

lea 751-882 Gasket. Cleaned and greased all wheel bearings. Cleaned and greased all landing gear. Filled brake and hydraulic reservoirs. Run up check

okay. No leaks noted. I certify that this aircraft airframe has been inspected in accordance with an Annual Inspectio• . was deter , ined o bet airworthy

condition. -END- •

/Jeffrey - yle I.A.2`7760788

Elite A -Hobbs:

AM 1 Pit I f- r. • ...:

• ;-, -.r, •• i., I _

1T5R947M .. , - ER,,, ,.... .. , .. AI - ii,vt. j... jaL.„ System & En- _ A _ complies with

3. Certified to _

—..tkihr I – - . - --

_ . t .


DATE 1.......

Airframe: 4655.6 Hrs Date 8-20-2004 Piper PA23-250 SN: 27-7554035

Hobbs: 2330.6 Urn Total Time Air Elite Aviation. Inc. 2820 Bobmeycr Road Hamilton, Ohio 45015 N6OOMP

Replaced both engine air tillers with 2ea BA3510 Filters in accordance with SIC SA71GL and Installation instruc ion Sec FAA Fo 337 .'s date for .

Hobbs: 2332.6 urn 2820 Bobmeyer Road Hamilton, Ohio 45015 N600MP Piper PA23-250 SN: 27-7554035

I I

Total Time Airframe: 4657.3 Firs

1

,. Je - - y 1 Whyle A& 97760788

- ' //

/

Date 9-15-2004_

, details.-END-

i

Elite Aviation, Inc.

Replaced the stabilator trim switch on the pilots yoke with lea 10670-2 Switch. Removed the oil temperature gages and probes, sent them to Instrument Rebuild for calibration, sec work order for details, and reinstalled gages and probes. Run up check okay. Ops check g.... No leaks noted.-END-

I :

Jeffrey byte A&•297760788

'....../AK-er .. d ./. . -

_

YEAR: RECORDING TODAYS TOTAL TACH FLIGHT TIME IN TIME 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.)

LOGBORDK ENTRY MAYDAY AVIONICS INC. tIFGP, rer AtioLVA-7)-3-D HoeBs033G, —7 A/C REG 1,3 (witvAr s/t, )7-7s5-qc35- 50# 11/ 7 5-7

--.

Elite Hobbs:

Fhte Bibb , Comp c,‘Illp ■

ADS! and dt Dram presst

- - - -- - hours impel Re0a comp

4 ...;;:e. A P F. ...li 449.11./t2 1 ge0.stqlla+ rivic, ,/ 60

AFTER SERVICE WAS PERFORMED THIS SYSTEM AND ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REOU *ED BY FAR 43.13 AND THE AIRCRAFT HAS APtft E FOR RETURN TO 6SE(V4g,

DATE 1 J 51 t-f CRS # IT5R947M

I I LOGBUK ENTRY . MAYDAY AVIONICS INC. MFG /71/2;az.- MD L ..04 ---217.-als-c, HOBBS _2./ 6 .L.... - A/C REG ia,/19' '.--.../N22:17 „5- "-SX4t__W_

/ ... . IA .%'5" . CZ- e-,:.. — -4 ,>

AF ER SERVICE WAS PERFORMED THIS SYSTEM AND lea 7 the ft 002 I Instal brad.x 753-: mmx deter

ALL ASSOCIATED SYSTEMS WERE GROUND TESTED AS REQUIRED BY FAR 43.13

AND THE AIRCRAFT HAS : N APPROV 0 FOR RETURN TO S V E. DA TE -25)6:_t_ CRS ft IT5R947M

1 1

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

DATE

Elite Aviation. Inc. 2820 Bobmeyer Road I lamilton, Ohio 45015 N600MP Piper PA23-250 SN: 27-7554035

Hobbs: 2350.9 Hrs Total Time Airframe: 4675.9 Hrs Date 2-23-2005 Replaced both landing lights with lea 6E4596 bulb and lea 6E4553 Bulb. Swung the compass and recorded the dev . ,tion No leaks noted.-END-

le ey J 4rle A&P2857210

Elite Aviation. Inc. 2820 Bobmeyer Road Hamilton, Ohio 45015 N600MP Piper P33250 SN: 27-7554035

Hobbs: 2369.5 Urn Total Time Airframe: 4694.5 Hrs Heater Hobbs: 1195.6 His Date 5-6-2005 Completed an Annual Inspection of this aircraft airframe on this date. Complied with AD80-18-10, amendment 39-3903, fuel control cable inspection. All

components are okay in accordance with paragraph (b)(1), and (b)(2),(i)and(ii). AD80-18-10 is next due by 4794.5 his total time airframe. Complied with AD81-04-05R1, amendment 39-4312, flap control inspection. No defects found in flap spar or flap arm alter inspection in accordance with paragraph (a)( I) and (bX2). AD81-04-05R1 is next due by 4794.5 his total time airframe. Complied with AD88-21-07R1, amendment 39-6272, fuel well drain inspection.

r Drains are okay by inspection. AD88-21-07R1 is next due by 6-1-2006. Complied with AD2004-21-05, amendment 39-13826, heater combustor decay

pressure test and pressure switch test. Pressure test is okay and replaced switch with lea 94E42-3 Pressure Switch. AD2004-21-05 is next due by 1295.6

ham's beater hobbs or April 2007. Complied with AD2004-25-16, amendment 39-14076, combustor heater fuel regulator inspection. Removed and

inspected regulator. Marked the date on the regulator and reinstalled valve. AD2004-21-05 is next due by 4794.5 hours total time airframe or June 2006.

