~fL~ - media.sandhills.com

AIRCRAFT RECORD - GENERAL INFORMATION

A, e /~/le.:roe -rN e " -r- 5,i\2. &:OZ O //- 7 MANUFACTURER ~fL~ __ fe,,-, ___ ____;cc..J._::::...-I ______ MODEL C 1 - v SERIAL .;;/' - ,o

REGISTRAT1ON NuMsER _ ___:__N_iS_:_:::3c..:.Z---=B:::__ ________ DATE MFG. Pee 0 , /C/CJZ ----=----f-1-----0_~-'--'---------

ENGINE(S) CURRENTLY INSTALLED.

MFG P1?1ur¢w J.117/VEY

fr,-1r-7<f MODEL _r_T_t,_A_Z____,'t' ____ _

F' f{:. D7 J

SERIAL PC£ 5 Oc$!.0-4- -.

MFG --------- MODEL ..c-;fJJ~'\.,__L_,6'----'---c=..-+/~S:~----- SERIAL JL.flL/'2-PROPELLER(S) CURRENTLY INSTALLED.

MFG /JAR.TZE:.LJ-

HUB MODEL HC.-8 :JrN-3 o BLADE MODEL T,02.02.N +4

MODEL 1-.,c- f33TN-3D/ r 102,e.,zN" -1- 4-•

SERIAL 8 ll L S034- SERIAL -----------SERIAL\:::'- 42-1 e :3 SERIAL 1:-14-21 B 7 SERIAL f/4Z.I 7 'l

BLADE MODEL ------ SERIAL ______ SERIAL ------- SERIAL ______ _

~ AiRcRAFT LOG

DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS

1El-2. TACH TODAYS TIME !N ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

F.eB~ 1.5 i .s- A'-A T-• "'~-- ._ - . •~•

Air Tractor, Inc. ~tion Fli;h;-i '-lll .t'Onn LW) Dared 'o/t?..fqoand

fnn .. .4 tn i.- ,. • -

Pilot Q ~ ,;( ~ . ., .

,.., ·- V .,,.y,.. f' _ _ t./- I 9 5"b6

DATE RECORDING

19q,z TACH TIME

F~G G::, -.~

1/-1-12 He

TODAYS FLIGHT

'I.C>

TOTAL TIME IN SERVICE

f~.s-

DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME, RATING ANO CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

,, ,, i

! ''

DATE

t9!j..z.. RECORDING

TACH TODAYS TIME FLIGHT


DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST SE ENDORSED WITH NAME, RATING ANO CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE SACK PAGES FOR OTHER SPECIFIC ENTRIES.)

. 355 PINSON DRIVE, CORPUS CHRISTI, TX 78406

y~ ~ -~RATIONS DATE RECORDING TOT.4

t-t-ts-9:l... NUMBER OF TACH TODAYS TIME FIC ENTRIES.) 19_ TIME FLIGHT SERVI

~ JJ";/w ~~~ .o.;~ o.r-~~ i~.

~ s.-rc,. ~i'\ 74:/;,<:'z s w. aiL .,< .. A-()-(, ~·

c:e.~ .JI v/ u) Q...,q_j_.\..;__,,_.~,,L ;1~~-/t-cl~ w .-~ - i) A o~~Q_ V ' Q,,;'.l.t),. f (,:,_{' I:::.

JI :2rJ/ e( cJ·L J:,6-~ f 1414 '°jo/J --t~~,e__ C - I i -~-,--~£ /1 uP,::J

-A+r~~J ~.,L ct 1 'i

1

--

DA TE RECORDING TACH TODAYS

19_ TIME FLIGHT


DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

DATE RECORDING TACH TODAYS

19_ TIME FLIGHT


nu


DATE

19_

Air Tractor S/N 502-0167

March 4,1996 Hobbs 1963.7

Replaced left and rt. inb. wing attach angles. Installed new rudder cables and tailwheel unlock cable.Replaced all main gear attach bolts,rt main tire,rt brake pads, and repainted both main gear legs. Weplaced tail spring and wheel bearings.Replaced left outboard elev.hinge bearing.Resealed rt fuel tank and replaced header tank quik drain.Replaced bad lamps,missing placards and seat covers.Replaced rt,windshield,flap switch,oil pressure gauge, and master relay.Aircraft treated with Corrosion X.

John Petter AP463944627

~~

---- --- -- - -----


19_ TIME FLIGHT

'' ! 1

~ ~-


DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS A ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CE

ND ALTERATIONS RTIFICATE NUMBER OF ER SPECIFIC ENTRIES.) MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR 0TH

- ~·----- - L_ - -- -- - -

AT-502 March 5, S/N 502-0167 N1532B Hobbs 19

Installed SatLoc GPS System per manufacturer's installation manual. See FAA Form 337 da~d Marc~95 for details. I~ .

Terry ieler AP452686050

- --·

--- ,·-- -

1996

63.7

DATE

~I

RECORDING TACH TODAYS TIME FLIGHT


DESCRIPTION OF IN ENTRIES MUST BE EN SPECTIONS, TESTS, REPAIR --~ECHANl~R ~PAIRD~~~~~II.:'ITH NAME, RATING ANSD ~~~IFIALTERATIONS ~ rc;.r:..i;~~ --~-~C_A_JE NUMBER OF

:IFIC ENTRIES.)

March 5,1996 Hobbs 1963.7 hrs. Air Tractor Inc.

S/N 502-0167 I certify that this Aircraft has been inspected in accordance with an Annual Inspection and was determined to be in an Airworthy Condition.

John Petter IA 463944627

~fi>~

DATE

199t

l/2-/t.

D~~ 19fl

RECORDING TACH TIME

TODAYS FLIGHT


--------

DESCRIPTION Of INSPECTIONS, TESTS, 1.tPA.11.5 A.ND A.l'UI.A.'t\()NS ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

1,tl

DATE RECORDING T(

TACH TODAYS Tl/ 19_ TIME FLIGHT SE

26 JAN 1998 AT-502 502-167

REPLACED TAIL SPRING & HARDWARE, ELEV AND RUDDER HORN BUSHINGS. COMPLIED WI

HOBBS 2700. 7 HRS. Nl532B ATOR STOP WASHERS, TH AIR TRACTOR

AND ELEVATOR HINGE SERVICE LETTER# 155. REPLACED RUDDER BEARINGS AS NECESSARY.

