d-g airways, inc. 3-18-2002

TOTALTIME INSERVICE

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

?//'£

- 3 6

BLf

CESSNA 340AMOD El

D-G Airways, Inc.

437

3-18-2002

REG. NO..N6240X

Huntington, WV 25704(304)453-1177

wo # 4327

TOTAL.

DRAIN SUMP, REMOVED AND INSPECTED OIL FILTER LEFT AND RIGHTENGINES. INSTALLED NEW CH48108 FILTERS LEFT AND RIGHT ENGINES ANDINSTALLED 12 QUARTS AEROSHELL 100W PLUS IN EACH ENGINE. DID RUN UPCHECKED FOR LEAKS. NO LEAKS FOUND.

'JAMESA-MOfZERA&P 292400351

DATE-

19

UK RfcPAlK rALILfTT. t>tt BALR

ECORDlNGTACHTIME

TODAYS

FLIGHT

TOTALw^mSERVICE

DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS

ENTRIES MUST BE ENDORSED Y/ITH-44AME, RATING AND CERTIFICATE NUM&ER OFMECHANIC OR REPAIR FACll^ffT \SK. BACK PAGES FOR OTHER. SPECIFIC ENTRIES.)

%$

ALTIMETER, STATIC AND TRANSPONDER CERTIFICATED-G AIRWAYS - I / /I ///•","Y 304-346-1105 400 EAGLE MOUNTAIN FID.

„„,, ^ fo^ YV /^ CHARLESTON, WV 25311, , , , , ( j | pD-G AIRWAYS

FAACRSDFZR102L

TTT 1.5

60

:.FT.

:FT.

O

_16

110.

-^c

_1L120

_30_

180

ModeL

SN

AIÎU/^L.±FT. haOl^/^ûn^ r—iCERTIFIED ALTIMETER PER FAR 43 APP. E. TOi%5/ > - - . .CERTIFIED AIRCRAFT STATIC SYSTEMS PER FAP( 91. 11 (A) (1).PERFORMED TRANSPONDER TEST REQUIRED BY FAR 91.413 (A) (C) AND 91.217 (B) IN

ACCORDANCE WVTH FAR 43 APP. E.-mr-KD ^ s^D - -ia. •K^îmint /I

BUND ENCODER

Make.

Model. •

TRANSPONDER MQDEF. / Â^ '^ ~ w« = ,_The Aircraft ancfor component identified hereon was repaired and Inspected Ii

ilntenance rules of the Federal Aviation Regulations, and is airwormy andapo?<

n' ^^^ O-&

artancewllh the current

i [or reti

| Make_

Model.

_Signec^Date

DATE

19

RECORDING

TACH

TIME

TODAYS

FLIGHT

TOTAL

TIME IN

SERVICE

DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS

..ENTRIES MUST BE ENDORSED WITH NAME, RATING AND

MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR

AND ALTERATIONS

CERTIFICATE NUMBER OFOTHER SPECIFIC ENTRIES.)

cA^> ALTIMETER, STATIC AND TRANSPONDER CERTIFICATE

) \* f* j 1/0,0 / lf^\ oiw*-j^b-i i DO 40o EAGLE MOUNTAIN RDÂA CRS DF2R1 02 L /^^ *^ /It- ^T ^ /I û ADI cry-ivm

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130

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a mMtt ,„ s-ô

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ind/or component identified hereon was repaired and inspected Ir axordance with the current /?s ol the Federally ation Regulations, and is airworthy andaA«^4d for retum» service? // //^.

• •> ir s

14 I

100

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110

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ALTIMETSR

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S/N " "

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S^J I^JÔ*^-

I

D-G Airways, Inc.400 Eagle Mountain Road

Charleston, WV 25311304-346-7188

DATE.

w.o. #_____MAiOOJ

TOTAL 594LO

AIRFRAMECOMPLETED AN ANNUAL INSPECTION l/A/W FAR 43 APPENDIX D.SERVICED MAIN FUEL SCREENS, REPACKED ALL WHEEL BEARINGS,LUBED AIRCRAFT AND LANDING GEAR. SERVICED BATTERY, REPLACEDGYRO FILTER P/N B3-5-1 CENTRAL FILTER NOT DUE. OPS CHECKED ELTMODEL NUMBER 110-4, TYPE ATREX, S/N 41187 PER FAR 91.207PARAGRAPH D. BATTERY DUE FEB 2004, C/W AD 2000-01-16 EXHAUSTSYSTEM, C/W ITEM B BY VISUAL INSPECTION, DUE AGAIN 30 DAYS OR50 HRS WHICHEVER LATER AT HOBBS: 3034.0. C/W ITEM C&E BY VISUALINSPECTION AND PRESSURE TESTED DUE AGAIN IN 12 CALENDARMONTHS DUE 9-03. C/W ITEM D VISUAL INSPECTION DUE AGAIN IN 500HRS AT HOB&J3484.0. P/C/W ITEM F BY CHANGING ALL EXHAUSTCLAMPS ON BOTH ENGINES AT 1-25-00 HOBBS: 2750.0 DUE 500 HRS

DATE

19

RECORDING

TACHTIME

TODAYSFLIGHT

TOTALTIME IKSERVICE


i

PAINTED RED LIMITS ON LOWER NOSE STRUT ASSY. iNSTALLED APUPLACARD ON APU DOOR AND INSTALLED NEW FUEL CAP SEALS P/NMS29513-232.. ADJUSTED NOSE LANDING GEAR STEERING CABLETENSION l/A/W CESSNA M/M AND RESAFETY, iNSTALLED NEW BOLTSP/N AN3-4 IN HINGES FOR RT AND LT NOSE BAGGAGE DOORS.INSTALLED NEW FWD AND AFT CABIN DOOR CABLES AND TIGHTENEDBOLT IN RUDDER HINGE AND LT ELEVATOR HINGE AND COTTERKEYED. INSTALLED NEW SHUNT ON BACK OF PROP AMMETER GAGE,OPS CHECKED NORMAL. 1 CERTIFY THIS AIRCRAFT HAS BEENINSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION ANDAPPROVED FOR RETURN TO SERVICE. -. / ^,f / »s?f^ /~ff ™fc~£fa(t

HOBBS: 2984,0 ACTT: 5947.0LT ENG SMOH: 1232.0 RT ENG SMOH: 1LT & RT PROP TT: 232.0STATIC ALTIMETER DUE 7-04ELT BATTERY DUE 2-04REWEIGH DUE 6-05

IATIONSNUMBER OF

FIC ENTRIES.)DE5CR.PT.ON OF .IN»ECTIOHS...TBtS.. JttPJURS

MODEL-34CT

P/N

DLTS

ENED

S/N340-437

REG. NO.N624UX"

