Aircraft Record General Informatiofl

Manufacturer Pi ~ MOdel---EO-n~Jy9----O---_ _~ _ ____

Serial 3~ - I 7 Registration Number N j 7 3 )-=-_ _ _~ _

_ l cl ( lt1Date of M anufacture

Engine(s) currently insialled

ManufacturerL_y_co ~pound~ Model -i- - j 3 ltto e- Serial ____

Manufacturer b ysD VVl J )-S Model - t) f0 -I IJ5 Serial _L - f5-J_~F Lj()

Propeller(s) currently installed

Manufacturer gtlllB J 21-LL HUB Model j J vV

Blade Model ~~_84 711 - d-Serial

Serial

11 W --l3

Model _Ifc - C J Y IL J S i L _ Serial

9 S Serial j lf39 e

IIJ L

Serial

Blade Model Serial Serial Serial

tb 1992 ASA

11111

III

DATE TOTAL TIME IN

19__ I SERVICE

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Current Weight and Balance Information

Empty Weight EmptyCG Useful Load Remarks

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DATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE19~ I~Technician or Repair Facility (See back pages for other specific entries)

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lATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of

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

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DATE

19J2 RECORDING ITO DAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certif icate Number of TIME SERVICE Technician or Repair Facility (See back pages for other specific entries)

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

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RO r ESTING SERV I CES CRS A78 R4S5J

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11111

III

DATE TOTAL TIME IN

19__ I SERVICE

a~~-7~6_5() middot 8

Current Weight and Balance Information

Empty Weight EmptyCG Useful Load Remarks

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DATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of TIME SERVICE19~ I~Technician or Repair Facility (See back pages for other specific entries)

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lATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of

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

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19J2 RECORDING ITO DAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certif icate Number of TIME SERVICE Technician or Repair Facility (See back pages for other specific entries)

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prrsCftl~ - IJ-yS II eer t i fy that~Mlt Transponaer

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

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lATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of

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

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DATE

19J2 RECORDING ITO DAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certif icate Number of TIME SERVICE Technician or Repair Facility (See back pages for other specific entries)

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II ATE RECORDING ITODAYS TACH FLIGHT

19 TIME

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

prrsCftl~ - IJ-yS II eer t i fy that~Mlt Transponaer

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

pj5 laquoqG- 1--1 S II Q ~Jt ifithat -t-h-i-amp IlA ~ Tr an-s-p 0 n a e r

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lATE TOTAL Description of Inspections Tests Repairs and AlterationsRECORDING ITODAYS TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certificate Number of

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

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DATE

19J2 RECORDING ITO DAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certif icate Number of TIME SERVICE Technician or Repair Facility (See back pages for other specific entries)

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

prrsCftl~ - IJ-yS II eer t i fy that~Mlt Transponaer

s rLLiiJ~ has been tested as regJlJred PAR 91413 Slgnature fru~( ~ Da t e 1gt 17 - ~ Wor-k-0-F-der-- _ 4 7 lt

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

pj5 laquoqG- 1--1 S II Q ~Jt ifithat -t-h-i-amp IlA ~ Tr an-s-p 0 n a e r

SNJ9 9r has been tested as re_quired middotmiddotmiddotFAR 9r- 4l3~ -Signat u re V ltb~

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DATE

19J2 RECORDING ITO DAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name Rating and Certif icate Number of TIME SERVICE Technician or Repair Facility (See back pages for other specific entries)

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

prrsCftl~ - IJ-yS II eer t i fy that~Mlt Transponaer

s rLLiiJ~ has been tested as regJlJred PAR 91413 Slgnature fru~( ~ Da t e 1gt 17 - ~ Wor-k-0-F-der-- _ 4 7 lt

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

pj5 laquoqG- 1--1 S II Q ~Jt ifithat -t-h-i-amp IlA ~ Tr an-s-p 0 n a e r

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II ATE RECORDING ITODAYS TACH FLIGHT

19 TIME

TOTAL TIME IN SERVICE

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

prrsCftl~ - IJ-yS II eer t i fy that~Mlt Transponaer

s rLLiiJ~ has been tested as regJlJred PAR 91413 Slgnature fru~( ~ Da t e 1gt 17 - ~ Wor-k-0-F-der-- _ 4 7 lt