·26 JAN.1998 AT-502 502-167

MICHAE LHUDSON AP45577 2075

~ ~

HOBBS 2700. 7 HRS. N1532B

REPLACED SIDE DOOR WINDOWS AND INDUC TION FILTERS. ROGERD ALE HERING AP45306210

~~

DATE RECORDlt-TACH

19_ TIME

26 JAN.1998 AT-502 HOBBS 2700. 7 HRS. 502-167 N1532B REPLACED BOTH RUDDER CABLES, ALL AILERON STOP WASHERS, RIGHT RUDDER BALANCE CABLE, FORWARD BELLY SKIN, RIGHT MAIN TIRE, AND BOTH BRAKE DISKS, CLEANED, INSPECTED, AND REPACKED MAIN WHEEL BEARINGS. TORQUED MAIN GEAR AND AXLE BOLTS.

26 JAN.1998

MALCOM DINGES AP449913536 7?70-_(cc>m Q1,~.s

AT-502 HOBBS 2700.7 HRS. 502-167 N1523B REPLACED STALL WARNING SWITCH, RIGHT FLAP ACTUATOR ROD END BEARING, TURN COORDINATOR, RIGHT INBOARD FLAP HINGE BEARING, AND LEFT CENTER AILERON HINGE BEARING. COMPLIED WITH AIR TRACTOR LETTER# 106.

PHIL CROCKETT AP527800001 £~ p_#'d C )?Lft" /CW,'l

ALTERATIONS 'ICATE NUMBER OF SPECIFIC ENTRIES.)


19_ TIME FLIGHT

26 JAN.1998 AT-502 HOBBS 2700.7HRS. 502-167 Nl532B REPLACED TAIL WHEEL UNLOCK CABLE, LEFT OUTBOARD AILERON HINGE BEARING, LEFT OUTBOARD & MIDDLE FLAP HINGE BEARING, FUEL HEADER TANK, REAR SPAR BOLTS, I RIGHT WING LEADING EDGE SKIN, AND 3 RIBS.CHECKED CONTROL SURFACE TRAVELS.

TERRY KIELER o/.2686050 '

/~~

26 ,AN.1998 AT-502 HOBBS 2700.7 HRS. 502-0167 Nl532B REPLACED BOTH SEAT COVERS, MAIN GEAR SPRINGS,AND HARDWARE, TAIL WHEEL BEARINGS & RACES, TAIL WHEEL LOCKPIN, BUSHING, AND LOCKPIN SPRING.

EVERETT SHELTON

wl~

DATE RECORDING I ~!~~. L~~DE~':;T!~~ <?~_!NSPECTIO~~- TESTS, REPAIRS AND ALTERATIONS TAC ~---~•-·--~BER OF

19_ TIMI DATE 26 JAN.1998

NTRIES.)

HOBBS 2700. 7 HRS. MODEL# AT-502 TOTAL TIME 2700.7 HRS. SERIAL# 502-0167

REMOVED ALL PANELS AND INSPECTION PLATES. INSPECTED FUSELAGE & EMPENNAGE STRUCTURE, WINGS, ALL STABILIZERS, ALL CONTROL SURF ACES, FLIGHT & ENGINE CONTROLS, ELECTRICAL SYSTEM, INCLUDING INSTRUMENTS, SAFETY EQUIPMENT, AND FUEL SYSTEM INCLUDING ENGINE. THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND FOUND TO BE AIRWORHTY.

EVERETT SHELTON

c;;:::)J]l:k_


19_ TIME FLIGHT



-------------=gN~~DBID~ ----------"-- I !.,A-Ive A-VIA no ti I AVIATION

TREATMENT DATE AIRCRAFT SN OR N NUMBER

l certify that this aircraft has been treated with Corrosion X (Mil-CB 1309E) to stop and arrest corrosion. Treatment 1s effective for 18-24 months, based on environmental conditions. Re-treating is recommended when effectiveness ends - as deterined by either time or visual inspection.

A & P NUMBER

• . tATIONS DATE RECORDING

TACH , 7 DEC.1998

NUMBER OF

TIME FIC ENTRIES.) 19_ AT-502 HOBBS 3147.3 HRS. S # 502-0167 Nl532B REPLACED RIGHT WINDSHIELD, BOTH SEAT COVERS, MASTER RELAY, BOTH FLAP ROD END BEARINGS, LEFT OUTBOARD WING ATTACH ANGLE, ELEVATOR TRIM TAB BUSHINGS & BOLTS, ALL FLAP HINGE BEARINGS, LEFT AILERON INBOARD & OUTBOARD HINGE BEARINGS, TAIL WHEEL BEARINGS, TAIL WHEEL LOCK PIN & SPRING, TAIL WHEEL CENTERING SPRINGS, TAIL WHEEL UNLOCK CABLE, RIGHT OUTBOARD MAIN WHEEL BEARING & RACE, WING REAR SP AR BOLTS, AND TAIL GEAR BOLTS. SEALED RIGHT FUEL TANK.COMPLIED WITH AIR TRACTOR SERVICE LETTER# 165, WHICH IS A ALTERNATE METHOD OF COMPLIANCE FOR AD 96-23-19. REPLACED RUDDER HORN BUSHINGS AND RUDDER SERVO BUSHINGS & BOLTS. CLEANED, INSPECTED, AND REPACKED ALL WHEEL BEARINGS.

ROGER DALE HERING AP453062102

~lJcA.1~


19_ TIME FLIGHT

.

7 DEC 1998 AT-502 S # 502-0167

HOBBS 3147.3 HRS. Nl532B

REPLACED RUDDER NAV LIGHT, BOTH WING QUICK DRAINS, ALL ABLES, BOTH MAIN AILERON STOP WASHERS, BOTH RUDDER C D LEFT FUEL TANK GEAR TIRES, AND LEFT BRAKE PADS. SEALE

AND WINDSHIELDS.

