341ST-Maintenance-Records-1.pdf - Princeton Airport
96
aidlog EODR NG AIRFRAME MAINTENANCE RECORDS 2 Log No. Aircraft Registration No. N 341ST Aircraft Mfg. Piper Model Ch PA 28-180 Serial No. 2-730 5476 Engine Mig.ycoming Model O-340-A4A Serial No. L_[7720-36 A Engine Mfg.. Model. Serial No.. Propeller Mfg.Senenich Model 74 EM8SS-0.L0 sSerial No. 12201 K Hub Design No.. Hub Serial No.. Blade Design No. Blade Serial No's.. Propeller Mfg. Model Serial No.- Hub Design No. Hub Serial No.. Blade Design No. Blade Serial No's.. (All applicable information must be filled in) ERO ECH PUBLICATIONS INC. PO. 8OX 528/ OLD BRIDGE. NJ 08857 (201) 679-5151 1979 AeroTech Publications Inc.
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Transcript of 341ST-Maintenance-Records-1.pdf - Princeton Airport
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Page No.
TACH
RECORDING METER
TIME
TOTAL DESCRIPTION OF WORK PERFORMED-
TI DATE
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
SERVICE
From Beok TOTAL brought forward from previous page
2912.08
12-14-68 2912.08212,D& Aiecraft Aanual luspection..
Airerat Ttal Time: 2412.0
ngine Tatal Time: 2412.0 Engine lima SMOH 6980r
Prepeller Tetal Tine: 29120f Propeller Time SMOH 0.0
1Repaieed ane adjust and reglace saal on cabinentranee door
2Re-upholsted bulk hend zndsiding inside thecabin.
sPephed teinindicader suire. Replaced L.tnd Right flexible lines.
sReglaced landing light. 4 lepeeed Gyta Silkers TReplaced Uacu regulailor ilhec.Replaced seals e fuel seclecter valse.
eved Rircandihaniag uat. Ce=pcesses lines, evapamte and drye
Replacee bagaaae daar seal eame eorrosion and treated surfaee xcoana the zst aie inlet. 1 Remate VHE xateabas, cetave corcosi ad treated surtace.lasled
th VHF zatunas zd check kcopetaio. .Replace beth kael tk veats aod Lines. Remaved Lndder and replace Lowereb rnd removed
CDerosiA
A hepleced LoL upper nd lawe hingebalison the iraddes Remaved corcasien znd teeated surtace on He spnrat veel in . Replacesenter op skin stshilatar. it. Replace belh aut board hinges on the stebilatar
11. Reglaced beth aut bozrd hinges thetabilatar támel 2912.0|SUB-TOTAL this page
21/2.0 TOTAL-Carry forward to next page
Page No
OTAL DESCRIPTION OF WORK PERFORMED
SIGNATURE & CERTIFICATE NO OE PERSON pERFORMING WOBK DATE ME RECCONG
METER SERVICE ME
2912.08 TOTAL brought forward trom previous page
So cerrigm
a.eeved zad treate d, stabilater rib ips. beth Li. Rt
aRepar both stabilztor tip fot craeks.
J. T.912.03
certify that this aircraft was weighed lA/W
A.C. 43-13-1Ain a level flight attitude on this
date t-I7- ?8- Scale readings are:-
M- R M 10
or Nose.75 Aircraft Weighing Servica Inc
NameSiznature A&P
2170!1 2(70l12
22, Remove carrosih zad teested skin n both left aad
cialt ailesoa. lastalled and check rigsinz13. KeuoJe corrosion and trezted Skinznd spar om bothe
Lestand rigkt spx laps. 24 Replase betl Lelt and Rigkt fael tauk hese s 2S. Remeve eorrocicn from fuel tank uwell as r badh wing
teraiedskin and tankr, Rnd installed boih huel banks. t. lasalled neplacacds fuel tanke indicating Capaciy
oetane ating, znd usealle fuel.
Kemeve beth main landing gear struts and had Leuer
secis cepair hy ArealdddingasdachiuinRepacke witl aew seals and Setvicee. Instal)ath nes hared-
s Rembue aase strut andhadsleaceccome andpalisk asTallel wth neu seals and service lai ledatk
30, Replace_bolk Leftaad Rigki beake Lines.
(Rol Preeisien Produt.)
SUB-TOTAL this page29/2.06
a/7.08| TOTAL-Carry forward to next page
Page No
OESCAITION OF WORK PERFORMED
DATE SiINA TUME 4 CERTIFICATE NO VE PERSION PENFO/MING NORK
SECE
TOTAL drovOnt forward from previous pa4 2912.0
B1. Replaced ELT B«thery and ekech foropemtion. Sept
AN nE
BU STER dEp. 91
2. Remoye ADF andenaa and install ADF aatenna M ou14o1O
Sense Aatenna and Coupler.
3. Replace bath lesland Rt windshield.
sz lnstall Anpmeter kit Yh 765-3o3 to comply with AD 61n-1
s Altaelec Eacsdec chech was dne by leningul Aeonie s
a t-12-87 2238 FrR L.170. Due Dde. 2-30-9
Trassponder ckeck done by lenisula Avionics 71387.
Due Date: 7-31-89
s Rrepair Aiccoat surkace, treated these areas ths has_carrasian, prine the surdzee Jor paating.
Pai nted 4Le airesaLA as felawS. Durethane Whte Du 2os8 Dacethane Red Du 724?2 Ducethant Gold Du 152L
. Repair lading wheelpanis and painted me calers 2s abve-
Icetify this airccaft has been inspected inaaerdance wit wautacturers Annal inspection regert a a30327and haue Complied with the follosing_AD'a AD-72-06-olR Main Ges Tarque Links. AD-74-24-07 lncorrect Plaeard AD-75- Pg.03 Fael Deaia Vzlves
Ap-75-24-D2R SestQuick-discounect SUB-TOTAL this page
TOTAL-Carry forward to next page
Page No.
TOTAL TACH OA DATE DESCRIPTION OF WORK PERFORMED TIME RECORDING
METER TIME
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORAK IN
SERVICE
2912.o TOTAL brought forward from previous page
A- 77-61-o Fuel QuanityGaGe AD-223-03 Cantrol Poc End Bea rings.
AD- 79- 24-0S OLE Eael Syslem Hoses
AD 87-0f-ok R2 Not Applicable.
AD--17-01 Ammefer Replacement hat are zpplicable
to the PA 28-/g0 zircraft. This zircraftmeets FAA
and Manutactuner's 5pecifications. Relurn to servicee.
IF72038 IA_
F.23989 2925. 33 Instila 1 Moeko b128cy Lotm lazvee w ITH A-1
Ctaw FT. Cuec OK Ss 337 And JeAs
AnD BaLaneé DATA SH TAS DTE fe DETALS-
ieoiey Fick3 A IY05916 1A
3--903181. Ax_ |2181.4 Aitcratt_Aanue lnspectin
AitetaltTtal timei 29£LLP E
Ensiae TLtal Lime211.L Engine ine SMbH 27.68
RropelTltime:a1k1.LkProp. lime SMoH 69.6
cedi this aircraft bas beea iuzpecded in aeseedane s thautaet ucec's Aanualinspectien reperi N 230-207
d have comled wdh +ke t.llawing AD's
AD- R4-2-a2 lnducia Aic £Etar AD- 76-12-2R Bendix Irgnition Suiteh.
AD --2-03R Seat Guisk Vscanneot AD-72-0 DL R Main GezrhrsuelinKs
This aicat meets FAAE Maautactuwers Speciliczions Retata Sa LE2203 IA to Service
SUB-TOTAL this page
TOTAL-Carry forward to next page
Page No
TACH OR TOTAL TIME DESCRIPTION OF wORK PERFORMED-
RECORDING DATE METER
TIMESIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
IN
SERVICE
TOTAL brought forward from previous page
13-20-9o 3022.3Jo)2.3Annual laspecfion
Aiceralt Total Time: 3022, 3
Engine TbtalTime 302. 3P SPMOH: 8O8, 3f Hpurs
Propeller TotalTime So22.3f SMOH 10.3 Hours
Cnplied withe the Slwing AD'3
A-oosRa AD 72-08-04 Main Genc Torgue links
AD-75-4-02 Seat Quick-Diseonnect
R- *Bendix g Isnitim Sutek
AD 28-01-67 Bendix Magneto |AN -24-02 Induction Air Eilters
|lcectiiy his aitesatt has been inspected in accordance
it Manalactuver's Aanual laspecties Repart 230-307.
This aire.calt Meets fhn £ Manufacturer's specitiation,
Return o seruice. a 172 038 1A
11-19.91 305o1so1
ll-24-11 30L2,14|3062,4Rem pued / Replaced Vzaccaa Pamp 211CC Sac GAGo04?72
A AP AtP 18)203-sUB-TOTAL this page
TOTAL-Carry forward to next page
Pag
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TOTA
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Repai N
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as
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ithM
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Page No.
T4CH OR
PECORDNG
METER TILVE
DESCRIPTION OF WORK PERFORMED TOTAL
TIME SGNATURE & CERTIFICA TE NO OF PERSON PERFORMING wORK
DATE IN
SERVICE
TOTAL Drought forward from prevrOus page
plnes s 31/2.7 lupa cactut 2vnAe crhl d
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SeevicEThe wlo®O43 )ZAsTalED oUEe-umE SiawRE maLOR
HauLeD o1L CooLER- AVEW 01L Fueu Hoses
ZsTAL6o Naste0p BouTs GEDUD Kaw tpwa
PeefoemED Lez5 OPEeAT IONAL CHECKS BorA
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97s AaeoSHEL wgo- oT Mw6RAL o
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23-93 Tn Taled new Alde cbin ka eeplaue sEA 00 Theolie pexeed
il2PAOS_A*_ SUB-TOTAL this page
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Page No. DESCRIPTION OF wORK PERFORMED
SIGNATURE & CERTIFICATE NO OF PERSON PERFORMING wOB TACH OR TOTAL TIME
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TOTAL brought forward from previous page
68/18-Co_} anedderk fer stml peuti PN 6E/18-C
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ANNUAL inspection, and was
ME 3149.0ues rU) etermined ta te in airworthy conditon of this date.
SMyH3,5 Nes 11E LAS2 ate 2Total Tima /I2.
tarele A4ALzarti lA 734240
|t95T| wVa 3-5 23
sUB-TOTAL this page
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Page No.
DESCRIPTION OF WORK PERFORMED SIGNATURE&CERTIFICATE NO OF PERSON PERFORMING WORK
TOTAL TACH OR AECORDING
METER TIME
DATE IN
SERVICE TIME
TOTAL brought forward from previous page
/NSRTED Aw A 100 H NSPRTTOw &RENED
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EL uE SEet 95. Lw AD 25-24-2 SET uLLK DscNNRE
OPERATOn ARLe.4E_wS TAXIE)L ND /_ DEFtZT|
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DATE TIME IN
TER TIME SERVICE
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n/sA3347 3417MAN He FAIRINSS KeMavED
A M
IS74.3 84o 13183.6
krPo¥3&03 723
/9/33A1 337 337L KEnovD PLeT 5IE sEA RALS INSTALLED.
NEW 4E 2AILS PN 2SS 70 SING ELHISTU RivET HLES
AND uD qvers STAT
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PR1 3394ZRJY.JIespectedian pijare 02he inspectos-LhLLA
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C.r ia this A!RCRAFT.E
DET Dectedin accordance with
RIAN ANUAL inpuiiun, and wt
247 NZhes Soc lasZuaaue
5 9s133717 339429|TPAL TI AE AeC vbi
31242Hes.ga4) Jyo I23.e2 * iermined to be in aliorthy condition
HRS, J) ME LAST 13 MoS 2 f7.22 of this data.
hate 5 21cial Tune3374..
HeS) A TÉ LAST A NVvaL JJi-4f asne Mana Maroid Marrart, IA 7.3
-2313197.2| 33 97.44- 7ZastallAereadza
Sceyellen tags _for Release l and |L_majn-
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IN ME TER SEAVICE SIGNATURE & CERTIFICATE NO OF PERSON PERFOAMING WORK
TIME
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839-95 3y3j34912 Qi caffinsected ann piper DO hL Inspecsh
Chec lst_c JLaebattury hyd luid, Serae
Tis ih die Seivatu ies stu wifh_DIJrogeC
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aft wiagateh pts. aD T-11- 2 Seas
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inspeathoa Lh ligt Leplace damangsdiePpre taileeae wth pein iperlhssuait lupprrheH\replureLwng
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certitynat this AIRCRAFTIEMam nE9 been inspected in accordance with
00+HAAN AAAUAL inspection, and wag Cetermined to be in airworthy condition
as of this date.
S Meid 43/8 ttes LaST Date 3 54Tota Time 35422 Ha:old Morrarty, IA 7342Ã0
12 53. 23 #es, Da7 57 uMV2L 22513.
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TIVE SERVICE
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etaAS penhAacbe
ICERTIFY THAI 1 HS
WITH HAS BEEN
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AND st Llla'ollHn e Cvst pehees
WAS DETEPMIM EYTDIG IY AIR WORTHY UCL ole hlen b3 S7, Pepnca eeDHTION AUTHORI7 sGMMTue J UMC Eke D°7Y CERTIFICATE NO Ato31 u DATE.11.7.. TOTAL TIME.3..da. clsAD 75-24-2 5ak hws cljs
duAD,76--/t Ay efpschork ok ycke) All wheel Saujkeesa Innlea)
tCERTIY THAT THIS RCkGEIHAS BE INSPECTED LN ALORDANCE WIIH A ANNUA iNSPECTIUN AND WhS DLiLaatiLi l0 b£ IN ALiR»Uail
JNUTTION.
DAIE 4-7IACH IME 3S88t S7 Sot eLAL TIME 3 S8 SM.A F7I-8
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CONDITION. AUTHORIZED SIENATU CERTIFICATE NO.A DATE2KZZTTOTAL TIHE2E22
SaRsN nllace
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E DATE SKGVATUAE CERTECATE NO OE PERSON PEREORMING WORK
VE TE
SERVCE
eeYe CERTIFY THAT THIS AIK «8
HAS BEEN INSDECTED IN ACCORDAN
WIT A Z0 K INSPECION A: WAS DETERMINED fo BE Iy AIR WOATY
CORED SIGNA 34 CERTIFICATE NO. k3372 DATEA 28 TOTAL TIME 3T22.
