AIRFORCE TURBINE SERVICE - Sandhills Global

1. Make

2. Model

AIRFORCE TURBINE SERVICE P.O. BOX 146

TYNAN, TEXAS 78391 (512) 547-3386

FAX (512) 547-7273

ENGINE LOG

h11rr ~ Mft/.A/57 {;,,vr:~p,., //t 11- / 5·-/1(-,

3. Specification

4. Manufacturer's Serial Number

5. Date of Manufacture

6. Aircraft Inspection Cycle

F.A.A APPROVED REPAIR STATION TQZR133K

DATE

BROUGHT FORWARD

12/19/97

~ .

TIME RUN

HAS. MINS.

ENGINE SERVICE AND TIME SINCE

NEW/OVERHAUL

HAS. MINS.

INSTALLATIONS, INSPECTIONS, NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

I - .____ -

AIRFORCE TURBINE SERVICE TYNAN, TEXAS 7839~

CERTIFIED REPAIR STATION TQZR~33K PRATT & WHITNEY PT6A-15AG SERIAl NUMBER PCE 14155

TOTAl TIME: 4,981.2 HOURS TOTAl STARTS & FliGHTS: 1558 & 7263 REPAIRED ENGINE. ENGINE RECEIVED FOR HOT SECTION INSPECTION AND SUSPECTED LEAK OF START FLOW CONTROL. ALL WORK PER PRATT & WHITNEY MAINTENANCE MANUAL.

COMPLIED WITH HOT SECTION INSPECTION REQUIREMENTS IAW PRATT & WHITNEY MAINTENANCE MANUAL 3030442R14 10/15/94 SECTION 72-00-10, TABLE 603. CLEANED & FLOW CHECKED FUEL NOZZLE ASSEMBLIES, ALL CHECKED GOOD. REPLACED START FLOW CONTROL WITH SERVICEABLE 3019109 SN 13210. INSTALLED 0/H T5 HARNESS ASSY 3028289 SN 1T077.

COMPUTED LIFE LIMITED COMPONENT STATUS PER SB 12102R4 DATED 10/14/86: CONSUMED REMAINING

E.m 3013111 3013712 3011713 3013176 3013411 3022412

NAME HUB 2ND STG DISK 3RD STG DISK IMPELLER CT DISK PT DISK

CYCLES/HOURS SIN CYCLES /HOURS 1161/4981 .2 4Y725 17839/10018.8 3590/4981.2 27A173 20410/ 10018.8 3050/4981.2 25A242 21950/10018.8 2338/4981.2 4D547 16662/10018.8 3789/4981 .2 22A549 12211/ 5018.8 1767/4981.2 12A742 18233/10018.8

FOLLOWING COMPLETION OF REPAIRS, ENGINE WAS REASSEMBLED; ENGINE PERFORMANCE WAS FUNCTIONALLY CHECKED. THIS CERTIFIES THAT ONLY THE WORK REQUESTED BY THE CUSTOMER AND DESCRIBED ON THIS WORK ORDER WERE ACCOMPLISHED lAW MANUFACTURER'S SPECIFICATIONS AND WITH CURRENT FAA REGULATIONS, AND THAT THIS ENGINE IS APPROVED FOR RETURN TO SERVICE. --j

PERTINENT DETAILS OF THIS REPAIR AR~~~j?~~CY UNDER WORK ORDER 02134.

~{tf~~ CHIEF INSPECTOR

_I .

CARRIED FORWARD

TOTAL THIS PAGE

TOTAL FROM PREVIOUS SUMMARY

TOTAL SINCE MFG.

1 ENGINE SERVICE AND MAINTENANCE RECORD

' I TIME RUN

T IM E S IN C E l REPAIRS, ADJUSTMENTS, MODIFICATIONS LICENSE NEW/~1- INil lAII AllONS. INSPECTIONS,

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COlUMNS S IGNATURE NUMBER DATE

r H AS. NO l l I JI"W HOIII/ 'fl/ 11 b AN! l Il l: MANY l iNES AS REQUIRED FOR COMPLETE ' MINS . HAS . M I N $ l

-;.ji / //7 ROU GHT .. l ORWARD

2~7#F- lzSffG ~C::vb.</cP?' :rl,.,.-4~.<- /;/~~..e> . / / .:...-: /-2 s-.z_% FT 72% A"'//h.-_k. ~~ ~ '/~t/o.Pzzj :19-7 / ( / ·-

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/ "-'MT ~ L>aru-r .L.'·h· a· -<-'~. 1'!1u-tw811 r::~,Jil.u I.T. 53 ti0 ,6

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/.)JCi( d"A/w;A/Ifi: .z~ #/"'.-«"<IT,.. 5 . d rru:LJ/J ;$5/A ()- /li~n -.1- f< r.~.o.J H_ , r //;,... 'Dn<; 'r:,.,,

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.. -z}i.lt, ~ A~r> S:'LL.t./ t 7!9? Engine Maintenance Entry SIN:_PCE14155

Jate:05/01199 Hobbs:_3011.8_ iT:_5404.4_ ·-~lf3S~ :z '/JZ.1 ;tJ~ j/.e S6AJ:~tr . ~rl> OfT- J!..,rp~ J")tcT 100 hr. service accomplished lAW PWC Maintenance r-JI- 'If

{- Ovrt.er fo~f:L {:,-L,'?; t..~ ' d..u:-«1> e;;,p b6'1El!<et...-. . Wanual_ RGB drained, chip detector inspected and unctionally checked, Starter generator, blown out, brushes

d.u.td> IG~.' < H'T¢"L.:> hit_ oP~o.J ( (.__,JwoJ , ~ ~kd, spline inspected and drive inspected for wear replaced

lr'>erA ~(.,,1{, ~~~.r:""'<rl> O ... Vrll.. lhn!.- "'.w..J... -/off.ri> drive seal. Inlet fuel filter inspected and cleaned, Outlet filter ep/aced. Oil filter inspected for metal and condition, Ignitors