_L -- --

7 DEC.1998 AT-502 S # 502-0167

MARK DANIELS AP4

m 93662790 ~

o-,l!::p~--.,.....c---- ------ --


REPLACED FUEL INDICATION SENDER IN RIG HT TANK. UGABSHIER DO

AP

~7~

u IER OF HRIES.)

7 DEC.1998 DATE RECORDING

AT-502 HOBBS 3147.3 HRS. ,TIONS TACH TC

19_ TIME FL S # 502-0167 N1532B NUMBER OF C ENTRIES.)

REPLACED ELEVATOR STOP WASHERS AND AIR SCOOP SCREEN. CLEANED OIL COOLER FACE.

EVERETT SHELTON

~Rb I I

-

7 DEC.1998 AT-502 HOBBS 3147.3 HRS. S # 502-0167 Nl532B REPLACED UPPER RUDDER PEDAL PIVOT BOLTS. COMPLIED WITH AIR TRACTOR SERVICE LETTER# 156 ON RIGHT RUDDER PEDAL.

TERRY KIELER

AP,268605~ ,,~ I I

DATE RECORDING

I TACH 19- TIME

!

..._

TODAYS

7D EC.1998 502 502-0167

AT-S#


FLIGHT REP LACED START CONTROL CABLE.

---- -- - _ _J_ --- --- -

DEC.7,199 AT-502

8

7 S # 502-016

MALCOM DINGES AP449913536

inakorn o,·~-s

ALL APPL ICABLE AD'S HA VE BEEN COMPLIED WITH ON THIS AIRCRAFT. REC URRING AD'S ARE LISTED BELOW.

EVERETT SHELTON

~8]LL

AD 84-26-0 2 DUE 3647.3 HRS. AD 96-18-1 4 DUE SEPT. 2005

'

ii ! I,

DATE

19_

RECORD DEC.7,1998 Nl532B 'IONS TACI HOBBS 3147.3 HRS. AT-502 UMBER OF TIMI TOT AL TIME 3147.3 HRS. 502-0167 ENTRIES.)

REMOVED ALL PANELS AND INSPECTION PLATES. INSPECTED FUSELAGE & EMPENNAGE STRUCTURE, WINGS, ALL STABILIZERS, ALL CONTROL SURF ACES, FLIGHT & ENGINE CONTROLS, ELECTRICAL SYSTEM, INCLUDING INSTRUMENTS, SAFETY EQUIPMENT, AND FUEL SYSTEM INCLUDING ENGINE. THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND FOUND TO BE AIRWORHTY.

EVERETT SHELTON

~8JIL_

DATE

19_

3 JAN.2000 AT-502 HOBBS 3619.1 HRS. S # 502-0167 N1532B REPLACED RIGHT OUTBOARD WING ATTACH ANGLE, ELEVATOR STOP WASHERS, AND RUDDER SERVO LINKAGE HARDWARE. REP AIRED RIGR( HORIZOlf.,Ah, STABILIZER STRUT ACCORDING TO FAA FORM 337 DATED THIS DATE. f;~ ~

TERRY l{IBLER AP452686050

- ---- -- _ _l

------+-- 3 JAN.2000 AT-502 HOBBS 3619.1 HRS.

----+- S # 502-0167 N1532B ----+- REPLACED SEAT BELT & SHOULDER HARNESS, LEFT NAV LIGHT, RIGHT TAXI LIGHT,

BOTH RUDDER CABLES, ENGINE ISOLATOR BOLTS, TAIL WHEEL LOCK PIN BUSHING, TAIL ----+- WHEEL TIRE, TAIL WHEEL UNLOCK CABLE, AND TAIL WHEEL AXLE. SEALED ----+- WINDSHIELD. INSTALLED AIR TRACTOR SERVICE LETTERS# 109 AND 114. CLEANED,

INSPECTED, AND REPACKED TAIL WHEEL BEARINGS. CHARLES JONES

APc7✓~-

•,

DATI

19_

3 JAN.2000 AT-502 HOBBS 3619.1 HRS. S # 502-0167 Nl532B ~ OF

REPLACED REVERSE CURRENT RELAY WITH OVERHAULED UNIT. UNIT OVERHAULED BY RIES.J

S & T AIRCRAFT ACCESSORIES, INC. UNDER WORK ORDER# 25634. SERVICED BATTERIES. CLEANED, INSPECTED,' AND REPACKED LEFT MAIN WHEEL BEARINGS.

3 JAN.2000

MALCOM DINGES AP449913536

maktJm L)J~s

AT-502 HOBBS 3619.1 HRS. S # 502-0167 N1532B REPLACED BACK SEAT COVER. REPLACED BOTH MASTER CYLINDERS ACCORDING TO AIR TRACTOR SERVICE LETTER# 166. REPLACED INDUCTION FILTERS, AND STICK YOKE BEARINGS, COCKPIT AILERON TORQUE TUBE REAR BUSHING. CLEANED, INSPECTED, AND REPACKED RIGHT MAIN WHEEL BEARINGS.