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CR S A7 8 R4 S-5 J

IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

pj5 laquoqG- 1--1 S II Q ~Jt ifithat -t-h-i-amp IlA ~ Tr an-s-p 0 n a e r

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Da t e 1 - 17 - ~ W-O-)k- G-rder-middot-tt-- y 7ltf

RO r ESTING SERV I CES CRS A78 R4S5J

I cert i fy t h a t the -Altimet-e_r -an-dshy~ tat i c Sy s tem tests requ ired by Y AR

Par-t-9~--411 --have-been perform~d Th e Altimeter WClS _ testeEl - t -o zooccCZ

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AERO TESTING SERVIC ES middotmiddot C-RS A7-S-rt4 J

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IIATE RECORDING ITODAYS TOTAL Description of Inspections Tests Repairs and Alterations TACH FLIGHT TIME IN Entries mu st be endorsed with Name Rating and Certificate Number of

HI TIME SERVICE Technician or Repair Facil ity (See back pages for other specific entri es)

pj5 laquoqG- 1--1 S II Q ~Jt ifithat -t-h-i-amp IlA ~ Tr an-s-p 0 n a e r

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14)1 liSA

DATE

19

RECORDING ITOOAYS TACH FLIGHT TIME

TOTAL TIME IN 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)

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Piper PA32-260 N7325 SIN 32-1171 Hobbs=8-HU Tach=295263 Jtth-t-2000 AFTT=2952637 l - ) tt1

Performed alUlllal inspection IA W Piper PA32 Service Manual Installed Knots-to-you wing root flt+irings 1AW STC SA1217GL -Re moved and replaced right aileron olltbd hinge plJ te PIN l ZE507500342214714 Removed and replaced carb heat control cable PIN 554-05 3 AD 70-26-04 PCW by installation of stabilator counterweight hea wbe AD 72-08-06 NI A by PIN of MLG torque links AD 72-14-07 sLltlbiIator hinge attach bolts PCW AD 72-1 7-05 _ electric trim switch inswllation PCW CIW AD 75-24-02 by inspecting scats ret legs quick-disconnects for correct retention lAW AD instmcllolls No derects noted CW AD 76-7-12 by operltltionally testing ignition 5 itch I AW AD instructions Ops ek ok CW AD 78-23-0 I by checking fuel drin leer cover ssy dr for proper operltltion nd locking of lever with door closed lAW AD instructions No defects notcd Ops ck ok CW AD Y4-01-03 by rcmo ing and replacing RH l11ltlgneto (S6LN-204 PIN 10-161050-0_ SIN 10(5247) coil ass and di slributor rotor lAW AD instmctions CW AD 99-05-09 by visually inspecting for affected induction air filter lAW AD instructions RCll1olcd and replaced induction ltlir filter PIN CA 161 PL ELT ba llc ry replacement due 1-0 1 ELT ops ck ok lAW 9 1 207(d) Brakes insp ok Flight control cable tension ck ok and lubed Repaired light 011 whiske) compass

I certify thaI this AIRCRAFT was inspected lAW an ANNUAL inspection and vas determ ined to be in an a irworlhy condition

C) Pshy~6-ltL-d ~2A 0 gt-( Rona ld Kasuske IA 5034654

19

DATE RECORDING TACH TIME

TODAYS FLIGHT

TOTAL TIME IN SERVICE

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FLIGHT TIME IN SERVICE

~I - lti c_ l~6571 ) 105

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 )

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Piper PA32-260 N7325 SIN 32-1171 Hobbs=8-HU Tach=295263 Jtth-t-2000 AFTT=2952637 l - ) tt1