/ a AD 7524-t A or Clw AD 76-7 uc ley ALKALNE BATTERY PACK P/N 9103S
Pipe/ser Reseu/ . Ge. Syste AA ADDd ststlonRrto inetretions befere tnetstsels
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PROR PATEShE InCn walé 597
I CERTIFY THAT THIS
HAS BEEN INSPECTED IN AGCORDANCE WITH A 2 A_INSPECTION AND MAS DETEPMINED IO BE IN AIR WORTHY CONDITION. AUTHORIzED SICNAIURE
CERTIFCAEca oIA JME sy hes_leak hars 36 OT
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P30e No
707
DATE TE ECORON pESCRIProN OF WORK PERFORMEO ER
SIGNA TUME & CERTIEICA rE NO OF PERSON PERFORMIN WJRK
SE®VCE VE
CERTIFY THAT TH8TAL DR »2from previous pag
HAS EEN INSPECTED IN ACCORDANCE WITH A L0O WAS DETERMINED tO Br Iy Ain woRJHY CONDITIK. AUTHORIZLD SIGNATUPE
CERTIEICATE NQ. s DATE
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107AL TAC{ OESCAIPTION OF WORK PERFORMED DATE TIME RECCADVG
VETER SIGNATURE & CERTIFICATE NO OF PERSON PERFORMING WORK
SERVICE TIE
TOTAL brought forward from previous page
CERTIFY THAT THIs CRC HAS BEEN, INSPEGIED IN AçcoRDANCE WITH Alo I ACcoRDANCE
WAS DETERMINED TO OE N AIR WORTHY CONDITION- AUTHORIZ�D SIGNATURE, GERTHECATE NO. 4ZL Y222 DATEZ-S:6/
INSPECTION AEd 7
TOTAL TIMES0Z
0 xest Da e 3765 diA 916-13
coulta bases ele seri 3705 c
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METE R TIME
TOTAL
DESCRIPTION OF WORK PERFORMED
SiGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK DATE TIME
IN
SERVICE
TOTAL brought forward from previous page
CERTIYTHAT THIS 2nc2AeL HAS BE�N INSPECTED IN ACCORDANCE WITH ALOG A WAS DETERMINED TO BE IN AIR WORTHY CONDHNAUTHORIZED SIGNATURE
AS
INSPECTION AND
CERTIFICATE DATE NO. ALE 244 ,t LealkcezAnG
Pe lloces R TOTAL TIMERLL. BUI3
T5nnot 9 ACna AD 25r 24-0
e b 373 -7-1
Cle 95-24-43 ol Coden hos khse
n As Jex AD Aert Dve 37B a Aan Ch Fac!go7 ok
chekesk MS76 ICERTIY THAT THIS
HSPLcIEDiN ACCORDANCE WIih AAUNuA IMiSPECTION AND WAS DETERMINED TQ BE IN AIRWOATX,
CORUTIOR
BAME2KC TME 315 ma TOTAL IME
SICED
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TACH OR DESCRIPTION OF WORK PERFORMED
SIGNATURE & CERTIFICATE NO. OF PEASON PERFORMING WORK DATE RECORDING
IN METER TIME SERVICE
TOTAL brought forward from previous page
OGRRTP THATT t nca -AS BEQ JANS 2IA ACGOMAAADHE-
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Ft, ck_ck brt Das Glo33
CERIFY THAT THISHTLAHE-
INSPCTED IN ACCORDARCE Wia NN uA INSP4CTION AND WAS DElLnliinbD |I0 BE I AlRuoTuY
-
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TOTAL TIME
TACH OR
DATE EOHDINGMETERIN
SERVICE TIME
TOTAL brought forward from previous page
At e have mUL huw
mate
T Ne 313
Tac 3
12 A &PAIRCRAFT MAINT. INC. MACARTHUR AIRPORT
RONKONKOMA, N.Y. 11779 63T-588-7771
TT Eng 313
Prop D
P.0. B0X 847
ALVA MUNICIPAL AIRPORT ALVA, 73717 (580) 327-1565 FAXH( 580) 327-0526
Al1714 SHIP T0: 5LLTO:
ORARI, BILL s6 CLEARMEADOW DR
CIORC MEADOW DR BILL I, 238 CLEARMEADO DR
EAST MADOW EAST MEADOW
NY 11554 11554
VIA FOB TEKMS ORDERH RE
UPS/SURFACE/CC ALVA CREDIT CAKO 10H13
P/N DESC RICE DIS 3 X
PIPER PA28-180 S/N 28-7305476 WK65339-02 K65339-02 ARMRE ST RI
WK99252-10 K99252-10 COVER EXHAUST V 2 2 WK79456-00 K79454-00 CAP ASSIST STRA
WK63149-17 K63149-17 RH UFPER BOW*
K76145-00 CAAIN DOOR HK76145-00WK99904-03UK99904-04
K99904-03 RH CTR WINOOU K99904-04 RH REAR WINDOW K99903-5 RH INDO FRorT K67550-02 TRIM (W1HDSHIEL
WK 99903-5 WK67556-02 03-3
wK 04-0 K99903-3 LH WINDOW FRONT
K99904-05 LH CTR WINOOu
**-02 LH AR WINDO
PROCESSING IS 4-6 WEEKS
Sl Reckuw tum sa mea nopetn k me mte
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SIGNATURE& CERTIFICATE NO. OF PERSON PERFORMING WOAK DATE TIME N METER
SERVICE TIME
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TTAC S13
Tac 343
Smeh 492 Tin 3613
A&P AIRCRAFT MAINT. INC. MACARTHUR AIRPORT-
RONKONKOMA, N.Y. 11779 631-588-777-
T Pp 313
MAINTENANCE LOG SUPPLEMENT
S.N. 28-7305476 N34 ST TiIME 365.sT Performes annual MSPectron iq.w FAR43 4gendix D .
Keplaced o service door hinqe aSsq .Replaces nductun. urbox Seal. Secured nese qear bonper rtta1ner,
EPfe cted munor repair te lower door hingt as f
AC A3.13 D, Pnttdh dhegEs ok. Kepla ced vacuom ilHer.kepla ced qyro He.Replaced u f R/4
fuel tank pla card S .Keylaced flap handle bushin boH Secured as necesrary. Kepla ced P.ots nversal gotnt.Replaced ELT Vattery due NoV. zo6. C/w FAR 91.207 < INSP.ejecks o. Rep laced A HDrake calioer o rings
TYPE A 28-180 DATE /0 PTEMBER 2o4
Ae TT 3S. EN6 TT36I5.4 ENSSMOH 499.4L PRo TT 36IS.6 PAoPSMoH 103.52
CONTINUED ertifieete- S gnea-
MAINTENANCE LOG SUPPLEMENT
TYPE PA 28-(80 S.N.28-7305476 DATE /0 SEfTENREL2oo4
N341ST TIME 361S.6T
Serviced tbled brake systeM .No luES noted. Keplaced 44 R{* brake pads. Replaced 2) foruard
hat hanmel capS .Replaced cadin het duct. Replaced a 4H $P/4 aileron rod ends .Kepaced inducti auv iHe. Eet ed minor repai +o
lo Coul as pew tC 43. 13 B.Replace2 harswave
e stabilator trim tab .ke/laced lower cou
boshing retauners (2). Pelaced nain wel dain asket Secured as necessary .Ao leag
0Ted. Reylaced cabin deor Sa. Adgus+es Stabilator trin cables p service manual. -lonTIJUED > Signed Sertificate
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TOTAL TIME
TACH OR
RECORDING DESCRIPTION OF WORK PERFORMED
SiGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK DATE N METER
TIME SEAVICE
TOTAL brougt MAINTENANCE LOG sUPPLEMENT
S.N.28-7305476N 34I ST TIME 361S.6T
Keplaced att Pao rod ends.Funttian checks ok.
TYPE PA 28-180DATE /O SEPTEMBER 2004
nstal es R/4 wing strut service plog. Tastalled flap handle sheil&. R«places LA I R/A bake discG.Replace d RA wheel assy inner tube as pev 3erice an val, torgu% servIeto to Specs,
No eqs noted. c/ AD. 44.05-09 Tductun riHters , Repla ce dIR, neut due a.20as ew A. D. 99-24-/0 Pre cise Rlight vacuUm Syste checks ok, next due Sept. 200S. C/w A.D. 96
l9-o3 Flap nandle a4tach bo t Keplaced harduare. clwA.D.s-2-13 oil coole hoses next due boHPST.1.S oR SEPT. 20o5. Sighed
-CoNTIADUED Gertifieate
MAINTENANCE LOG SUPPLEMENT
S.N.28-73o5475 DATE ( EPTEMRER2o4
C AD 76-07- 12 Bendik switch , net doe Sept. 2o0S. Clw A .D 75,24 02 Loose seatS n@xt due Set. 200s, cl» A. D 7S o8 o3 Fuel-
drain alue. c/w A.D. 72 -08 -o6 Man ln9 qeav tovg lbS next due e 411S.6T.I ceriy hat his ARFRAM E hes been nsecr ed in accordence wtn an ANAOAL
TASPETION and was detemited to be n
N341STL TYPEPA8-180 TIME 36S.6T
arwo ry condtuo
Certificate #425?063 1.A.1 Signed
N341ST 2/4/2005 PA28-180
Installed customer supplied vertical compass card. Performed compass swing. N=002 30-27 60-57 E-87 120=119150-149 S=181 210-214 240-246 W-276 300-305 330-335
Michael Tarascio A&P 2924231
Page No.
TACH OR
RECORDING METER
TOTAL DESCRIPTION OF WORK PERFORMED TIME DATE
SIGNATURE & CERTIFICATE N0. OF PERSsON PERFORMING WORK IN
SERVICE T IME
CERTIY THAT HIS ypoefes as pez 1os tm cheek WAS DEHEAMINED TO BE|IN AIR WORTAYHAcs tallstasks _Pepecha
CERTIE 7NO ALG7278
TOTAL brought forward from previous page
HAS SENNSPEGTED IN AGCORDANCE WITH ALA0 AA INSHECTION ANDtPMAI RRdlec Segucal Kaffos
CONDITION. AUTHORtZED STGN�TUREaeo
kherl bavdais Lulka/all an keok ofoTAL TIME 323S m-oq ri a p TAC323
T3mo4i
7320A &23
Lnegan age ik ok felMmard kase Tje
N34IST September 2, 2005, Aircraft TT: 3735, Engine TT: 3735, Engine TTSMOH: 618, Propeller TT: 3735, Propeller TTSMOH. 823, Tach. 3735 I certify that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an
etermined to be in an airworthy condition. AD BI-weekly summary checked ANNUAL INSPECTION and wa through 2005-17. Complied with all AD's due this 100/Annual as per 100 hour insp. this date. Emergency Locater
Traasainer jspeçed jnacordance with FAR 91.207(dM14). ELT battery replacement due Sep 2006
Kendalí Leek ÁALP*073237431A
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TOTAL TACH 4OR DESCRIPTION OF WORK PERFORMED
RECORD'NG METER
TIME
TIME DATE SIGNATURE&CERTIFICATE NO. OF PERSON PERFORMING WORK N
SERVICE
TOTAL brought fonward from previous page
AncencLHAS BEN NSPECTED IN ACCORDANCE eko Ns pen lco m che
WITH A 04. - INSPE¢TION AND WAS DETERMINED TO BE|IN AR WØRTHY saia Ps, tss , skk CONDIT'ON, UTHORIZEh SIGNATURE
CERTIFIGATE/NO L72st. fernekr/ al1 eel bn DATE7UA6 TOTAL TIME iU
1736 7sr14 7o7
CENTIFY THAT THIS
a AD 21-02 A lk us/ja No ck Da
ole a 921 lAD 26-07 kena Sts
eloAD25ws Loos Srd D A7 duAD z5-vss3 Fel elea.d Pre 9lo n RDok Dar 3<2/
et lo7ot4ls Test ltm os_checá/ k N341STSeptember 19, 2006, Aircraft TT: 3821, Engine TT: 3821, Engine TTSMOH: 704, Propeller TT: 3821,
Propeller TTSMOH: 909,Tach: 3821 I certify that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an ANNUAL INSPECTION and was determined to be in an airworthy condition. AD BI-weekly summary checkedthrough 2006-18. Compliedwith all AD's due this 100/Annual as per 100 hour insp. this date. Emergency LocaterTrsgsmterpetedinardance with FAR 91.207(d)(1-4). ELT battery replacement due Nov. 2006.
Kendalí Leek ARP07323743IA
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TOTAL TIME
IN SERVICE
TACH OR DATE RECORDING
METER TIME
DESCRIPTION OF WORK PERFORMED SIGNATURE &CERTIFICATE NO. OF PERSON PERFORMING WORK
TOTAL brought forward from previous page CERTIFY THAT THIS ATEAGHAS CEFN INSPE¢TED IN AccORDANCE wHTH A OA INSHTCON AND/,2 4e2u/LedWAS DETERMINED TO BE NAIR WORIAY- Sepuzey 5 le,botes, Ts CONDITIQN.
AUTHORIED SIGNATURE yd pes5 labbedAl Ten e DATE 0 PAR2257
fOTAL TIME 84L
TSpp 122|
G 6-13 codh hsy 6y pqk Dat
3%_h Ap 26-07-/t Sandes seytiG A en ADok bnv 349 A0 7C24-6r bos
ael
N34ST
September 18, 2007, Aircraft T: 3891, Engine TT: 3891, Engine TTSMOH: 774, Propeller TT: 3891,
Propeller TTSMOH: 979. Tach: 3891
I certify that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an
ANNUAL INSPECTION and was determined to be in an airworthy condition AD BI-weekly summary checked
through 2007-18. Complied with all AD's due this I00/Annual as per 100 hour insp. this date. Emergency Locater
Transtaitter inspoercdaccordance with FAR 91.207(d(14). ELT battery replacement due Dec. 2009.