0 flf ~\( .. ~~e-L . /l.A..., 6'>-1 '-' · • 4f,.t ~. tl·f(. SoV.(!ql inspected and ops checked, Engine inspected externally,

t.~lt$e-N . control rigging checked, Inlet area inspected, Exhaust duct

~ "''"''"' - ~· """"' '"'l£1[ .6);~ )./!' Sl/ lyj 7t9J-:> ; recovery wash was accomplished_ , 1

i Yuba-Sutter Aviation Name· ~

~-'YJ - q)( r;('J /,), 2 ~ '07, '7 Engine Maintenance Entry SIN.· f ( F I'-! !55" 1 Marysville, Ca. Cert. #: ~ll ,

Dale.:Zil!?.12ft· Hobbs zq071n5!J<X:S Engine Maintenance Entry SIN: 1-1155 100 Hr. Service items accomplished lAW Allied-Signal

Date.:JJJ.i@ Hobbs~n 55 /-3 .1 Maintenance Manual, Fuel filters changed, Soap sample taken, oil filler replaced, First stage compressor ckd for FOD,

100 hr. service accomplished JAW PWC Maintenance Exhaust ckd for oil leaks, Starter Generator spline ckd, Manual. RGB drained, chip detector inspected and brushes checked, carbon blown out, and reinstalled, Input

\ functionally checked, $1f!rter generator, blown out, brushes gearbox drain ckd, magnetic chip detector ckd, Flow divider ckd, spline inspected ana drive inspected for wear. Inlet fuel

screen cleaned, Ignitors ops ckd and inspec:;;;., General I filter inspected and cleaned, Outlet filter replaced. Oil filter

condition inspection OK, Engine was I was ]lJ inspected for metal and condition, Ignitors inspected and ops

'"''""" ""' """"oc' ~ ' ' checked, Engine inspected externally, control rigging Yuba-Sutter Aviation . checked, Inlet area inspected, Exhaust duct area inspected.

Marysville, ca. C0/1 C'l ? l iJ'Jt1Jt1 , Engine was washed externally, a power recovery wash was I ~accomplished.

Nam~?fil' CAR Yuba-Sutter Aviation TOTAL THIS PAGE Marysville, Ca. cert. #:Air_~~

'REJfb"d~ tnW~ARY ~ H O URS.

i TOTAL SINCE MFG. t

-.•. - _-" ,;,~:--;::::::"- .,Q;.lZ·f; ~~--ks-11# 18> ..:~~...--~V I I 1\.1. JV"VV

IGINE SERVICE AND MAINTENANCE RECORD •

INSTALLATIONS, INSPECTIONS, l

REPAIRS, ADJUSTMENTS, MODIFICATIONS LI C ENS E NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE I ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. SIGNATURE NUMBER

~

l I ..

e Entry SIN.· (~/!5{: _; i

JS: :;2,2:-) ,,·.) '

ished /A W PWC Maintenance ;hip detector inspected and arter generator, blown out, brushes ·d drive inspected for wear. Inlet fuel ned Outlet filter replaced. Oil filter co;dition, Ignitors inspected and ops ted externally, control rigging , Jected, Exhaust duct area inspected. emally, a power recovery wash was I Oil changed, Fuel nozzles cleaned r

I •.

Name;~:.}: /'); ~~ ,:"-, i . . (;,-:!, . ·'If - -~ Cert. #:li".1 ·~ R:tJ· (:,_-<.-

I ,I I ~

~o)ek~ ft:AD 3?:>']_11, ~ ~~c( n:~~A- Q.l•I:>J i<.u.O._ 1t:ll1t.p.

R~~'"' ' eJ.. Ft.v ~ :rx.sktillo~ 06+ U,v·,J ;;)S';)_IJ.4-40 ·- S o/1-1 A 7 (oo3

~ 6~~~ 1 ~~.a~ rQ.Jlel b12L0 ~oih%£ Rof.&!~t

it~ ' i. I

MAXIMUM HOURS BETWEEN OVERHAULS HOURS. ·tl II '

:NGINE SERVICE AND

ion

rT: 6218


Marysville, Ca Fax (530) 743-6955

;omplished lAW PWC 311 duct P/N 3012060, S/N 17490 installed 16 each T019438 new

nbled and installed with new 1ce ground to .013, installed 14 ea lied 0/H Buss Bar PIN 3027628 31ve and tested, Engine ground run ance OAT: 11 C Baro:29.89 Chart 3/43 Np: 2200/2200, NG 97.1 /92,

1 MAINTENANCE RECORD

REPAIRS, ADJUSTMENTS, MODIFICATIONS ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. SIGNATURE

MAXIMUM HOURS BETWEEN OVERHAULS HOURS.

•.i

LICENSE NUMBER

~ ~ 11 .

-,

~NGINE SERVICE AND

L INSTALLATIONS, INSPECTIONS, NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

Lf \ '3 ~ tyQS fl, rc .--aft \ U c/ t'c<.-n eJ l J..JJJ .

::A 3 "2,'0 Q \ \

CARRIED FORWARD

MAINTENANCE RECORD

REPAIRS, ADJUSTMENTS, MODIFICATIONS ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

shed+ 4' V6rU-S~ \ Im

SIGNATURE LICENSE NUMBER

~ Jr· --------------------------------------------~-----------r-----


-.,

l I

DAT E

::JUG HT AWARD

ENGINE SERVICE AND

MINS


1'1\STl •KIOI -•\NillMl'll.( 1\'EMl·X:· 0 IIH' . .!h;&

Am FORCE TURBIN I' SERVICE 1'.0. llOX 146

TYNAN, TX 78391 Certifif,d Hq1:1ir Station TQZ.Ht JJ1{

woru< onnER #03602 Sln ·r~o:nnunt

DATI-:: 26-J an-04 L._ !"T6A I ~AG t•CE . f.~.\ 0--- .f'O\\'ERSI·:C fiON PCE 14155- 1110

HOOUS' 4935.11 ( L\Cjlft.j. >) . ) .L Hli:S ~

TOTAL TIME 7327,(, L 7 34 D o.o ~ TI~E SINCE OV~mt! A UL :"1/E\V TIME ~1!'\CE li ST:

Rf.:O ; IVEili'OWF.H SECTW!"i FOR A on:RHAUl - f'JW ,\ ~·OWER SI\CTION OVF.HHAUL AND I NSTALLF:!I ,'1: FACl OR\' N[W l:t; UEAIHNG PER Cl :ST01\1[ 1~S HEQUES T. n:ST01\11::R ,\l.SO tU.::::CTED TO RI:: INSTA LL ED !!IS l'T BLA tH :S wrru 7J~H• HOURS O!'li l ll l:l-,·1. A L! ST OFNEW, OHI AN U REWOHKF.D I'Mf.TS INSTt...LU:'. \1 ON T HIS .10 1> W ILL r.; c: Sf':!'<·;· SO TIL.._l. C t;ST01'11[H CAN ATTAOU:U IT TO HIS LOGBOOK AYS 0/U 1'\0T RECE I\'~~ . .11. L0GB()O!(, O NLY co::-a:s OUT OFTfiE LOG BOOK. A

FI JNLI!ONAL TEST \\'AS C/\\' tJS i i~G A GAS C E!\ SECTION !-- 'i-:01'·.1 \ TS 'S S HOP. I'OW~R SECTION \\·,\S TEST ACC!:TTI-:Il W!TH _~-,.TWO IIO fiR RUK IN WITU l'\0 I' ROiJLEMS f\'OTE D.

LH:r. UMIT ~:n ('01'1[!>{)!\i-:NT STATljS AS l' 'l'".ll SE!{V ICE. tHJLLETIN ;I 11.10m.:.

l~-;;;~2~~~~~,i<~-ll:~ii,;~~~lm§~~f~dJk7~~=t}~:~f~~i THIS CERTlFIES Til AT O NLY WORK f.:Et,!UESTED BY Tlll:o: Cl!STOMI::R WAS AC('0~1PLJSUCD 11'. ACCOROANt:l: WIT!! TH £ M.\NUFACT; :if.ER'S:Sl'I<:CtFICATJONS A!'iD CURRENT fAA Rl<:GULATJONS. A!'liJ TillS ENGINl:~ IS AI'PHOVLD FOI~ P. iCfl ~ r>.N YO S~:nVtCC. I'EHTI~I::NT DETAI LS Of THIS l ~l: rr~I R ARl'. 01': l-ILE UNDUl Tfl E WOHK O:WUt #UJi.02.

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Ai' U·REY H. HE INAMAK Clli£F JNSI'ECfOR

MAINTENANCE RECORD

REPAIRS, ADJUSTMENTS, MODIFICATIONS ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS

- 03602

--'~,__ SUTTER BUTTE 40604-100

- 1/26/04

-_. PARTS

----

------.....__

'--

-------.....__

-

~

~---

--L-

-L-

~

LIST PRICE

QIY PART# SERIAL# DESCRIPTION CONO PER UNIT

1 3036488 880032695 #6 BEARING NEW $7.057

1 3028282 FN0722 REAR RED, HOUSING OVH s 25,282.00

1 3024765 73 E030 1ST STG. SUN GEAR NEW $ 5,976.70

2 3032389 THERMOCOUPLES OVH s 583.70

1 3111 230-01 SEAL RUNNER OVH $ 640.00

1 3026652 PROP SEAL NEW s 152.00

1 ATS-COAT COATINGS $ 1,750.00

1 ATS-K003 POWER SECTION OVH Kl NEW s 2,144.84

1 ATS-K002 BALANCE CONSUMABLE$ NEW $ 165.00

1 ATS-K012 MISC. HARDWARE KIT NEW s 770.00

1 3109949-01 WASHER KEY NEW $ 602.00

Yuba-Sutter Aviation, Marysville, Ca.

--~ .... ~ 530.743.0688, Fax 530.743.6855

2/9/2004 Hobbs: 4943.8 Total Time: 7340

Hot section inspection complied with in accordance with Pratt & Whitney Maintenance manual .. Shroud housing repaired by Turbine Weld, small exit duct was repaired by Turbine weld , installed new segments, compressor inspected , engine assembled install ed 14 overh auled fuel nozzle tips. Grou nd CT clearance to .013. Engine ground run for leaks and operation_ The work described above was accomplished in accordance with the current Federal Aviation Administration Regulations and was determined to be in an airvvorthy condition with respect to the work accon?flished only.

S IG NATURE

===3=-~-+----+-+-----------===-=~:;:~~~~ ~~ ~ ,fi=p 5"97/o/707/

TOTAL THIS PAGE

TOTAL FROM 'REVIOUS SUMMARY

TOTAL SINCE MFG.

CARRIED FORWARD l

I --- -- - --~ '·--- -·- --· ·-·-- ,.,,.-~ '' ' "(,


LI CENSE NUMBER

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I TIME RUN DATE l HAS. MINS.

lUGHT • lWARD

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Y'lAi{ 03 ~107 . !e ......

lAy' - CS_ !liD

fJUP-Ql /09

~""''"' - (:) -:$ -\- lot

00I.J 03 +7q

r:EB- fJ-bO'-f _.«'

~-- to. tq rj£.6.

TOTAL THIS PAGE

TOTAL FROM lEVIOUS SUMMARY

TOTAL SINCE MFG.

ENGINE SERVICE AND MAINTENANCE RECORD . TIM E SI NCE

' NEW/~ INSTALLATIONS, INSPECTIONS,

REPAIRS, ADJUSTMENTS, MODIFICATIONS LICEN SE NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

ENTRI ES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. S IG NATURE NUMBE R HAS. MINS

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MAXIMUM H O UR S BETWEEN OVERHAULS HOURS.

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DAT E

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ENGINE SERVICE AND MAINTENANCE RECORD TIME S INGE NEW/~

HAS. I MIN$.

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INSTALLATIONS. INSPECTIONS, NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE REPAIRS. ADJUSTMENTS. MODIFICATIONS

ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS.

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Yuba-Sutter Aviation, Marysville, Ca.