Performed alUlllal inspection IA W Piper PA32 Service Manual Installed Knots-to-you wing root flt+irings 1AW STC SA1217GL -Re moved and replaced right aileron olltbd hinge plJ te PIN l ZE507500342214714 Removed and replaced carb heat control cable PIN 554-05 3 AD 70-26-04 PCW by installation of stabilator counterweight hea wbe AD 72-08-06 NI A by PIN of MLG torque links AD 72-14-07 sLltlbiIator hinge attach bolts PCW AD 72-1 7-05 _ electric trim switch inswllation PCW CIW AD 75-24-02 by inspecting scats ret legs quick-disconnects for correct retention lAW AD instmcllolls No derects noted CW AD 76-7-12 by operltltionally testing ignition 5 itch I AW AD instructions Ops ek ok CW AD 78-23-0 I by checking fuel drin leer cover ssy dr for proper operltltion nd locking of lever with door closed lAW AD instructions No defects notcd Ops ck ok CW AD Y4-01-03 by rcmo ing and replacing RH l11ltlgneto (S6LN-204 PIN 10-161050-0_ SIN 10(5247) coil ass and di slributor rotor lAW AD instmctions CW AD 99-05-09 by visually inspecting for affected induction air filter lAW AD instructions RCll1olcd and replaced induction ltlir filter PIN CA 161 PL ELT ba llc ry replacement due 1-0 1 ELT ops ck ok lAW 9 1 207(d) Brakes insp ok Flight control cable tension ck ok and lubed Repaired light 011 whiske) compass

I certify thaI this AIRCRAFT was inspected lAW an ANNUAL inspection and vas determ ined to be in an a irworlhy condition

C) Pshy~6-ltL-d ~2A 0 gt-( Rona ld Kasuske IA 5034654

DATE I RECti~NG TODAYS TOTAL

TACH 19~ I TIME

FLIGHT TIME IN SERVICE

~I - lti c_ l~6571 ) 105

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 )

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Piper PA32-260 N7325 SIN 32-1171 Hobbs=8-HU Tach=295263 Jtth-t-2000 AFTT=2952637 l - ) tt1

Performed alUlllal inspection IA W Piper PA32 Service Manual Installed Knots-to-you wing root flt+irings 1AW STC SA1217GL -Re moved and replaced right aileron olltbd hinge plJ te PIN l ZE507500342214714 Removed and replaced carb heat control cable PIN 554-05 3 AD 70-26-04 PCW by installation of stabilator counterweight hea wbe AD 72-08-06 NI A by PIN of MLG torque links AD 72-14-07 sLltlbiIator hinge attach bolts PCW AD 72-1 7-05 _ electric trim switch inswllation PCW CIW AD 75-24-02 by inspecting scats ret legs quick-disconnects for correct retention lAW AD instmcllolls No derects noted CW AD 76-7-12 by operltltionally testing ignition 5 itch I AW AD instructions Ops ek ok CW AD 78-23-0 I by checking fuel drin leer cover ssy dr for proper operltltion nd locking of lever with door closed lAW AD instructions No defects notcd Ops ck ok CW AD Y4-01-03 by rcmo ing and replacing RH l11ltlgneto (S6LN-204 PIN 10-161050-0_ SIN 10(5247) coil ass and di slributor rotor lAW AD instmctions CW AD 99-05-09 by visually inspecting for affected induction air filter lAW AD instructions RCll1olcd and replaced induction ltlir filter PIN CA 161 PL ELT ba llc ry replacement due 1-0 1 ELT ops ck ok lAW 9 1 207(d) Brakes insp ok Flight control cable tension ck ok and lubed Repaired light 011 whiske) compass

I certify thaI this AIRCRAFT was inspected lAW an ANNUAL inspection and vas determ ined to be in an a irworlhy condition

C) Pshy~6-ltL-d ~2A 0 gt-( Rona ld Kasuske IA 5034654

f1ATE Description of Inspections Tests Repairs and Alterations of

ri~~~~~~~~~~~~~~~~~~~~~~~ --~ ~~~~~~~~~~~~~~~ ~ laquo~ middot~~ ~24~~~~~i~s)

Piper PA32-260 N7325 SIN 32-1171 Hobbs=8-HU Tach=295263 Jtth-t-2000 AFTT=2952637 l - ) tt1