Kendan Leok AKP1073237431A
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DESCRIPTION OF WORK PERFORMED
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK TOTAL TACH OR
TIME RECORDING DATE IN METER SERVICE TIME
TOTAL brought forward from previous page
LCERTIE THAT THIg_Izcha HAS BEEN INSPECTED IN ACCORDANCE
Tnspe-kene e dd dheof
WIT A O E 4NSPEGTHON AND- 5e2UL Tes, Safa WAS DEERMNED fo BE AN AR WORTHY CONIL AUTHED SINATURA
yed ssstArbtla{so
Lst. elnesro DATE0/4 ToTAL TIME 324O opn ee hc34fo
md S26 bank pak_bo-ios phces
l 75 24-0i cosst Sa]ldue Fo_ lw AD 75 003 e dnsn d Da 9los AD 72 os on landui ges As pea AQ ek
By|Lasp_s Dar :7 Test ele_choka
N341ST September 9, 2008, Aircraft TT: 3940, Engine TT: 3940, Engine TTSMOH: 826, Propeller TT: 3940,
Propeller TTSMOH: 1028, Tach: 3940 I certiífy that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an ANNUAL INSPECTION and was determined to be in an airworthy condition. AD BI-weekly summary checkcd through 2008-17. Complied with all AD's due this 100/Annual as per 100 hour insp. this date. Emergency Locater Traagelfterdspocted ip aepordance with FAR 91.207(d(14). ELT battery replacement due Dec. 2009.
Kendall Leck A&P1073237431A
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TOTAL TIME
TACH OR PECORDNG DATE
IN
SERVICE METER 7IME
DESCRIPTION OF WORK PERFOAMED SPGVATURE & CERTIFICATE NO OF pEASON PERFORING WOAK
N341ST
October 8, 2009, Aircraf TT 3982, Tach 3982 Changed vacuum regulator filter (B3-5-1) and repBaced intake sy stem air filter BA 1O4 with element (BA3). Seniced tires, hattery. stnts. fncl filter w/scal (462-049), hvdraulic brake resavoir and inspected & repacked all whacl bearings Complied with SB11RI (MLG cast strut lugs) by inspection. OR Replaced right front (62061-002) & rear (62061-804) wingwalks, for dctails of this nepair. see FAA or 337 this datc. Repaired nose stnt bracket. replacod bumper (452.047). 2 cisor bolrs (AN5.1A, let brake caliper "o ing (MS28775-222). right brake caliper "o" ring t bolts (101.1160), hth MILC es (600x6 6ply (Condor). l outbd brake pad (o6-10500), both ailcron outed static wicks (SW10-96) and tetMLG front fairing clip (63342-0)). Cleancd battery box & paintcd with acidproof paint. tightened all
nght top. 2 Jcft inner top & 3 right lower ldg gear stnut bolts. Repaircd right front cowl pin mount on
upper cowl. Aircraft serviced and hubricatcd in accordance with Piper Service Manual Pertformed
operational check of systems, ON
attecting airworthiness of this aircraf. W 7/7-/CW p AOYS14 6N N Dy Ceruiy that this AIRCRAFT has been inspected in accordance with a 100 HOUR INSPECTION and was
determined to be in an ainworthy condition.
Aircraf owner has been given list of discreprancies to be repaired not
Roberto Ruiz A&P3233677
N341ST
October 8, 2009, Aircraft TT: 3982, Engine TT: 3982, Engine TTSMOH: 868, Propcller TT: 3982.
Propeller TTSMOH: 1070, Tach: 3982
Certity that this AIRCRAFT including ENGINE and PROPELLER has been inspccted in accordance with an ANNUAL INSPECTION as per FAR 43 Appendix D and was determined to be in an airworthy condition. AD
B-weekly summary checked through 2009-19. Complied with all AD's due this 100/Annual as per 100 hour insp.
this date. Emergency Locater Transmitter inspected in accordance with FAR 91.207(d(14). ELT battery
replacement due Dec 2009
Sean McFadden A&P856681211A
N341ST November 1, 2010, Aircraft TT: 4010, Tach: 4010
Changed vacuum regulator filter (B3-5-1) and intake system air filter element (BA3). Serviced tires,
battery, struts, hydraulic brake resavoir, fuel strainer and inspected & repacked all wheel becarings.
Replaced hose clamp to carb heat duct, right inbd static wick (SW10-96), left nav light bulb (W1290-14V)
and 2 bolts in left MLG strut housing. Complied with SB 1131 (MLG cast strut lugs) and SB 856
(stabilizer attach bolts) by inspection, OK. Complied with AD76-07-12 (Bendix ign switch) by operational
check and AD75-24-02 (scat quick disconnect) by inspection, both OK for return to service. Aircraft
serviced and lubricated in accordance with Piper Service Manual. Performed operational check of systems,
OK. I certify that this AIRCRAFT has been inspected in accordance with a 100 HOUR INSPECTION
and was-determined to be in an airworthy condition.
Roberto Ruiz A&P3233677
N341ST November 1, 2010. Aircraft TT: 4010, Engine TT: 4010, Engine TTSMOH: 96, Propeller TT: 4010,
Prop TTSMOH: 996, Tach: 4010.
I certify that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an
ANNUAL INSPECTION as per FAR 43 Appendix D and was determined to be in an airworthy condition. AD
BI-wcekly summary checked through 2010-21. Complied with all AD's due this 100/Annual as per 100 hour this date.
Emergency Locater Transmitter inspected in accordance with FAR 91.207(dX14). ELT battery
replagement dre Jan, 2013.
Kendall Leek A&P107323743IA
Page No.
DESCRIPTION OF WORK PERFORMED SIGNATURE & CERTIFICATE NO. OF PERSON PERFOAMING WOAK
TOTAL TACH
TIME RECORDING DATE METER
TIME IN
SERVICE
TOTAL brought forward from previous page
CERTIF THAT THIS eAK
HAS BHN NSPE*D N CORDANCE
WITH L00 HA WAS DETE O 17tat- wORIH) S¢EVce ydrAss Sa Adp nds
COND'TIDN AUTHORZED SIC:NATURE
C :ON ANDD
t1.
CERIIFICAT� NO. | LP2L2E- - lwAD 24-07-12 bmlepsurheb DATE/Z0T
Re 403 TmbA V07Y
wl check k alwAD2S 24- vr dr 3
Sent h elssensk Dne /3 n wra-/
TOTAL TIME #O3Z
Pen0TB
dopo9 -1S eder:lun " SB 3/ enaui tel s25 ist si-
/3 MeAD 22-oruu Langkuis ae peu NO
Plls 20 N341STDecember 20, 2011, Aircraft TT: 4032, Engine TT: 4032, Engine TTSMOH: 1018, Propcller TT: 4032,Propeller TTSMOH: 1018, Tach: 4032 I certify that this AIRCRAFT including ENGINE and PROPELLER has been inspected in accordance with an ANNUAL INSPECTION as per FAR43 Appendix D and was determined to be in an airworthy condition. AD Bi-weekly summary checked through 2011-24. Complied with all AD's due as per 100 HOUR INSPECTION this date. Emergency Locater Transmitter inspected in accordance with
FARSY207AELTbetery replacement due Jan. 2013.
Kendall Leek A&P107323743IA
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TOTALTIME
7A
DATE ECORD OESCAIPriON OF wOK PERFOMMED- ET TER SiGNATURE A CERTIFICATE N0 OF PERSON PERFRMING WORK SERVICE VE
TOTAL brought forward trom previouS page
I THA THS AI A SEEN INSOr IN ACc.oRDANE WHH A/80 |n YSpraGN ANB.
AUTHORIZED SiGNATUAE kes, lasb "ai'Zl GOND TION. C
etRFIRNCATE NO AA 522
74 44U3
stans: by reA sk. Pae 4/36 inn
b 25 24- sint Qmck.desumet _ Zispel_
7 ok
N341ST Apr. 2, 2013, Aircraft TT: 4038, Engine TT: 4038, Engine TTSMOH: 1023, Propeller TT: 4038, Propeller TTSMOH: 1023, Tach: 4038 I certify that this AIRCRAFT including ENGINE & PROPELLER has been inspected in accordance with an ANNUAIL INSPECTION as per FAR43 Appendix D and was determined to be in an airworthy
condition. AD Bi-weekly summary checked through 2013-05. Complied with all AD's as per 100 Hr Insp this date. Emergency Locater Transmitter inspected in accordance with FAR91.207(d(1-4). ELT batteryreplaçed(BP1035)aext replacement due Feb. 2014
Kendall Leek A&P*07323743IA
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Page No.
TOTAL TIVE
TACH O RECOD4G
DESCRIPTION OF wORK PERFORMED=
DATE TER SGVATURE & CERTIFICATE O OE PEASON PERFORMNG WOPK
SERVICE TIVE
TOTAL brought forward from previous page
EN NSPECD IN AGCORDANCE INECnON AND Hyd Rsc AS
WAS DETEAMNED TÒ BE aIR wOATHY Tsm Set
CONDITION. AUTHORIZED SiAJRE CERTIEICATE NO : DATEZlIE
WITH
T5met d 30
CluAD 25T0 clers ps )s AD dDie A/(M NY
7 7-2 k dusard As ynct YAo 7£ 0S- os
a eel ChAP 2013 02 -/3 shb 41bk }/ayrel
dh eded aAd N341ST
Sep. 15, 2014 Aircraft TT: 404, Engine TT: 4044, Engine TTSMOH: 1030, Propeller TT 4044,Propel I certify that this AIRCRAFT including ENGINE & PROPELLER has been inspected in accordance with an ANNUAL INSPECTION as per FAR43 Appendix D and was determined to be in an airworthy condition. AD Bi-weekly summary checked through 2014-18. Emergency Locater Transmitter inspected in acçordance vith FAR91.2074d)(14). ELT battery replacement due Feb. 2015
TTSMOH: 1030, Tach: 4044
Kendall Leek A&P107323743IA
ta Had7.3 heosed JaDn,segnd
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ARO FA REPaR STarCN Ne tes
9at INrERNATTCNAL AIRPORT (AH) 11300
34 NW Jh sTeEET MtAMI SPRINGS, FLORICA NES0N USA
SEEN NEOPO S ENSMaiL ADOnESS c aox t MtaMI, FLORIDA 1318t USA
Tvpe
CKD4DITHON MUHDITED SSNATRE C TFFEODATE NO
Part NioSAD15.4 Serlal No 3 336E
OVERHAULED Customer Ocaol kea Type of Service
slr 3) Inspected By dl 2 9 1987
che Tasy et 1t AD2-67-r,
W) 7S-c-¢S l chknng As A ol e " un i
D75 24- Jail G oliskawds Asp
GT AD 22 -o S -o Ljrd 99/ >a p t 0E)-1
/dt
Bnllogo 1o 3 a
N341SP Oct. 5, 2015, Aircraft TT: 4051, Engine TT: 4051, Engine TTSMOH: 1037, Propeller TT: 4051
Propcller TTSMOH: 1037, Tach: 4051
I certify that this AIRCRAFT including ENGINE& PROPELLER has been inspccted in accordance with
an ANNUAL INSPECTION as per FAR43 Appendix D and was determined to be in an airworthy
condition. AD Bi-weckly summary checked through 2015-18. Emergency Locater Transmitter inspected in
accordance with FAR91.207(d)(1-4). ELT battery replaced (BP1035). ELT battery replacement due Dec.
2017.
Kendall Leek ARPI073231431A
CERT THAT TH 2SEEN IN9PECTFD IN ACCORDANC
A[Q0NA DETERMNFD TO PE IN AIR WORTHYCnt tioON. Ae niZED SIC¥ or
n5,1ec ns pon 1eo cps, ls sgI
iNSPECTON AND
s AD ol Dee unn dhr AD 72 05-«7_LY*9
DAIE/TT
T OS7
N341ST
Nov. 2, 2016, Aircraft TT: 4057, Engine TT: 4057, Engine TTSOH: 1043, Propeller TT: 4057,.
Propeller TTSMOH: 1043, Tach: 4057.
I certify that this AIRCRAFT including ENGINE & PROPELLER has been inspected in accordance with
an ANNUAL INSPECTION as per FAR43 Appendix D and was determined to be in an airworthy
condition. AD Bi-weekly summary checked through 2016-20. Emergency Locater Trans1mitter inspected
IAW FAR 9V207(¢)(1-4), next battery replacement due Oct. 2017.
Kendall Lcek A&P107323743IA
Page No.
DATE OESCAIPrION OF WOAR PERFORMED
SIGNATU2E & (ERTIFICATE NO OF PERSIIN PEaFOAMING WORK
TOTALS brought rorward from previos pag
N341ST 06/2/2018
TACH 4062.78 ACFT TT 4062.78
AD 72-08-02 Landing gear torque links, Next inspection due @ TACH 4115.6
AD S-08-03 Fuel drains OK at this timme next due @TACH 4162.78. AD 7514-02 Seat quick disconnects OK at this time next due @TACH 4162.78.AD 2010-15-10 Control wheel shafts OK at this time next dueTACH 4162.78.
AD 2013-02-13 Stabilator control system no defects noted next inspection due 9/2022 or Tach 7044.
AD 2017-14-04 Engine oil Type D hoses, needs to be addressed at this time. AD 2018-07-03 Fuel selector placards, OK at this time.
T l2RI Bendix ignition switches no defects noted ops check good next inspection due Tach 4 162.78.
nis aircraft has been inspected has been found to be safe for one-time ferry flight from KFRG to HWV to have
Annual inspection performed. Alexander Duran A&P2677910
8/1/2018N341ST ACFT TT 4062.78 TACH 4062.78
KOutine 100HR inspection accomplished 1.A. W. FAR Part 43 Appendix D checklist. Replaced ELT battery next exp
08/2020. Performed ELT test I.A. w. FAR 91.207. Replaced vacuum regulator filter PN B3-5-1. Replaced induction
air ilter PN BA-3. Replaced all flexible fluid hoses with new hoses firewall forward supplied by PHT. Oil cooler
noses are Type D. Treated flap brackets for corrosion and painted. Treated nose wheel for corrosion primed and
painted. Vacuumed out tail cone, floors and battery box area. Re-riveted Aft Left top cowling latch as required. C/W
SB 1242. Replaced Rudder bar support assembly PN 63451-000. Next inspection due @ TACH 5262.78 as per SB
242 dated January 30, 2015. Rigged Rudder pedal system and nose wheel steering system TAW Piper AMM, no
defects noted. Ops check ok.
AD 72-08-02 Landing gear torque links, Next inspection [email protected]. AD 75-08-03 Fuel drains OK at this time next due @ TACH 4162.78. AD 75-14-02 Seat quick disconnects OK at this time next due @TACH 4162.78.