4 Replaced the ELT battery with lea BPI010 Battery. The ELT battery expires May 2007. Complied with FAR 91.207 para (d). ELT inspection. All ELT

components are okay by inspection. Replaced the vacuum filters with 2ea mRAB3-5-I Filters and lea RAD9-I 8-1 Filter. Replaced the hydraulic filter with

lea 751-759 Filter. Replaced both engine air filters with 2ea BA3505 Filters. Replaced the left engine oil temp probe with lea 553-672 Probe. Replaced

I die fuel quantity sender in the right outboard fuel tank with lea 33855-003 Fuel Sender. Replaced the pilots and copilots yoke shaft rollers with 6ea 16851-

E102 Rollers. Removed the fuel flow gauge and sent it to Aircraft Quality Instruments for repair. See maintenance release and work order for details.

j Installed gauge after repairs. Replaced the left main gear outboard door forward hinge with lea 31304-000 Hinge. Replaced four brake linings on the right

brake with 4ea 066-06200 Linings. Serviced and charged battery. 1.ubed all control surface hinge points. Cleaned Mel strainers and sealed each with lea

753-205 Gasket and lea 751-882 Gasket. Cleaned and greased all wheel bearings. Cleaned and greased all landing gear. Filled brake and hydraulic reservoirs. Run up check okay. No leaks noted. I certify that this aircraft airframe has been inspected in accordance with an Annual Inspection and was determined to be in airworthy condition. -END- 1<—

Jeff y J °Pyle I.A. 2857210

-o I to co :7' IwIP .


DATE

Elite Aviation, Inc. 2820 Bobmeyer Road Hamilton, Ohio 45015 N600MP Piper Hobbs: 2410.4 Hr s Total Time Airframe: 4735.4 Hrs Replaced the right voltage regulator with lea B-00286-1 Regulator. Ops check good.-END-

MAYDAY AVIONICS. INC GERALD R. FORD INTERNATIONAL AIRPORT

Flight adjusted autopilot to diminish rate of descent.

PA23-250 SN: 27-7554035

Date 9-7-2005

/

Jeffrey hyle A&P2857210

The above work was performed in accordance with current FAA regulations and in respect to work performed on the aircraft identified below is approved for return to service_ Pertinent details of the work performed are on file at this repair station under Service Order No 42757

DATE 5-17-5 MAKE Piper MODEL PA-23-250

SIN 27-7554035 N# N6OOMP

FOR FAA CRS 1751,2847M HOBBS 2372.8

- 5500 44TH STREET SE - GRAND RAP1DS,MI 49512

YEAR:

DATE

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.)

.0 12 ir 1-1 1 12 N 600MP

Airframe log book entry Date: 9122/2005 Hobbs Time: 2414.7

Make: piper Model: PA-23-250 Serial No: 75544035 Total Time:

Replaced ring terminals on aircraft side EGT Probe harness. Installed EGT probe and shrink wrap connections. Ops checked EGT. Ops checked good.

Cleaned, and inspected left and right engine fuel injectors. Reinstalled and torqued fuel injectors. Reattached lines and fittings to injectors. Performed leak check and ops check. Ops and leak check good. Complied with AD 2002-26-01 by visual inspection with no defects noted. AD due at next access.

The work identified above was performed in accordance with the current Federal Aviation Regulations and was

found to be airworthy for return to servic e ent 51.ej...ls are on file at this agency under;

WorkOrder# 43520 Signed: for CRS N81R81 2N

Northern Air Inc., P.O. Box 888380, Gerald R, ord Intl Airport, Grand Rapids, MI. 49588-8380

YEAR: I RECORDING TODAYS I TOTAL I Descrintin f I _n n --a- --at 1111......Aseinns

Northeast Aviation, Inc. 19 Apr 06 N600MP DATE Northeast Philadelphia Airport

11301 Norcom Road PA-23-250 Philadelphia, PA 19154 s/n 27-7554035 Hobbs 2432.7 TTAF 4739.1

Performed Annual Inspection per Piper Aztec Maintenance Manual and FAR 43, Appendix D checklist.

1) Replaced Brackett BA-15 filter elements. 2) Removed all required panels and performed required inspections. 3) Inspected ELT i/a/w FAR 91.207 (d)(1-4). Battery replacement due 03/10.

replaced Switch battery- due 03/09. 4) Serviced brake and hydraulic reservoir with 5606 fluid. 5) Washed and lubricated aircraft. 6) C/W A/D 72-14-05, engine exhaust stacks inspections i/a/w SB #319. 7) C/W A/D 79-26-01, stabilator rivets i/a/w S/B #606. 8) C/W A/D 80-18-10 by inspecting swivels and cables i/a/w SB #507. 9) Airworthiness Directives search completed for aircraft. See updated recurrent

T-Data list. 10) See entry of work performed for conformity inspection dated 18 Apr 06

I certify that this aircraft has been inspected in accordance with an Annual Inspection and was found to be in an airworthy condition and is returned to service.

• . heast Aviation,

- Patilick Byrnes A&P 9504512 I.A..

A

I SERVICE

ame, Rating and Certificate Number of

TIME I Technician or Hepair tee back pages for other specific entries.)

DATE I DeGol Jet Center 775- 580 S. Loyalsock Ave. _ ret Montoursville, PA 17754 _

Phone 570-368-2651 Fax 368-8651

<>N600MP<>PA23-250<>S/N#27-7554035<>Hobbs: 2433.9<>

Date: 4/20/2006

Complied with Weight and Balance of Aircraft and completed all paperwork. This Weight and Balance

supercedes the Weight and Balance dated 5/9/2000. ± END ±

The aircraft, airframe, aircraft engine, propeller, or appliance identified above was repaired and

inspected in accordance with current Regulations of the Federal Aviation Agency and was

determined to be in an airworthy condition and is approved to return to service.

W/O #2006042001

Repair Station CR #e :r R3 • .0# ;-

Signatti AiNI■ Date

YEAR:

•■•••

YE

—

DA

Northeasi A, ugh°. 04-05-07

11401 Nonuun Rd — — N6OOMP

ldelptim A 19154 Phia P

stNPA 23271277S4035 Installed no, 11 T batter, 10 Surial number 94232 Now ELT All don< in au‘ordance with Piper Stmt.* Manual e".- ..,- '-----....,....w......„-------\ For Northeasi Avuttion. Pairwk tivrtirs AAP 119504512 ---

.