Performed alUlllal inspection IA W Piper PA32 Service Manual Installed Knots-to-you wing root flt+irings 1AW STC SA1217GL -Re moved and replaced right aileron olltbd hinge plJ te PIN l ZE507500342214714 Removed and replaced carb heat control cable PIN 554-05 3 AD 70-26-04 PCW by installation of stabilator counterweight hea wbe AD 72-08-06 NI A by PIN of MLG torque links AD 72-14-07 sLltlbiIator hinge attach bolts PCW AD 72-1 7-05 _ electric trim switch inswllation PCW CIW AD 75-24-02 by inspecting scats ret legs quick-disconnects for correct retention lAW AD instmcllolls No derects noted CW AD 76-7-12 by operltltionally testing ignition 5 itch I AW AD instructions Ops ek ok CW AD 78-23-0 I by checking fuel drin leer cover ssy dr for proper operltltion nd locking of lever with door closed lAW AD instructions No defects notcd Ops ck ok CW AD Y4-01-03 by rcmo ing and replacing RH l11ltlgneto (S6LN-204 PIN 10-161050-0_ SIN 10(5247) coil ass and di slributor rotor lAW AD instmctions CW AD 99-05-09 by visually inspecting for affected induction air filter lAW AD instructions RCll1olcd and replaced induction ltlir filter PIN CA 161 PL ELT ba llc ry replacement due 1-0 1 ELT ops ck ok lAW 9 1 207(d) Brakes insp ok Flight control cable tension ck ok and lubed Repaired light 011 whiske) compass

I certify thaI this AIRCRAFT was inspected lAW an ANNUAL inspection and vas determ ined to be in an a irworlhy condition

C) Pshy~6-ltL-d ~2A 0 gt-( Rona ld Kasuske IA 5034654

DATE

19 _ _

RECORDING TACH TIME

ITODAYS FLIGHT

TOTAL TIME IN SERVICE

Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Technician Dr RepCt r Facility (See back pages for other speci fic entries)

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lATE

III

RECORDING TACH TIME

TODAYS FLIGHT

TOTAL TIME IN 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 )

Date January 24 2002 Tach 299fl Toil t ime 299f3

Removed landin~ ear tires and pac ke d barir ~s with aeroshell ~reas eN o defec ts fou n d on land in ~ ~ear I nstalled new left navi~ation l i ht l ens (red) F iT ch eck~~ r AW 91207(D) Lu b r i cat ed fli trh t control s with lps 2 Remove d corrosion throu~h out aircraf t as n e ed e d Filled battery wi th d is t i lled water and rechar~ed Fainted bat t e ry b ox and reseal e d ba t t ery compartment Glued wal l l i ners inside caro bay ( forwar d) All AD notes tnroutrh 99-05- 09 compl i ed with I cer i t t f y that this ai rcraft has been ispecte d in acco r da nc e with the annual insp ection and de te rmined to b e in airworth y condit ion

F D~UA REff~~rSTA-_ ~4 ~tf b plaquolt ~

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lATE

III

RECORDING TACH TIME

TODAYS FLIGHT

TOTAL TIME IN 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 )

Date January 24 2002 Tach 299fl Toil t ime 299f3

Removed landin~ ear tires and pac ke d barir ~s with aeroshell ~reas eN o defec ts fou n d on land in ~ ~ear I nstalled new left navi~ation l i ht l ens (red) F iT ch eck~~ r AW 91207(D) Lu b r i cat ed fli trh t control s with lps 2 Remove d corrosion throu~h out aircraf t as n e ed e d Filled battery wi th d is t i lled water and rechar~ed Fainted bat t e ry b ox and reseal e d ba t t ery compartment Glued wal l l i ners inside caro bay ( forwar d) All AD notes tnroutrh 99-05- 09 compl i ed with I cer i t t f y that this ai rcraft has been ispecte d in acco r da nc e with the annual insp ection and de te rmined to b e in airworth y condit ion

F D~UA REff~~rSTA-_ ~4 ~tf b plaquolt ~

Aamp 3174R R91f ~

- - _ - ---- - _-_J -1 1- t - ---- - -- -- - - - -_

DATE

19 __

RECORDING ITOOAYS TACH FLIGHT TIME

TOTAL TIME IN SERVICE

Description of Inspections Tests Repairs and Alterations Entries must be endorsed with Name Rating and Certificate Number of Techn ician or Repair Faci lity (See back pages for other specific entries)

c 1001 AS

N4732S

Piper PA32-260 SN 32-1171111 Til

11042010 Tack reads 3055 hrs 3055 hrs TIAF HI

100 Hour Airframe using Piper Service Manual amp checklist Jacked aircraft amp inspected landing

Gear Cleaned amp packed all wheel bearings Inspected brake linings amp rotors Cleaned amp lubed

brake mount stubs checked brake reservoir Installed 3 new 850 X 6 6 ply Air Trac tires Installed

new seals in nose strut amp replaced all bolts in torque links amp steering system Serviced three struts with

hydraulic fluid amp nitrogen replaced two VI 302DN HP valve cores Replaced the vacuum regulator sock