AD 99-24-10 Precise flight stby vac system OK at this time next due @TACH 4162.78.
AD 2010-15-10 Control wheel shafts OK at this time next due @ TACH 4162.78. AD 2013-02-13 Stabilator control system no defects noted next inspection due 9/2022 or Tach 7044.
AD 2017-14-04 Engine oil cooler Type D hoses C/W No further action required. AD 2018-07-03 Fuel selector placards, OK at this time. AD 76-07-12RI Bendix ignition switches no defects noted ops check good next inspection due Tach 4162.78.
This aircraft has been inspected I.A.W. a 100HR inspection and was determined to be in airworthy condition.
William Sullivan A&P 3734799
8/1/2018N341ST
ACFT TT4062.78 TACH 4062.78
I certify that this aircraft has been inspected I.A.W. an ANNUAL inspection and was determined to be in airworthy
condition.
Alexander Duran 2677910IA
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Page No.
N341ST12/22/2019 TACH 4076.23
ACFT TT4076.26
Nune ANNUAL inspection accomplished LA.W. FAR Part 43 Appendix D checklist. ELT battery next exp
erformed ELT test 1.A. W. FAR 91.207. Replacedvacuum regulator filter PN B3-5-1. Replaced induction ariter PN BA-3. Cw SB 1242. Next inspection due @ TACH 5262.78 as per SB 1242 dated January 30, 2015. AD 72-08-02 Landing gear torque links, Next inspection due @ TACH 4115.6. AD 75-08-03 Fuel drains OK at this time next due @ TACH 4176.23. AD 75-14-02 Seat quick disconnects OK at this time next due @TACH 4176.23.AD 99-24-10 Precise flight stby vac system OK at this time next due@TACH 4176.23.AD 2010-15-10 Control wheel shafts OK at this time next due @TACH 4176.23.AD 2013-02-13 Stabilator control system no defects noted next inspection due 9/2022 or Tach 7044. AD 2017-14-04 Engine oil cooler Type D hoses C/W No further action required. AD 2018-07-03 Fuel selector placards, OK at this time.
T 2RI Bendix ignition switches no defects noted ops check good next inspection due Tach 4176.23. ns aircraft has been inspected 1.A. W an ANNUAL inspection and was determined to be in airworthy condition.
Alexander Duran 26779 101A
Airframe Logbook Piper PA 28-180 S/N: 28-7305476 Reg: N341ST Tach:4077.17
Kemoved parkingbrakemaster eylinder and overhauled with new O-Rings P X: MS28775-012. MS28775-114 & MS28775-113. Removed right toe brake cylinder and overhauled with new O-rings
P'N. MS28775-110 (2 each) & MS28775-113. Removed left toe brake cylinder and overhuuled with neW
O-rings P N: US28775-012. Ms28775-113 & MS28775-110. Reinstalled left. right toe brake eylinder and master brake cy linder. Removed and replaced left and right caliper O-Rings with new MS28775-222. Replaced left brake caliper back plate assembly with new PN: 755-886. Installed new APS 066-1000
braking lmings on let and ight brake assy. Serviced brake system with 5606 and bled system as required. Leak checks and system checks good. All work perfomed I.i Piper service manua.
C OK for retum tservice.
Gabriel Acevedo Jr June 10, 2020
A&P 2827501
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adlog
ENGINE MAINTENANCE RECORDS
2 Log No.
Aircraft Registration No. N 341ST
Engine Manufacturer ycomng
Model 0-340-A4A
Serial No. L-17720-3LA
Date installed on aircraft.
Time Between Overhauls (TBO) 2,O0O _Hours
If used on multi-engine aircraft:
RightFront
Left Rear
ERO ECHPUBLICATIONS INc.
P.O. BOX 1178/FREEHOLD, N.J. 07728(201) 462-5330
1979 AeroTech Publications Inc
Page No..
TOTAL TIME
TOTAL TACH OR DESCRIPTION
OF WORK PERFORMED
RECORDING
METER DATE TIME SIGNATURE&
CERTIFICATE NO. OF PERSON
PERFORMING WORK
IN SINCE
OVERHAUL SERVICE TIME
rom Bos |A 2912.0kL9.or or2912,o
TOTALS brought forward from previous page
12-/6-88 2912.DP_698.2e29120rAnnuainspection:
2912.08
Airereft Te tel time: 2912.08
Engine Total kime:
Peapeller letal kime: Engine Time SMOH:
Peapeller SMOH:
Remave Reglacedoillilles CH 4P110 andSae
2.Drain ¢Replacad dL RSilledwith ChevtonAreo
2112.08
49808
0.00
3 Campcessitn test
. 79o 2. 2 3. o t.h
4Replaced fael pump blast tuee.
s. Reploced Cool Air blsasi iahe toheat
exchaager
Clezned and Gaped REM 38 Spark plug.auk . Prepeller Ovechaul (Major) B, Avition
Propellers Inc. lastalled and safeties k. Cauki.mgbetk Mepec / Lower repaired far
Ctacks, hole änd wbEn 2¢ezs. hinted znd_ insalled.
Replace clatina steip onte tire wallL
oleplace Stacder bendix Geac Ice is engine has heen inspeeted in accore ance witl mznuacturers inspedian regert.Anna) hado-z07.and have _somplied weth th Lllewing ADs; AD F-26-2, AD 1t-2-2,AD 74-7-12,| hat ste zpplic aele fe the 03Lo-44A Egine
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Page To TOTAL
TIME TOTALTIME
SINCE OVERHAUUL
TACH OR
AECORDING METER
DESCRIPTION OF wORK PERFORMED SiGNATURE & CERTIFICATE NO. OF PERSON PEAFORMING WORK
DATE IN
SERVICE TIME
2912, o8| 698.2912,08 TOTALS brought forward from previous page
installatien. This Engine meels FAA «nd Manutacturefs
Specilicatins Relurn to service. k Sn 18720 3 1I
2-8-902981.4 767.68 29n.6y Annual lnspection Aircealt T.T. 29P.4
Engine T.T 2991.68 5MOH 747.L8Propellec TI Repve £ Replaced oL Fltee CH 4PMo 4 Sefetied
. Draineil and leilled witk chevron Ares /00
291.L SMOHL 69.
presien Test: so 2, "20 3. ho4. "o
. Cloaned nod Gaped REM 38 champein Spask plug
latilytkis engine kas bren nspected inRmcordac with manuacturers inspechos eper h 23o-so7.and haue co plied witL the fllowing Ad's: Ad R1-4-2 Facei(Macvel-Seheblec) arburetor
Did nat xeply. by serial aunbet. AD Y-2 28 lndueien A hter. AD 1-9-7Re3 RBendix Magneto. -Ihis esgine_neet FAA tManutacturers specikicahien Reutata seciice enLd 2036 IA, a 22
12-24-90303Gotint|30.38|Anauzl lnspechim
|Engine TaialTime 3om3 SMOH808.38 Camgcess Tsst, h» a? 32o 1 Daia elEnd refi ith chevnn Area /0o Remaved ispecion 2ud eplkced Ster. cA HEUDisA
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DATE sERVCE
'ceri, s sine e inspecfed
aee , pee luSpectint cke ek list.
NR3o a07 This esne meets FAA fnu hackurers Pecficatio, Returs servic e.
J9 72o3& 1A
9.q1 3a 1 81 enAaL ie Coaf. C *4 , ou A l cna, RRL ?Les
-16-230449 So.5 30y.AanuaL aspectio
clean Gap Plugs. Tested énsll.I cectity this enzine has beeainspected
accordaude th Rper Hecat laspectiom ceport a 230-207 his essgine mcets FA4 4 Madufaatutei's speatiktinKetuen to SeniseE
bund Ck
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Page No.
TOTAL TIME
TOTAL TIME DATE TACH OR
RECORDING IN
SERVICE DESCRIPTION OF WOAK PERFORMED
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK SINCE METER
TIME OVERHAUL
wapIOTALS brought forward from previous page
oehr A A
TurcAutma his is to certity that the engine described hereafter has been overhauled to manufacturer's new parts
S by Penn Yan Aero Service, inc. Engine disassembled, cleaned, and inspected in accordance with nuiacturer's instructions. All steel parts magnafluxed, reassembled in accordance with manutacturer's
urtrent overhaulmanual. Engine test run. All applicable Airworthiness Directives are in compliance. See A.D. list supplied. A description of these repairs is on file at this agency under:
w.O.# 10943 DATED 2/25/93MFG. Lycoming MODEL 0-360-A44A
Serial No.L-17720-36A Time in svc.
PENN YAN AERO SERVICE, INC. Airport, Penn Yan, New York 14527 APPROVED REPAIRSTATION NJR350K
BY PENN YAN AERO
Authorized Signature
OIL RECOMMENDATION STEEL OR NITRIDED CYLINDERS
Use non-detergent SINGLE ViscosITY mineral oil for the first 50 hours or until oil consumption stabilizes at a satistactory level - up to 100 hours. Then change to SINGLE VISCOSITY ashless
dispersent (AD) type oil. Penn Yan specifically recommends that you do not use multi viscosity, synthetic, or semi synthetic prod-ucts. Use of these products will void warranty on valve stickinng. Change oil & filter after the first 10 hours, then at 15 more hours and every 25 hours thereafter.
WE DO NOT RECOMMEND THE USE OF MULTI-VISCOSITY OIL!
The Accessories Listed Below Were Overhauled and Supplied With This Engine
DATE 2/25/93 SIN
ENGINE:0-360-A4A SN. I-17720-36A P/N
10-163045-3, A193541RT MAG LT MAG 10-51360-45, A102082
ALY 6422, 8LO0014 ALT/GEN
INUCARB 10-3878, G-50-8221
EUEL PUMP LN-15472 NEW
STARTER MZ 4206, B000279
TURBO CHARGER NA +10 Nitride Bores
PENN YAN AERO SERVICE, INC. APPROVED REPAIRSTATION NJIR35okAirport, Penn Yan, New York 14527
W.O. No. 10943 Authorized Signature
nuINGMETER
TIME
DESCRIPTION OF WORK PERFORMED- SIGNATURE & CERTIFICATE NO. OF PEASON PEAFORMING wORK oVERHAUn
TOTALS brought forward from previous page
R6 3-5-933ua 2 3l.11 as+nLLED gaeE Sae*L:/7720 30A Ow
N34/ST AFTER Major OuGA HAUL IeeformE0 GeDua ei lsad QPs CHECK Goot
Date4-5Hours t O and Filter Chanaed
echanic eone Le. 2BACA
91-1|3147. |31 3H7 |npaTd 1//w q/00 lu nslasCqlhoda e04T, Changas ei and ks Suresd
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=143/4242 3 3/42 e7T4LT)4E RIL#-boen inepected-in aceerdane- th A ID RIAN ANNUAL inspection, ánd w
nbwE3/422 PeS1/TAH 9etormined to tetairworthyr comdtrooof this date.
pate 2 IToar Time Maned /iLL22eaou s ypt B//8 He S, Ti VE L9:7
win sUB-TOTALS this page
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Page No
TOTAL TOTAL TACH OR DESCRIPTION OF wORK PERFORMED
SIGNATURE & CERTIFICATE No OF PERsON PERFOAMING WORK
TIME DATE SAE
SINCE
TI RECORDING N TER ME
TIME SERVICE OVERHAUL
TOTALS brought torward from previous page
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TOTAL TACH OR
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Page No. TOTAL TOTAL TACH OR
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TOTALS brought forward from previous pagee
|CERTIFY THAT THIS -HAS BEHN INSPEQTED IN ACCORDANCE
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MAINTENANCE LOG SUPPLEMENT o $
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Type: PA 28-180 s.N
. 28-7305476 E
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Date: 1O
sEPTEMBER 2004
Per form
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411Compression test pur formed
as % llows: C
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. Drained oil ¢ eplenched wf Aeroshell 1S»SO
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. 7`406 .No
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no
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SUB-TOTALS this page
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to n
ext page
Page No.
TOTALTIME
TOTAL TACH OR
RECORDING TIME
SINCE OVERHAUL
DATE METER
TIME
DESCRIPTION OF WORK PERFORMED SIGNATURE & CEATIFICATE NO. OF PERSON PERFORMING WORK
IN
SERVICE
MAINTENANCE LOG SUPPLEMENI N 34USST Type: PA 28-180 s.N.: 28-730547 Time: 3G15.0T Cleaned engine. Secved intake mani told rubDer
Date:/0 sePTEMBER 2004
boots as Aecessaru, Pertoraes avound run, engia- oPs funtim eheck normal. Ua couled qngi,, A0 lE Pound. Cou led engine ¢ returned to nomed. TCW AD 2004 -10- 14 ,net doe Pop strikel Sujden stag Cr hat 4his engin has been nspeor h aCcordan ce with an AannUAL TNSPECTIOU and was deterintd to be in ainwomy CondHM
Certificate 925H3 1A.
N341STTIME: 3o34.06T
MAINTENANCE LOGSPPLEV 20(0 27 TYPE PA ZE-BO DATE: 14 OCTOEER 2004
Uncouwles engine. Drained oil.0il ganple2 tak en for anals sis. Removed , cut ofen inspected o+ie. No defects nted.Lnst a.lLes new oil lter cH4810-t torq el gafetied. Rapleni shed oil with 8gts.ot. Aero shell 15 w So .Perfor med arourd run, no leaks notes . Cowles ergine retum-
ed 4o nôr mal.
cERT.NO. A P 42589OL3SIGNED
3/wesTA 36s6
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Page No.