~ ~ ~ 530 743 0688, Fax 530 743 6855

7!1412004 Hobbs : 5267.7 TT: 7659

Performed Hot section inspection in accordance with Pratt and Whitney maintenance manual. CT vane was replaced (class 13.29), shroud housing repaired, CT disc was in spected by Prime Turbines. Engine assembled and

ground run satisfactory ·

DATI 30 JUNE 2004 BOORS: 5267

TOTAL TIME 7659,, TtMT. SINCE OVERHAUL N/A

PA$TlJR£u.ND IMI"RO'iEMENTCORI' oiJ>o

AIRFOJ~CE TURBINE SERVICF. P.O. BOX 146

TYNAN, TX 78391 Certified Repair Stalion TQZRllJK

WORK ORDER 003742 SUTil';R-BUlTE DUSTER.<;

POWER SECTION PCE -14 155 -100 t'T6A-I SAG

TIME SINCE HSl: 289.6

CJ - 1· 1 I

RECEIVED POWER SECTION FOR PT DISK OR BLADE RUB. POWER SECTION WAS niSASSEMBL£D AND l"TlERE WAS SOME RUB NOTED AROUND TilE PT VANE RING BAFFLt=;: TUAT IS CONTROLLED BY THE THE EXHAUST DUCT. RUN OUT WAS OUT BY Jl-tO DUE TO A BrRD STRIJ(E. EXHAUST DUCT WAS SENT OU"f FOR REPAIR AND HEAT TREATED. POWER SECTION WAS MATED WfrD GAS GEN. SECllON AND F)}'NCTIONALY RUN FQR 2 HOURS WITH NO OIL LEAKS AND NO RUBS. POWER SEC110N WAS TEST AcCEPTED.

602 TOTAL STARTS SiNCE 12/111/97 12,128 TOTAl. FLIGHTS SINCE 121111197 LIFE Ul\fiT£0 COMPONENT STATtJS AS I'ER SERVICE BULJ.~nN N 12102 R5

c<»""wt.-ffiF.I"o'T PART# SERIAL # ·oouRs. -cYCLES CYCLES The work described above was accomplished JAW the

current FAR's and was determined to be in a airvvorthy

--------.-jr---t---+---1--=I condit)ffA w~h resp'1'\ toy~ work accomplished only. 4aalh o~ot /j~ ~&P549197097

151 STG. uun ~STGDISK 3 5T G DISK JM.PELU:R CTDJSK PTDISK

3013111 JOIJ7J2 3011 713 301Jl76 3013411 JU22412 t i/\742

CONSUJ\U:.D CONSUMED H.EMAINING 659.6 2411 :~ 7659.6 7457

7659.6 6335 ~-......... 7651l.6 ..., llJ.!! 7659.6 6161 9,839

,7659.6 ., .. 15.454

TOTAL THIS PAGE


TOTAL SINCE MFG.

c

BLADE INFORMATION: PARTII ..2_TY TOTAl , URS. DATI: INSTALLED CONDITION

I PT BLADES I 3013102 I 41----==-::l?6S9., ======:J TilTS Ct;RilnES TllAT ONLY WORK REQUESTED BY THF. CUSTOMER WAS ACCOMPLISRtD IN ACCORDANCE Wrlll HIE MAN1JFACTURE.lt"SSPECIF1CA110NS ANn CrJRRtNT lo' AA REG1fLA110 NS, AND lUIS ENGIN!l: IS APPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THIS REPAIR ARE ON FILE UNDER TIIE WORK 0RDE51#.0J74l , t• """""\

!L . .t"-''1 o/1. ·~·~ AUBREY H. HEINAMAN

ClllEF INSPECTOR

s·onn.<(

_HOURS.

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...,

ENGINE SERVICE AND MAINTENANCE RECORD

I TIME S INCE TIM E RUN NEW/OVERHAUL INSTALLATIONS, INSPECTIONS, REPAIRS. ADJUSTMENTS, MODIFICATIONS LI CENSE

DATE I NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. S IG N ATURE NUMBER HRS. MINS. H AS. MINS.

!OUGHT • 7 WA .J<;r

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tJP.i/f(ff< (i) 1:; {'1~ Rtl.- J.Jn-,}J,.< u;~;n,';_ 7:7: {0. .2 ,_ ~ f3o+J.. 572 ~ T. 50 9'11 F=£8. 'Q/_ • d.-."-11-;;:; FLLD(l CARRIED FORWARD "i '" . ..n S/I.LI-<"'P¥1 ° v Po~ LP--h /57£ ('~ /3r ,<::k...-..J a Luj,o D.--:tx' sLJ!i'l·tP

TOTALTHISPAGE ~~I /1/1. ~ ~ ~ ~ r :~ 1_ • -;;-ila7 .•. ~ ~ r/ DK. &w._~c.iij, .~/1,(},, /{--,Ps-7.3J?ug 7~( TOTAL FROM s ~ ~ '- - ~ MAXIMUM HOURS B~EEN OVERHAULS I HOURS.

REVIOUS SUMMARY

TOTAL SINCE MFG.

•• . ' ' , _ _, . .. · .... -"'-•· "'-~- 5-< 9iA.A. -& '-!t · -' · "·•'· 'o----)-· 'p-•- ' -