B3-5-1 amp installed a new ACS A-510-2 magneto switch with diode assembly Installed 2 PN DW4K2

Stabilator mount bearings Checked cables amp lubed pulleys rod ends amp controls Cleaned amp lubed

Trim jack screw Replaced SCAT 6 defroster hose under panel Installed missing placards Made up new

ATP AD Note list revised equipment list amp weight amp balance for changes made amp not recorded

GW 3400 Ibs EW 1882 Ibs UL 1518 Ibs EWCG 7792 inches EBC ELT installed Ops check UAW FAR

I 91207d Battery date is 8201_2_ _ _ _ _ _ _ ___ 70-26-04R2 SB 576 is CWo PN 69024V balance weight tube with green markings is installed

76-18-04 gt SB 519 Ran engine with fuel selector valve in OFF Checks OK

95-26-13 New oil cooler hoses using Aeroquip 303 hose installed at 3055 hrs 10242010

Replace by 4055 hrs or 10302018

99-05-0-9 NA New Facet 460-632 air filter installed at 3055 hrs 10242010

10-15-10 NA SB 1197A Control wheel taper pins at U jOints amp measured edge distance OK

84-26-02

93-05-02

Imiddot i

5 12-23-2011 N4732S PA-32-2601 Q~gtc SIN 32-1171 ACTT 30760 TACH 30760

Airframe bull Completed an Annual Inspection IA W FAR Part 43 Appendix D and the Mfgs inspection guide lines bull AD 77-12-01 on the fuel selector valve IH26-2 completed by complying with

Para (a) by performing inspection in accordance steps(a) 1 through 6 Due again in 50 hours Para (c) by installation of fuel selector kit 760-687 Para (d) by installation ofthe vent tube kit 765-560 Para (e) by inspection and replacement offuel hoses

bull AD 75-24-02 on the seats by inspection bull AD 77-12-01 on the fuel selector will be due in 40 hours bull FAR 91207 (d) ELT Inspection completed in accordance with the manufacturer instructions and FAR bull ELT battery dated August 2012 bull Airframe battery box corrosion removed and treated bull Installed new G-35 battery SIN G02688359 bull Repaired rotating beacon bull Left brake caliper resealed and the brakes bled bull Repaired brake reservoir bull Serviced nose strut bull Installed new wheel bearings in the nose wheel bull [nstalled new wheel bearing in the outboard wheel ofthe right main bull Secured seal in the bottom cowling bull Installed new CCA-1550 fuel drain valves in the left tip and main tanks bull [nstalled new AN4-22A bolt in the nose wheel steering stop bull Reapplied nose-turn ing limit placard bull Installed placards at the tip tank filler port bull Installed new fuel quanity sender gaskets in the main tanks bull Replaced brittle scat hose behind instrument panel as needed bull Replaced fitting on the electric fuel pump bull Fuel selector valve PIN 1026-2 repaired by BampS Aircraft Parts

CONTINUED ON NEXT PAGE 199 1ASA

CONTINUED FROM PREVIOUS PAGE Au to pilot bridal cable tension adjusted to the proper tension Elevator trim jackscrew bushings replaced and system rigged Secured abrasion boot on the horizontal stabilizer Inspected fuel pump and fuel line in accordance with SIB 557 Inspected main landing gear struts in accordance SIB 1131 The following items have been deactivated and placarded as INOP in accordance with FAR 91213 Some instrument panel post lights are INOP 2 Nav rad io antenna broken at the rea r of the rack Cabin speaker is INOP T ransponder 91413 compliance

I ltfrtiry that this aircraft has been inspected in discrepancies and unairworthy items dated 11I2J120 11 as been provided for the aircra~ ork Order 6519 ltnw Mark Lehrkamp for Quest Aviation Inc I I(S OW5R108N 605-225-8008

1 lIairworthy Discrepancies 1) 2007-26-09 on the propeller 1) 2005-14-11 on the propeller I) 21106-24-07 on the propeller