TOTAL
TIME SINCE
OVERHAUL
TACH OR RECORDING
METER
TIME
TOTAL DESCRIPTION OF WORK PERFORMED TIME
DATE N SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
SERVICE
TOTALS brought forward from previous page
HAS BEEN INSPECTED IN AÇCORDANQE inyalod taler,checbas CERTIFY THAT THTS
WITH A7d0 N NSPECTION AND WAS DETERMINED TO BE IN AIR WORTHX S4Rvned Dg gonSOplgz XC CONDITION. AUTHORIZED SIGNA�URE CERTIFICATE NO PLIZ 22502 75 DATE2100 TOTAL TIME3235L 2,-1Ae 323
2
Y25/o Tck 371781ISMIHE 6
CERTIFY THAT THISAS- HAS BE�N, INSPEQTED N ACCORDANCE
WITH A 0 h_ NSAECTION AND h(2durlWAS EMINED TO BE/A A1R ORTHY os p/ C { eaE677 COMITON AUTHCP"^ SiGNATURE cEATIEICISNO Ei Le Lekler 8o2 2 252
DATE ZIU toTAL TIME 3 Lhhla Sve Dl RAME* TjsI 704
ue aa senui NO 200-8-1
AO JLp 5tute A his, Tj 4n baly
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Page No. TOTALTIME
TOTAL TACH OR RECORDING DATE TIME
DESCRIPTION OF WORK PERFORMED SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
IN SINCE OVERHAUL METER
TIME SERVICE
TOTALS brought forward from previous page
/3/2lo 7hL3SYL
eove 1 Peplncas Unea
Dm SA 24430
3-30-07 39S48|937 J7LRYS CHAN Onl+ FILTb DPoseS PRof
CH 48HO FIprr 33HRS 0deu.
CERTIFY THAT THIs AS BEEN TNSPEÇTED N ACCORDANCE aansed oiit he ahedh!tu WITH ALD0A INSPECTION AND k seeea fr dnsUph,//p4 XC WAS DETERMINED TO BE IN AIR WOATHY CONDITION. AUTHORZED SIGNATURE . CERTIFIdATE, NO.DLMEILEKO 2 DATE 2EC2 |OTAL JIME 3
26 2 7/ l4heo
T3o 72 Tap Atestes all ahuje
QUANTITY DEOunrnon-
9 O 0-08
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Was
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d l
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cn
gin
e co
ntro
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d i
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on
e m
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nti
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(LW
11
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7).
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lace
dal
tern
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bel
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2-54
1) a
nd #
2&3
valv
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ver g
aske
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7590
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Com
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rea
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s as
fo
llow
s: #1
: 70
/80,
#2:
74/
80, #
3: 6
6/80
, #4
: 62
/80.
Per
form
ed e
ngin
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nup
and
lea
k ch
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OK
. I
certi
fyth
at th
is E
NG
INE
has
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insp
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acc
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nce
with
a 1
00 H
OU
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CT
ION
and
was
deter
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d to be
inan
airw
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ndit
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Rob
erto
Rui
z A
&P
3233
677
SU
B-T
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AL
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pag
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Page No. TOTAL TOTAL
TIVE TAC 0
DATE TIME ECOROGIN OESCAIPTION OF wORK PERFORMED-
SHGNATUE & CERTIEICATE NO Or pERSON PERFOAMING WORK SNCE TER SERVICE OVERHAU T VE
N341STNovember 1. 2010, Engine TT: 4010, Engine TTSMOH 9%, Tach 4010 Performed prc inspoction nin p and checked paremcters, all within normal limits Changed engine oil
(Phillips 20W50XC) and oil filter (CH48110). safetied Cleaned. gapped. tested spark plugs and reinstalled with new gaskcts (M-674) Replacod 44 cvtinder asey overhauled by FÄA CRS# AV2R 704K
on their Wo 94268 dhd 9/149 installd with new gaskets seats Refaced all ex hanst pipes and repairedbaffle for #4 cyl. Washed engine and hubed engine controlsfollows: #1: 72/80, #2 65/80, # 72/0, #4 600 Checked magneto to cngine timing, O K Performed
engine runup and leak check. O K. I certify that this ENGINE has been inspected in accordance with a
starter drive Compression readings as
100 HOUR INSPECTION and was determined to be in an airworthy condition
Roberto Ruiz. A&P3233677
N341ST February 07. 2011 Tach: 4018
Drained engine oil and serviced with 8 quarts Aeroshell 80w oil. Replaced oil fiter with new CH48-110 hter
and safeted. Compresion readings were as follws: #1 71/80. #2 74/80. #3 73/80. *4 7160 an engne and leak checked. no leaks noted. All work was performed in accordance with current applicable manufacturers recommendations. This aircraft is appreoved for return to service regarding these repairs. this date and tme
Roberto Ruiz, A&P 3233677
CERTIFY THAT THs s HAS BEENNSPEGHED NA6GORDANCE In4pected s_ pen /13 Ae eh ak li
WITH A LOóHN INSHECTION AND WAS DETERaED TO-8t NAA weRTHY hAnpd eil kkteg checka 2
CONDITION AUTHOTKED S TURE CERTIFICATE NO. RLeak lomn : S0_
23 soca plus,eluaappu+Textel seIs1t
2 24 rebo!b/ Ta 031 TSMoH l61s
oalamy tvalu/ ayen saens AD doo4-10-/4 LA
Casbous ean lok chakas_ok
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TOTALSCarry forward to next page
Page No. TACH O
RECORDING
METERTIME
DESCRIPTION OF WORK PERFORMED
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK TOTALTOTAL TIME
SINCE OVERHAUl
TIME DATE IN
SERVICE
TOTALS brought forward from previous page
CEATFY THAT THS HAS BEEN TNSPECTED INTAGCORDANCE
speck WITH LV.ML.- IN$PECTION AND chnged ol) hllachelez WAS DETERMMNED TO BE IN AIR WORTAY
CONDITION. AUTHORIZED SIGEArURE CERTIFICATFNo A47202 2vaivpblhr LebtS104 . DMTE ZIZTOTAL TIME OZS
Tonts k 102Y
Scheh
*****
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Page No. TOTAL TIME
TOTAL TACH OR
RECORDING TIME
DESCRIPTION OF WORK PERFORMED DATE METER TIME
IN
SERVICE SINCE OVERHAUL SIGNATURE& CERTIFICATE NO. OF PERSON PERFORMING WOAK
TOTALS brought forward from previous page
lagl|O47 039 An_c'oda
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YTHAT TH -AS. BEEN INPECTED INAGCONDANE WITH A200.AnWAS DETERMHNFD TO B IN A6 WERTH CONDITION AUTHQRIZED S"NAHIRE,
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SUB-TOTALS this page
TOTALS-Carry forward to next page
Page No.
TACH OR TOTAL TIME
TOTALRECORDING
DESCRIPTION OF WORK PERFORMED TIME
SINCE
OVERHAUL DATE SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING wORK
MET TER
TIME IN
SERVICE
TOTALS brought forward from previous page
BEEN INGPECTED N ACCoROANCELAsDeeta E Jen Jog k chel WAH A i00AL. iN nON AND WAS-DETERMNED TO BE NlAIn WORIHY CONDITION.
AUTHOR{zED SIGNAJRESRTIFICATE NO. NR7 ATE 0AL TME 2 O 2d asUNll2s2cei leheszaTheo5:7ShmittTo43
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N341ST 8/1/2018TACH 4062.78 SMOH 1048.78
Routine 100HR inspection accomplished I.A. W, FAR Part 43 Appendix D checklist: Compression test as follows, cyl #1)70/80 #2)75/80 #3)75/80 #4)76/80. Changed oil and filter, Serviced oil sump with 8 quarts of Phillips 20/50X/C and installed CH48110-1 Oil filter. Replaced alternator adjustment bracket to engine case bolt. Adjusted alternator belt tension. Replaced exhaust clamp bolts. Tightened intake tube coupling clamps. AD 2017-16-!1 Lycoming cornecting rods NA by date. Run up on ground satisfactory no defects or leaks noted. I certify that this engine has be.n inspected I.A.W. a l00HR nspectiom and was determined to be in airworthy condition.
William Sullivan A&P 3734799 N341STTACH 4062.78 I certify that this engine has been inspected L.A.W. an ANNUAL inspection and was determined to be in airworthy
8/1/2018SMOH 1048.78
condition.
Alexander Duran 2677910IA
SUB-TOTALS this page
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Page No N341ST
12/22/2019 TACH 4076.26 SMOH 1062.26
Routine ANNUAL inspection accomplished I.A.W. FAR Part 43 Appendix D. Compression check as follows evlinder #1) 76/80 #2)80/80 #3) 80/80 #4)80/80. Oil and filter changed serviced oil with 8 qts Phillips 20W/50 and installed AA48110-2 oil filter. Cleaned, gapped and rotated spark plugs. Tightened all rocker box cover screws and oil drain coupling clamps. Retimed both magnetos to engine. AD 2017-16-11 Engine power section NA by date of overhaul Run up on ground satisfactory no defects or leaks noted. I certify that this engine has been inspected LA.W. an ANNUAL inspection and was deternmined to be in airworthy condition
Alexander Duran 26779 101A
SUB-TOTALS this page
TOTALS Carry forvard to next page
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Not
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PRECI8ION AIRMOTIVE CORPORA TION
MODEL MA-4-50-387 PART NUMBER:
SERIAL NUMBER: G-SO Y 11
MFG(REBUILD)OVERHAUL DATE 2113
Service Bulletins Description complied with
MSA-1 Metal Float Installed
MSA-5 Only Genuine Precision Airmotive Parts Installed
| Airworthiness Directives complied with
Description
63-22-03 1-Piece Venturi Installed (A4-63)
69-24-03 Inspected Bowl for Contamination (A1-69)
72-06-05 New Style Throttle Shaft and Arm Installed
89-04-02 New Style Stop Pin Installed (A1-88)
93-19-04 No CFS Float (MSA-4) Numbers enclosed by parenthesis denote applicable Marvel Schebler, Facet, or Precision Aimotive Service Bulletins
The carburetor identified above was manufactured, rebuilt, or overhauled by Precision Airmotive Corporation, using only genuine Precision Airmotive parts, and complies with the above listed Service lletins and Airworthiness Directives.
Questions regarding the above should be directed to your distributor or to the Precision Airmotive Product Support Department.
PRECISION AIRMOTIVE CORPORATION PRODUCT SUPPORT.
Thank you for your contimued support of Precision Airmotive products.
PFC11201 4/94
PRECISION AIRMOTIVE 3220 100th Street S.W. Suite #E Everett, Washington 98204 FAA Repair Station # HJ6R589N Tel: (206) 353-8181 Fax: (206) 348-3545
PRECISION AIRMOTIVE CORPORATION
W.O. No. 233
Name of Part Canb Ue TeA Part Number -3EZF-
Serial Number G50822/
Type/ModelPL-LS
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Puel p
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wORK ORDER/ INVOICE #:GCOl.
GCG AIRCRAFT SERVICE COMPANY
sUSSEX coUNTY ARPORT
2 RUDDER LANE
GEORGETOWN, DELANARE 9947
(302) 855-9706
TO: L LE APTE PoBox o79 N.CoAY Ne HAmeSHIRE
DATE ORDERED: 3-73-
P.0. 4: VEeBAL AIRCRAFT:N34IST JOB LOCATION: GEOEGETDw DE
STARTING DATE: 2:3-93 ATTENTION: LE o3960
TERMS
WORK
DESCRIPTION:TeUBE SHQUT EwguE PeoBLEM 3.0Hzs33.0/HRBEmoLE ANDRELLSTALLEmqaE
BemOLs CoeroSLOO fRomEgE MouaT 2o.oHes Q33.00/HR_
5 Hes (@3.00 He
MATERIALS USED:
QUANTITY PART NUMBER| DESCRIPTION UNIT PRICE AMOUNT
Lo-3S HoSE KT 4j-90 l3-40 L7uEM8S5
3 AN-44A AN3lo3-770 HqTEMP LoCK NOTS
3FSCAT 12
EAQIE HOSEs logD EQIarE MouATS Paae muT Bour KI EqE MocAT Baurs
1a5o.00311.76 7o.50 2o. 2.12
29.4uL
las8818
DuCT HosE 3.50 lO.50 .2 23.52
203o Ae FiLTER 7.21
8085O 712, 5 29235
8050.00
WORK ORDERED BY: uOLEE TOTAL LABOR: DATE COMPLETED : 3-93 TOTAL MATERIALS:
CUSTOMER SIGNATURE:_ TOTAL SHIPPING
TOTAL OUTS IDE VENDORS:NOTE Masa6EmAST Fe6 rs
15% PaeTS 5 Foe 5qȑ
TOTAL TAX:
MANAGEMENT FEE: 530.922TOTAL INVOICE:
sss DE oSITS' 235. O0
Due I165.403-RO-23
Vet Oer Ne00
PLE APrE Dey P33:218-350L Keeo33 E
sap2
How Mee 23APe COMP aied How_ Eatimaued hae
Toal Eaiu Fig Tee Y on / Aner
Operetioe Na 1 arC No DiecepaayEQIAE (osT RouoGR MADE_loun ALSEMecaais -InapaceJ.
Comecs Anio EmOE loa IRouAie SHOT FooADEsuALsTVALk KeoKE ofT CiL Mea THROEHQUT KceonMEADES
Meceak lener Opaaio Na 2 APC N
Corrective AcionEmoUED E20IÄ2E-EAT To osAr FoR ma iR2
Dhse HAUL KaTUSTAUED Ea01ADE AFTEEO/8 sTALKD.
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CoNTIASUED Opentioa Na 3 AC Na Discpa TsTACLEA QV6R HA ULEN OILnERMeckesic laspecae
KEPAcED Yao moDsST BoLTS DuE Th (hegoSIO
Cormectie Acioa: sAAED (neROSID FroK)lSIDE DAmETES
OF PenR VcpAcED SCAT TOBE Foe CAsiA) KsAT CHAR GED BAITEE L
eoA AK2fag/A2GAcoeNIA o A AAs KEtomENDATION S
CaTIAUGOpentoe Na 4 ArC Na Diec panyEEFOEmad OPERAT IONALE (5AK CHECKMachanis -laupecser
A2e LeAKS AOTED AT THIS TimE. OPsCHECKS Ccco
Comeche Ario SEE Kaers lasTs ATTACHED
TimE: FAT One ***** **
.
*
-..
Wart Order Na:GO0 CN Number NZHI ST
Mechanis laapecia atioa Na ArC No:
erecave AcionClEALE DSoeeoSIOA1Eimad ¢ taINTED
r Hes Mechanie Inseetou
APC Nox Dicrepanc Opsratioe NNa
Corrertive Anioa
Mechanie Inspaciar penioa Na APC No Discrepancyy
orecti Actioa:
pertioa Na ArC No: DicTepanc. Meshanis laspecior
oTect Actioa:
peratioa No. APC No: Dicrepanc Mechanis. Inapeca
Comectii Atio
peatioa Na APC No: Discrepancy. Mechaaic - Inspectau
oetive Action:_
penioe Na APC Na DiucrepancV Mechanic laapectu
Asioa"
adlog
PROPELLER MAINTENANCE RECORDSS
Log No.