D-G Airways, Inc.400 Eagle Mountain Road

Charleston, WV 25311304-346-7188

DATE

w.o.#

HOBBS

TOTAL

11-01^03

MATTB1

298573cr^o -,

AIRFRAMECOMPLETED AN ANNUAL INSPECTION I/AM/ FAR 43 APPENDIX DREMOVED AND SERVICED AIRCRAFT BATTERY, CHARGED ANDREINSTALLED. OPS CHECKED ELT MODEL NUMBER ELT 110-4, S/N41187 PER FAR 91.207 PARAGRAPH D, BATTERY DUE 2-04. C/W AD 2000-01-16 EXHAUST SYSTEM BY C/W PART B BY INSPECTION FOUNDNORMAL DUE AGAIN IN 50HRS. TIS OR 30 CALENDAR DAYSWHICHEVER OCCURS LATER ( HOBBS: 3035.3. C/W ITEM C&E BY VISUALINSPECTION AND PRESSURE TESTED DUE AGAIN IN 12 CALENDARMONTHS, DUE 10-04. P/C/W ITEM D, DUE AGAIN IN 500 HRS AT HOBBS:3484.0, P/C/W ITEM F BY CHANGING ALL EXHAUST CLAMPS ON BOTHENGINES AT 1-25-00 HOBBS: 2750.0, DUE 500 HRS, DUE AT HOBBS:3250.0 P/C/W ITEM G BY CHANGING EXHAUST SYSTEM ON RIGHTENGINE AT HOBBS: 1450 DATE 5-94 AND LEFT ENGINE AT HOBBS: 1750DATE 4-95 DUE AGAIN 2500 HRS OR 12 YRS WHICHEVER OCCURSFIRST. RIGHT 4250 OR 4-07. INSTALLED NEW STATIC yVICK P/N DG 1^630

TACHTIME

TODAYSFLIGHT

TOTALTIME INSERVICE

DESCRIPTION OF INSPECTIONS, TESTS, HEP AIRS AND ALTERATIONSENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OFMECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

I l._J ..

ON LEFT ELEVATOR AND INSTALLED NEW AUX FUEL COVER GASKETSP/N 0726002-1 ON RIGHT AND LEFT TOP AUX COVER.REMOVED HSI.REINSTALLED HIS P/N 066-3046-01, S/N 15112 AFTER REPAIR ATDUNCAN AVIATION SEE 8130-3, W/O MAXEA OPS CHEKCED NORMAL.INSTALLED NEW FIRE EXTINGUSTER MODEL 1600, S/N A590753WITHNEW MOUNTING BRACKET. I CERTIFY THIS AIRCRAFT HAS BEENINSPECTED IN ACCORDANDE WITH AN ANNUAL INSPECTION AND

APPROVED FOR RETURN TO SERVICE.

HOBBS: 2985.3 ACTT: 5948.3LT ENG SMOH: 1233.'3 RT ENG SMOH: 1533.3LT PROP TT: 233.3 RT PROP TT: 233.3STATIC/ALTIMETER DUE: 7-04ELT BATTERY DUE: 2-04A/C REWEIGH DUE: 6-05

MODEL,

S/N

CESSNA 340A .

340A-0437

REG. NO. N6240X

D-G Airways, Inc.1433 Airport Rd.

Huntington, WV 25704304-453-1177

ANNUAL INSPECTION

W.O. #

HOBBS 2985.7

4432

TOTAL5948.7

PERFORMED ANNUAL INSPECTION IN ACCORDANCE WITH FAR 43 APPENDIX D. INSPECTEDAND LUBRICATED ALL CONTROL SYSTEM AND ATTACHING PARTS. PERFORMED SERVICEITEMS. JACKED AIRCRAFT AND SERVICE LANDING GEAR. PERFORMED LANDING GEARRETRACT AND EMERGENCY EXTENSION. SERVICED WHEELS AND BRAKES. SERVICED ANDINSTALLED NEW GILL'BATTERY P/N 246, S/N G01970367..RlPLACED ELT BATTERY WITH P/N452-0130, DUE REPLACEMENT JAN '07. OP'S CHECK AIRTEX ELT MODEL 110-4, S/N 41187 PERFAR 91.207 PARAGRAPH D. OXYGEN BOTTLE HYDROSTATIC TESTED AND SERVICED WITHOXYGEN. C/W AD 2000-01-16 EXHAUST SYSTEM BY INSPECTION^UE AGAIN IN 50 HOURS OR 30CALENDAR DAYS. C/W PART C&E BY VISUAL INSPECTION AND PRESSURE TESTED DUE

,AQAIN IN 12 CALENDAR MONTHS, PART.D DUE AT HOBBS 3^& j£B3$l DUE AT 3250.0 HOBBSIT G DUE ON RIGHT ENGINE AT 3950 HOBBS OR«?OTl^TmiINE AT 4250 HOBBS Ofc4'C/W AD 2004-21-°5 HEATER DECAY TEST. DUE AGAIN AT HEATER HOBBS 307.6 OR 24

MONTHS. C/W AD 2004-25,16 BY VISUAL INSPECTION OF FUEL REGULATOR SHUT-OFFVALVEJDUE AGAIN 100 HOURS OR 12 MONTHS. AD 76-02-07 DUE 3084 HOBBS. AD 96-12-07 DUEHOBBS 3150. AD 97-26-17C DUE AT ENGINE OVERHAUL. RUN-UP AND LEAK CHECK OK. ICERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN AiNNU.INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

DONALD RICE

A&P400880718IA

DATE RECORDINGTACHTIME

TODAYSFLIGHT

TOTALTIME INSERVICE

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

ALTIMETER, STATIC AND TRANSPONDER CERTIFICATE304-34S-1105 "?Arf?>*3/,V*? . WO EAGLE MOUNTAIN RD.D-G AIRWAYS

FAACRSDFZR102L

TEST ALT.

X 1000 FT.TOL.

±FT.

ACTUAL

±FT.TEST ALT.

X 1000 FT.TOL.±FT.

ACTUAL

±FT.

-1

20

20

130

20

o22

140

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20

25

155

20

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30

180

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1.5

25

35

205

30

40

230

30

45

255

35

50

260

40

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LEAK!TOL-100 FT.

TEMP.

C

60

1080

12

90

HYSTERSIS

TOL+75 FT.

50%MAX.40%MAX.

CERTIFIED ALTIMETER PER FAR 43 APP. E. TQJ^/60P FT.CERTIFIED AIRCRAFT STATIC SYSTEMS PER FAR 91.411 (A) (1).PERFORMED TRANSPONDER TEST REQUIRED BY FAR 91.413 (A) (C) AND 91.217 (B) INACCORDANCE WITH FAR 43 APP. E.

Date

The Aircraft and/or component Identified hereon was repaired ana Inspected inrnalntensnce nJJes of the Federal AvlaHonJleijnlations, and te airwagtiy and apj

.Sig

14

100

16

110

18

120

ALTIMETR

BLIND ENCODER

Make

Model.