,- ,.., Llr\ C1 '1CAT7'J7'l P. Ol


DATE I TIM E RUN

I HAS. I MINS

TIME SINCE N EW/OVERHAUL

HAS. I MINS.

~~~~~~ • I 181/S I/ APr, 1-o 1P I ..0' I IBtLB.~

1 :;t I _....r- I 8/30 ie'

-MriV-fJ& l+q~..~-- iB;:ycJ.e-=

-1'\'\A<.{-OI'o \+/O(Q IA~3.:21JY

M l-iY- 0~ -t'7 ~B39V


REPAIRS, ADJUSTMENTS, MODI FICATIONS ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMN S. S IG NATURE

LICEN SE NUMBER

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TOTAL THI S PAGE


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I TIM E RUN TIME S INCE

NEW/OVERHAUL INSTALLATIONS, INSPECTIONS, REPAIRS, ADJUSTMENTS, MODIFICATIONS LICEN SE DATE I HAS. NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS S IGNATUR E NUMBER MINS. H AS. MINS.

BROUGHT ... ~M tY ~~').O'J-H~ FORWARD

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TOTAL THIS PAGE



TOTAL SINCE MFG.

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I TIM E RUN TIME S IN CE

NEW/OVERHAUL INSTALLATIONS, INSPECTIONS, REPAIRS. ADJUSTMENTS, MODIFICATIONS LICEN SE DATE I HAS. NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS SIGNATURE NUMBER

MINS H AS. MINS.

.ROUGHT .. yof30 &783~ ORWARD

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~-•,::: 550.--!5.cir .. 't'!. Fax 551/.-~5.1:>855 . "-&«/t>'l Hobbs. c;; qu,E'!J,iz ~·· / .Y/ :s-.:5-

Date: 400 hour service accomplished in accordance with Pratt & \IVhitney Canada Maintenance Manual. Reduction gear box drained. chip detector inspected and functionalfy checked. Starter generator blown out. brushes checked, spline and drive inspected for wear. Inlet fuel filter inspected and cleaned. outlet filter replaced. Oil filter inspected for metal and condition. Igniters inspected and operationally checked. Engine inspected externally. control rigging checked. Inlet area and exhaust duct area inspeded. Oil changed, fuel nozzles cleaned and now checked. Engine was washed externally, a power recovery wash wa~ accomplished. The work descn"bed above was accomplished in accordance with the Federal Aviation Regulations and was determined to be in an airworthy condition with z~rk accomplished only

Name:~ ~ Cert#: Ar';Cl2 uu 7/ L/2'

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CARRIED FORWARD u

TOTAL THIS PAGE

TOTAL FROM MAXIMUM HOURS BETWEEN OVERHAULS HOURS. PREVIOUS SUMMARY

SllJ:Cn}FG - - --

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IRO UGHT 'ORWARD

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TOTAL THIS PAGE


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HAS. I MINS.

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ENGINE SERVICE AND TIM E S INC E NEW/~

HAS. I MINS.


CARRIED FORWARD

MAINTENANCE RECORD

REPAIRS, ADJUSTMENTS, MODIFICATIONS ENTRIES DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. S IG N ATURE

MAX IMUM HOURS BETWE EN OVE RHAULS HOURS.

LI CEN S E NUMB ER

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ENGINE SERVICE AND MAINTENANCE RECORD .-... ........ .

TIME RUN TIME SINCE

DATE NEW/OVERHAUL INSTALLATIONS, INSPECTIONS, REPAIRS, ADJUSTMENTS, MODIFICATIONS LICENSE

NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE ENTRIES. DR AW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS S IGNATURE NUMBER HAS. MINS. HAS. MINS. ~

BROUGHT ... FORWARD

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,, - + - 530.743.0688, Fax 530.743.6855 Engine Log ' 1:-711412010 Tach: 7878.6 Ag Cat G 164-B N3627G

1. Removed, cleaned, inspected, and reinstalled bleed valve. " 2. lnstafled new right hand igniter harness. ~ 3. Installed new primary nozzle fuel line. . The worl< described above was accomplished in rrdance with the current Federal Aviation ' Regulations and was detennined to be i".;;ZI hy condition with respect to the work I

accompti:!P/ only. ~ rf17'/ l ~eil

A&P 3099466

' !

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CARRIED FORWARD

TOTAL THIS PAGE

TOTAL FROM MAXIMUM H OURS BETWEEN OVERHAULS HOURS. PREVIOUS SUMMARY

TOTAL SINCE MFG.

-- ---·- -- - -

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/ . · MAINTENANCE RECORD ENGINE SERVICE AND I TIME RUN I TIME SINCE I d NEW/OVERHAUL ~ ------~~~~=-----~::::~::::~==~~====~~~~~==~~~------~------------------r--------

REPAIRS, ADJUSTMENTS, MODI FICATIONS DATE

BROUGHT FORWARD •

HAS. I MINS. HAS. I MINS. SIGNATURE ENTRI ES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINE S IN DATE AND TIM E COLUMN S.

INSTALLATIONS. INSPECTIONS, NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIR ED FOR COMPLETE

0 . ~ rt 6{0 . u

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- '

CARRIED FORWARD

MAXIMUM HOURS B ETWEEN OVERHAULS HOURS.

.,.--..~,....,.,--.~.~-.,.., ~~.--.. ---· ~-~· ~.~~- -~':7-~- - -~---""' • .,._-~-:""~·~~ ,_, <i ., .. JlMi< .,f< •· . ..-:;; ,,\ .... f3- ~ -~__,-,.,,..,~..,.,.-,.,,.,..,.,.,._...,.,.,....,,....,,_...., ..... _______ ~-----------------....

DATE

BROUGHT ... FORWARD

~/s /;c_ ./ /

TOTAL THIS PAGE


TOTAL SINCE MFG.

ENGINE SERVICE AND

TIME RUN TIME SINCE

NEW/OVERHAUL INSTALLATIONS, INSPECTIONS,

HAS. MINS. HAS. MINS. NOTE: USE BOTH PAGES AND AS MANY LINES AS REQUIRED FOR COMPLETE

DATE: 4/05/12 ENG. MODEL: PT6A- 15AG ENG. S/N: PCE-14155 HOBBS: 8271.4 ENG. TSN :

1.

2.

3.

4.

5. 6. 7. 8. 9.

10.

11.

12.

Performed a Sudden Stoppage Inspection in accordance with Pratt & Whitney

Maintenance Manua l for PT6A-15AG engines, P/N 3030442, Rev. 39, dated

12/10/10, chapter 72/00/00, paragraph 12, L, pages 652-653. Constant Speed Governor P/N 8210-002-01, S/N 2257349 was overhauled by Rocky Mountain Propellers on W.O. 38220.