THOMAS PERRIGUE AP457637J42

"'1""Jv,,t,te,J fci1,-,':JvC

1: '" j! ""

l l11

i 'ji

,,, I,

DATE

19_

3 JAN.2000 RECOI A T-502 HOBBS 3619.1 HRS.

TA S Tl, # 502-0167 N1532B

REPLACED BOTH WING QUICK DRAINS, FUEL HEADER TANK, ELEVATOR TRIM TAB INKAGE BUSHINGS & BOLTS, REAR SPAR BOLTS, AND ALL TAIL GEAR BOLTS. L

_ ___l_______ t L

3 JAN.2000 HOBBS 3619.1 HRS. TOTAL TIME 3619.1 HRS.

ROGER DALE HERING

~~~ Nl532B AT-502 502-0167

REMOVED ALL PANELS AND INSPECTION PLATES. INSPECTED FUSELAGE & EMPENNAGE STRUCTURE, WINGS, ALL STABILIZERS, ALL CONTROL SURF ACES, FLIGHT & ENGINE CONTROLS, ELECTRICAL SYSTEM, INCLUDING INSTRUMENTS, SAFETY EQUIPMENT, AND FUEL SYSTEM INCLUDING ENGINE. __ _ THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND FOUND TO BE AlRWORHTY.

EVERETT SHELTON

~~

'1 i

'il 1

ii! 'lfi:

\

J

\ J

DATE RECO V

19- Tl

3 JAN.2000 lLTERATIONS

AT-502 HOBBS 3619.1 HRS CATE NUMBER OF

502-0167 N1532B SPECIFIC ENTRIES.)

ALL APPLICABLE AD'S HA VE BEEN COMPLIED WITH ON THIS AIRCRAFT. ' SEE AD COMPLIANCE REPORT.

EVERETT SHELTON AP383601081t.k.

~

I I I FEB 09, 01 Nl532B AT-502 HOBBS: 4126.7 HRS SIN 502-0167 T.T.: 4126.7 HRS

INSTALLED OVERHAULED ITT GUAGE 1N COCKPIT. PIN 159871 SIN AF-56276

~ ,?~ p...., e,. .-;_p e MAS PERRIGUE

AP 457637242 I I I

I I I


19- TIME FLIGHT

FEB 9, 2001 AT-5~ SIN 501:-0167



N1532B HOBBS: 4126.7 HRS T.T. 4126.7 HRS

RESEALED RH FUEL TANK TO STOP LEAK, CHANGED BOTH FRONT WRAP AROUND WINSHIELDS, AND FRONT GLASS WINSHIELD. REPLACED RIGHT HAND STROBE POWER SUPPLY, REPLACED BOTH RIGHT AND LEFT HAND RUDDER CABLES, INSTALLED NEW BATTERIES, REPLACED HOPPER LID GAS.KET, ADDED SIDMS TO CONTROL STICK AS NEEDED.

. 0~ r""~.5 (l.,,9,e_ ~~MAS PERRI6UE

AP 457637242

DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF

19_ TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

------ L .. - - -- - - - - - --- - -- - - ---- -- - - ----- ----

FEB 9, 2001 Nl532B ---J AT-502 HOBBS: 4126.7 HRS

SIN 502-0167 T.T. 4126.7 HRS ----

REPLACED ELEVATOR TRIM QUADROSTAT IN COCKPIT, REPLACED RIGHT HAND, AND TAIL NA V LIGHT BULBS, INSTALLED NEW BRAKE LININGS AS NEEDED ON BOTH RIGHT --AND LEFT HAND MAIN WHEELS, JNSTALLED ALL NEW MAIN GEAR BOLTS AND AXLE --BOLTS, TORQUED TO MANUFACTURES RECOMMENDED SPECS, ROTATFD LEFT HAND MAIN TIRE, REALIGNED BOTN MAIN GEAR TIRES.REPLACED ELEVATOR STOP WASHERS. --

rrltJJtdYL/),'n~ ----

MALCOM DINGES AP 449913536 --


19_ TIME FLIGHT

FEB 9, 2001 AT-502 SIN 502-0167


DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER Of MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES-)

N1532B HOBBS: 4126.7 HRS T.T. 4126.7 HRS

REPLACED LEFT HAND FLAP BEARING AND RIGHT HAND INBOARD FLAP BEARING, REPLACED RIGH HAND BALANCE CABLE, REPLACED FLAP MOTOR RUBBER COUPLING, CLEANED PRIMED AND PAINTED STABILIZER STRUTS. REPLACED AILERON STOP WASHERS, CLEANED AND PAINTED BOTH THE INSIDES OF THE BATTERY BOXES, REPLACED REAR SPAR BOLTS AND TORQUED TO MANUFACTURES RECOMMENDATIONS.

/;,,u,)1 g_;_, TERRY KIELER AP 452686050

l,il

DATE

19_

RECORDING TACH TIME

FEB 09, 01 AT-502

TODAYS FLIGHT

SIN 502-0167



Nl532B HOBBS: 4126.7 HRS. TOTAL TIME: 4126.7 HRS

-- !

ALL APPICABLE AD'S HA VE BEEN COMPLIED WITH ON THIS AIRCRAFT.

SEE AD COMPLIANCE SHEET. / _L_ # ,a • ~-·~ .L A If .£7; t:il, 7t:> rJ..S?

iii '!,


19_ TIME FLIGHT


DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.) __ __,...,.,........., .......................... _-____ ..... _________________________ ~--- - -

FEB09, 01 AT-502 SIN 502- 0167

N1532B HOBBS: 4126.7 HRS. TOTAL TIME: 4126.7 HRS

THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND FOUND TO BE AIRWORTHY.

D.AI~ _k~lhll:. [ ~ ~ ~ APRIL 5, 2001

~ AT502 502-0167

__ [ _ Y~TAL _L -- ---~-~~-----------~~------~!EPAIRS AND ALTERATIONS

HOBBS 4169.5 HRS lG ANO CERTIFICATE NUMBER OF NlSJ2B :S FOR OTHER SPECIFIC ENTRIES.)

PERFORMED SERVICE LEITER 206. WING CENTER SPLICE CONNECTION HAS BEEN INSPECTED IN ACCORDANCE WITH SNOW

- ENGINEERING PROCESS SPECIFICATION PS 197 AND FOUND TO BE _ FREE OF CRACKS. NEXT INSPECTION DUE ~T 4569.5 HRS ~~URS.

_ ~ff};kc;mfl)lil/n.<2. MALCOM DING-is -AP 449913536

I;

i I


19_ TIME FLIGHT



JUNE sm, 2001 AT-502 SIN 502-0167

N1532B HOBBS: 4248.4 HRS

AIR TRACTOR SERVICE LETIER #197 HAS BEEN COMPLIED WITH BY INSTALLATION OF PART NUMBER 20988-1 PLATE, AND PART NUMBER 20983-1 &-2 LOWER SP AR SPLICE BLOCKS ACCORDING TO DRAWING NUMBER 20989. THIS MODIFICATION TERMINATES THE INSPECTION REQUIREMENTS OF SERVICE LETTER#l79.