,., -. ..^jrc^uwMS, K5TS, REPAIRS AND ALTERATIONSENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OFMECHANIC OR REPAIR FAriliTY /<:RC B*<-" nl~~ -—

.... ._ ^.^^ ..,.n o/^/rtc, KAIING AND CERTIFICATE NUMBER OFMECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

ALTIMETER, STATIC AND TRANSPONDER CERTIFICATED-GAIRWAYS . x- •*.- i- ^ i tr* •***«•"<••

CERTIFIED ALTIMETER PER FAR 43 APP. E. TOJ^gflO FT.CERTIFIED AIRCRAFT STATIC SYSTEMS PER FAR 91.411 (A) (1).PERFORMED TRANSPONDER TEST REQUIRED BY FAR 91.413 (A) (C) AND 91.217 (B) INACCORDANCE WITH FAR 43 APP. E.

I

The Aircraft andfor component identified fierecn was repaired and Inspected imaintenance rules of the Federal Aviation Regulators, and Is alrw^ftfiyar)dapn<(

Date O ~

BLIND ENCODER

Make.

Model.

S/N

CESSNA 340AD-G Airways, Inc.

400 Eagle Mountain RoadCharleston, WV 25311

304-346-7188

ANNUAL INSPECTION

TOTAL

i MAINTENANCE "•>£•?$

js :, -; - .vsREQUIREMENT 85%, RbMuvnj^r^,^^, .... ,SYSTEMAND:.-:> ":,,'|

/VL i^_ . TS,LUBED AIRCRAFT PER MANUAL 100 HOURAND 12 MONTH • • ' - ' ' / ••-• ' ." ;': :'$REQUIREMENTS, CHANGED VACUUM RELIEF FILTERS CENTRAL FILTER NOT DUE, REMOVED • ,; •'ELT ARTEX M/N 110-4, S/N 41187 OP'S CHECKED PER FAR 91207 PARAGRAPHD DUE AGAIN 12' •'£MONTH 3-07 BATTERY DUE 1-07, JACKED AIRCRAFT GREASED GEAR CHECKED TENSION . . '&DOWN LOCKS PER MANUAL, RETRACTION CHECKED, EMERGENCY EXTENTION CHECKED, -1 **•INSPECTED AND GREASED WHEEL BEARING AND INSPECTED BRAKES, AD 76-02-07 ' ' • ; 'INSPECTION OF REAR BEARING ON BOTH ALTERNATOR CHECKED OK DUE AGAIN 100 HOURS, '•'*•"AD 2000-01-16 COMPLIED WITH CAW INSPECTION REQUIRED BY PARAGRAPH B DUE AGAIN 50,; 'HOURS OR 30 DAY WHICH IS LATER, HOBBS 3036, PRESSURE CHECKED ITEM C AND E12MONTH REQUIREMENT DUE AGAIN 3-07, ITEM D DUE HOBBS OF 3480 ITEM F DUE ALL CLAMPS 'CHANGED ON BOTH ENGINES 1-25-00 HOBBS OF 2750 DUE 500 HOURS ORHOBBS 3250 , ITEM GCHANGING EXHAUST WAS COMPLETED ON RIGHT ENGINE 1450 DATE 5-94 LEFT ENGINEEXHAUST CHANGED 1750 DATE 4-95 DUE AGAIN 2500 HOURS QSOOJaiAB ; AD 2004-21-05

e^^s/ . ' " • ' * •

m

1

M

' i!i'A

HEATER PRESSURE DECAY CHECK NOT DUE C/W 2-05 HEATER HOBBS WAS 207 DUE AGAIN 307OR 2-07, FUEL REGULATOR INSPECTED PER AD 2004-25-16 PRESSURE CHECK OK VALVE WASCHANGED 8-2001P/N C23D04-1 INSTALLED AT THAT TIME. AD-97-26-17 DOES NOT APPLY NBENGINE DOESN'T HAVE AIR MELT CRNKSHAFT NO FURTHER ACTION. AIRCRAFT RUN UP ANDOP'S CHECKED OK ENGINE FUEL FLOWS CHECKED PER TELEDYNE SB SID97-3. THIS AIRCRAFTHAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNNUAL INSPECTION AND IS APPROVEDFOR RETURN TO SERVICE.

HOBBS 2987 A/C TOTAL 5950

LEFT ENGINE 1235'RIGHT ENGINE 1534

&P 198S375IA

JOHN H. WOL^E,

LEFT AND RIGHT PROP AND GOVERNORS 235 INSTALLED 1-2000

ALTIMETER AND STATIC DUE 3-07

EKT BATTERY DUE 1-07

O2 BOTTLE HYDROSTATIC DUE 2-2010

TOTAL

sr^s^^Sis:B;T1wr- ^n r«T,FicA . (;TRitS.)^:

• • i i i ' • "•- •• — -"

19.

, ^^^SBSSSSffl"853^"-SRS^s&M*™"-.*"1"1"*-1 •ws=£ErgI.—c-ss^'-»»r.ss s«™IOT.•.*MSSf£S£^E

DATE

19 .

RECORDINGTACHTIME

TODAYSFLIGHT

TOTALTIME INSERVICE

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

OF WINCHESTER, INC.615AIRPORTROAD#1C9 - WINCHESTER, VA 22602

(540)678-1661

DATE: 12-13-07 HOBBS: 2988.1 TTAF: 5951.1 N6240X S/N: 340A04371 INSPECT AmCRAFT IAW AN APPROVED CHECK LIST PER CFR 43 APP. D.2. OPEN ALL ACCESS PANNELLS AND LUBRICATE ALL PULLIES, HINGE POINTS, BELLCRANKS, & RODENDS.3. LUBRICATE MAIN & NOSE LANDING GEAR. & PREFORM RETRACT TEST IN NORMAL & EMERG. MODE.4. TEST ALL LIGHTS.5. REPLACED ELT BATTERY P/N 452-0130 AND TESTED ELT IAW FAR 91.207d_BATTERY, DUE: Dec. 09.6. SERVICED ALL TIRES7. CLEANED DEBRIS FROM INSIDE OF8. SERVICE BRAKE FLUID RESERVOIR9. REMOVED AND REPLACED AffiC~ '10. C/W AD'S 00-01-16ll.C/WAD'S04-25-16Rl

ALL WORK ACCOMPLISHED^.I CERTIFY THAT THIS ATRCRAIWITH AN AJSmiAL INSPECTION AND

TIMOTHY J. FOLTZ AP229

DATE

19

RECORDINGTACH

' - -1TOTAL

TODAYS | TIME INDESCRIPTION OF INSPECTIONS, TESTS, REPAIRS

ENTRIES MUST BE ENDORSED WITH NAME, RATING ANDAND ALURATiaplfllJ

\L AVIATION !HST. & AVIONICS 10880 AVIATION LANG MANASSAS, VA 20110 OY1R391KI LOG I0#.i906 07-J<inu9ry-20Q3 WO* 2877S CA 11 HOBBS 2988.6! NG240X S/N WOA0437 CESSNA

l oeer.itional ch»ck of ULI roo 11 OT: inclijciing simulated full ILS. Unable 10comul.iint. recommend r! iqhr ce<t.

