AIRCRAFT CORPORATION · 2013. 8. 15. · cooler p/n CAM 649479. See 337. Exhaust slip joints...

AIRCRAFT CORPORATION

ENGINEMAINTENANCE RECORDS

Log No.

Aircraft Registration No. l\ h *- r\

Engine Manufacturer

Model . .

Serial No.

Date installed on aircraft j i f 76?

Time Between Overhauls (TBO) .Hours

If used on multi-engine aircraft:

CTRight D Left

817/752-8,381Waco Regional Airport • P.O. Box 5219 • Waco, Texas 76708

FAX 817-752-3307 1-800-445-9713

"LOGBOOK FORMAT REPRINTED WITH THE PERMISSION OF AEROTECH PUBLICATIONS, INC.,THE ADLOG (TM) SYSTEM, COPYRIGHT 1979."

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DESCRIPTION OF WORK PERFORMED—SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK

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AIRCRAFT CORPORATION

Waco RegionsalA^ovrt '

Engine Previous Total:Hour Meter:'

Since Remanufacture:Propeller Total:'

Date:"TSIO-520-NcNB S/N R-228513-R

1185.4"00.0oo.o -oo.o

- 7/19/96

Above referenced engine remanufactured to new parts limits to conform w/TCM SM X-30574.All gears cleaned, polished when required, inspected, magnafluxed and no cracks found.Finish and dimensional limits within RAM Gear Inspection Criteria - RAM Repair StationReport No. 1818 dated 10/16/95. Installed above referenced engine modified to TSIO-520-NB 335 HP per STC SE4327SW in right position of Cessna 340A, s/n 340A-0436. See337. Installed new RAM camshaft p/n 1058-3SL, L95078 per STC SE4327SW, Rev. 4.Installed heavy style case p/n 643207 with new channel chrome cylinders. Cylindersmodified to RAM p/n 1158-2 per STC SE36731SW. Crankcase modified to RAM p/n 1157-7 perSTC SE3 63 0SW. Cylinder hold-down nuts replaced and torqued per Overhaul ManualSupplement. Installed Floscan transducer per STC SE5726SW. Installed new McCauleypropeller model 3AF32C515, s/n 960924. Fire extinguisher bottle removed and sent outfor inspection and weight check. Re-installed per service instructions. See servicetag dated 7/5/96. Engine accessories exchanged for remanufactured or new units.Installed new prop governor. Re-used customer's vacuum pump, tach generator andhydraulic pump. Installed factory overhauled turbocharger. New Slick pressurizedmagnetos p/n 6320 installed per STC SE4651SW and pressurized. See 337. SB94-8 onmagneto timing procedure c/w per timing to STC degree requirements with TDC locator andprotractor with pointer. AD 86-13-04 R3 N/A per cylinder p/n. Installed modifiedconnecting rods p/n 1162-1 with bearing p/n 630826 per STC SE4327SW as FAA-PMA approvedreplacement. Installed RAM/FAA/PMA rocker arms p/n 1158-4 and -5 (single-piecebushing) . Cadmium plating of engine hardware and associated lines and fittings per Q.Q.-P-416C Class 2, Type II. C/W AD 75-23-08 R5 per inspections outlined in para's I A£1) (2) (3) of components in Table II. Installed new Aeroquip integral firesleeved fueland oil hoses meeting TSO-C53A Type D and TSO-C75 Type III. Inspected complete exhaustsystem upon disassembly. Turbo inlet clamps replaced this date with non-life limitedclamps p/n NH1000897-20's along with wastegate inlet 400-hour limited clamp p/nMVT68892-200. Wastegate clamp due replacement in 400 hours. Installed new NDM oilcooler p/n CAM 649479. See 337. Exhaust slip joints modified per STC SA4331SW. See337. AD 93-08-17 not applicable per engine model. AD 78-06-01 c/w previously per newintake tube p/n 642590. AD 79-05-09 c/w previously per current design plunger assy.Replaced at this time with new assy. C/W AD 89-24-01 Rl per installation of starteradapter p/n 642085A11 with current scavenge pump gears. Service Bulletin compliancethrough CSB96-8 in RAM Manual. Engine serviced with Phillips multi-grade 20W-50 TypeM mineral oil. See RAM Recommended Oil Grade Maintenance Tip M-lb for recommended oilsafter 25 hours. AD 76-02-07 n/a per installation of ALV9510 alternator. AD 87-23-08is n/a per crankshaft p/n. TCM SB 92-16 c/w per installation of VAR crankshaft (n/ato TSIO-520"B" series crankshaft). Above referenced engine was made eligible for 1600hr. TBO per TCM M91-08 Note 3. All aluminum, alloy engine parts were coated per RAMSpecification No. 1142. Crankshaft assy. , connecting rods, pistons, piston pins,alternator rotor and turbocharger compressor wheel assy* s. were balance per RAMSpecification No. 1161. See RAM Certificate. Propeller balanced per Service Manualwith spinner and bulkhead installed. Installed spring loaded induction clamps p/n1170-2 per STC SE3632SW. installed RAM-FAA-PMA rocker box cover gaskets p/n 1387-1.Installed RAM FAA-PMA oil cooler baffle p/n 1253-1. Cylinders flowed per RAM CylinderFlowing Specification No. 1242. C/W AD 93-16-15 per TCM SB M93-9 Rl installation offuel pump drive coupling p/n 653359. All engine systems checked for leaks. Engineapproved for return to service for RAM Aircraft test flight procedures. Pertinentdetails on filed under Work Order No. 2232.