Northeast Aviati(n. Inc. (16 Apr 07 Northeast Philadelphia Airport N600MP 1 1 301 Norcom Road PA-23-250 Philadelphia, PA 19154 sin 27-7554035 Hobbs 2455.5 TTAF 4761.6

Performed Annual Inspection per Piper Aztec Maintenance Manual and FAR 43, Appendix D checklist. 1) Removed all required panels and performed required inspections. 2) Inspected ELT iia/w FAR 91.207 (d)(1-4). Battery replacement due 03/10. replaced Switch

battery- due 03/09. 3) Serviced brake and hydraulic reservoir with 5606 fluid. 4) Jacked aircraft lubricated gear and Performed retraction check 5) Washed and lubricated aircraft. 6) C/W A/D 72-14-05, engine exhaust stacks inspections i/a/w SB 4319. 7) C/W A/D 79-26-01, stabilator rivets i/a/w S/B 4606. 8) (/W A/D 80-18-10 by inspecting swivels and cables i/a/w SB 4507. 9) Airworthiness Directives search completed for aircraft. See updated recurrent T-Data list.

I certify that this aircraft has been inspected in accordance with an Annual Inspection and was found to be in an airworthy condition and is returned to service.

For Northeast Aviatio

-

terations 'umber of

s.)

-

____

--

1

m.

-

—

_

_

_

_

_

—

—

—

—

— atrick ymes A& 9504512 IA..


DATE • Northeast Aviatun 4/30A)8

11301 Notoom Rd. NSOOMP Philadelphia, PA PA 23-250 19154 27-7554035 Hobbs: 2468.2 1TAF: 4774.3

Performed an Amami Inspection Per Piper Aztec Mamaenanix Manual and FAR 43, Appendix D Checklist.

I) Removed all required panels and performed required inspections. 2) Inspected ELT i/aAv FAR 91.207 (d)(1-4). Battery replacement due 3/10. Switch battery

Due 3/09. 3) Serviced brake and hydraulic reservoir with 5606 fluid. 4) Jacked aircraft, lubricated gear, and performed retraction check. 5) Washed and lubricated aircraft. 6) CIW A/13 72-14-05, engine exhaust stacks inspections i/a/w SIB #319. 7) CAV A/D 79-26-01, stabilator rivets daAv SB #606. 8) C/VV AO 80-18-10, by inspecting swivels and cables i/a/w SB #507. 9) Airworthiness Directives scorch completed for aircraft See updated reciarent T-Data list_

I certify thai this aircraft has been inspected in accordance with an Annual Inspection and was found to be in An airworthy condition and is Maimed to service. For Northeast Aviatipn,

k._ Pain& BVmes A&P a 2

/1/410 _ID.2 ,q — _77g.5 040 tq C -- /4/-07 73 ,i tyspE_ezza,_<)

i, eRvic6 B010,11 :3 4-f 2.e- I Wet c_LA/d-E._

Ney -24:,_ e-AT/A)4.-

r . oe -n-AF if s78„5 " or td 1 f lAe6,-.1.64f: ,

1111111.L____1= ..3q 477- 1 i ri 1 .)7. i

- I TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations

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

— Northeast Aviation, Inc. 19 Aug 08

Northeast Philadelphia Airport N600MP

11301 Norcom Road PA-23-250

— Philadelphia, PA 19154 s/n 27-7554035

Hobbs 2472.4 TTAF 4778.8

1) Replaced Nose landing gear Trunnion p/n 31768-03with serviceable part s/n 07247 from S&B Industries CRS QESR142N

2) Replaced Nose wheel tire with new Mc Creary 6:00X6 3) Repaired frayed Taxi light wires on NLG strut Performed operational check of landing gear retraction system, Nose gear steering, and Taxi light, all checked good. All work performed IAW piper Aztec service manual. Aircraft is returned to service.

• st Aviation,

• •.•

o 0, co

8

■o

CN I

zr-o. Z

id Alteration s ate Number of specific entries

.ièsA&P laug4e-1,_

at. r

YEAR:

DATE

RECORDING TACH TIME

TODAYS FLIGHT


De ri ion of Inspections, Tests, Repairs and Alterations Ent ' s st be endorsed with Name, Rating and Certificate Number of tr

,u Tec n or Repair Facility. (See back pages for other specific entries.)

Vincent LicoIli 05/05/2009

Piper PA 23-250 27-7554035

N600MP 4781.5 TTAF

Hobbs 2475.1

Performed an Annual/100 Hour Inspection i/a/w FAR Part 43 Appendix D and Piper Aztec Maintenance

Manual. Inspected ELT i/a/w FAR 91.207(d)I-4. No defects noted. Replaced Battery with new BS-2I66 battery.

Battery replacement date now 05/11. Serviced brake and hydraulic reservoirs with 5606 hydraulic fluid and replaced hydraulic filter with new p/n

751-759 element and o-rings. No defects noted. Replaced vacuum filters with new RAB3-5-I Garter filter elements. Replaced left and right engine Brackett air filters with new BA-3505 elements. Remove & installed Oxygen Bottle from aft location for hydrostatic certification. Inspected battery box and cables for condition. Charged and serviced battery fluid level. Installed Overhauled p/n 441-CC17 Air Pump (acceptable substitute for 441CC-7 as removed per Neal @ Aero Accessories) , s/n 65256, on right side, i/a/w Maintenance Manual guidelines. Operational check

satisfactory. Cleaned all fuel screens and inspected, replaced p/n 753-205 & 751-882. No defects noted.

Lubricated aircraft i/a/w lubrication guidelines Section II. Jacked aircraft and performed gear swings. Replaced p/n 31909-02 knob due to crack. Completed gear swings verifying no leaks, proper fitting and actuating of doors and gear, and warning lights and hom.

Weighed CO2 bottle. No defects noted.

REPLACE ELT BATTERY BY:

MAY 11

Iterations 'lumber of ific entries.)