Overspeed Governor P/N 8210507, S/N 2477235W was overhauled by Rocky Mountain Propellers on W.O. 38219. Replaced #6 Bearing with P/N 3102227-01, S/N BB9812833 overhaul ed by Bearing Inspection on W.O. 707965.

Replaced Exhaust Duct with serviceable condition P/N 3111780-01, S/N 1E630. Performed Run-out of Propeller Shaft, less than 0.001." Replaced Torque Piston Seals with new P/N 3012456 and 3012457.

Remaining Power Section was disassembled, inspected, cleaned and reassembled . Complied with a Hot Section Inspection in accordance with P/N 3030442, Rev. 39, dated 12/10/10, chapter 72-00-00, paragraph 10 and table 604.

Combustion Liner P/N 3109264-01, S/N 3E475, was repaired by Aviation Welding on W.O. 6923. Compressor Turbine Disk Assembly was inspected determined to be serviceable, Diameter 8.550."

Rebuilt Inner Exit Duct Assembly . Replaced Shroud Segments with new PF3019438 CL 9, (16) each from Precision Fliterparts on W.O. 3209-11. Installed Small Exit Duct and Final Ground Segments to a clearance of 0.012."

13. Cleaned and flow checked all fuel nozzles OK. 14. Reassembled Engine at "C" Flange. 15. Complied with a Periodic (100) HR Inspection in accordance with P/N 3030442, Rev.

39, dated 12/10/10, chapter 72-00-00, paragraph 8, and table 601-602 . 16. Inspected Main Oil Filter and Chip Detector OK.

17. Replaced High Pressure Fuel Pump discharge Filter and cleaned intake screen . 18. Tested I.T.T. Indicating System OK. 19. Inspected Compressor Blades OK.

20. Lubed Engine Controls and Starter/Generator Splines. 21. Performed a Compressor Wash.

22 . Inspected P3 Air Filter.

All work performed in accordance with manufacturer's maintenance manual and current FAA regulations.

-MAINTENANCE RECORD


AUTHORIZED RELEASE CERTIFICATE 1 Approving National Aviation Authority / Country

FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

FAA I UNITED STATES

4. OrganiZation Name and Address

Rocky Mounta in Propellers, Inc , 2865 Airport Drive, Erie, CO 80516 USA FAA FR6R545N • EASA145.4827

6 Item I 7. Descript ion: I 8. Part Number I 9. Eligibilrty: •

I Woodward Governor I B210507 I NI A 13. Remarks:

I 10. Oty: l l I

3. System Tracking Ref. No

38219

5. Work Order, Contract, or Invoice Number·

38219

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

2477235 w I Overhauled

Overhauled governor in accordance with Woodward Service Manual #61 -20-37 , Rev. 9. Complied with Service Bulletins thru 33580M. No AD's currently apply. Overhaul due 6 years or 6500 hours 1f unit is operated 120 hours per year continuously.

A complete Description of work performed is on file at th e above referenced organization under the work order and system tracking reference number indicated in blocks 3 and 5. Notice: An Airworthiness Directive may apply to the article(s) described hereon. The installer is responsible for ensuring complete compli ance with any applicable Airworthiness Directives "Certifies that the work specified in block 12 / 13 was carried out in accordance with FAR Part-145 and EASA Part-145 and in respect to that work the component is considered ready for release to service under FAA FR6R545N and EASA Approal Number: EASA.145.4827"

14_ Certilles the Hems identified above were manufactured in conformity to·

0 0

Approved design d<lta and are in a conditiQn for safe operat ion. Non-approved deSign data specified in Block 13

15. AuthoriZed Signature 16 .. Approvai / Aulhorizat ion No

17. Name (Typed or Printed) 18 Date(rn/dly)

" [!] 14 Cf R 43 9 Return to Service [!] Other regulahon spectffed 10 Block 13

CerttfleS that un~s othervnse spectfH!'O in Block 13. tne w ldenttfied 11'"1 Bloc!( 12 and descnbed m Block 13 ·.vas accomplished tn aCCOfdanee Ynth Title 14, Code of federal Regulat iOI"'Is. pan 43 and 10 respect to that work, the ~ems are approved for return to serviCe

22'"lrame{~tea):·

Stephen Robertson

23. Date (mldiy)

Mar 12. 2012

User / Installer Re~ons i b ilitie s

It is important to understand that the existence of this document alone d<>K not automatic:al!y constitute author ity to install the part f component / assembly. Where the user 1 insta ller performs work tn

accordance with the national regulat ions of an Airworthiness Authority different than the airworthiness authofity of the country specifted in block 1, it is essent ial that the user I tnstaller ensures that hts 1 her airworthinessauthorityacceptsparts / components / assembl ies fromtllea irvmrth10essauthorityofthecountryspecifiedtnblock1 . Statementsinblock 14and 19 donotconst itute installat ion certification . In al l cases, aircraft maintenance records must conta in an instal lat ion certtficat ion issued in accordance with the national regulations by the user f installer before the aircrall may be flown

FAA Form 81 30-3 (6-01 ) • Installer must cross check el igi bit ~y vltlh appl icable technica l data

AUTHORIZED RELEASE CERTIFICATE \.Approving National Aviation Authority/Country

FAA Form 8130-3 , AIRWORTHINESS APPROVAL TAG

FAA I UNITED STATES

4. Organization Name and Address

Rocky Mountain Propellers, Inc., 2865 Airport Drive, Erie , CO 80516 USA FAA FR6R545N - EASA.145.4827

6. Item: I 7. Description I 8 Part Number 9. Eligibility: ·

I Woodward Governor I 8210-002-01 NIA 13. Remarks

I 10 Oty l I I

MSN· 0052-00-012-9005 J

3. System Tracking Ref_ No

38220

5. Work Order. Contract. or Invoice Number:

38220

,, Serial /Batch Number I 12. Status / Wo~

2257349 I Overhauled