Part.1'

leak tsot ? .11 led pr»! tin nary 'Jhec'K at greater th-m 350 fpm. Troubleshooting system'd jub3tatitia1 di i-isieum t v of -'ockpit and instrument panel. Isolated le.ik^ to autopilot".i4, :-*-v.ch. copilot j?tTTip<:er ant! cooilot air^p^ed indicator. Removed CP Altimeter and ASI40^-01 ser ia l " : ^~4. Rtunavjii autouilnt mrspeea switch and replaced vn tii new umt.ill-it CP A'lrimerer and ''-SI after repair. Rtj.is'jemBlsd instrument'pans! and cockpit.

t- ALTTHETFR. TRANSPONDER. STATIC. AND ALTITUDE REPORTING SYSTEMS HftVE SEEN TESTED AS REQUIREDF.iP.'i 1J.411 ANr,' 9L.41; AND M£ET TriE REQUIREMENTS Of FAR PART 43 APPENDIv E AND F.

TTHETERfs'i: TESTED TO *O.UOO FTTIMliTEft' 1. o/H 45!0v-ui.:3 S/H ISbl

244015170

THii AIRtRApT, aiRFPAME. AjpCPjXFT tNtjINg. PROPELLER. OR APPLIANCE ICENTIFIED ABOVE WAS. R.EPAIREDAND iNSPECfEU IN ACCORDANCE '«IT*H -CURR&NT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED ?OP. RETURN TQ •JEftVIC^.. ^RTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIRSTATION j ipER THE^M

s/S .

tfaIf \JHfl

~4/»=S?/5yfn«J:/£>^^TsweT RT^itTjeA" ' * -' "WS. ••;;'

'j ' '*ffi- - --- - • • - • " ~~ "" "M, " ;T" Mj!

i- i •;£

' 5ai

' ' *«

- . - / • • : - • 'ft.; • • • • v4

^1mmwSBimIn!•191if'Urn0m

DATE

T9

RECORDINGTACH

. TIMETODAYSFLIGHT

TOTALTIME INSERVICE

DESCRIPTION />F INSPECTIONS, TESTS, REPAIRS AND ALTERATIONSENTRIES MUST BE Eh/DORSED WITH NAME, RATING AND CERTIFICATE NUMBER OFMECHANIC OR "REPAIR FACILITY. (SEE BACK PAGES fOR OTHER SPECIFIC ENTRIES,}

• Royal Aircraft Services, LLC IDBA JRA Executive Air

18335 Airpark Rd.Hagetstown, MD 21742

301-791-3642 - FAX: 301-791-7368CRSJZRR651K

Date 3-11-08 . , Hobbs 2989.5.N 6240X Cessna 340A S/N 340A0437Stripped and repainted this* aircraft, the flight controls have been balance checked as perCessna M/M p/n P653-2-12 before being installed. Replaced left flap outboard push rod p/n0862100-52 and checked flap operation. Replaced both flex hoses at recirculation pump onleft tip tank, replaced cracked fitting at pump. Leak checked good. Installed a PM 64abrasion boot on the nose. The aircraft has been repainted using Jet Glow Express MatterhomWhite CM 0840-1 03 G, U2000 Silver FLNA '9137 and U2000 FLNA 90446 Berry. Thelanding gear has been cycled and lighting checked.The aircraft identified above \yas inspected in accordance with the current regulations of theFAA and is approved fbY return to service. Pertinent details of the maintenance are on file

repair station under work ordej># 0801004.

Bernard Han Aircraft Services, LLC. / IRA Executive Air

DATE

19__

RECORDINGTACHTIME

CAPITLOG1

N624fl

Recoverecovsseat

color25. SS

ucdattp'rovlpane iSystenFas'c;C663Q.Engin

press,Clean-in L/Perfoin. •

THE A.

APPROSTATT

f*-

TODAYSFLIGHT

TOTAL ,TIME INSERVICE


"~~ f~ \ '

AL AVIATION INST. & AVIONICS 10660 AVJ*T]ON LANE, MANASSAS, VA 2Q110 OY1R391K '.D#51S4 or-May-2003 WO* 29044 C A T , HOBBS 2992.1X S/N MOAG437 CESSNA 340A ;

Pg 1 M •

red Headliner / Revred all cabin chairn leather and sheepjlstered cargo areascoated. Entry seepcriteria. Burn Ce

ophaser on/off synt; P/N DBOG90C-01. Ijioned for future au

Pho/nric jacks Irisn P/N ATD300 S/N 418

See FAA Form 337.L6-0101 S/N 3533', reiering Intercom Syst>erformed I.A.W. man/depress switch P/Njd, removed corrosioi engine pylon 'area,-med aircraft weightheight & Balance dat

[RCRAFT. A1R.FRAHE, A•JSPECTED IN ACCORDANJED FOR RETURN TO SS3N UNDER THE ABOVE *rt

-7/^^

sals, sidewalls, carcet. Disassembled, inspected, painted anda in leaLher. Uissassemdled, inspected, painted and recovered crewskin. All sear foam replaced. All seat belts rewebbed.in. .gross point,- replaced. airstair matting. All interior plastics

5 painted. All leathers, fabrics, 'foam and carpenzing meet Part-fification on file and copies available upon request. Repaired prop:h and indicator light wiring. Installed KLN90E one time databaseistalled passenger cabin intercom photie/mic jacks and wiring,Jio panel installation. Wiring cap & stowed behind pilot's instrumentCalled and placarded at seat positions. Installed Monroy Traffic5. work performed r.A.W. manufacturers instructions and apalicsble

paired on^bench, reinstalled same unit back in aircraft. insran»o PSm P/N PM1000 S/N LM-S997 interfaced to Pilot and Copilot positions.

376-3196. Removed and replaced L/H and R/H deice boots on honionta^.i and painted battery box with acid proof paint. Secured loose. -wiring

Removed and replaced upper airstair door extender P/N 5211369-?.ig procedures I.A.W. manufacturers instructions and AC 43.13-13 Chptra. entered into .aircraft records, '

:RCRAFT ENGINE, PROPELLER., OR APPLIANCE IDENTIFIED ABOVE WAS REPAIRED

WICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR3RK ORDER.

CRS OY1R391K Ma^K Granger


TOTALTODAYS | TIME INFLIGHT I SERVICE

DATE

19

RECORDINGTACHTIME

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' .

! CAPITAL AVIATION INST, « AVJONILOG !D# 5194 22-May-2008 WO;N6240X S/N 340A0437 CESS

f

Aircraft.will not pressurize,functional. Ops check good, cvalues. Reseated door on aftoperation. O2 bottle cart notcheck good. Found struts to tAD ff 2004-2S-16 fuel regulate

THE AIRCRAFT, AIRFRAME, AIRCflAND INSPECTED IN ACCORDANCE VAPPROVED FOR RETURN TO SERV1CSTATION UNDEfVTHE ABOVE 'rtORK

^/^ ? 6OY1R391K MIKE F. CAROTHERS

£'30152 CA11 HOBBS 2993.0 ,

•^7" ^gfnO Pgl/i:

packed Aircraft to determine if squat switch was mating and

pressure bulkhead. Test flight required to verify properbe turned off. Adjusted cable at bottle to provide clearance, op'se vuiUi i i i I tin i Li no aclion required. Lompl led with jamtroi neaterr shut off valve inspection. No defects noted at this time.