RAM Aircraft Box 5219, Waco, Texas 76708 CRS VA1R551K

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Hour Meter : ^ 2SMOH : gf gDate : *?//<?/<?<#

Engine pump pressure," idle, mixture, fuel flow, max RPM, manifold pressure, andoil pressure adjusted per TSIO-520-NB specifications. Engine ground run powertest good. Details are on file under Work Order No. 2282.

— RAM Aircraft Corporation, P. O. Box 5219, Waco, Texas 76708 CRS VA1R551K

Hour Meter : ^ 2Since Remanuf acture : ^£,2?

Date : *?//%/'?£

- Oil drained and engine re-serviced with Phillips multi-grade 20W-50 Type Mmineral oil. Oil filter inspected for metal particles and found satisfactory.

_ Installed new Champion oil filter CH48108. Run and leak checked satisfactory.Pertinent details are on file under Work Order No. 2282.

RAM Aircraft Coloration, P. O. Box 5219, Waco, Texas 76708 CRS VA1R551K

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h«s ben inspected in accordance wfth a

mined to be in an airworthy condition.

^r-W^C-A^- .„ /*S

K«vin S. Laukaitis ^jA Jfe H Wy«>4^y4&-^ r

McKinney Exec Air1 500 E. Industrial Blvd.McKinney, TX 75069

972-562-5555

Reg n N6239X Make: CESSNA 34UA ™'"0'UDate: 06-12-97 S/N: 340A0436 TTSN:

CHANGED OIL AND FILTER; ADDED 1 1 QTS AEROSHELL SOD. ^-^ ) (J

fAGE 1 OF I

\^ /[ [//^KDavid Pyeatt A&P 46 i584871A

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6'

/£%}

8-26-98

Perform oil chaengine with 11

filter, no defeleaks noted. Ap

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4

DESCRIPTION OF WORK PERFORMED—

SIGNATURE & CERTIFICATE NO. OF PERSON PERFORMING WORK


JT

/W-6- tnfllcaterj_^^-^r Hours. Date ^x^>"

1 certify that this powerpiant/airframe hss be&n Inspected

in sccoroance witn a n //™ -/ in.^psntinn ana was

rtetprrninfid t<) HP In airworthy rnnHiHnn

AD conformity r.hRnk-Rri thrnnph r?rd tyi? ?#-<?£'

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HOBBS 0374.1 N6239X RT 1WC

nge and oil filter P/N CH48108. Sft-nrfrP

Qt's Aeroshell 100. Cut open old oil

proved for return to service.

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DaleTach ( ) Hobbs (T. Sine

T, Airfram^ ( ) 1 ngm§

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MAKE TT. yN No.

TOTAL TIME TACH READING 45/.M DATE

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7T/£?f.pTOTAL ENGINE TIME

TELEDYNE MATTITUCK SERVICES, INC.