Aircraft Registration No. N341sT
Sen senichPropeller Manufacturer
Hub Model. 7 EM B S5-0-6oBlade Design No.
Hub Serial No. 12209k
Blade Serial No's.
1.
2.
3.
4.
Pitch Range:
High Low.
Feather Reverse
Governor Manufacturer
Model No..
Serial No.
Date installed on aircraft.
Time Between Overhauls (TBO). Hours
If used on multi-engine aircraft:
Right OLeft
Front Rear
(All applicable Information must be filled in)
ERO ECH PUBLICATIONS INC.
P.O. BOX 1178/FREEHOLD, N.J. 07728
(201) 462-5330 1979 AeroTech Publications Inc.
Page No. TACH OR
TOTALTIME
TOTAL TIME PECORDNG
DESCRIPTION OF WORK PERFORMED- sIGNATURE A CERTIFICATE NO. OF PERSON PERFORMING wORK TER
DATE IN SNCE TEVE OVERHAUL
SERVICE
TOTALS brought forward from previous page
CERTHy THAT H HAS t' * D I CCOBDANCE
wIT TON ANND WAS
COAT AUTH
CERTIFICATE NO. AZ: DATE 5 INTR�L
LCERTIAV THAT HIs _ HAS BEEN, INSPETED IN ACCORDANGE
ALTHALDAL
wAS DEFERMINED TO BE IN AIR WORTHY GAAHHSN.ALITHORZED SIGNATURE,
tNSFEEHAM AND
ETHF DATE -22 TOTAL TIME 2602
CERTY THAT THIS
TRSPEEtttsRDAaCE wru A Aalak
NSPEQTION AND WAS DEltkuiiED TÙ BE AN ÁLRMUala
coNDITION.
DATE
ADS ChckedNms
CERTIFY THAT THIs 2 HAS BEFN INSPEgTED IN ACCORDANCE
WITH A100 INSAECTION AND WAS DESERMINED TO BE {N AIR WØRTHY CONDITION. AUTHORIiZED SIGNATURE
I CERTIFY THAT THIS
TNSPECTED TN ACCORDANCE WIT WSPECTION AND WAS DETERialied (o BE N AURKOZÁA
CONOITION DATE CERTIFICTE NO_|ALUAI5S 2 T 30b
DATE 0O ToTAL TIME b0 G JACH TIRNE DE PRUE
A F ob
6ED
SUB-TOTALS this page
TOTALS-Carry forward to next page
a N
E SCHPriON OF WORK PE 13FORMED. DATE O NG E
AE SE VT SIGNA PUE A CE1T1A IrE N pENSON ERFOMIN NOnK
E
TOTALS brought forward rom pravioun gy
T CERTIFY THAT TH'S HAS BEN, 1* *** WITHA t¢ WAS Dc TO RE ' AIR WORJAY CONDITION
hopele ORDANCE ":ON ANO
CNJTON
AUTHORIZED siCNATURI 3TJ CERT ELCATE NO DATE 20 IOTAL TIME S.M H
CERTIFY THAT THIS uLEA TNSPECTEU IN ACCORDANTt WttH ATANTLU
HAS EN ICERTIFY THAT THIS Ko_ HAS BEEN INSPECTED ttt ACcoRDANCE WITH A /071 wAS DETERMINED TO BE IN ATR WOTAY CONDITIOON.
AUTHORtZED STGNATURE CERTIFIÇAT� NO ANG Z2254
DATE 27TO TOTAL TIME KZR
IN$PECTION ANO INSPECTION AND WAS DETE RMIED T0 B& IN ArARiY
caNDIION.
DATE 7fr/ozmCH TIME G3 PROR;MIAL IIME S.MO.H,
SICED
CERTIFY THAT THIS HAS BEEN
ICERTIY THAT THSglleu_i
INSPECTED IN ACCORDANCE WITH MAALLAL_INSPECIIO AND WAS DETERMLB-t bE tAIRNUKIN
WITH AZOT HEDIN_ACcORDAMC
WAS DEIERMINEDTO BE INAIR WORNAY CONDITION.
AUTHORzED SIGNATYRE CERTIFICATE NO. DZ}1ZEUDDATE LY FeTAL FHMEh34
hc B3,9|
NSPECTION AND
cOtDIION.
DATE 7-T7-05ICH UNE MoB
SUB-TOTALS this page
TOTALS-Carry forward to next page
Page No. TACH OR
TOTAL TIME
DESCRIPTION OF wORK PERFORMED-
SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK TOTAL RECORDING
METE TWE
TIME
DATE SINCE oVERHAUL
IN
SERVICE MAINTENANGE LOGSUPPLEMENT
N34 ST Type PA 28-180 sN28-730547
O sEP oA ACTT 3IS.bo
36bo
DATE:/0 sEPTEMBER 2004 Time 361s.6T
Pe. fovmed annual inspecti 1.a.w FAR43appehdi D
PRoe T 365. LD Dresse d propelle. Cheked toaye i Satety, Pond
PROP SHaH 703.52 0K. I cer+ity thed this prpele has bevr
insoctes in actor dan ce wuth an AdN UAL
INSPECTLD and was detrmined to be
atr worhy condition.
Signed MausUlaE _Certificate#92S89063TA.
cERTIF THAT THIS
HAS BEEN WITH AZQO H
WAS-DETtottED Tp BE N ATR WORTAT CONDITION.
AUTHORIZz�D SIGNATARE,
lassas pe_ brabrsPEGTED t AÇCORDANQE
INSPECTION AND
DATE2 IITO
L 735 TOTAL TIME23
CERTIFY THAT THIS HAS BEEN INSPECTED TN ACCORDANS Echesse kpseelchele
WITH AINSPECTION ANDD» Snkly_ WAS DETERMINED TO BE INVATR VYONTHYCONDITIQN. AUTHORI}ED SIGNATrRE,
CERTIEICATE NO, 4DZZ Zf0|
DATE gioL foTAL TIME35Í
T CERTEYTHATHTHHS- HAS BEEN INSPECTED IN ACCORDANCE
WITH AZAEZHA tNSPECTIAN AND WAS DETERMINE TO BE IN AIA WORTHY CONDITON. AUTHORIZED SIGNATURE
CERTIFICATE NOZ}AB DATE 2/KICIOTAL TIME 26G/ Tbm 97| SUB-TOTALS this page
TOTALSCarry forward to next page
Page No. TOTAL TOTAL
TIME SINCE
OVERHAUL
TACH OR DATE TIME
DESCRIPTION OF wORK PERFORMED SGNATUAE & CERTIFICATE NO OF PERSON PERFOAMING WORR
RECORDING IN
METER SERVICE TIME
HAS BEEN INSPEÇIED IN AGGORDANGSE CEotncesejate cheko TOTALS brought forward from previous page
CERTIFY THAT THIS WITH A OO WAS DEERAIN�D|TO BE AIN wORTHY" CONDITIDN
AUTHORIZED SIANATURE CERTIFIGATE, NO. DATE OLI rorat inME 9K
INSPECTION AND
N341ST October 8, 2009, Propcller TT: 3982, Propeller TTSMOH: 1070, Tach: 3982 Removed & reinstalled propeller to replace crankshaft seal. Dressed and paintcd propellcr. rtiy that this PROPELLER has been inspectod in accordance with a i00 HOUR INSPECTION and was-detornincd to bc in ar'airworthy condition.
Roberto Ruiz A&P3233677
N341STNovember 1, 2010, Propeller TT: 4010, Propeller TTSMOH: 1098, Tach: 4010
Removed spinner and inspected propeller, then reinstalled spinner assy. Dressed and painted propeller.
Icertity that this PROPELLER has been inspected in accordance with a 100 HOUR INSPECTION and
was detenmined to be ipan airworthy condition.
Roberto Ruiz A&P3233677
CEATy IHAI THIS Ln
HAS BEN INSPECTED IN ACCORDANCE dasso L pmteyhspededss NSPEGTHON AND-
WAS DETERMINETO BE I AIR WOHTH
6ONDHTON-AUTHOFIZED SIGNATURE
CERTIFIATE NO: ALP44254h
DATE/2/20|1L| TOTAL TIME Z034
AIR THAT TH HAS BEEN, INSPECIED IN AÇCORDANCE
WHA A NSPEGTION ANe- WAS DETERMINED TO BE IM AIR WORTHY
cONDttHeeN AUTHORIZED S:GNASURE
CERT f2. TOTAL TIME o33 LTyH024
sUB-TOTALS this page
TOTALS-Carry forward to next page
Page No.
TOTAL TAL TACH DR DESCRIPTION OF WORK PERFORMED
RECORDNo DATE TIME N AE TER
TIME
SIGNATURE& CERTIFICATE NO. OF PERSON PERFORMING WORK SINCE
SERVICE OVERHAUL
TOTALS brought forward from previous page
deesed ipnrky psjeek H8EENOECIEN INA¢GORDANCE WwTH A JO0NA-- NSP�CnoN AND AS DEFAANED TO aE 4wORIH NE ) 0YAL
CONDITHOAUTWOMDGNAnRE
AC4044 TmH| 036
Y THATN-MS BEEN INSPECTED IN4CCORDANC WAHH HEA N�LION AND, WAS DETERMMNFD TO BE AR WORTHY CONDITION.- AUTHORIZED SIGNATURE CERTIFA ATELLIg FOTAL TME H AELINO
TA HOSIT
P OYTAT TH o RAS BEEN TN9PECTFO INCcORDANCIt wITH 00 HAL.
WAS DETERHNED TO FEIN ATR wORTHY CONDIT CON
AUTHOAZED SIGAT TO CTIFICATF, NO. An
IN:ECION 4ND
OIFL THME 0 O57| S molao43
N341ST 8/1/2018 TACH 4062.78TT PROP 1048
Routine 100HR inspection accomplished L.A.w. FAR Part 43 Appendix D checklist. I certify that this propeller has been inspected I.A.W. a 100HR inspection and was detemined to be in airworthy condition.
ZUUSI William Sullivan A&P 37347999
N341ST 8/1/2018TACH 4062.78
TT PROP 1048
I certify that this propeller has been inspected L.A.W. an ANNUAL inspection and was determined to be in airworthy condition.
Alexander Duran 2677910IA
Page No.
N341ST TACH 4076.26 12/22/20 19
TT PROP 1062.26
Koutine ANNUAL inspection accomplished 1.A.W. FAR Part 43 Appendix D. I certify that this propeller has been inspected LA.W. an ANNUAL inspection and was determined to be in airworthy condifion. Alexander Duran 26779101A
SUB-TOTALS this page
TOTALS-Carry forward to next page
A e - P
09-03 SENSENICH:Amdt. 3 761 as amendacd bv Am ina nt O furt he me nded by Amendment 39 1102. Apolies to Sengentch vpa MSEM M e M bEM8, and 76EMBS5 mode i r Opellers inst alled on yco1 1 ng Utpa
g es, except the )-360-A4, an 3)A4 SO r ankshaft ngiries
Compliance equired as i ndicat ed.
a) 1o prevent propeller blade tip faiiures avoid Conti rHIOUS a', in
between 2150 and 2350 Tpm.
D Mark engi ne tachometer with a red arc from 2150 to215S0 rpm wth
The next 25 hours time in service after the effect ive date ot this A
C PTOpellers with 500 r more total hours in servLCe, 1 nspe¢t. jO K
OTeplace 1n accordance with par agr aph (F) within the nextS0 noLirs ti me
n service after the effective date of this AD .
(d) Pr opellers with less than 500 hours total hours in servicei nspect, Tework or replace in accorda nce with par agraph (t) prior to ti
accumulation of 550 hours time in service
Propellers whose prior service historyis unknown, i nspect, reGT (e) Or replace in accorda nce with paragraph(f) within the next 50 hours tin*
in service after the effective date of this AD.
(F) Remove propeller and return to manufacturer for i nspec t ion and reconditioning in accordance with "Recomme nded Action" in Se nsenich Service Bulletin No. R-14 dated March 23, 1970. or an equivalent methodapproved by the Chief, Engineering and Manufactur i ng Branch, FAA, Easter n
Region.
(g)Propellers which have been inspected, rewor ked or replaced in accordance with this AD and found satistactory wil1l be identif ied witn a
suffix letter "K" after the serial number. New product ion propellers wnich
are in accordance with this AD and considered satisfactory include change
"K" or subsequent changes.
Subsequent r epair or recOnditioning of "K" propellers may be (h) per formed as required by any FAA certificated prOpeller repair station
( Sensenich Pr opeller Bulletin No. R-13 dated April 11, 1969 and R-14 dated March 23, 1970, per ta i ns to this subject.)
Amendment 39-761 effective May 9, 1969.
Amendment 39-808 effective August 7, 1 969.
This Amendment 39-1102 1s effective November 10, 1970.
DKE
adlog
S DKEEPING
AVIONICSMAINTENANCE RECORDS
including transponder biennial checks)
Log No. 2 Aircraft Registration No.. N 341ST
Aircraft Manufacturer Piper Checokee
PA 28-1&OModel
Serial No. 28-730547%
EQUIPMENT LISTINGList all installed avionics, autopilot and flight director equipment.
Mfg. Model Serial No.
1. Pipec Aute Flight T 25912 AT 5DATransponder
M8TR Marker Beae on CPAS Audio Bane uGR-2A GlideSupe kee ADE-4 TSO DME KN 42A dvOR-200
2. NARCCO
3. NARCo lncorpotated. 4. NARCco AN6 5. NARCo
6. NARCD 50714 13897 7. King
8. Hoskins
COM 120 TSO * COM 120 TS0 #2 NAU 12 VHE Rec.
9. NARCO 6S2
10. NARCD 21617
11. NARSD
12. NARCO
13. Morow boran 12 BCU 64 3S 14
15.
16.
17.
18.
19.
20.