J\FT ENGINE, PROPELLER, OR APPLIANCE IDEfrrTFIED ABOVE WAS REPAIREDKTH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND IS

ORD>*..

7^

DATE

19

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TODAYSFLIGHT

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DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONSENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBEIMECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC EHT1

1PITAL AVIATION INST. 4 AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391K jOG ID* 5354 £J4-August-2G08 WO#302Q6 CA11 '

I N6240X S/N 34QA0437 CESSNA 340A |I Pg 1 /1'

.v**» ITEM a 30206-1 Repair Aircondition System ""**DISCREPANCY: Air Condition System -mopACTION: *•*** DESCRIPTION OF SERVICE WORK PERFORMED "-^CPen up Aircraft for access. Pressurized system and discovered hose on compressor at engine tobe leakina. Manufactured new'hose and installed, leak check good, operated system anddiscovered" blower (aft) motor inop. Replaced blower motor Ops check good. Closed up aircraftand operated system. Removed old compressor to install new compressor. New compressor styledifferent. Reinstalled old compressor.":' ° ITEM it 30306-2 Replace lamp In compass ****DISCREPANCY: Replace lamp in comoassACTION: Relamped compass, op's check good. . - .**-~ ITEM * 30206-3 Aircraft will not pressurize "***DISCREPANCY: Aircraft mil not pressurise.ACTION: Checked outflow valve and safety valve control head and switch and checked emergencyexit door. Found seal on emergency door'separating. Repaired seal and reinstalled door-. Plewaircraft and aircraft pressurised'but noted control cable seals leaking at rear bulkhead,Replaced cable seals. \a_~*** ITEM * 30206-4 Install 134 a converison kit s"*DISCREPANCY: Install PJl34a air conditioning system.ACTION: installed R134a air conditioning system IAW STC SA09472SC. Weight and balance has notbeen affected.«*-.** ITEH 3. 30206-S suto pilot control head locking pawl brn **ilrDISCREPANCY:'Auto pilot control head locking pawl brokenACTION: replaced locking pawl. ;, • •THE AIRCRAFT, AIRFR£ME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE 'WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED TOW RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT'.THIS REPAIRSTATION UUKffll THE 4BOVE WORK ORDER.

OY1R391K MIKE F. CAROTHERS

DATE

19

RECORDINGTACH TODAYSTIME FLIGHT

.

CAPITAL >AV!A

[ N6240X ; SftII

i DISCREPANCY:' ACTION: -***

Troubleshot

•J91Q004-12 a'- ch?ck ^.d cp

s*3~ ITEM /DISCREPANCY:ACTION: R &

KSCREPANCY:

Trouble shotchaffed air!D23S5S, Alsc

TOTALTIME INSERVICE

., , —

DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTERATIONS. ENTRIES WUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE NUMBER OF

MECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES.)

^_ „..,.. — _ — ,.., . . .

T!ON INST. & AVIQNiCS 10660 AVIATION L^ANE MANASSAS, VA 201101(Kluty-Z008 WO# 30431 ' - CA 11 ; '

J340AQ437 , CESSNA 340A

AUX tr'ansfDESCRIPTTG

system. Chefaulty (In

nd installs' 5- check- gc

30431-2 CS-Change,4fla

R'd engine

J0431-3. Si,Suction Ga

DESCRIPTION

suction1 gi-nne frcm aiinstalled

X' transfer p"urnp"blowihg 'breaker' **«er pump' blowing -breaker.1 •N OF. SERVICE -WORK, PERFORMED :**.*?

eked 'breaker, wiring and pump. Removed power atternally grounding out). Drained , fuel • from auxd,,new pump_ pN^^EOSpez^LoT.Jk.qSlOOS. ,Heplaced.fbd™7*"" *; ' ' ' ' ~ " ; • • " • - • • . • .n".. "" •-, i

ange flap HandTes-*7*"* - .ip, Candles '. , • . „ . . . . . . '; . . . . .cowl flap' handles, op's check good

ction ' Gauge" -Ihop sn*=1-' . -" • -lijage Tnop • • • \F SERVICE WORK PERFORMED"***' " ' ". ' '

age. .Found left hand. air , pump to have1 a.sheard.r pump. .Removed airpUmp model 442cw.s/n 71072.rubber antichaff strip on chaffed airline. Ops

OY1R391K i

Pg1/2l -

pump and breaker did nottank. Removed old pump PNu.e.'K.-An.to • aux' tanks Leak.-

*$'

splined shaft, also foundInstalled p/n R442CW s/ncheck and leak check

Customer supplied1 part:.' .* ' ' ' ' '

*•*** ITEM *• DISCREPANCY:

30431-4. Treat' boots ***-,- Treat boots : • • - ' • • • • •

1 ACTION: Cleaned- and. treated L/H & R/H wing boots inner and outer; L/H• -and. vertical , 'stab' boot.'. • , ' • ' • '

1 '-•***" ITEM #DISCREPANCY:

30431-5 ."Left landing gear light out ~-*-"=Left landind -gear lignt out

moed bulb1, op^s check good. • - • • • ' - . • *

& R/H horizontal boots,

.

K*$i'

DATE

19

RECORDINGTACHTIME

TODAYSFLIGHT

TOTALTIME INSERVICE

DESCRIPTION OF INSPECTIONS, TESTS, REPAIRS AND ALTER ATtONS^^ENTRIES MUST BE ENDORSED WITH NAME, RATING AND CERTIFICATE .NUM'BEI |aMECHANIC OR REPAIR FACILITY. (SEE BACK PAGES FOR OTHER SPECIFIC* ENTOEral

^sSwcj

CAPITAL AVIATION INST. & AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391K' *• f

LOG !D# 5364 QfrAugust-2008 WO* 30935 CA 11N6240X S/N 34QA0437 CESSNA 340A ' - ' J • -t

V _ - • • } ' Pg1/1

/' 'JH, '1•I"!

•m*-ft- ITEM £ 30935-1 Right engine will not startDISCREPANCY: Right engine will'.not startACTION: opened cowl to gain access to starter, checked for power at starter, power was present,determined starter to be faulty. Replaced old starter Prestolite p/N MH34003ECH With KellyAerospace starter P/N 64627S-1 S/N I07044E. Op's check good.

•4fc«i ITEM 30935-2 A/C not blowing cold =i=iOISCREPANCY: A/C not blowing coldAC!TON: Checked for leaks at service area under rear floor board, none noted, serviced systemwiTi- 2 Ibs R134a freon. System produced cold air. Awaiting expansion valve for forwardevap irator.

TH£ AIRCRAFT. AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS'-REPAIRED"AND IN- PECTE* IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVE.) PC* RETURN TO SER-VIG . PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR*STATION -INI ER THE ABOVE, WO£^ORDER.