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N4732S

Piper PA32-260 SN 32-1171111 Til

11042010 Tack reads 3055 hrs 3055 hrs TIAF HI

100 Hour Airframe using Piper Service Manual amp checklist Jacked aircraft amp inspected landing

Gear Cleaned amp packed all wheel bearings Inspected brake linings amp rotors Cleaned amp lubed

brake mount stubs checked brake reservoir Installed 3 new 850 X 6 6 ply Air Trac tires Installed

new seals in nose strut amp replaced all bolts in torque links amp steering system Serviced three struts with

hydraulic fluid amp nitrogen replaced two VI 302DN HP valve cores Replaced the vacuum regulator sock

B3-5-1 amp installed a new ACS A-510-2 magneto switch with diode assembly Installed 2 PN DW4K2

Stabilator mount bearings Checked cables amp lubed pulleys rod ends amp controls Cleaned amp lubed

Trim jack screw Replaced SCAT 6 defroster hose under panel Installed missing placards Made up new

ATP AD Note list revised equipment list amp weight amp balance for changes made amp not recorded

GW 3400 Ibs EW 1882 Ibs UL 1518 Ibs EWCG 7792 inches EBC ELT installed Ops check UAW FAR

I 91207d Battery date is 8201_2_ _ _ _ _ _ _ ___ 70-26-04R2 SB 576 is CWo PN 69024V balance weight tube with green markings is installed

76-18-04 gt SB 519 Ran engine with fuel selector valve in OFF Checks OK

95-26-13 New oil cooler hoses using Aeroquip 303 hose installed at 3055 hrs 10242010

Replace by 4055 hrs or 10302018

99-05-0-9 NA New Facet 460-632 air filter installed at 3055 hrs 10242010

10-15-10 NA SB 1197A Control wheel taper pins at U jOints amp measured edge distance OK

84-26-02

93-05-02

Imiddot i

5 12-23-2011 N4732S PA-32-2601 Q~gtc SIN 32-1171 ACTT 30760 TACH 30760

Airframe bull Completed an Annual Inspection IA W FAR Part 43 Appendix D and the Mfgs inspection guide lines bull AD 77-12-01 on the fuel selector valve IH26-2 completed by complying with

Para (a) by performing inspection in accordance steps(a) 1 through 6 Due again in 50 hours Para (c) by installation of fuel selector kit 760-687 Para (d) by installation ofthe vent tube kit 765-560 Para (e) by inspection and replacement offuel hoses

bull AD 75-24-02 on the seats by inspection bull AD 77-12-01 on the fuel selector will be due in 40 hours bull FAR 91207 (d) ELT Inspection completed in accordance with the manufacturer instructions and FAR bull ELT battery dated August 2012 bull Airframe battery box corrosion removed and treated bull Installed new G-35 battery SIN G02688359 bull Repaired rotating beacon bull Left brake caliper resealed and the brakes bled bull Repaired brake reservoir bull Serviced nose strut bull Installed new wheel bearings in the nose wheel bull [nstalled new wheel bearing in the outboard wheel ofthe right main bull Secured seal in the bottom cowling bull Installed new CCA-1550 fuel drain valves in the left tip and main tanks bull [nstalled new AN4-22A bolt in the nose wheel steering stop bull Reapplied nose-turn ing limit placard bull Installed placards at the tip tank filler port bull Installed new fuel quanity sender gaskets in the main tanks bull Replaced brittle scat hose behind instrument panel as needed bull Replaced fitting on the electric fuel pump bull Fuel selector valve PIN 1026-2 repaired by BampS Aircraft Parts

CONTINUED ON NEXT PAGE 199 1ASA

CONTINUED FROM PREVIOUS PAGE Au to pilot bridal cable tension adjusted to the proper tension Elevator trim jackscrew bushings replaced and system rigged Secured abrasion boot on the horizontal stabilizer Inspected fuel pump and fuel line in accordance with SIB 557 Inspected main landing gear struts in accordance SIB 1131 The following items have been deactivated and placarded as INOP in accordance with FAR 91213 Some instrument panel post lights are INOP 2 Nav rad io antenna broken at the rea r of the rack Cabin speaker is INOP T ransponder 91413 compliance