11Jda,m!J' MALCOMDINGES ~ AP 449913536

,11

DATE RECO!r'-''.._l__ - _ _J --~"P ... l - I -- - --- l!!II..LL~l"I...I.ft.Yl..ft..A..l..__~....l.~YJ~ T.lt£..T:L .ll.I.B.A..UtC _A..Mft AJ.,TERATIONS TAI

LANE AVIATION, INC. , TE NUMBER OF

19_ w AIRFRAME LOG ECIFIC ENTRIES.)

REG#: N1532B DATE: FEB22 2002 MODEL: AT-502

S/N: 502-0167 A/CTT: 4550.4HRS HOBBS: 4550.4 HRS

REMOVED ALL PANELS AND INSPECTION PLATES, INSPECTED FUSELAGE & EMPENNAGE STRUCTURES, WINGS, AND STABILIZERS, INSPECTED ALL FLIGHT CONTROL SURFACES, ELECTRICAL SYSTEMS, INCLUDING INSTRUMENTS, SAFETY EQUIPMENT, AND FUEL SYSTEMS. REPLACED BOTH SIDE WINDOWS AND BOTH DOOR TINTED WINDOWS

SERVICED BRAKE RESERVOIR, REPLACED LEFT HAND FUEL SENDING UNIT WITH NEW SENDER, REPLACED PUSH TO TEST BUTTON FOR CHIP DETECTOR, REPLACED BOTH RUDDER CABLES, REPLACED

TAILWHEEL UNLOCK CABLE, ~CED A.U. BOLTS IN TAILWHEEL, AND REPLACED TAILWHEEL TIRE, REPLACED ALL BRAKE PADS,

AND RIGHT HAND MAIN TIRE.

PATRICK KLECKA ~Md~ AP 453533063



DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.) 19_ TIME FLIGHT

LANE AVIATION, INC. AIRFRAME LOG ENTRY REG#:

5/N:

N1532B

502.{)167

DATE:

A/CTT:

FEB22 2002

4550.4 HRS

MODEL:

HOBBS:

THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDINANCE WITH AN ANNUAL INSPECTION AND FOUND TO BE AIRWORTHY.

NO APPLICAB E Q000UGH Bl-WEEKLY 2002-02.

ENPSENCI~ IA 459270259

AT-502

4550.4HRS

DATE

19_ LANE AVIATION, INC. AIRFRAME LOG

REG#: N1632B DATE : MARCH 1 2003 MODEL : AT-602 S/N : 502-0167 HOBBS: 4873.6 HRS

REMOVED ALL PANELS AND INSPECTION PLATES, INSPECTED FUSELAGE & EMPENNAGE STRUCTURES, WINGS, AND STABILIZERS, INSPECTED ALL FLIGHT CONTROL SURFACES, ELECTRICAL SYSTEMS, INCLUDING INSTRUMENTS, SAFETY EQUIPMENT, AND FUEL SYSTEMS. REPLACED RIGHT HAND FRONT WINDSHIELD, FILLED BRAKE RESERVOIR, REPLACED RH QUICK DRAIN, REPLACED WORN AILERON HINGE BEARINGS, REPLACED REAR SPAR BOLTS, REPLACED BOTH RUDDER CABLES, REPLACED AFT BELLY SKIN, REPLACED RUDDER HORN BUSHINGS, REPLACED ON TAILWHEEL: HOUSING BUSHINGS, ALL BOLTS, AND BRASS PLATE. REPLACED BOTH RIGHT AND LEFT HAND MAIN TIRES, REPACKED MAIN GEAR BEARINGS, AND CHANGED RIGHT AND LEFT HAND BRAKE PADS, REPLACED HOPPER LID GASKET, TAILWHEEL UNLOCK CABLE, FRESH AIR DUCT, PEDESTAL BEARING, AND REPLACED SPRAY VALVE BOTTOM BELLY BOOT.

~&JI-_ STEVEN BRITTON AP 463775000

OF ES.)

I.,,

'

; I 111 1·

. ' ' '


19_ TIME FLIGHT



LANE AVIATION, INC. AIRFRAME LOG

REG#: SIN:

N16328 6028~167

DATE: A/CTT:

MARCH 1 2003 MODEL : 4873.6 HRS HOBBS :

AT~028 4873.6HRS

IN ACCORDANCE WITH AD 2002-26~6, THE LOWER WING SPAR CAP IS LIFE LIMITED TO 1650 HRS TIS. THIS WING CENTER SPLICE CONNECTION HAS BEEN

INSPECTED IN ACCORDANCE WITH SNOW ENGINEERING PROCESS SPECIFICATION PS197. AT THIS TIME NO CRACKS WERE FOUND. THIS AIRCRAFT IS OK TO RETURN

TO SERVICE. ~

Tfh1@m MALCOM DINGES AP 449913636

,di


19_ TIME FLIGHT



LANE AVIATION, INC. AIRFRAME LOG ENTRY REG#:

S/N:

N1632B

602-0167

DATE:

A/CTT:

MARCH 1 2003 MODEL :

4873.6 HRS HOBBS :

AT-102

4873.6 HRS

THIS AIRFRAME HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND FOUND TO RWORT~ll'Pll'I.ICABLE AD'S DUE THROUGH Bl-WEEKLY 2003-03

LISTEDB AD~ CKS FROM OCCURRING IN THE LOWER SPAR CAP. ,,


19_ TIME FLIGHT



______ LANE AVIATION, INC. AIRFRAME LOG

----+-----+---REGt:

SIN: N1532B 502-0167

DATE: HOBBS:

JAN 132005 5659.5 HRS

MODEL: AT-502

----1------+-- INSPECTED AIRFRAME FOR ANY PROBLEMS THAT MAY BE PRESENT, CHECKED FUEL FOR WATER, AND DEBRIS, REPLACED FIREWALL FUEL FILTER, AND INDUCTION

----1------+-- FILTERS

JI.- ,..,,,;:>r,-r ,11"-<"" THOMAS PERRrGuE AP 457&37243

---05-17-05 DATE

19-

Hobbs 5562.3 TTAF5562.3

AT502 #0167 N1532B

PT6A-15AG PCE-14142

Performed annual inspection on this airframe in accordance with FAR 43 appendix D. Removed all inspection panels and cowlings, and cleaned & treated crossion. Checked all controls,

---control bearing, cables, and pulleys. Changed rudder cables, cable pulleys, and tail wheel lock ___ cables. Removed all controls, and stabilizers. Replaced all worn, and froze up bearings, and rod

ends with new ones. Complied with SL 195A (see 337 dated 15 Feb. 05) which will permanently --- comply with AD 2004-15-15 .Reinstalled all controls, and stabilizers with new hardware. Removed ___ tail wheel and spring; cleaned, painted, and reinstalled with new hardware in the spring, and clamp.