C/W A/D SO-1840, Fuel Selector Valves and Cables, by inspection va/w paragrapn (nit anu m(z)ti- ii). No defects noted. Due again 4881.5 TTAF. C/W AID 81-04-05R1, Flap Spar Hinge Attachment, by inspection i/a/w A/D paragraph (a)(I) and (b)(2). No defects noted. Due again 4881.5 TTAF. C/W AID 88-21-07R I, Fuel Filler Compartment, by inspection i/a/w AID. No defects noted. Due again 4881.5 TTAF. A/D 03-09-13 P/C/W, Flap Control Torque Tube, i/a/w AID. Due again 5239.1 TTAF. C/W A/D 03-14-03 . Rotary Fuel Pump Relief Valve Screws, left engine only, by torque inspection i/a/w AID paragraph (4). No defects noted. Due again 4831.5 TTAF. C/W A/D 04-21-05, Janitrol Heater, para ft3), decay check i/a/w Janitrol Maintenance Manual p/n 24E25-1, section 3, pars (3.3.1-13). Performed pressure switch test on p/n 94E42-3. No defects noted. Inspection due again 1312.8 Heater Hobbs C/W A/D 04-25-16RI, Janitrol Heater Regulator, by inspection. Marked date and Hobbs time on regulator shroud body. Operational check of heater performed with no defects noted. Due again 4881.5 TTAF or 05/2010. C/W A/D 08-14-07, Fuel Injector lines, left and right engines, by inspection i/a/w SB 342E. No defects noted. Due again 4881.5 17AF, or when lines or clamps are disturbed. AID 09-02-03 D/N/A, RSA Series plugs, by install & service dale. No defects noted. See complete A/D Listing for airframe and accessories in AID Compliance Section. Performed Operational and Run-up Checks with no defects noted.

I certify this aircraft has been inspected i/a/w an Annual Inspection and was determined to be in airworthy dition and is •, ved for return to service.

I t#P'4 es M. Cherry

A&P 2700481 I.A.

.--

Ammon Newest Avalon Authorty/Couney

FAA/United States 4 OrgenuestemNsma MO MOMS

Awe Accessories, Inc.. 1240

3 rack Number 2 AUTHORIZED RELEASE ER1 F1CATE

Form

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Springwood Avenue • Glbsonville, 21

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N/A 1 (475:25-42 Overhauled

Overhauled & Tested in accordance with FAA approved data

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YEAR Alteration s • Number of cific entries.)

15,511PW 1771M GOSS OWN out:pony wen applica(5,e ORM. FAA ban 81303 4001)

Jev complete A/D Listing for airframe and accessories in A/D Compliance Section. Performed Operational and Run-up Checks with no defects noted.

— - I certify this aircraft has been inspected i/a/w an Annual Inspection and was determined to be in airworthy — -- - dition and , sr v e d for return to service.

—

es M. Cherry. ?...'.-- A&P 2700481 LA.

I I I

Vincent F Licolli

11/09/2009

Piper PA 23-250

27-7554035

N6OOMP

Hobbs 2475.8

Removed pilot's windshield hot plate. Installed patch to secure against moisture seepage

into airframe. Aircraft is not approved for flight into known icing conditions. Placard

affixed to control.

Aircraft has been repaired in accordance with current FAA Regulations and is approved for

return to service with respect to the work performed.

11_4 es M Che 700481 A&P

YEAR: RECORDING TODAYS TOTAL ...,

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

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TOTAL TIME IN

Description of Inspections, Tests, Repairs and Alterations

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 I

Vincent Licolli Piper PA 31-350 N6OOMP Hobbs 2476.6

01/25/2010 27-7554035 47810 TTAF

C/W AD 09-13-06, Nose Baggage Door and placard, daisy para (12. &

31 and SB I194A, part I & II (Part! due again 5783.0 TTAF, Part II due again 4883.0 TTAF)

!certify this aircraft has been inspected with respect to the work performed and was determined to be in

:.,

. rthAco 'on d is approved for return to service.

es M. Cite

A&P 2700481 LA.

Walt 614 tOv

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YEAR: Vincent Licolli 03/05/2010 Piper PA 23-250 27-7554035 N7OHH TTAF 4784.7 Hobbs 2478.9

DATE Performed an Annual/100 Hour Inspection Ua/w FAR Part 43 Appendix D. Inspected ELT i/a/w FAR 91.207(d)I-4. No defects noted. Battery replacement date 05/11. Serviced brake and hydraulic reservoirs with 5606 hydraulic fluid and replaced hydraulic filters with new p/n 751-759 elements and o-rings. No defects noted. Replaced vacuum filters with new RAB3-5-I Garter filter elements. Replaced left and right engine Brackett air filters with new 13A-3505 elements. Inspected battery box and cables for condition. Charged and serviced battery.

Completed gear swings verifying no leaks, proper actuating of doors and gear, and warning lights and horn. No defects noted.

Cleaned all fuel screens and replaced o-rings and inspected for leaks. No defects noted. Lubricated aircraft iialw lubrication guidelines Section II.

C/W A/D 03-14-03 , Rotary Fuel Pump Relief Valve Screws, left engine only, by torque inspection i/a/w AID paragraph (4). No defects noted. Due again 4834.7 TTAF.

C/W A/D 04-25-16R I , Janitrol Heater Regulator, by inspection Marked date and Hobbs time on regulator shroud body. Operational check of heater performed with no defects noted. Due again 4884.7 TTAF or

03/2011.

C/W A/D 08-14-07, Fuel Injector lines, left and right engines, by inspection i/a/w SB 342E. No defects noted. Due again 4884.7 TTAF, or when lines or clamps are disturbed. C/W all 1CAW's for supplemental installed equipment. Sec complete A/D Listing for airframe and accessories in A/D Compliance Section. Performed Operational and Run-up Checks with no defects noted.

1 I certify this aircraft has been inspected i/a/w an Annual Inspection and was determined lobe in airworthy

itixand ' approved for return to service. _

ames M. C A&P 2700481 I.A.

r -2= I ft"

and Alterations tificate Number of er specific entries.)

_____........ ....-. YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations 1 TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of


DATE —

6 -1 I-10 WO 9218 N600MP HOBBS 2509.8

— REMOVED CLEANED AND REINSTALLED RIGHT WING TIP FUEL TANK

._ CHECK VALVE. LEAK AND OPS CHECKS GOOD.