I ltfrtiry that this aircraft has been inspected in discrepancies and unairworthy items dated 11I2J120 11 as been provided for the aircra~ ork Order 6519 ltnw Mark Lehrkamp for Quest Aviation Inc I I(S OW5R108N 605-225-8008

1 lIairworthy Discrepancies 1) 2007-26-09 on the propeller 1) 2005-14-11 on the propeller I) 21106-24-07 on the propeller

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5 12-23-2011 N4732S PA-32-2601 Q~gtc SIN 32-1171 ACTT 30760 TACH 30760

Airframe bull Completed an Annual Inspection IA W FAR Part 43 Appendix D and the Mfgs inspection guide lines bull AD 77-12-01 on the fuel selector valve IH26-2 completed by complying with

Para (a) by performing inspection in accordance steps(a) 1 through 6 Due again in 50 hours Para (c) by installation of fuel selector kit 760-687 Para (d) by installation ofthe vent tube kit 765-560 Para (e) by inspection and replacement offuel hoses

bull AD 75-24-02 on the seats by inspection bull AD 77-12-01 on the fuel selector will be due in 40 hours bull FAR 91207 (d) ELT Inspection completed in accordance with the manufacturer instructions and FAR bull ELT battery dated August 2012 bull Airframe battery box corrosion removed and treated bull Installed new G-35 battery SIN G02688359 bull Repaired rotating beacon bull Left brake caliper resealed and the brakes bled bull Repaired brake reservoir bull Serviced nose strut bull Installed new wheel bearings in the nose wheel bull [nstalled new wheel bearing in the outboard wheel ofthe right main bull Secured seal in the bottom cowling bull Installed new CCA-1550 fuel drain valves in the left tip and main tanks bull [nstalled new AN4-22A bolt in the nose wheel steering stop bull Reapplied nose-turn ing limit placard bull Installed placards at the tip tank filler port bull Installed new fuel quanity sender gaskets in the main tanks bull Replaced brittle scat hose behind instrument panel as needed bull Replaced fitting on the electric fuel pump bull Fuel selector valve PIN 1026-2 repaired by BampS Aircraft Parts

CONTINUED ON NEXT PAGE 199 1ASA

CONTINUED FROM PREVIOUS PAGE Au to pilot bridal cable tension adjusted to the proper tension Elevator trim jackscrew bushings replaced and system rigged Secured abrasion boot on the horizontal stabilizer Inspected fuel pump and fuel line in accordance with SIB 557 Inspected main landing gear struts in accordance SIB 1131 The following items have been deactivated and placarded as INOP in accordance with FAR 91213 Some instrument panel post lights are INOP 2 Nav rad io antenna broken at the rea r of the rack Cabin speaker is INOP T ransponder 91413 compliance

I ltfrtiry that this aircraft has been inspected in discrepancies and unairworthy items dated 11I2J120 11 as been provided for the aircra~ ork Order 6519 ltnw Mark Lehrkamp for Quest Aviation Inc I I(S OW5R108N 605-225-8008

1 lIairworthy Discrepancies 1) 2007-26-09 on the propeller 1) 2005-14-11 on the propeller I) 21106-24-07 on the propeller

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CONTINUED FROM PREVIOUS PAGE Au to pilot bridal cable tension adjusted to the proper tension Elevator trim jackscrew bushings replaced and system rigged Secured abrasion boot on the horizontal stabilizer Inspected fuel pump and fuel line in accordance with SIB 557 Inspected main landing gear struts in accordance SIB 1131 The following items have been deactivated and placarded as INOP in accordance with FAR 91213 Some instrument panel post lights are INOP 2 Nav rad io antenna broken at the rea r of the rack Cabin speaker is INOP T ransponder 91413 compliance

I ltfrtiry that this aircraft has been inspected in discrepancies and unairworthy items dated 11I2J120 11 as been provided for the aircra~ ork Order 6519 ltnw Mark Lehrkamp for Quest Aviation Inc I I(S OW5R108N 605-225-8008

1 lIairworthy Discrepancies 1) 2007-26-09 on the propeller 1) 2005-14-11 on the propeller I) 21106-24-07 on the propeller

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DATE

19

RECORDING I TODAYS TACH FLIGHT TIME

TOTAL TIME IN 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)

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