Also installed new bolts in tail wheel housing, and replaced tail wheel bearings. Cleaned and lubed --- all wheel bearings. Checked all main gear bolts, and installed new brake pads to the right main gear. ___ Replaced all bad, and frozen bearings, and rod ends with new ones. Eddy current was preformed at

this time to extend the safe life of the wing lower spar cap under AMOC to 8,000 hrs .. Next eddy current inspection is due at Hobbs 63623(See a copy of the AMOC in the records). All AD's

___ checked complied with through I May, 05. I certify this airframe was inspected in accordance

With an annual inspection, and was found to be in Satisfactory conditio r return to service.

26284

RATIONS : NUMBER OF IFIC ENTRIES.)

RECORDING TACH TODAYS TIME FLIGHT

S'f .z.11'.?



DATE

2ff7 RECORDING

TACH TODAYS TIME FLIGHT


/'Jl5IZ 6 DATE

19_

--

RECORDING TOTAL DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME, RA TING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

-- - - - - - - - - - -- - - - --- -- -- --

~ ------ -

Date:IO/.Jufe 7 AT- 5oz. S/N5oz- C>lt..'1 N 1532.B AFTT ~,;7.;J.~. i Following AD 2006-24-10, at tz Z 0, I hrs TIS an Eddy current inspection has been performed IA W Snow Engineering Process Specification 197, page 1, revised June 04, 2002; pages 2 through 5, revised May 03, 2002, with no cracks detected at this time. As of now the safe life listed in the AD no longer applies to this aircraft. This Aircraft must be Eddy current inspected at intervals not to exceed 8a;:) hrs TIS. The first of thest inspections is due at O Z.l:, • ' rs TIS. In espect to the work listed above, this aircraft is approved for return to service. M A&P3061908

DATE

19_

TOTAL HME IN SERVICE

REFERENCf OF MAJOR REPAIRS AND MAJOR ALTERATIONS TO FAA FORM ACA-337 BY DATE, OR TO THE WORK ORDER BY NUMBER AND THE APPROVING AGENCY.

rtA-1.rllG .1

DATE TOTAL TIME IN SERVICE

REFERENCE OF MAJOR REPAIRS AND MAJOR ALTERATIONS TO FAA FORM ACA-337 BY DATE, OR TO THE WORK ORDER BY NUMBER AND THE APPROVING AGENCY.

Date: 4-1-08

Tach: 6307.6

Comments:

Enter Comments Here.

Aircraft # N 15238

Total Time: 6307.6

Serial# 502-0167

SMOH:

inspected this airframe in accordance with FAR 43 appendix D. Checked all AD's complied with to this date using Zook's disc 2007-12D. AD 06-23-14 PCW (SL# 247 done 3-30-06 see 337 this date). AD 06-24-10 eddy current inspection done at 6226.1 TIS due next at 7026.1 TIS.

I certify this airframe was inspected in accordance with an annual inspection and was found to be in satisfactory condition for return to service.

Miche~I BryaP--:J

Al:;:;~~

- ~ - -DATE TOTAL A. D.

AIRWORTHINESS DIRECTIVIS ,. ·:?_J"),.g.. 7.T ~ NUMBER TIME IN 19_ SERVICE CHRONOLOGICAL LISTING OF COMPLIANCE AND METHOD OF COMPLIANCE. .$?/D • :l

FROST FLYING MAINTENANCE, INC. Marianna, AR 72360 Phone: (870) 295-3776

Date: 22 SEPT 2008 N#:1532B Hobbs: 12.4 Model: AT-502 S/N#:502-167 TT: t.sz42-0 ·¢ REPAIRED R/H WING AFTER WIRE STRIKE, SEE FAA FORM 337 THIS DATE FOR DETAILS. REPLACED ',

, ELEVATOR AND AILERON BUMPER STOPS. REPLACED BOTH CURVED GLASSESS. REPLACED ELEV ATOR i

PUSHROD BEARING. REPLACED RUDDER RETURN SPRINGS. REPAIRED CRACK IN MID BELLY SKIN. ' REPLACED ROD END ON DRY HANDLE ROD. REPLACED ROD ENDS AND BUSHINGS AS NEEDED ON WET i

HANDLE. REPLACED 4 ELEVATOR HINGE POINTS. TORQUED TAIL GEAR AND HOUSING AND SAFTIED. REPLACED L/H STEP AND HARDWARE. REPLACED R/H MASTER CYLINDER AND BLED. REPLACED WIPER ARM AND STOP. REPLACED MAIN LANDING GEAR AND HARDWARE. ALIGNED GEAR. REPLACED ALL 4 WING ATTACH ANGLES AND HARDWARE. REPLACED RIVITS AND HARDWARE ON UPPER RUDDER HINGE POINT (S/L). ALL WORK PERFORMED IA W MANUFACTURES MAINTENANCE MANUAL.

I CERTIFY THAT THIS AIRCRAFT IS APPROVED FOR RETURN TO SERVICE FOR WORK PERFORMED. rr---..

Signature: ~)~ CLAY EDGIN 526395114 A&P = ,.

I I

.. I

:ij

iii,

16 Feb 2009 N1532B S/N502-0167 Hobbs 0031.3 T.T.A.F. 6438.9 - ) PWC_PT6A-15AG S/NPCE-14142 T.T.8055.7 - ~ Hartzell HC-B3TN-3D S/N BUA29813 876.6 since new hub _ ~· Completed annual inspection IAW 14CFR43apdxD and AT owners' manual dated 21 Dec 2007. ~ Eddy current insp on wings done 22 Sept. 2008 per 337@ T.T. 6420 ref. AD 06-24-10 dated 01/08/07.

- e ~ This aircraft complies with wing life extension per AMOC. Next insp. Due @ 7238. 9 T. T .A. F. Comp · with AD 08-11-17 dated 07/07/08 by installation of SIL#97 skid plate brackets. Controls checked and