1 — MOUNTAIN VIEW AEROMOTIVE MARTIN LDEN

4 2501 STATE, ALAMOSA, CO. 719-589-9100 A&P 2825930

__

—

I I I

- 8-1-10 WO 9264 600MP HOBBS 2531.1

REPLACED STROBE LIGHT POWER PACK WITH NEW PN 01-0770028-05

PERFORMED RETRACTION CHECK AND SERVICED HYDRAULIC SYSTEM WITH MIL 5606 FLUID. ALL LEAK AND OPS CHECKS GOOD.

MOUNTAIN VIEW AEROMOT1VE MARTIN ' LDEN

2501 STATE, ALAMOSA, CO.

719-589-9100 A&P 2 30

TI

11111.11111111E YEAR RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations

TACH FLIGHT TIME IN 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 12-14-10 WO 9385 N600MP HettS 2574.6

REPLACED LEFT MAIN LANDING GEAR TIRE AND TUBE WITH NEW 700-6 FLIGHT CUSTOM III AND NEW GOODYEAR TUBE. SERVICED AS

-I REQUIRED. REPLACED ALL LEFT MAIN BRAKE LININGS WITH NEW

066-06200. OPS CHECKS GOOD.

MOUNTAIN VIEW AEROMOTIVE MARTIN OLDEN

2501 STATE, ALAMOSA, CO. --

719-589-9100 A&P 2 25930

=

YEAR: Tr.% Yr. ....WAAL - -

I WO 9481 N6OOMP TAO-1 2608.8 TTAF 4914.6 LT ENG SMOH 1519.4 LT PROP SM01-1 178.1 s RT ENG SMOH 1519.4 RT PROP SMOH 178.1 HEATER HOBBS 1244.6

OATE INSPECTED AIRCRAFT PER FAR 43 APPENDIX D C/W A/D'S 80-18-10 INSPECTED PER (b)(I)(2) 81-04-05 RI INSPECTED PER SB671, 88-21-07 RI INSPECTED PER (a), 09-13-06 INSPECTED PER — PART II SB NO. I194A, 04-21-05 INSPECTED PER PARA (f), 04-25-16 INSPECTED AND DATED — PER BULLETIN NO. A-107A, REPLACED BOTH ENGINE AIR FILTER ELEMENTS, REPLACED VAC AND GARTER FILTERS, CLEANED STALL WARN SWITCH LEAD ENDS, REPLACED — HEATER COMBUSTION PRESSURE SWITCH WITH NEW P/N 94E42-3S SWITCH, REPLACED 3 _ RIVETS ON RIGHT BOTTOM COWL FRONT LOWER FAIRING, REPLACED LEFT ENGINE NACELLE LEFT TOP NOSE BOWL HINGE, TIGHTENED RIGHT WING OUTBOARD TANK —

CHECK VALVE, REMOVED LEFT WING OUTBOARD FUEL TANK UPPER ACCESS PANEL AND _

REMOVED WRINKLES FROM TANK BLADDER AND REINSTALLED TANK PER MM, REPLACED LEFT WING OUTBOARD TANK FUEL CAP, REPLACED RT MLG TIRE AND BRAKE - PADS, REPLACED NOSE GEAR CENTER LINK BUSHINGS IN SCISSORS AND SHIMMED UPPER _ _

SUPPORT STEERING COLLAR, REPLACED ALL 0 RINGS IN HYDRAULIC SQUAT SWITCH. TIGHTENED ALL LANDING GEAR TRUNION HARDWARE ON BOTH MLG ASSEMBLIES, -

INSTALLED COTTER PIN ON LEFT LOWER PASSENGER BRAKE MASTER CYLINDER

RETAINING PIN, TIGHTENED AND SAFTIED ELEVATOR TRIM TAB JACKSCREW BELL CRANK HARDWARE, REPLACED ELT BATTERIES, NEXT DUE 4-2013, CHECKED ELT PER -

91.207d, ALL TEST RUNS AND OPS CHECKS OK. I CERTIFY THIS AIRCRAFT HAS BEEN

INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETRM1NED TO BE

IN AIRWORTHY CONDITION

MOUNTAIN VIEW AEROMOTIVE 2501 STATE, ALAMOSA, CO. VE COLMAN

- 719-589-9100 IA 3460205

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RECORIENZ TACH TIME

MAYS FLIGHT


Description of Inspections, Entries must be endorsed Technician or Repair

with Name, Facility. (See back

OVERHAULED WO# W011591.

WO# 36761.

MARTIN

Tests, Repairs and Alterations Rating and Certificate Number of

pages for other specific entries.)

10-21-11

REPLACED FROM AEROSPACE

WO 9623 N600MP HOBBS

RIGHT VOLTAGE ROTABLES

PERFORMED ENGINE FUEL BOOST

THE AVIATION ALL LEAK AND

VIEW AEROMOTIVE ALAMOSA, CO.

N6OOMP

BRAKE CYLINDER WITH MOUSE

AEROMOT1VE CO.

2761.8

REGULATOR WITH INC. SEE 8130-3 RUN AND SET VOLTAGE.

PUMP RIGHT SIDE GROUP INC. SEE 8130-3

OPS CHECKS GOOD.

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PN B-00286-1 REMOVED

- SN 39983. AND REPLACED UNIT FROM SN 110788.

WITH OVERHAULED

PN B8001-H

EN

_ MOUNTAIN 20I STATE, 719-589-9100 A&P 2825930

4-18-12 —

TURBO — _ __ MOUNTAIN

2501 — 719-589-9100

REPLACED

W/O 9746

ED RIGHT WASTEGATE

VIEW STATE. ALAMOSA,

k■

C > > X

0 RINGS AND SERVICED WITH MILK.

5606, LUBED RIGHT

VE COLMAN A&P 3460205

_ 1

. . _

YEAR: T. TIME i nvluei Technician or Repair Facility. (See back pages for other specific entries.)