ECH PUBLICATIONS INc. P.O. BOX 1178/FREEHOLD, N.J. 07728
(201) 462-5330
1979 AeroTach Publications Inc.
Page No
DESCRIPTION OF WORk PERFOAMED
SKGNA TURE A CERTIFICA rE NU OE PERSON PERFORMING WORK TiE
DATE SE E
2 4- 29 2.011/2.08 Tspender ehecked 7-13-n Due 7-31-89
d hé Atosone G. Aimec shlle
AcE A Bo D sda Un 20 ALTIn
Lntall ATian ce. o W ATC booA
Gettey M ekhng M 1956916 IA
THE PITOT STATIC SYSTEM, ALTIMETERs, AND ENCODER TESTS AS REQUIRED 6Y FAR PART 91.411 IN ACCORDANCE WI TH FAR 43
APPENDix E, HAVE BEEN PERFORMED. PITOT STATIC LEAK CHECKED AS PER, PARA. A. THE PILOTS ALTIMETER, S/N_Z326cOPILOTS S/N HAS BEEN TESTED TO Q 04 e FEET AS PER PARA. B. THE ENcODER S/N3X034 SECOND ENcoDERS/N
DATER- . Z4ÉZ sIONED_LalmiLBIU PENINSULA AVION ICS FAA CRS QPIR337K
ATC TRANSPONDER TESTs AND INSPECTIONS AS REQUIRED BY FAR 91.413, IN ACCORDANCE WITH FAR. 43, APPENDIX F, HAVE BEEN
PERFORMG 50 A MODEL 504 MODEL DATE/E-42_w.o.5 PENINSULA AVION ICS FAA CRS QPIR337K
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Page No.
AIRFRAME AVIONICSDESCRIPTION OF WORK PERFORMED
SIGNATURE & CERTIFICATE NO OF PERSON PERFORMING WORK TIME TIME DATE
N IN
SEAVICE SEAVICE
/2 losl9s ST . 3601
S/1 28-7365476 BRAILARD AIRPORTARTPORD, Ci 06114 PA28-180
A/C 3534.7
AR 91.411 BAS BEB ACCOMPLISHED IAN PARY 43 APP BPAR A,B,D IS IKRIBR KAS BEBI IESIID T0 20,.c00 IBET AIB 1OUID SAYISCORY 1OR RRRURI O SERYYCK./PBRMINEIT DBTAILS' ARE O PILS Af TAIS ACILITY. IISPECTOR y/ NAKB Uaited/
on ygard Dater 12/8/95 NODBL5934P SERIAL 83826
AUFOMATIC PRESSURE AL YIYUDE RKPORTING STSYRN YESTED fo 20,000 FEB? AS REOUIRED AY/AR 91/411 IAW IAR 43, APP B. PARA. C. IISPECTOR ACT7hyN NODBL John A-30 ygard Date 12/8/95
SBRIAL t1 29294
ATC TRAISPOLDER 2BSES AND INSPCTTORS REUIRED BAR PR39348) 1208/45 AMD YOUMD PcOKPLY TIPa AR PART 3 aPP. IISPECFORr m MAKB King ( John YGARD
NODBL KT76% SERIAL 95025
ALTIMETER CORRECTION CARD DATE: -8-95
TRUE ERROR TRUEERROR ALT ALT S/NB336 INSP:
FRICTION| -1000 14000 1000 16000 F/0 JL2000D
3000 S0 |5000
1000015000 20000 25000 30000
20 500 1000
18000 20000 220001500
2000 3000 4000
2500030000
35000 60 0 8000
10000-12000 A5
HYSTERISIS 50% 40% O
o 35000CASE GO LEAK _/K
VIP AERO INSTRUMENTS AND AVIONICS FAA REPAIR STATION #TH5R223N
Paye No AIRERAME AVADNS TiVE
E SCRTION O WORK PEnFORMIED SHANA TU1E CETIEICATt NU EUN 1EnonMIN WO?K
DATE IN
SERVICE
Islip Avionics, Inc. FAA CRS# FJIR|4IK The ATC Transponder nests and mspectons required by FAR 91 41 were pertorrmed this date and found to conply with 'AR 43 Appendix F Details are on tile at thrs repay tation under work order 2/l8 Registration * N341ST Tach 3AS TT #1 Make Model
DAE 173-A
S/N 9 SoS #2 Make Model
N
Authorized Signature
PROPi# AVIATiON SERVIES,INC
Altimetpr System Test and Inspection Model AnihodDate 2 13loy Tach 54.94 At lana Repaiman 1iA Kak Certned Inspected in accordance with Part 43, App. E and found airworthy PROPair Repair $tation # 1DDR252K
SN_
# Ridn4
Transponder System Test and Ins_pection Model T 76A_ Date 12 13_/0Tach 3(0.94 Ataoee Repaiman /AJ Bu Certified Inspected in accordance with Part 43, App. F and found alrworthy PROPalr Repalr Staton # IDDR252K
SNYSO2S
#ReMong
APPROVED FOR RETURN TO SERVICE
N341ST 2/24/2005 PA28-180 TT: 3671.09
Installed exchange intercom Pt # AA80-001 Ser # 1387. Ops check ok.
Michael Tarascio A&P 2924231 / |STELLAR Avionics Services, LLC Tweed-New Haven Airport East Haven, CT 06512 FAA CRS YZSR344YLOG ID# 1211 17-March-2006 W/O A6026
N341ST S/N 28-7305476 PIPER PA-28-1800
Pg 1/1 1) King KX-155 Nav/comm S/N 21619: Replaced Display Ass 'y, Tested per Manufacture.2) King KN-53 Nav s/N 8823: Replaced Display, Tested per Manufacture.
3) King KN-72 VOR/LOC Conv. s/N 8959: Replaced R-140 Variable Resistor, Aligned voR & LOC, Tes ted per Manutacture Details on file at this Repair station under work order #A6026 4 Narco ADF-141 Rece7 ver Inop, Determined Beyond Economical Repair. Unit Placarded "ADF INOP"Details on file at this Repair station under work order FA6026,
---END---- ***********-***--->+---
YZSR344Y Date
Page No.
AIRFR RAME ASIONICS DESCRIPTION OF WORK PERFORMED
TIAE TiE DATE IN SiGNATURE & CERrIFICATE NO OF PEASON PERFOAMING WORK
SERVICE AVCE
STELLAR Avionics Services, LLC Tweed-New Haven Airport East Haven, CT 06512 FAA CRS YZSR344Y
LOG ID# 1371 22-November-2006 W/O A6815 N341ST sN 28-7305476 PIPER PA-20-180
Pg 1/1|
1) Compied with FAR 91.413 8iennial Transponder Test/Inspection for *ing KT-764 Transponder s/N
95025 in Accordance wi th FAR Part 43, Appendix F, and Found Airwor thy. Details on file at this Repair Station under work order #A6815
------****tNU**************
a/22/pYzSR344Y Date
STELLAR Avionles Services, LLC Tweed-New Haven Airport East Haven, CT 06512 FAA CRS YZSR344Y
LOG ID# 1377 11-December-2006 W/O A6880 N341ST SN 28-7305476 PIPER PA-28-1800
Pg1
1) Complied with FAR 91,411 Biennial Altimeter Test/Inspection for united Altimeter S/N B3828 to
20,000 in Accordance with FAR Part 43, Appendix E, and Found Ai rworthy.
2 Complied with FAR 91.413 Biennial Transponder Test/Inspection for King KT-76 Transponder S/N 95025 1n ACCordance wi th FAR Part 4, APpendix F, and Found, AirworthY:o0. etails on file at this Repair Station under work order #A6880
----END---*
YZSR344Y Date
ALTIMETER CORRECTION CARD ALT S/IN:33 DATE: /2-/- INSP: B URe TRUE ERROR TRUE ERROR |
14000 16000 18000 20000 22000 25000 30000 35000
LIFRIOCTION 1000 2 2000 3000
5000 10000 0 15000 0 20000 2 25000 30000 35000CASE
O00 t0
500 1000 1500 2000 3000 4000
6000 O B000 10000 AS 50% O
12000 O|40% HP
HYSTERISIS
LEAK STELLARAVIONICS SERVICESS
FAA REPAIR STATION# YZSR344Y
Page No.
AVIONICSs TIME
AIRFRAME
DESCRIPTION OF WORK PERFORMED SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK
TIME DATE IN IN
SERVICE SERVICE
STELLAR Avionics Services, LLC Tweed-New Haven Airport East Haven, CT 06512 FAA CRS YZSR344Y LOG ID# 1946 09-November-2009 REF# A98466 N341ST S/N 28-7305476 PIPER PA-28-180
Pg 1/1
1) comp1i ed with FAR 91.411 8iennial Altimeter Test/Inspection for united 5934P Altimeter s/N 83828 to 20,000" in Accordance with FAR Part 43, Appendix E, and Found Airworthy.
2) comp1ied with FAR 91.413 Biennial Transponder Test/Inspection for King KT-76A Transponder s/N 95025 in ACCordance with FAR Part 43, Appendix F, and Found Ai rworthy .
The aircraft, airframe, aircraft engine, propeller or appliance identi fied above was repaired and inspected in accordance with currene, regulations of the Federal Aviation Administration and approved for return to service for the work performed. Pertinent details of the repairs are on file
at this repair station under the wWork order 1isted above. ---- END-----*****--.
SR344Y Date ALTIMETER CORRECTION CARY
ALT S/N:538FDATE: 7-9-9INSP: RA TRUE ERROR |TRUE ERROR| ALT FRICTION|
14000 -20 16000 /O 18000 -20 20000 22000 25000 30000 35000
-1000 T000 2000 3000 500
1000 1500
5000
10000 2000 3000 4000 6000 B000 TOO00
12000 30
15000
200007o25000
HYSTERISIS 50% 3L 40%
3000 35000 CASE
LEAK-O C
STELLAR AVIONICS SERVICESFAA REPAIR STATION # YZSR344Y
STELLAR Avionics Services, LLC Chester Airport Chester, CT 06412 FAA CRS YZSR344YLOG ID# 3164 25-September-2017 WO# 16685 REF# A16685
N341ST S/N 28-7305476 Pg 1/1|
PIPER PA-28-180
1) Complied with FAR 91.413 Biennial Trans ponder Test/Inspection for King KT-76A Transponder S/N
95025 in Accordance with FAR Part 43, Appendix F, and Found Airworthy.
The aircraft, airframe, aircraft engine, prope]ler or appliance identifi ed above was repaired and
inspected in accordance with current regulations of the Federal Aviation Administration and is
approved for return to service for the _work performed. Pertinent details of the repairs are on file
at this repair station under the work Order isted above.
---------------------END----
YSR344Y Dateu
N431ST 6/10/2019
TACH 4070
Installed Skybeacon ADSB wingtip beacon PN UAV-1001856-002 SN 1004071 STC # SA04362CH dated Nov 27
2018 installed as per Uavionics installation instructions document No, UAV-1002305-001, Form 337 generated.
Alexander Duran 26779101A
ARCRAFT
RECOROKEEING
Applicable Airworthiness Directives ID No:351 adlog Page No:1
Date: 10/ 20/95SgelPA-28-180, S/N: 287305476. Taii No: N3413T AD NUMBER SuperseAD Number
s
TYPE SUBJECT NA
ENGINE(s): -360-A4A
PROPELI.ER(s) : 76Ei5-0-60
MAGNE TOs) Rendix
72-06-O5R2 N MARVEL -SCHERIER L.ARRUR TR
7208-06 R MAIN iEAR TROUE L. INS
73-23-01R4 N LYCOMI NG ENGTNE
74-09-04 REAR SEATREL T INSTAL.LATION
74-26-07 N INORRECT PLATARD 7 4-26-09 N HENIIX MACNETU
7-02-03 N NOSE WHEEL FORK ASSEMBLY
75-08-03 N FLIEL LIRAIN VALVEES
75-08-09R3 N LYTCMING ENGINE
7-24-02 R EAT UICK-IISCOiNNECT
76-07-12R1 R BENDIX IGNITION SUITCH
7-16-02 N AIREORNE VACUUM PUMPP
77-01-01 NM FUEL UANTI TY BALIGE
N CINTROM. ROD ENII BEARINGS
78-09-07R3 | R BENDIX i1AGNETO
79-07-02 EEFECTIVE RATTERY
79-13-O3 N AIREORNE IRY AIR PUMP
79-105R1 N I THIIM BATTERY 7 )-02
79-26-05 N OIL & FLJEL SYSTEM HOSES
1-18-04R2 NN LYC:MING ENGINE
2-20-01 BENDIX MAGNETO
4 -02 R INIICTICN AIR FILTERS
1)a N AIREIRNE DRY AIR PLIMP
17-01 N AMME:TER REPLACEMENT &0-24-03
| 7-08-O8R3 |N WING SPAR INSPECTIIN
37-10-06R1 N LYC:COMI NG ENGI NE
-04-02 N FACET (MARVEL-SCHERI.ER) CARBLIRETOR
91-14-22 LYCOMING ENGINE
2-12-05 LYOM ING ENGINE 93-1111 FLIE PUi1P N
93-0-21TVDe of AD (adlog subscribers-this designation appears in the upper right corner of each adNote page): NNon-Repetitive. NR-Can be either Repetitive or Non-Repetitive, depending on the method of compliance.
R-Repetitive. NM-Non-Repetitive, but has more than one compliance requirement. Not applicable.
adlog CRA
MAINTENANCE
RECORDKEEPING
SYSTEM
Applicable Airworthiness Directives
ID No:3351
Page No:
Mo de 1: PA-28-180, 5/N: 287305476,Tail Na N341S AD NUMBER
Date: 10/20/2S
TYPE Supersed9s AD NumberSUBJECT
N/A
ENGINE ( 5) C30-A4A
PROPELIER( E ): 76E13SS-0-60
MAGNE TO(s): Hendix erie5
94-01-03R2 N BENDIX 11AGNETO 73-07-94
4-06-09 N TCM (BENIIX ) NAGNETU
95-07-01 N IEFECTIVE ONNECTI NG RUD EMLTS
Type of AD (adlo, N-Non-Repetitiv6. RRopetitive.
NRCan be either Hepeuve Or NOnNOpeuuve, Oepending on the method of compliance.
AO (adiog subscriberghis de81gnation appears in the upper right corner of each adNote page): NM-Non-Repetitive, but has more than one compliance requirement.
Not applicable.