- lubed as required. Serviced batteries. I certify that this aircraft has been inspected and has been _ found to be in airworthy condition. ~ /J' r _ ~ 2,1' J? 22 t( /l/µ 7'f1

DATE TOTAL TIME IN MANUFACTURERS MANDATORY SERVICE llULLETINS

111fi="'=====~===============,...,,,,===--======--==""'===='=""'=====~--FROST FLYING MAINTENANCE, INC. Marianna, AR 72360

Date: 30 JUNE 2009 Model: PT6A-15AG

Phone: (870 295-3776

N1532B Hobbs: 357 .2 SIN#: PCE-14142

C/W 300 HOUR INSPECTION. REMOVED & FLOW CHECKED FUEL NoizLES. CHECKED MAIN OIL STRAINER. NO METAL NOTED. REMOVED MAIN FUEL INLET SCREEN, CLEANED & REINSTALLED. REPLACED MAIN FUEL OUTLET FILTER. CLEANED FIREWALL FILTER. CHECKED IGNITORS. CHECKED CHIP DETECTOR. NO METAL NOTED. REPLACED AIR FILTERS. REPLACED BETA BLOCK. CHECKED BATTERIES.

- LUBED ALL CONTROLS & LINKAGES. GROUND RUN & LEAK CHECK PERFORMED. GROUND RUN SATISFACTORY & NO LEAKS NOTED. ALL WORK PERFORMED IN ACCORDANCE WITH MANUFACTURE'S MAINTENANCE MANUAL.

I Certify this engine has been inspected in accordance with a 300 hour Inspection and is found to be in an airworthy condition for work performed.

Ii I

' I

DATE

19_

TOTAL TIME IN SERVICE EMPTY WEIGHT

CURRENT WEIGHT AND BALANCE INFORMATION

EMPTY C. G. USEFUL LOAD REMARKS

8 Dec 2009 N1532B ATS02-0167 Hobbs 569.0 T.T.a.f. Season starts 157 Season flights1290 PWC PT6A-15AG s/n 14142 Hartzell HC-B3TN-3D sin BUA29813 TT- &f76, i,,

Completed annual insp. IAW 14 CFR43 apdx d and manufactures owners manual. No new ad's this event. AD 06-24-10 dated 01/08/07 due each 800 hrs w/262.3 hours remaining. Replaced tai gear bolts as needed. Serviced bearings as needed. R/R starter generator for scheduled mainte Lubed controles as needed. Serviced batteries. Serviced brake fluid. Serviced firewall fuel filter and cleaned air inlet filters. Ground run and leak checked sat. I c~rtify that this aircraft has been inspected and has been found to be in airworthy condition. ZIL ¼ I, .-: 11 o 2 oz ·n;y I// ' 10 May 2010 N1S32B Hobbs 716.4

.,, Performed general 100 hr. line services and engine air inlet and firewall fuel filter changes. Serviced batteries. Lubed hinges, bearings and control rod ends and T/W spindle and axel bearings. Complied with the following AD's: 04-15-15 dated 07 Sept 2004 due each 100 hrs by insp. of aft tubing;

;,:t --~-06-23-14 dated 21 Dec 2006 due each 100 hrs by insp. of rudder hinge; 09-11-05 dated 0 1 June 2009 due each 100 hrs by insp. of engine mounts. ,,

Replaced rivets in out board left elevator .. h. i~rac~ound .. run and leak checked sat. Airworthy. Robert Craig '12.J, -,j. • 'f 283~224A/P

FROST FLYING MAINTENANCE, INC. Marianna, AR 72360 Phone: (870) 295-3776 i

Date: 18 MAY 2010 Nl532B Hobbs: 764.6 Model: AT-502 SIN#: 502-0167 TTAF: 7172.2 I

PERFORMED EDDY CURRENT INSPECTION IA WAD 2006-24-10, S/L 205 AND USING P/S 197, NO CRACKS NOTED. ~ NEXT INSPECTION DUE AT 7972.2 HRS TT. WING SAFE LIFE IS 8000 HRS TTIS.

' , THIS AIRCRAFT AP~OVED&OR RETURN TO SERVICE FOR WORK PERFORMED. I

Signature: ~~-~'\ CLAY EDGIN 526395114 A&P~ u AOQITIOn QT ....,-pliUil'-il .;'1..,'r''" .. '""

D Removal of Optional Equipment

D Addition of Required-Exchanged for Optional

D Removal of Required-Exchanged for Optional

D Addition of Optional Equipment




D Addition of Optional Equipment




15 Feb 2011 Nl532B Hobbs 1135.6 T.T.A.F. 7543.2 AT502 SIN 502-0167

- PT6A-l5AG SIN PCE-14142 T.T.I.S. 9160.0 Since HSI 0.0 DATE Hartzell HC-B3TN-3D SIN BUA298l3 SMOH =0.0 l980.9hrs on Hub

r 19-Pilot records 108 season starts 890 season flights.

I - Completed annual insp. IA W l 4CFR43apdxD and AT owners' manual and various Equipment

ICA's as contained in 337 record. Removed tail group and dressed and painted as needed horizontal stabs an~ "v" braces per Sherwin Williams Aerospace coatings epoxy corrosion resistant primer and Airtech poly-urethane practices. Refit tail group Equipment

with new hardware as needed. Installed new T/W lock cable. Installed new rudder cables w/fore/aft attach bolts and cotterpins. Installed new engine air inlet filters. Installed new airframe batteries. Removed propeller for routine maint. and refit same unit in 0/H condition. (ref. Memphis Prop. WO# 18299.) Replace right aileron/flap

Equipment

connect rod end bearing. Owner installed various minour panelling patches. Removed starter/generator for routine maint. and refit same unit (ref. Memphis Prop. invoice) Removed fuel tank covers as needed and resealed L/R tanks as needed. Complied with the following AD's----------------------------------------------------------------