DATE

8-14-12 WO 9808 N600MP TACH 2801.3 TT 5107.1 LT ENG SMOH 1711.9 LT PROP SMOH 370.6

RT ENG SMOH 1711.9 RT PROP SMOH 370.6 HEATER HOBBS 1277.7

INSPECTED AIRCRAFT PER FAR 43 APPENDIX D C/W AD 80-18-10 INSPECTED PER (bXIX2), AD 81-04-05 RI INSPECTED PER SB671, AD 88-21-07 RI INSPECTED PER (a), AD 03-09-13

- - REPLACED FLAP TORQUE TUBE WITH 104622-004 TUBE ASSY AD NO LONGER APPLIES, AD -- 09-13-06 INSPECTED PER PART II SB NO. I194A, AD 04-21-05 INSPECTED PER PARA (f), 04-25- 16 INSPECTED AND DATED PER BULLETIN NO. A-107A, REPLACED BOTH ENGINE AIR FILTER ELEMENTS, REPLACED VAC AND GARTER FILTERS, REPLACED MISC. RIVETS ON — LEFT AND RIGHT BOTTOM COWL LOWER FAIRINGS, REPLACED RIGHT WING STROBE BULB, REPLACED LEFT WING NAV BULB, REPLACED 0 RINGS ON RT MLG BRAKE CYLINDER, REPLACED NLG TRUNNION P/N 31768-03 S/N JTI4 FROM S&B INDUSTRIES, INC. — W/O 9527 DATED 1-8-09, REPLACED FUEL PRESSURE SOFT LINES IN BOTH ENGINE NACELLES, REPLACED P/N 491-973 OXYGEN FILL VALVE, REPLACED RIGHT ENGINE — MOTOR MOUNTS, TIGHTENED RUDDER BAR BEARING BLOCKS, REPLACED PARALLEL — WIRE BETWEEN VOLTAGE REGULATORS AND SET PARALLEL WITH BOTH ENGINES RUNNING, CHECKED ELT PER 91.207d, ALL TEST RUNS AND OPS CHECKS OK. I CERTIFY — THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETRMINED TO BE IN AIRWORTHY CONDITION

MOUNTAIN VIEW AEROM() I I VE - 2501 STATE, ALAMOSA, CO. ...- 11:, COLMAN 719-589-9100 IA 3460205

I I I I


BATE

• , , Depot Avionics, Inc. 15 Ji1 21 , 1.? . •

4 4

Airframe Entries

121 KT-76 Transponder Sensitivity test fails .. Removed KT- 76 after failed bench check Replaced with transponder on item #3 131 Replace transponder Installed serviceable TSO'd Bendix/King KT-76k sin 20027, Transponder, from ROI/30332 in the previous transponder location IAVV Bends/King IM p/n 006-00143-0007. rev 7, Jul/2002 Connected to existing Altitude encoder system and existing antenna System ops checked correctly with TR-220. ICA INFORMATION none given by the manufacture THEREFORE These units require no periodical maintenance as a condition for continued airworthiness Maintenance should be performed when the equipment no longer properly performs the function for which it is intended 1N&B change negligible. 141 61-Anneal Inspection . Removed and reinstalled altimeters #45181. C3503. and encoder #67413 after bench check Altimeter al static system tests required by FAR 91.411 were performed and comply with FAR 43 Appendix E. on N600MP Altimeters SIN 45181 & C3503 were tested to 20000 feet. ATC transponder tests required by FAR 91 413 were performed and comply with FM 43 Appendix F. on Model KT-76A with TR-220.... 15> #1 Corn transmit garbled.. Removed and re-installed KY-196. s/n 14585 after bench repair on R030303. System ops checked correctly.

DLTE 29 July 2013 SIGNED: Work Order 30322

Mark ,r Printed by EBis 3 (datcomedia. corm

5 iggl el? I 0 *

Depot Ayionics. Inc

11111111- , Aidnime Entries D

0 KT-76 Transponder Sensstmry test fads Removed K7 'ri Ott 5,, Wephoce transponder Installed sennceaNe TSO'd Bendw kpg K 1111billue transponder location lAVY Bendu/King IM pin 006-001434 swim and ensting organs System ops checked correctly *nth 1`,., 111/311EFORE - These unts regire no periodical maintenance as a , 2 pulimed Wien the equipment no longer properly performs the fun r--I Illasessf Inspection Removed and reinstalled altimeters 145181 Mille system tests required by FAR 91 411 were performed and co 4501A C3503 were tested to 20000 feet ATC transponder tests 43 pow* F, on Model KT-76A well TR-220 15)61 Corn trans( after bench repair on R030303 System ops checked correctly

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VIM IIEDNIONIC TOOATS TOTAL Description of Inspections, Tests, Repairs and Alterations

TAO MONT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of


•■•••

YEAR: RECORDING TODAYS TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN

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

Depot Avionics. Inc

Airframe Entries

(2) KT-76 Transponder Sensitivity test fails._ Removed KT-76 after failed bench check. Replaced with transponder on item #3.. (3) Replace transponder.. Installed serviceable TSO'd BendedKing KT-76A, sin 20027. Transponder, from RO#30332, in the previous transponder location JAW Bendix/1(ing IM p/n 006-00143-0007, rev 7, Jul/2002. Connected to existing Altitude encoder • system and existing antenna. System ops checked correctly with TR-220. ICA INFORMATION: none given by the manufacture THEREFORE , These units require no periodical maintenance as a condition for continued airworthiness Maintenance should be performed when the equipment no longer properly performs the function for which it is intended W8.8 change negligible., (4) Bi-Annual Inspection. Removed and reinstalled altimeters #45181 , C3503, and encoder #67413 after bench check Altimeter a static system tests required by FAR 91.411 were performed and comply with FAR 43. Appendix E. on N600MP. Altimeters SIN 45181 & C3503 were tested 10 20000 feet. ATC transponder tests required by FAR 91.413 were performed and comply with FAI 43, Appendix F. on Model KT-76A with TR-220.... (5) #1 Corn transmit garbled.... Removed and re-installed KY-196. sin 14585, -- after bench repair on R030303. System ops checked correctly.