'OY1R391K MIKE F. CAROTHERS

DATE

19

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.. . ._ /_


..„ . _„_. . .... — . -

CAPITAL AVIATION 1NST. & AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391KLOG I0# 5306 1Q-Jufy-20QS WOJf 30431 CA11N6240X S/N34QAQ437 CESSNA 340A

P g 2 / 2 j

**** ITEM # 30431-6 Auto pilot "control head loose ****DISCREPANCY: Auto pilot control head loose • • - , . ;

-ACTION: Tightned control head.. , . . ..... .."",

THE AIRCRAFT, AIRFRAHE, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED. ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED FCff? RETURN TO SERVICE. PERTINENT: DETAILS' OF/THE-REPAIR ARE ON FILE AT. THIS REPAIRSTATT.QW-UN1PER THE ABOVtL-VOWt' ORDER."

CAPITAL AVIATION INST. & AVIONICS" 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391KLOG ID# 5412 25-August-2008' WO# 31146 CA11 HOBBS 3017.0N6240X S/N 340A0437 CESSNA 340A

Pg1/1i

Removed left oil filter and cut-filter to check for metal. No metal noted in filter installednew-filter P/N .CH48108-1. Ran' LH engine no leaks noted no oil servicing was required.

Drained down A/C system. Replaced right.hand expansion value and-reserviced system with 1 2 Ibsor R134 refrigerant. A/C system ops check good and leak .checks good.

opened up left wing inboard leading edge to check for corrosion. Corrosion removed and metaltreated. ;' • . •

THE AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER,.OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE V.T7H CURRENT REGULATIONS OF THE. FEDERAL AVIATION AGENCY. AND ISAPPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON PILE AT THIS REPAIRSTATION UNDER THE ABOVE WORK ORDER.

DlMCANAVIATION

Make: CessnaHours: 59/34

1)

abovgjg_scrlb_ed repair pjjrtaintenance sf~

Signed .Far Duncaa AviT«outtn"c. Battle ceek

tr^ _feekMTCRSEB\R4SOD Phone: SOO-52S-2376

i —

DATE

19

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CAPITAL AVIATION INST. & AVIONICS 10660 AVIATION LANE-'MANASSAS, v,LOG fD# 5675 23-Oecem6er-2QG3 WO* 31143 CA 11 HOBBS3017.?N6240X S/N 340A0437 CESSNA 340A

OY1R391K

Pg1/3i

Removed Pilot s EA-S173 Air Speed Indicator P/N C66IG40-021G S/N 3536, RCSC1/10-A VerticalSpeed Indicator P/N C661009-01G1 S/N SS93, G-340A Gyro Computer P/N 43080-00003 S/N 3490, KingKI227 ADF indicator P/N 056-3063-00 S/N 1469S, King KI52SA HSI P/N 066-3046-01 S/N 15112, KingKG102A DG P/N 06S-0015-00 S/N U9364, King KA51A Slaving Accessory P/N 071-1053-04 5/N 14963.Relocated the ARC EA-SOlA Encoding'Altimeter p/N'43300-6123 S/N'1561 from the pilots instrumentpanel to the copilot's instrument panel, installed Garmin G600 Display system consisting of:GDU 620 Display P/N 011-01254-00 5/N 165000350, GRS 77.' AHRS Unit P/N 011-00363-10 S/N 42010117,GDC 74A P/N 011-00352-10 S/N 20605S24. GMU "44 Magnetometer P/N 011-00370-00 S/N 47511763, GTPS9 Temperature Probe P/N Oil-00973-00 S/N 47911202. Removed Instruments, inc. OATIndicator P/N C663S20-0100 S/N 7316. >. Installed Aspen Avionics EFD1000 PFD P/N A-OS-110-00 S/N001472, Config. Module P/N A-05-114-00 S/N00143-7', Remote Sensor P/N A-OS-111-00 S/N 001443, and

uerw/Marker

Reciever P/N 522-2037-011 s/N 5639 and PS Engineering intercom P/N PMIOOOII 5/N LM-S997.installed Gannin <>1A340 Audio panel w/ Marker Receiver and Intercom' P/N 011-00401-10 S/N962S5459. Removed Collins VHF-2S1.Ccmm Transceiver P/N 622-207S-001 S/N 23431, Collins VIR-3S1Nav Receiver P/N 622-2080-011 S/N 2S32V Collins.GL5T35Q.Glideslope P/N 622-2034-001 S/N 3550,and Collins pwC-lEO Power Converter P/N 622-2093-001 S/N JL62S9. Installed Garmin GNSS30WWAAS/GPS/Nav/com P/N 011-01064-00 S/N 23S20203 and Garmin GA3S GPS/WAAS Antenna P/N '013-00235-00 S/N 40756. Removed Colljns VHF-251'Com Transceiver P/N 622-2078-001 S/N 23673 andVIR-3S1 Nav Receiver ?/N 622-20SO-011 5/N 26731. Installed Garmin SL30 Com/Nav P/N430-004O-303 S/N 2550 906-. - Insta]led Garmin GDL59 >N DataTink System consisting of: GarminGDL69A Data Link Receiver P/N Oil-00937-00 S/N 47760993,' GA5S'XM Antenna P/M 011-01033-00 s/N37509379. GRTTO Wireless Remote Kcvr- P/N 011-01SS7-00 S/N 14Q000952, and GRC10 Wireless denoteControl P/N 01-1-01ES3-00 S/N 14R000914. , Rewired Collins TDR950 Transponder P/N 622-2092-0015/N S440 as secondary ATC sourcs. installed Garmin GTX330 TIS Transponder P/N OU-004S5-00 S/N34131177 as primary ATC source,. , Remo'/ed Pilot's Instrument Panel, Center Instrument panel andCopilot's instrument panel assemolies. 'planned instrument/equipment arrangements andfabricated new instrument panels l.A.w. Capital Aviation Drawings $ D-5300-340AG437-040,D-5300-340A0437-050, and D-S3GO-340A0437-060. Placards were replaced l.A.w. Capital AviationDrawings * D-S30O/340A0437-010, D-5300-340A437-020,' D-S3QO-340A437-030.' Honeywell KLN906 GPSP/N 066-04031-12£1 S/N 21139 with <A92 GPS Antenna P/N 071-01553-0200 S/N 02446, interfaced as

0'i1 ^^r. -O

IjKfcAS-:

DATE

19.

& AVIONICS . 10660 AVIATION LANE MANASSAS, VA 2Q110 OY1R3S1K*A11 HOBBS 3Q17.2C A T .