Overhauled governor in accordance with Woodward Service Manual #61-20-14, Rev. 3. Complied with Service Bu llet ins thru 83053-61 -019. No AD's currently apply. Overhaul due 6 years or 4500 hours if unit is operated 120 hours per year continuously

A complete Description of work performed is on file at the above referenced organization under the work order and system tracking reference number indicated in blocks 3 and 5. Notice : An Airworthiness Directive may apply to the art icl e{s) described hereon. The instal ler is responsible for ensuring complete compliance with any applicable Airworthiness Directives. "Certifies that the work specified in block 12/13 was carried out in accordance with FAR Part-145 and EASA Part-145 and in respect to that work the component is considered ready for release to service under FAA FR6R545N and EASA Approal Number: EASA.145.482r

14_ Certilles the rtems idenltflfd above were manufactured in confor~n~ty to

0 0

Approved design data and are in a condition for S<l fe operation Non-approved design data specified in Block 13

19

[!] 14CFR43.9Returnto Service [!] Otherregulationspecifiedin Block 13

Certifies that unless otherwise specified in Block 13. the work identified in Block 12 and described in Block t3was accomplished in accordance with Tttle 14. Code of Federal Regulations. part 43 and in respect to that work, the items are a proved for return to service

15 .. Authorized Signature 16. Approval / A uthorization No. (~b.ouzed-~~ __::: 21_ Approval I Cert ificate No

FR6R545N

17. N•me (Typ<d 0< P•i01oo) 18 Datetm/d/y)" 22 Name (Typed or Printed)

Stephen Robertson

User / Installer Responsibilit ies

23. Date(mld/y)

Mar 12.2012

It is important to understand that the e~ i stence of this document alone does not automatic_a lly constttute authomy to mstall the p<lrt I com.ponent l assembly. Where the user I instal ler performs work i_n accordance w~h the national regulations of an Airworthiness Authority different than the atrworthiness autnonty of the country spectfted tn block 1.' ~ IS essen1ial that the user l mslalle~ ensur~ that hts I her airworthiness autllOI" tty accepts parts I components I assemblies from the atrv~htness authorrty of the country spectfted in block _1. Statements m block 14 and 19 do not constitute mstallalton certification. !n all cases, ai rcrall maintenance records must con ta in an instaltatton certtf1cat ion 1ssued tn accordance wrth the nahonal regulations by the user I mstal ler before the aircraft may be flown

FAA Form 8 130-3 (6-01) • lnsla ller must cross check elig ibility with applicab le technical data MSN: 0052-00-012-9005

SIGNATURE

I

MAXIMUM HOURS BETWEEN OVERHAULS -------HOURS.

LICENSE NUMBER

BROUGHFORWAR!

DATE: 3-5-2013 HOBBS: 8,273.6

--

1/8/13 N3627G HM 8273.4

Removed engine s/n PCE 14155 from N3627G for inspection. IMPLETE

ENG MODEL: PT6A-15AG n : 10,666.2

Received Engine for I.R.A.N . on Compressor. Engine was disassembled l o the extent necessary to perform repairs, cleaned, inspected and repaired in accordance with Pratt and Whitney MM 3030442 Rev. 40, dated May 18, 2012.

The following repairs were made: 1. The following Compressor Components were recoated b'f J&S Plating and Repair on Work Order's 173251, 173252, and

173253. P/N 3014679 S/N 24551- 3'd Stage Spacer, P/N 3013602- 2nd Stage Blades, P/N 3013603- 3'd Stage Blades, P/N 3013632 S/N 17560- 2nd Stage Spacer, P/N 3013661 S/N 7246315 -1'1 Stage Stator, P/N 3013662 S/N FNOS67C- 2nd Stage

Stator, P/N 3013663 S/N FN0963C- 3'd Stage Stator, P/N 3013821 S/N 4Y725- Hub, P/N 3010607- Blade Retaining Ring, P/N 3013712 S/N 27 A173- 2nd Stage Disk, P/N 3011713 S/N 25A242- 3'd Stage Disk, and P/N 3014020- Rotor Air Seal.

2. Replaced #2 Bearing with P/N 3006146 S/N RS85, Overhauled by Bearing Inspection, Inc. on Work Order 701297. 3. Compressor Assy. was balanced with CT Disk P/N 3013£\11 S/N 22A549 by Southwest Airmotive, Corp. on Work Order 7340. 4. Reinstalled Compressor and CT Disk. Verified satisfactory Impel ler clearance- .025" and CT clearance- .013" . 5. Remated Power Section to Gas Generator. 6. Saftied Engine and prepared for return to customer.

All work performed in accordance with manufacturer' s ma inte r.an~·c: : ;~2, r, u al ar;d current FAA regulations.

J!)~ttHA~ Don Morrison A&P 2811730

TOTAL THIS PAGE


TOTAL SINCE MFG.

3/16/13 N3627G Hm 8273.6

Reinstalled engine PT6A-15AG s/n PCE 14155 on Schweizer G-164B s/n 729B after repair by Pro Turbine. Ground test. Adjusted beta rigging.

Gary S. Bums A&P 3602449

..

CARRIED FORWARD

-DA' ENI ENI

IN!

GA

RE

~ A&

ENGINE SERVICE AND TIME RUN

TIME SINCE

DATE N EW/OVERHAU L INSTALLATIONS, INSPECTIONS,

HRS. M INS. HRS. MINS. NOTE: USE BOTH PAGES AN D AS MANY LINES AS REQUIRED FOR COMPLETE

BROU G HT ... FO RW A RD

~ ) 'z_c..//3 , I

Engine Type/Model : T.T. 10779.9 Hobbs: 8387.3

PT6A-15AG T.C. 10779

Engine Serial Number: PC-E 14155 T.S .O. unk. C.S.O. unk.

Engine partially disassembled for vibration analysis. Balanced compressor assembly. Re-assembled engine. Installed 0 /H BOV s/n 28A484. Engine tested and vibration data found within limits. All work performed IIA/W current FAA regulations and current manufacture' s data. Pertinent details are on file at this facility. WorkOrderNo. 02228 Date 07/22/20 13

Signed by~ ~~ 0

For: R.T. Turbines Inc. 3397 Hwy. 121 West Marianna, AR. 72360 CRS # MW9R61 OJ

July 24, 2013 N3627G Hobbs: 8388 ____ Engine removed for repairs by RT Turbines. Engine reinstalled following repairs.

Serviced wtth 'f)1:80 ~~d ground run ok.

_ _ ___.J Steve A. Hal~ A&P 3702438

CARRIED FORWARD