—

DATE 29 July. 2013 SIGNED, Work Order 30322 _ _ _

Printed by EBis 3 (dateomedia.com )

rn .•<= I ,.̀f, I 0 I 0

01

8-1-13 WO 10074 N600MP HOBBS 2874.9 IT 5180.7 LT ENG SMOH 1785.5 LT PROP SMOH 444.2 YEAR

: RI ENG SMOH 1785.5 RT PROP SMOH 444.2 HEATER HOBBS 1306.2 --

S

INSPECTED AIRCRAFT PER FAR 43 APPENDIX D C/W AD80-18-10 INSPECTED PER (b)(1X2),

DATE

AD81-04-05 RI INSPECTED PER SB671, AD88-2 1-07 RI INSPECTED PER (a), AD09-13-06 INSPECTED PER PART II SB NO. I 194A, AD04-21-05 INSPECTED PER PARA (f), AD04-25-16

INSPECTED AND DATED PER BULLETIN NO. A-107A, AD04-21-05 PERFORMED PRESSURE —

DECAY TEST, HAS P/N 94E42 AIR PRESSURE SWITCH, REPLACED HEATER COMBUSTION AIR -- BLOWER MOTOR, REPLACED BOTH ENGINE AIR FILTER ELEMENTS, REPLACED VAC AND

GARTER FILTERS, ROTATED BOTH MLG TIRES, SEALED HOLES IN BOTH ENGINE NACELLE

FIREWALLS, ADJUSTED BOTH PROP DE ICE SLIP RING BRUSH ASSEMBLIES, REPLACED ELT — BATTERY, NEXT DUE REPLACEMENT SEPT 2015, WELDED CRACK ON ENTRANCE STEP,

INSTALLED BUSHING ON RIGHT ENGINE ALTERNATE AIR VALVE, CHECKED ELT PER 91.207d, ALL TEST RUNS AND OPS CHECKS OK. I CERTIFY THIS AIRCRAFT HAS BEEN _ INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETRMINED TO BE

IN AIRWORTHY CONDITION

MOUNTAIN VIEW AEROMOTIVE

2501 STATE, ALAMOSA, CO. STEVE COLMAN

719-589-9100 IA 3460205

12-23-14 WO 10452 N600MP HOBBS 2953.7 Ti' 5259.5 LT ENG SMOH 1864.3 LT PROP SMOH

--- 573.0 RT ENG SMOH 1864.3 RT PROP SMOH 523.0 HEATER HOBBS 1352.2 tions

'I' rof

INSPECTED AIRCRAFT PER FAR 43 APPENDIX D C/W AD 80-18-10 INSPECTED PER (b)( I X2), Ties.) AD 81-04-05 RI INSPECTED PER SB67 I, AD 88-21-07 RI INSPECTED PER (a), AD 09-13-06

DA INSPECTED PER PART II SB NO. I 194A, AD 04-25-16 INSPECTED AND DATED PER BULLETIN NO. A-I07A, REPLACED BOTH ENGINE AIR FILTER ELEMENTS, REPLACED VAC AND

- GARTER FILTERS, REPLACED LANDING LIGHT BULB, REPLACED LEFT ENGINE EGT PROBE, REPLACED OXYGEN BOTTLE P/N 800112-13 S/N M664096/951, CHECKED ELT PER 91.207d, ALL TEST RUNS AND OPS CHECKS OK. I CERTIFY THIS AIRCRAFT HAS BEEN INSPECTED IN

- - ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETRMINED TO BE IN

AIRWORTHY CONDITION

- MOUNTAIN VIEW AEROMOTIVE 2501 STATE, ALAMOSA, CO. VE COLMAN

IA 1.4A(I)(IS

R. 41 I It. 1 7s.

IIMIllihibApproving National Aviation .

FAA/UNITED STATES

Authonty/Country 1 Approving National Aviation 2

Authonty/Country

FAA/UNITED STATES AUTHORIZED RELEASE

FAA FORM 8130-3, AIRWORTHINESS CERTIFICATE

APPROVAL TAG

poirn iiscping NUrriper

35287

4 Organization Name and Address Aerospace Turbine Rotolo!. Inc.

3414 W 29th St South Wichita, KS 67217 US Ph, (316) 943-6100, Far (316) 943-2917

FAA Approval Holder NV2R045L

ern unction t • rt ` um.er tgl.rllty tl.uentdy

5 Work Oder. Contract or Invoice Number

W011591

coat : tc m , H

REGULATOR 550-390 13-00286-1 NIA 1 00 39983 OVERHAULED

13 REMARKS

Overhauled and certified IAW the documents listed Manual a LAMAR 170, ReVsion 0 SECTION 2, Rewsion Date 121111981

Full details of work performed held on work order

The work specified In Block 12/13 was performed In accordance with EASA-Pant 145 and with respect to the work. the aircraft component is Considered ready for release to service under EASA

Approval Certificate EASA 145 4033

14: Cartiairathe Marna Idaotrad abovatvaretraondsoturadin conformity Lou

0 Applovactdaiton daditind.we in $004141800 for oak operation.

014661463961NOCI 919461 data specified In Block 13

19 E 14 CFR 43.9 Return to Service E Other regulation specnied in Block

Codifies that unless otherwise specified in Block 13, the work identified in Block 12 and described In Block 13 was accomplished in accordance with Tide 14. Code of Federal Regulations, pad 43 and in respect to that work, the items are approved for return to sennce

It A.4la_ud85at0lr It. Appm411Authortunfon No: i 20. Atithonzed Signature

A-

21 Approval/Gerhficate No

NV2R(145L

: 2 Name (Typed or Printed) 23 Date (m/d/y)

JuV2212011 - NladdiCD/P0 m•Rirdid}' 18 Ora Onkthh.