LOGICS 5675 £3-Oecsmber-2QOS

It :secondary IFR GPS navigation source''interfaced to copilot Aspen PFD1000 for nayigariion-yuauinformation only, Vjorfc performed I.A.W. manufacturers instructions, STC #SA02-iSEl_A;v;STC'îSAl0322SC. STC i SA01933LA, STC * SA014S7SE, DER Antenna installation• Engirieepihgi'b'rawingjSlN6240X-0909QS-2 and applicable FAR'S. See FAA Form 337's dated 12/22/2008:. 'Weight:.:&'B'a,]&nc,and Equipment List information revised. pitoE/static pressure system tested:I'.A.W; . A '-. a ,91.411. all parameters within limits FAR. Part *3 Appendix E. performgd''ATC;Tr.^spQnder^cKeid'I .A.W."FAR Part 91.413, all parameters within limits FAR part 43 Appendix1, pi'.'. Removed . JcjoggGauge P/N 4615S S/N 236019, repaired on bench, reinstalled same/repaired wlt bacic tj aiSRemoved post lights and installed UMA light bezels I.A.W. manufacturers. instructS'pns/ano^âpplicable FAR's as minor alteration. Lighting intensity to be contrQlled;by^xis;tring.'&;:i3!rheostat in airplane. Replaced left and right side glareshield'defrost-jvent [plenums ' emcând replaced QME L-Band antenna P/N CllOS-iS S/N 2074E, and coaxial., cable.•• Removed;exceSS° 'vnring' feedthrough porting compound and disconnected remaining nose hay wiring.-. ;;RemoVedM*existing nose wiring feed through panel, planned and refabricated feedi±roiignâhey.'Tr;;A'*w;.5B

Capital Aviation drawing $ D-5324-34QA0437-010. Installed pressure 'sealed bulkhead^cdnnectoRfor nose bay vnring. work performed as minor alteration I.A.W. applicable •FAR.IiSii,.ou'e ."to.. 3existing ELT Remote Switch capability, currently not being utilised, is mandatory,for",.ArtexSj'110-4 ELT installation, installed Artex Remote switch P/N 345-6196 and wired to ex^sting'^Sl

• SLT chec1* good I.A.W. Artex installation Manual and FAR part'91.207. installedAcustcmer^*^supplied Track Plus Svstem I.A.W. manufacturers instructions and applicable FAR-Vs .as..mihofcâlteration. Antenna installed on oressure vessel I.A.W. DER Engineering 'Drawing.V':,-.'/:•*'•':<••

• fcN6240X-102203-l. Removed and replaced Annunciator Press to'Test Switch: P/N'MPA406R04'.'T&-{J(I.Replaced volt/Ammeter rotary switch P/N D4G0205H. Removed G-S50A ,FD. indicator1 P/N ,44670r00081

S/N 3077D, C-S31A Control Panel P/N 41090-102S S/N 557, S-S50A Mode.Se^ctoc-lRaneVjf/KsiU*^!42710-0000 S/N 1119, and CA-SSQ AP Computer P/N 426SO-0003 S/N 630; shipped to AutopiToi:,'; ^Central for evaluation - reinstalled same units with exchange CA-S50 ap Computer, .P/M'H,2680^0<^Q

• S/N S 9 S S . Installed new Cessna Baggage Light Assembly P/N C622002-Q10=lv •• ••-•-•-'^^~'^^^-iîii»3t

\L AVUVTION INST. & AVIONICS 10660 AVIATION LANE wwâ^,lLOGJD#5675 23-Oecember-2008 WCW3114S CA11 HOBBS 3017.2.

1N6240X S^N3^0A0437 CESSNA 340A

THE AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER, .OR APPLIANCE IDENTIFIED ABOVE' WAS "'REP AIRED Vfei?;

AND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY..AND 'isV'-Y.'. ?•,,'APPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE "AT -THIS"'REPAIR V>'.- j,v^sSTATION UNDER, JWE ABOVE WORK. ORDER. " ' '" !':"''v", :'t'1 '""1-:'"T-r^q

CRS

OFIES.)

DATE

T9

RECORDINGTACHTIME

TODAYS.FLIGHT

TOTALTIME INSERVICE

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

iCAPITAL AVIATION INST. A AVIONICSLOGID#5679 29-December-2008N6240X S/N140A0437 CESSNA

10660 AVIATION LANE • MANASSAS, VA 20110 OY1R391KO# 32432rt REF#32432 CA11 HOBBS3017.2

34QA -

Pg 1 / " I !

Installed Software version 2.02 inrGDU620 p/N 01G-OQ4S2-00 S/N 16S0003SO according to GarminSoftware Service Bulletin No. : 0343. System tested and found to function as intended.

THE AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAMD-INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS'OF"THE" 'FEDERAL'AVIATION AGENCY AND ISAPPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIRSTATION UNDER THE ABOVE WORK ORDER.

CAPITAL AVIATION t«ST. & AVIONICS" -10660 AVIATION LANE: MANASSAS, VA 20110. OY1R391KL'OGlD#56a5 31-Oecemfaer-2008 WO#31195/2 CA11 HOBBS 3017.2N6240X S/N'340A<1437 , .CESSNA -340A - . . .

Removed and replaced Flap Preselect Control Cable P/N 5315001-17 and aft mounting bracket p/N5360000-43. Rigged Flap Control Cable and indication I.A.W.-Cessna 340 Maintenance Manual.i ' ' '

THE'AIRCRAFT,. AIRFRAME, 'AIRCRAFT .'ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED .IN ACCORDANCE-WITH^aJRRENT ^REGULATIONS 'OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED FOR.RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIRSTATION UNDER THE ABOVE W3RK, ORDER.

CRS OYTR391K Mark/Granger

OF WINCHESTDATE: 1-16-09 HOBBS: 3019.2 TTAJF: 5982t£oNft4e& $M*1. INSPECT AIRCRAFT IAW CHECKLIST PER 14 CFR 43 APP. ff'678"1661

2. OPEN ALL ACCESS PANELS AND LUBRICATE ALL PULLEYS, HINGE POINTS, BELLCRANKS,3. LUBRICATE MAIN & NOSE LANDING GEAR & PREFORM RETRACT TEST IN NORMAL & EMERG.4. TEST ALL LIGHTS.5. TESTED ELT IAW FAR 91.207d BATTERY DUE DEC 09.<>. REPOSITION AND SECURE PNUEMATIC HOSES IN LH WTNG ROOT TO PREVENT INTERFEARANCE

WITH LANDING GEAR,7. INSTALL GROMnT ON LH HEATED FUEL VENT3. CHECK RH AND LH FULL FLAP TRAVEL, BOTH *9. TIGHTEN AND RESAFETY LH NLG DQOjftpJpl10. STOP DRILL CRACKS: OB RH MLG-p%>B^^%WEK^K/riP

fvr-Wv'jSfe^ 2ftL^ff$' tttO'a.11. INSTALL AND TORQUE SELF Jp^^g'NJllS NOSEWHEEU AXE.12. REPAIR BROKEN RUDDER B,ol«)fN%S13. INSTALL 12 10-32 SCREWS

LF EO(»NS'NpEKmNOSEWHBEL AXEDnyss-'UiS'vs? t^~--^NJl.'L.V \ JC~>' \ • • \l\'

BOND^STlA iee:% iW AcW'iNTEpoMÂAi^Sv^'îlrft^J

VALVE P/k^2H48-% " / (. ff V^ 11r~*~*i

14. INSTALLED LH OH DEICE VALVE P/H^2H48-^ j (M \. COMPLIED WITH THE FOIXO\Wg^^S:OO^f67^25'J^ ' 6PC(^£&:

1-15-09 FORDETAJLS. A^T 'ÂLL WORK ACCOMPLISHED IAW CESSNA'Sl

I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED iNltCÔRDANCEWITH AN ANNUAL INSPECTION AND BETE^MtNEDvTOCHRIS M. COLLINS A&P/IA 448708617

.DATE • :

;1,9.