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MAINTENANCE RECORD


July 24, 2013 N3627G Hobbs: 8388 Prop removed for engine repairs and reinstalled following.

'11Us propeller balanced .... ACF.S 201S ProbaJanoer ~

Steve A. Hall Q L . g._{kt p - A&P 3702438 ~ 'l

July 24, 2013 N3627G Hobbs: 8388 Replaced starter/generator with s/n 98296; replaced voltage regulator with s/n AVR304; replaced tail wheel bearings; removed hopper gatebox and replaced

gaskets;~ ~~Lf

Steve A. Hall A&P 3702438

SIGNATURE

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ENGINE SERVICE AND I 1 TIME S INCE I

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MAINTENANCE RECORD

REPAIRS, ADJUSTMENTS. MODIFICATIONS I /41 1111 ti I !I iAW A DIAOONAL LINE THROUGH ANY UNUSED LIN ES IN DATE AND TIME COLUMNS SIGNATURE

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f ·moil· ~oreHJAuRepoinnc .com • hllp.// ww.,.AirReporrlnc .com

___ February 6, 2015 N3627G Hobbs: 8876 Total: 10638.6 I 00 hour inspection completed; oi l filter inspected ok; oil changed; fuel filters

--- cleaned or replaced as required; fuel nozzles flow checked ok; igniters checked; --- engine ground run Dk.

TOTAL.

-mTA Steve A. Hall PREVIO~; A&P 3702438

SINC

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BROUGHT FORWARD

ENGINE SERVICE AND

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f-motl salestiA~rRepamnc.com • http://www.AirRepairlnc.com

____ January 14,2016 N3672G Hobbs: 9086 Total: 10849 _____ 1 00 hour inspection completed; oil filter inspected ok; fuel filters inspected ok; fuel

nozzles flow checked ok; igniters checked; engine ground run OK. -----

:~::e~~~~~g/t;A~:~~L INSPECTION AND WAS DETERMINED~

~g~ ----- Steve A. Hall ---- A&P 3702438

DATE: 1/18/2017 ENG MODEL: PT6A-15AG ENG S/N: PCE-14155

I FOR COMPLETE

HM: 9358.0 ENG TSN: 11,121.0 Complied with a Hot Section Inspection in accordance with Pratt & Whitney MM P/N 3030442R45 dated Aug-

24-2015 Chapter 72-00-00 paragraph 11 & table 604. 1) Split Engine at "C" Flange. 2) Removed Hot Section for inspection, all components found to be in serviceable condition.

3) Reinstalled Hot Section components. 4) Reinstalled C/T Disk P/N 3013411 S/N 22A549, C/T Vane Ring class PWC F/C: 13.45.

5) Measured C/T tip clearance at .0125 average. 6) Function tested T-51ndicating System- OK. System resistance measured at .7252. 7) Visually inspected GG Case, Exhaust Duct and P /T Vane Ring- OK. 8) Containment Ring AD 14-11-07 does not apply to this engine due to P/N 3109595-01.

9) Clean and Flowed Fuel Nozzles- OK. 10) Installed (2 ea.) New Champion CH34055 Igniters. Function Tested OK.

11) Re-mated Power Section at "C" Flange. This engine must be leak checked and performance checked before return to service.

All work done in accordance with manufacturer's manuals and current FAA regulations.

~7/Jfo $-<=' Chris Marchese A&P 3050079

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REPAIRS, ADJUSTMENTS, MODIFICATIONS ENTRIES. DRAW A DIAGONAL LINE THROUGH ANY UNUSED LINES IN DATE AND TIME COLUMNS. SIGNATURE

South Delta Aviation Helena-West Helena, AR 72390 870-572-9011

N3627G Date: 4-4-17 Hobbs: 9358.0 SHOT: 0.0 TTE: 11,121.0 Completed annual inspection this date: Checked lines, hoses, fittings, mounts and controls. Replaced oil filter. Replaced fuel bowl filter and cleaned inlet screen. Cleaned firewall fuel filter. Removed starter-generator s/n 98296 and reinstalled after overhaul by Arkansas Aeronautics Accessories. Cleaned induction air filter and reinstalled. See AD list in aircraft records for details of compliance. Ground run up found to be satisfactory. All parameters normal and no leaks detected. I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH A 100 HOUR INSPECTION AND FOUND TO BE IN AN AIRWORTHY CONDITION.

Michael D. Schlesselman A&P3469 I 89IA

South Delta Aviation

N3627G Model: PT6A-15AG

Helena-West Helena, AR 72390 870-572-9011

STATUS OF LIFE LIMITED PARTS

Hobbs: 9358.0 Date: 4-4-17 sin: PCE-14155 TIE: 11,121.0

Flights since last sheet: 327 Service Bulletin: 12102R6 Starts since last sheet: 78

Descnpt1on p IN s IN eye es consume d I I' . ACF FCF eye e 1m1t eye es remammg Hub, 1st stage 3013111 4Y725 3327 19,000 5 .43 15,673 Disk, 2nd stage 3013712 27Al73 10,291 24,000 5 1.33 13,709 Disk, 3'0 stage 3011713 25A242 8,742 25,000 5 1.13 16,258 Impeller 3013176 4D547 8,491 19,000 2 .53 10,509 CT Disk 3013411 22A549 8,960 16,000 10 1.78 7,040 PT Disk 3022412 12A742 5,851 20,000 10 .83 14,149

ATC= [starts+ (flights - starts/ ACF)] X FCF

The above was calculated using the most recent revision of the applicable service bulletins, past aircraft records, pilot supplied information and is true and correct to the best of my knowledge.

Michael D. Schlesselman A&P3469189 ~~.L?~«:4:1 ,e

L>ICENSE NUMBER

-----· --- -------~-----------------------------'------------1-----South Delta Aviation

N3627G Hobbs: 9358.0

Helena-West Helena, AR 72390

SHOT: 0.0

870-572-9011

Date: 7-15-19 TTE: 11,121.0

Completed annual inspection this date: Checked lines, hoses, fittings, mounts and controls. Cleaned firewall fuel filter. See AD list in aircraft records for details of compliance. Ground run up found to be satisfactory. I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH A I 00 HOUR INSPECTION AND FOUND TO BE IN AN AIRWORTHY CONDITION.

~<~~44-_ Michael D. Schlesselman . A&P3469189IA

MAXIMUM HOURS BETWEEN OVERHAULS ________ HOURS.

AIRFORCE TURBINE SERVICE - Sandhills Global

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