Equipment

09-11-05 dated O l June 2009 due each 100hr by insp. of engine mount frame welds.

Equipment

AD 06-24-10 dated 01/08/07 eddycurrent insp. has 429hrs remaining and the wing

Exchanged for Optio

spar retirement has 456.8 hrs remaining. Equipment

Pilot ground run and leak checked sat. 580*C ITT start.temp. I certify that this

t arrcraft has been inspected and ~und to be in ah-worthy condition.

Equipment

'

'

-Exchanged for Optio

,,. '

. · 1/),~ l1f'P37.J-2_tj ~·

' - J

11!1

!·•·

Reg. No. :Nl532B Model:AT-502

S/N:502-0167

DATE:1/24/12 Hobbs Time:1656.8

TOTAL TIME:7998.9

-~-The foiowing repairs were completed to Air Tractor ModelAT-5025/N 502-0167, N1532B on 1/24/12. Hobbs ------meter: 1656.8 Total Time 7998.9 hours in service. Repaired/modified wings per SL 80OD inboard spar structure replacement and drawing 20989. Installed new P/N 21058-1/-2 lower spar caps. Lower spar cap SIN for L/H 4810 and R/H 4832 paired with blocks S/N 7111-11. Spar cap and blocks have been line reamed and cold worked per PS205. Lower spar cap safe life is 9800 hours.

_ Installed new 20988-2 fail safe plate. Repaired 20106 and 20107 ribs per SK547. Repaired nose ribs. Repaired fuel tank lid doublers as required. Replaced #1 & #2 leading edges, bearings, and fuel tank placards on both

_ wings. Replaced 70109-1 and 70109-7 rudder pedal mounts. Repaired mounts on air craft for rudder pedals. lnsalled new aft & mid belly skins. C/W SIL 195 pedestal.lnsalled r/h step and I/h strut repaired strut mount on I/h

_ and r/h sides.Replaced side skins as asked see parts sht. Replaced aft deck skin.dust cover.fit windshield to hopper. Installed new header tank. Installed refurbed hopper. Repaired R/H & L/H stabilizers. Repainted wings,

_ wing tips, ailerons, and flaps. Weighed airplane, weight and balance revised this date, see AFM.

_ All work cited above was repaired and inspected according to the current FAR's, approved drawings and process ______ _ specifications. The work cited above is approved for return to service. Details of this repair/alteration are on file

_ at this repair station under Work Order # 11-2338.

Date 1/4¢:i-Tractor, Inc. - Municipal Airport - Olney, TX 76374

940-564-5616 Fax: 940-564-5612 FAA Certified Repair Station AXTR327C

_...

i "-r,\if t

··, '

l

Minuteman Air Service1

Inc. (5Ml)1 DeWitt1

AR 72042 870-946-0390

01 March 2012 N15328 AT502S/N0167 Hobbs 1689.1 T.T.A.F.8031.2 Starts 143 Flts 1171 PT6-15AG SIN PCE-14142 T.T.I.S 9648.0 T.S.hot 488.0 Hartzell HC-B3TN-3D S:'N BUA29813 S.M.O/H 488.0 (Feb 2011 O/H) Completed annual insp. IAW 14CFR 43apdx D and AT owners' manual and the ICA's per the 337's recorded. Removed non-approved equipment as needed. Complied with the following AD listing----------------------------AD 09-11-05 dated 01 June 2009 par (e) (2) (i, ii) due each l00hrs by inspection of gusset upgrade. New engine air inlet filters installed. Serviced airframe fuel filter and batteries. Removed, cleaned and inspected Starter Generator. Brushes are @ ½ life limit and blew carbon dust from unit and refit with lubed splines. Serviced bearings as needed. Ground run and leak checked sat. I certify that this aircraft has been inspected and

has been fo"nd to b, in airworthy condition. ~Ii. _ :;J/".J / ~ ~ fl#,r;,e

--

i.1111,r,h -t•,i_ 1J1~J2.a 1rso1.-,1•1 Jl.411 n1.1..1 Ti,,J,. /1.,J IU-W (,) ,tJ.7.177&-.. Pl' b,-.·n1s 1r1 ¼ IJf.u.f lrJ.t. ,J..py. w 1J!t.,J. ~.,~lfltt wrel ,ti,.( Jl.s,,ol, f4uJ, ~.I I.di lrJc ~I fet/t.l ftt/J

AJu,..6/ k)tll. ,,.., kJ-1 Mlf/. W,1. ~ ;.,1:,7UI/ A,,. ____ _

~~~ ------- ----~-- - --

Minuteman Air Service. Inc. (5M1)1 DeWitt, AR 72042 870-946-0390

08 May 2012 Nl532B Hobbs 1828.4 T.T.A.F. 8170.5 AT502-0167 Completed 100hr insp. IA W 14CFR43apdx D. Lubed bearings. Installed owner's spare wheel and brake assembly. Service airframe and engine fuel and air filters. Serviced batteries. Complied with AD 09-11-05 dated 0 1 June 2009 par ( e) (2) (i.ii) due each 1 00hrs by insp. of engine mount. Lubed generator splines. Lubed and dressed prop blades. Ground run and leak checked sat. I certify that this aircraft has been inspected and has been found to be in airworthy condition. -~ ~ .:J.~3ll..~111/1

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