Re vonsIbIllties User/Installer

J 15n12111,1, constiote authordy to install the part/component/assembly

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is Important to understand that tne existence

'here

the usellinstaiter work In accordance with the national regulattons of an ainfrodhiness authorry different than the airworthiness authonty of the country specified in Block 1 it is essential that

e aserAnstalLer ensures that hts/her airworthiness authority accepts partS/cornpOnents/assemblies from the ainvonhiness authentic( the country specified in Block I

In Bhocks 14 and 19 do not constitute installation certification In all cases aircrafr maintenance records must contain an installation cerfilication iSsueo In actaxuemx -----

by the user/installer before the aircraft May be flown.

data

1. Approving NitIlwol Ail.. Anttiority/Count,:

United States

A Organization Nome and Address)

AUTHORIZED RELEASE CERTIFICATE FAA Form 81311-3, AIRWORTHINESS APPROVAL TAG

3. Form Tree,lig Nuns,

S11109-9527

S & B Industries Inc. / 333 West 6160 South / Murray, Utah I 84107 a Dew

S. Work Order/Cootraelehmoice Number)

9527 I Des ription A Part Num 0 0. EII&lbltlly.• 10. 5wn119- 11 Stria Batch Nom ri 12 StatudWora

1 NLG Trunnion 31768-03 PA 23 I each . JT 14 inspect & repair 13. Remarks:

Inspect and repair JAW S & B proprietary data. SBI 131

14. Certifies Me items identified above Imre manufactured, conformity W

0 Approved design don wd um , • runWtIon for lafe II penal..

0 Non•approved design data specified le Block 13.

M. VA 14 FOR 4110 Retitle to Sere, 0 Other regulation tpecifted In 89.19 00

emit, 6.9 .93,,, otherwlw eptelfied In Bltfia U. Me smirk identMed la Bieck 12 and dearth., Rio. 13 el. accumplithed in amardance AIM 1111e 14. Code of

WW1, Reg Wel., part W and in respect to that nark the ltems we •ppreved for return lo sent,

. 13 Authorized Signature: 16, Approval/Authorization No.:

XXXXXXXXXXXXXXX

20. athortted Sigwiure:

fü (A) --r-•••• 21 Apprm HICertificsie No :

E5R142N

17, Nan, (Typed or Printed))

XXXXXXXXIOCXXXXXXXXXXXXXXX

M. Date (m/d/y):

XXXXXXXX XXXXXXX

11' 'ller int N m ITYPd oPr

Bruce W. Taft

13. Bate wed/yr

118/2009

III, important to understand that Me X.1PIICe of fhb, document abne duel not automatically constitute outhority to Install tho pamIcompunonlialstaubly.

Where the userfinslalkr performs work In accordance with tht national regulation , of on airworthIncsi authority different than the Mrstorth,ess author', of Me count, snrcfiled ...- Block 1,11 1. esmulad that iho user/Installer entures that 93/her airwurthInesii authority o‘reP. P6)1•WwWmentautscinblIes too, the 9 - • , of mem, op,::Muck 1.

Slatements to Bloc, 14 and 19 do not constitute Installs.. cm-Mee/ion, 1..11 toms, eirendl staintensni e records wtll contain an WWII:Won certilksMn issued, acciirdao.. 0s00n09 regulations lob. user/Installer before the aircraft may be Bonn.

FAA Form 01611-316-All •InstedIer must endsveclock lIhghhlllhV with 'malleable lo,lmlool dma

A:ZhagitiN,T.7cafi:ol: Itsr::::

[

IT ..org.nizmonN

2 AUTHORIZE]) RufASE CRE.RTIFIC THE AVIATI and Address:

6. Item: 7. Desert tion:

I PUMP

AA F IINESS APP VALTAG

ATE 3. For3m6T7ra6c1cling

5. Work OrderfC

nyeis

WM 8136.3, '

Number: 0 CROUP,

INC. 211 PROSPECT PARK, PE -

8. Part Number:

v tketiO Serial .

E CITY, 7 300.269

/Batch Number: 12

ii. 36761

OVERHAULED 110788

NISTRATION AND IS

8800141

, ) S REGULATIONS OF THE FEDERAL „. E WITH CURRENTwR. 36761 ., corumen

THE

13.Remarks: TIM ABOVE APPLIANCE WAS OVERHAULED AND

. IN I '

TO THAT WORK.

CesTED IN A... '" vial °leads held o

APPROVED FOR RETURN TO SERVICE. Manual: J-000096 Reasiona:111

ITE RESPECT idon Dateloe'

ART 145, AND W , WITH EASA P CERTIFIES NA [THE WORK SPECIFIED IN BLOCK 12/13 WAS CARRIED

Pf'DANCFOWMBER: EASA.145. 4208 13"03VAL N

C

OMPONENT IS CONSIDERED READY FOR RELEASE TO SERVICE DICBC(R

3UT

DERAL AVIATION ADM

t•INSTALEER MUST CROSS CI DICK ELIGIBILITY WITH APPLICABLE TECHN1Cilitt°"

—

LIFE LIMIT PARTS MUST BE ACCOMPANIED BY MAINTENANCE IIII, it HO INCL0171 ITOTAL TIN1E/TOTAL CYCLES

14.Certifies the items identified above were manufactured in conformity to:

0 Approved design data and are in a condition for safe operation.

Non-approved design data specified in Block 13.

14CFR 43.9 Return to Service El Other regulation specified in Block 13

Certifies that unless otherwise specified in block 13,160 work identified in Block IT and described in Block 13 was accomplished in accordance with Title 14, Code of Federal Regulations, part 43 and M respect to that work, the items are approved for

return to service.

IS. Authorized Signature:

VG0R7281.,

(Typed or Printed): 18. Date (m/d/y) ;lame (Typed or Printed):

23. Date (rtimmidd/yyyy)

:

Richard H. Hewitt 30N/2412011

Il ls important to understand :1611 the existence of this document alone dots not autoinan' 7 "'''''" — -

Where the user/installer performs work in accordance with the national regaled° of iniirooribiness authority different than the airworthiness authority of the country specified in

Block lit is essential that the user/installer ensures that his/her airworthiness no117ori9099'" parts/Components/assemblies from the airworthinesS authority of the country specified

in 11lockl.

111111

Slokin,ni , in Bli.ks 14 and 19 dO notc001lilUleirllollutiInterlifitltio0 In all nnnei atoll maintenance records must contain on intifflotion mill-motion issued in accordance with

national regulations by the 0er/installer before the aircraft may be flown.

THE FAA form 8130-3 and JAA Form One are equivalent. Othercmmtries such as Canada also have equivalent acceptable documents.

elnIn NON: 0052-00-012-9005

ii log the standard - aest-sales.com · i&j via (ion inc. date 3-19-2002 bra total time...

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