FAA Repair Station T10R507Y MATTITUCK

W.O. No. Authorized Signature

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DateTach( tt t Tfr^rrrframe-{—>•

T. PropT. Since fvlajory that this airframe ( ) engine ( "1 has oeen

e- with—an—annual ( "? orcerti

inspecin-

^r •&ccGfcicirhour inspection and was determined to be in an

airworhy condition. A.D. conformity checked througt

$7


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hour inspecfton and was determined to be in a'orthy condition. A.D. conformity checked througr

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HagerstCacti

14235 Oak Spring

DATE 07/27/06 Hobbs


own Aircraft Services, Inc.tied Repair: Station: CKi> HbUKObUUs Road, Hagerstown, MD 21742 (301) 733-7604

Nft 6239x MAKE CONTINENTAL MODEL TSIO-520-NCNB S/N f>-~ 3.a.fen -1?

Removed enand cleaned reinspection on. JDivco W0#reconditioningAl, new conn654490, new <CO 6 094. Instalnew gaskets an340A S/N 340oil lines. Servchecked O.K. CC/W AD 97-2Cin respect to \and current fed

Slgned_Paul MHagerstown AiFAA Approved

Hageic

14 2 35 Oak Sp

jine from aircralated parts. Per11 non-ferrous

311998. Installjy Aircraft Specacting rod bearrank gear bolted new fuel pi.d seals. InstalleA.0436 right harced engine wit"ompression che-17 crankshaftjrk performed, tera! aviation reg

Richter : ^

RIGHT HAND ENGINEft and capped and sealed all fuel and oil lines. Disassembled enginerbrmed a magnaflux inspection of all steel pans, and a Zyglow

id same crankshaft S/N SI52490-1 TCM s/n (861047) afteriahies(W/0 1533821 with new main bearing set P/N AEC646592-ngs P/N 642398, new rod bolts P/N 655961, new rod nuts P/N

P/N 536379. Installed new RAM camshaft P/N 1058-1A S/N

i new oil filter CH48 108-1. Installed engine back ontoN6239X C-d side. Attached, secured, and saftied all control nahlfi;';, fuel anH

h 12qts Aeroshell I5vv50 oil. Ground ran engine. Leak and opseked cyls. #1 76/80 #2 78/80 #3 76/80 #4 78/80 #5 73/SO #6 72/80.-iltrasomc inspection. Engine is approved tor return to service only\\\k was performed I/AAV manufactures maintenance manuals

^^^ ^^-^^ ^£^s££^craft Services, Inc HagerstCwhT MD 21742epair Station H5GR0500

rstown Aiertified Reprings Road,

rcraft Services, Inc.iir Station: CRS H5GRO5OO

DATE 12/14/11 HOBBS 612.7 EHG SMOH 612.7 EHG TT 1798.1 w/o 0603111

Changed

19-07 la

oil with 12qts Aeroshell 15Wd new CH481Q8. Compression 1

H/ft due to no EQ3 cyls instto verify that no hydr

installed during affeccer t i fy this' engine hato be in airworthy conper formeregulati

HageFAft

aulic liftersching engine rted time perios been inspectdition and is

d I/A/H manufacturer's maintons. f\: Joseph S. Hartt .v&ZA,

;0. Cut oil filter open to inspect and found O.K.

illcd. C/W AD2Q10-11-04 by researching engine records•lere installed during affected time period. C/H'?ords t"" v p r i f y rhn r rhp ^rart-pi- arlapfpr wa-i nnf .i. Ground ran engine. Leak and ops checked O.K. I3d I/A/H an annual inspection and has been determinedaooroved for return to service, fill work wasjnance manuals and current federal aviation

4\ . l/rowi!rstown Aircraft Services, fnc Hagerstown, HD Z1742Approved Repair Station H5GR0500



AIRCRAFT CORPORATION · 2013. 8. 15. · cooler p/n CAM 649479. See 337. Exhaust slip joints...

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Transcript of AIRCRAFT CORPORATION · 2013. 8. 15. · cooler p/n CAM 649479. See 337. Exhaust slip joints...