Applicable Airworthiness Directives
ID No:8351
adlog
Model: PA-28-180, s/N: 287305476, Tail Na: N3415L
AIRCRAF NCE
RECOROKEEPING
SYSTEM Page No:1 Date: 03/01/941
Supersedes AD Number AD NUMBER TYPE SUBJECTT N/A
ENGINE(s): C360-A4A
PRUPELLER(s): 76EMBS5-0-60
MAGNETO(s): Bendix Series
72-060SR2 N MARVEL-SCHEBLER CARBURETOR
72-08-06 RV 73-07-)4R1| NY
MAIN GEAR TOROUE LI NKS
BENDIX MAGNETO0
73-23-01R4 NV LYCOMING ENGINE
74-09-04 NY REAR SEATBELT INSTALLATION
74-26-07 NY INCORRECT PLACARD
74-26-09 NY BENDIX MAGNET0
75-02-03 N NOSE WHEEL FORK ASSEMELY
75-08-03 NY FUEL DRAIN VALVES
75-08-0IR3| N LYCOMING ENGINE
75-24-02R R/
76-07-12R1| R V
SEAT ICK-DISCONNECT
BENDIX IGNITION SWITCH
76-16-02 NV AIRBORNE VACUUM PUMP
77-01-01 NM FUEL QUANTITY GAUGE
77-23-03 CONTROL ROD END BEARINGS
78-09-07R3 R BENDIX MAGNETO
79-07-02 N DEFECTIVE BATTERY
79-13-08 N AIRRORNE DRY AIR PUMP
79-18-05R1 N LITHIUM BATTERY
79-26-05 N N 01L & FUEL SYSTEM HOSES
81-18-04R2 N LYCOMING ENGINE
2-20-01 NY BENDIX MAGNET0
34-26-02 R INDUCTION AIR FILTERS
-01-06 N AIRBORNE DRY AIR PUMP
36-17-01. N AMMETER REPLACEMENT
7-08-0BR3 NV WING SPAR INSPECTION
7-10-D6R1 N LYCOMING ENGINE
-(04-02 FACET (MARVEL-SCHEBLER) CAREURETOR
91-14-22 R/LYcOMING ENGINE 12-05 N LYCOMING ENGINE
of AD (adlog subscribers-this designation appears in the upper right corner of each adNote page):R-Repetiinve. NM-Non-Repetitive, but has more than one compliance requirement.
"Not applicable. s t Hspalili v
Ai a e itnsr Repeilvs of Non-RepetiUve, depending on the method of compliance.
AIRCAAR ECORDKEEPING
Applicable Airworthiness Directives
THE
adlog ID No:8351 SYSTEM
Page No: 2
Model PA-28-180, S/N: 287305476, Tail No N341ST Date: 03/01/94AD NUMBER
TYPE Supersedes AD Number
SUBJECT NIA ENGINE ( s ): 0-360-AMA
PROFELLER( s ) 76EM8S5-0-60
MAGNETO(s): Bendix S SerieS
93-11-11 NVFUEL PLMP 4-01-03 NVBENDIX MAGNETO
Not applicable. na of AD (adlog subscribers-thIs designation appears in the upper right corner of each adNote page):
Type N-Non-Repetitive. R-Repetitive.
NRCan be either Repetitive or Non-Repeitive, depending on the method of compliance. NM-Non-Repetitive, but has more than one compliance requirement.
3IS 7 AIRCRAFT REGISTRATTON NO
94-1-3 N
adNote AD NUMBER
28-73oSY76 AIRCRAFT SERIAL NO
Pa 18-80 TYPE AIRCRAFT
Bendix Magneto
R/H 1O-16304S 3,AI93SYI
A 102O8A f multi-engine: Left Right UFront Rear Part No/Serial No: 4/H 1o S30-4S TACH OR
RECORDING METER TINME
COMPLIANCE TOTAL TIME AT COMPLIANCE
AUTHOAIZED SIGNATURE & NUMBERDATE METHOD OF COMPLIANCE
AT COMPLUANCE
3/16/94 3SHRs 3Is At KS-rP1eRC3723 mundeeand S8 (37|
AT O1994 AeroTech Publicatlons lnc., All rights reserved
c) After compliance with paragraphs (a) or (b) of this
AD, as applicable, and prior to further flight, mark the
magneto in accordance with the ldentification Instruc-
tions of TCM SB No. 637, dated December 1992.
(d) An alternative method of compliance or adjustment
of the compliance time that provides an acceptable level
of safety may be used if approved by the Manager, At-
lanta Aircraft Certification Office. The request should be
forwarded through an appropriate FAA Principal
Maintenance Inspector, who may add comments and
then send it to the Manager, Atlanta Aircraft Certification
Office.
Amendment 39-8785. Docket 93-ANE-44. Supersedes AD 73-07-04, Amendment 39-1731 (Bendix AD).
Applicability: Teledyne Continental Motors (TCM) formerly Bendix) S-20, S-200, and S-600 series magne- tos with red or black Bendix (not TCM) data plates having serial numbers without any letter prefix, or serial numbers lower than A16058 having the letter "A' prefix: S-20, S-200, S-600, and S-1200 series magnetoswith blue Bendix (not TCM) data plates having serial number 901001 and lower, and S-1200 series magnetos with red
Bendix (not TCM) data plate's having serial numbers
without any letter prefix, or serial numbers lower than
A132844 having the letter "A" prefix. These magnetos are
installed on but not limited to reciprocating engine pow- ered aircraft manufactured by Beech, Cessna, Maule,
Mooney, and Piper.
Compliance: Required as indicated unless accom-
plished previously. To prevent magneto failure and subsequent engine
failure, accomplish the following:
(a) For TCM (formerly Bendix) S-20, S-200, and S-600
series magnetos, replace Bendix ignition coils and rotat-
ing magnets identified in the Detailed Instructions of
TCM Service Bulletin (SB) No. 63Z, dated December
1992, with appropriate serviceable ignition coils and ro-
tating magnets at the next 100 hour inspection, the next
annual inspection, the next progressive inspection, or the
next 100 hours time in service (TIS) after the effective
date of this AD, whio
(b) For TCM (formerly Bendix) S-1200 series magnetos,
replace Bendix ignition coils identified in the Detailed In-
structions of TCM SB No. 637, dated December 1992,
with appropriate serviceable ignition coils at the next 100
hour inspection, the next annual inspection, the next
progressive inspection, or the next 100 hours TIS after
the effective date of this AD, whichever occurs first.
NOTE: The rotating magnets on the S-1200 series mag-
netos already incorporate the improved TCM design.
NOTE: Information concerning the existence of approved
alternative methods of compliance with this airworthi-
ness directive, if any, may be obtained from the Atlanta
Aircraft Certification Office.
(e) Special flight permits may be issued in accordance
with FAR 21.197 and 21.199 to operate the aircraft to a
location where the requirements of this AD can be ac-
complished. () The replacement shall be done in accordance with
the following service bulletin: Documenl No. Pages Revision Dale
TCM SB No. 637 1-2 Original December 1992
Tolal pages:2.This incorporation by reference was approved by the
Director of the Federal Register in accordance with 5
U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained
from Teledyne Continental Motors, P.O. Box 90, Mobile,
AL 36601: telephone (205) 438-3411. Copies may be in
spected at the FAA, New England Regional Office of the
Assistant Chief Counsel, 12 New England Executive
Park, Burlington, MA; or at the Office of the Federal Reg
ister, 800 North Capitol Street, NW., suite 700, Washington, DC.
() This amendment becomes effective on March 3,
ever occurs first.
1994.
N341S7
MAJOR REPAIR AND ALTERATION
(Airframe, Powerplant, Propeler, or Appliance)
Form Approved OMB No 2120-0020
For FAA Use Only
Office ldentiicaton US Department d Transportabon
Federal AvMationAdminkuato
RUCTIONS: Prirtor type al entries Se FAR 439 FAR 43 Appendir B, and AC 43 91 (or subeequent revision hereo or
ns and disposition of this form This report is required by aw (49 U S C 1421) Fatlure to report can resut in a civ penany not to
Coed $1,000 for each such viola tion (Secton 901 Federad Aviabon Act of 1G8)
1. Alrcrat Make PA28 180
PIPERNationally and Rmgdrutlon Mark
N341ST Seriel No
28-7305476 Ardresn As shown on rmgintrathn eetesMe)
Name (As shon on mgistraion ceric OHN R RINGLE
2. Owner 838 FRANKLIN PL FRANKLIN SQUARE, NY 11010
3. For FAA Use Only
5. Type 4 Unit dentieaton
Serial No. Repair Alteration Unit Make Model
X
AIRFRAM (As described in item 1 obove)-
POWERPLANT
PROPELLER
Type APPLIANCE
Manufacturer
6. Conformity Statement C. Certificate No.
B. Kind of Agency
|X {U.s. Cortificated Mechenic A. Agency's Name and Address
A&P3233677
ROBERTO RUIZ
JEFFERSON ST MASSAPEQUA, NY 11758
Foreign Certificated Mechanic
Certicated Repair Station Manufacturer
D. Icertify that the repair and/or ateration made to the unit(s) identfied in item 4 aboe and described on the reverse or attachments
hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviaton Regulations and that the
infomation furnished herein is true and comect to the best of my knowledge. Signature of Authorized Individual
Date OCTOBER 8, 2009
7. Approval for Retum To Senvice
Pursuant to the authority given persons specified below, the unit identifed in item 4 was inspected in the manner prescribed by
the Administrator of the Federal Aviation Administration and is APPROVED LREJECTED Other (Specify)
FAA FH. Standards Manufacturer X Inspection Authorization
BY nspecor Person Appoved by Transport Canada Ainworthiness Group
Signature of Authorized Individual FAA Designee Repair Station
Certificate or Designation No. Date of Approval or Rejection
oCTOBER 8, 2009 A&PO56681211A FAA Form 337 (12-88)
INTEGRITY AIR SERVICES, INC. 63 TOM HARVEY ROAD
ADDITIONAL EQUI PMENT LIST /REVISED WET GHT AND BALANCE
BY
IRy., WESTERLY, RI 02891
SueecEEQED
FAA CRS WwZR309K
SoSO .1-97
Los ATEY
N' NUMBER N-341ST MAKE DATE 6-22-94
PIPER PA-28-181
TACH MODEL S/N wORR ORDER # A-40995
28-73054 76 tttttt
WEIGHT ARM MOMENT
PREVIOUS A/C EMPTY 585.00 88.53 1403 20.05 REMOVED ITEMS
COM. 20 COM. 120
NARCO 4.00 58.00 232.00 NARCO 4.00 58.00 232.00
NAV-12 NARCO 3.40 59.00 200.60UGR-2A NARCO CP-25 NARCO
223.80
43.75 1.20 86.50D
0.70 62.50
INSTALLED ITEMS
NAV-COM KING 155 4.70 58.00 272.60
185.60D 104.55
COMM. KING 197 3.20 58.00 AUDIO PANEL KING KMA-24 1.70 61.50
NEW A/C EMPTY 1581.300 88.50 139950.64
NEW A/C E.W. NEW A/C c.G. NEW USEFUL LOAD
1581.3088.50
868.70
SuPEzeeBED BY JOHN E./NYGARD
ENT2Y AUTHORI}ED SIGNATURE INTEGRITY AIR SERVICES, INC. ABOVE INSTALLATI ON PERFORMED 5119Y
IN ACCORDANCE WITH MANUFACTURERS
SPECIFICATIONS AND IS APPROVED
63 TOM HARVEY ROAD WESTERLY, RI 02891
FAA CRS wWZR309KFOR RETURN TO SERVICE
******* * **************************** * ******** ****
SeE Lo6 Bool ENTey ol3)19% 3347 rTAC
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AIRCRAFT WEIGHT AND BALANCE REPORT 94-1825
DATE WEIGHEDM er PA-28-180 SERIA305476 March 15, 1994
PLACE WE IGHED WEIGHING PERSONNEL
Danbury Municipal Airport (DXR|) Eric Propper
SCALE READING
REACTION NET WEIGHT
TARE ARM MOMENT
673 0 673 LEFT MAIN
637 637 RIGHT MA IN
1310 105.95 138795 SUB-TOTAL (BOTH MAIN)
X NOSE OTAIL 568 568 49.85 2831
TOTAL AS WEIGHED
1878 88.98 167109
CONFIGURATION AND MEASUREMENTS
78.4 inches forward of DATUMwing leading edge.
O O LEVELING: Screws LHS fuselage
below fwd window.
2755
Washington Heights Medical Service 38-44 East 30th Street
OWNER New York NY 10016
PAGE 2-REPORT 94-1825
COMPUTATIONS
DESCRIPTION NET WEIGHT ARM MOMENT
TOTAL (AS WEIGHED)1878 98.99 L57199
OIL IN AIRPLANE
QUARTS 13 32.50 427
FUEL IN AIRPLANE (USABLE) (FROM COL. 1 BELOW)282 26694
TOTAL OF ITEMS WNEIGHED BUT NOT PART OF BASIC WEIGHT
(FROM COL. 1 BELOW) 0
TOTAL OF BASIC ITEMS NOT IN AIRCRAFT WHEN WEIGHED
(FROM COL. 2 BELOW) 2 324
BASIC EMPTY AIRPLANE 1585 88.53 140312
% M.A.C.
BASIC EMPTY AIRPLANE
WITH FULL OIL 1600 88.01 140800 OTS % M.A.C.
COLUMN 1 COLUMN 2
ITEMS WEIGHED BASIC ITEMS NOT BUT NOT PART WEIGHT ARM MOMENT| IN AIRPLANE WEIGHT| ARM MOMENT
OF BASIC WEIGHT WHEN WEIGHED
FUEL LB.7GAL.
50
5.88 Tow bar 2 161.8 324
294 95.0 27930 12 IO03
GALS. UNUSABLE T236
USABLE FUEL- 29-294-7-26694- 0 0.0
0 0.0 0
0 0.0 0 2 161.8 324 TOTAL TOTAL
ELECTRONIC WEIGHING KIT TYPE: C-55800-3-5
REACTIONS USED:
Wing jack pads Under fuselage stiffeners December 1993
CALIBRATED: CG LIMITS: 87.4" to 93.0" 2450 lbs.
82.0" to 93.0" 2050 lbs. . .or less.
REGISTRATION: N3 41ST
2413 Rev.41 TYPE CERT. NO.
MAXIMUM GROSS WEIGHT: 2450 LBS.
USEFUL LOAD 850 LBS. WITH 8 QTS. oIL Pire bottle aboard.