RECORDING•-TACH ..TIME

•TODAYS •.FLIGHT '.

-TOTAL" |TIME ,iw i•SERVICE :•

(DESCRIPTION lOF ; INSPECTIONS, tTISTS, .REPAIRS AND AtTtRAIlONSENTRIES ;M,UST /BE •-ENOO.RSED %WITH :N>ME, ;RATING ;AHD -CERTIFICATE /NUMBER OF(MECHANIC iPR sREeXlR /fACILIT/r;. jfSEE .BACK :f*AGES ,fpR -OTHER .SPECIFIC .ENTRIES.)

CAPITAL AVIATION 1NST. & AVIONICS 10663; VVIATION LANE^; MANASSAS, VA 20110 OY1R391KLOG JEW 5775 1 G-February-2009 WO# 32531 CA 11 HOSBS 3019.1N624QX S/N340A0437 CESSNA 340A \ ' -

Pg l /1

Deprogrammed GTX33O for 'Message' Audio. Moved Mopray Traffic Audio wiring to Com3 selecredinput, performed GDL69A XM.Radio Refresh ,via :xw website. Complied with Garmin G600 ChortviewUnlock and updated database card for charts via customer Jeppeserrweb account. Removed andrep laced_stall Vane circuit breaker, switch' P/N W31-X2K1G-S. Removed Pitot probe and cleanedout debr-ie, performed pitot/static'system-pressure'cneck'T.A.W:- FAR,.'part'91.411. Installed newtrim markers on throttle quadrant., Modified ,glareshie]d for Push.-to-test switch clearance.Installed/interfaced post light.for= Altitude Alerter- Replaced pilot/copilot overhead lightlamps P/N GE0.309. Installed laent-'signa'T direction'diode in TDR9SO ident 'wiring. 'Transpondertested l .A.W. FAR part Si.413. . • • . ' . . . . ' ^

THE AIRCRAFT, AIRFRAME,' AIRCRAFT'ENGINE,' PROPELLER. OR APPLIANCc IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED FOR'RETURN TO SERVICE. PERTINENT DETAILS Of' THE-' REPAIR 'ARE ON 'FILE AT THIS 'REPAIRSTATION UNDER THE' ABOVE ViORK ORDER..' " . -

CAPITAL AVIATION INST. & AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391KLOGlD#5979 05-May-2009 lWO# 33598' CA-11, HOBBS3049.5 , -N624QX S/N340A0437 CESSNA 340A

Installed Cessna alternator fi l ters 'P/N

THE AIRCRAFT, AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR. APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED FOR RETURN TO SERVICED-eftKTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIRSTATION UNcfe THExftH&VE WO

DATE

19

RECORDINGTACHTIME

TODAYSFLIGHT

TOTALTIME INSERVICE

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

CAPITAL AVIATION INST. A AVIONICS 10660 AVIATION LANb MANASSAS,VA 20110 OY1R391KLOG ID# 5859 11-March-2DQ9 WO# 32997 CA11 HOBBS 3030,2 .,N6240X S/N340A0437 CESSNA 340A V

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Removed copilot Aspen EFO1000 Display P/N A-OS-HO-OO S/N 1472 and Installed warranty exchanqeDisplay P/N A-OS-110-00 S/N 2535. Complied with configuration module update to softwareversion 1.1. verified configuration module settings. Complied with compass swinq.procedureinterfaced the existing *2 Navigation Receiver (SL30) to the existing Copilot EFD10GO DigitalNavigation Display. Programed the EFDIOOO for navigation display information. Work performedas minor alteration I.A.W. manufacturers instructions and applicable PAR'S. All around checksgood.

THE AIRCRAFT, AIRFFWWE, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIrTED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY AND ISAPPROVED FOR. RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THISSTATION UNDER THE ABOVE WORK ORDER.

DATE

19-

RECORDItTACHTIME

Hagerstown Aircraft Services, Inc.Certified Repair Station: CRS H5GRO5OO

1423S OaJc. Springs Road^ Hagerstown, MD 21742^(^01} 733-7604

DATE 05/28/09 HOBBS 3049.5 W/0_09p5178

Removed then reinstalled rudder and elevators after inspecting for jetblast damage and confirmed they are safe for the intended flight.Inspected hinges, belcranks, travel stops, and actuating mechanism onrudder, elevators, and ailerons. Replaced several sheared rivets onhorizontal stabilizer hinge brackets. Confirmed proper control surfacemovement, adjusted degrees of travel as necessary, confirmed propercontrol surface cable tensions. All work performed I/AAVmanufacturer's maintenance manual. I certify this aircraft is safe for aferry flight from Manassas, VA (KEF) to Hagerstown, MD (HGR) formaintenance.

Signed: JosephJL Hartt ^d/a^k^ ->* - .-_. ,Hagerstown Aircraft Services, IncHagerstown, IVID 21742FAA Approved Repair Station H5GRO5OO

ERATIONSre NUMBER OFCIF1C ENTRIES.)

y— — ^_1 iw ~ : ^ - .... . • ' • • / , , . ' . . . <'vlf,J&g|

DATE TOTA1 " ! r -:•••, '.:' -'i-BaM

19

TOTALTIME INSERVICE

PA* FOBM Ar^f^^MAJORl REPA| . AND MAJO* AtTERÎONtf TO> 'V .-} ''>.$ - ÎB^ FAA FORM ACA-337 BY DATE, OR TO THE WORK ORDER BT NU/AB^R: XMt5'. THE APPROVl^ Xd^cV ''v|| i

*r ' • ' -«*S88 @fl• -: ' . - • 881Hagerstown Aircraft Services, Inc. - . . . • _ " • '''''^V^^î

14235 Oak Springs Road, Hagejrstown , MD 21742 (301) 733-7604 • ' . "' ' '_ /';!i: ^S|

DATE 02/30/10 HOBBS 3050.1 A/FTT 6013.1 W/O# 0905178 - • • ,;, , ' •,*';:'' ?ffi §9

stabilizer. ' ' " • ; •-:• '~ — '"'•• '' ; ' 'f^ffl2 - pecfoLroed repairs to the rudder assembly by the following work: Fabricated: 1 each • :„ '*; ". '' Jv'''«i$j&BSlskin p/n 0831002-11, 1 each skin p/n B31002-13, 1 each skin p/n 0831002-13,.! each rib ' \ • • • • • ' .'-. !'?lVS^9i

edges co clean and inspect forward spars for defects. Ho defects noted. Installed ' ' • ' - • "s^SffiBJj

included in Che service kit p/n SK421-13QB. Re-assernbled elevators as necessary. • ; ' ' •' j •','."'*. -''sSjjj&Bi

, TTAF of Sm.l. Horizontal uss stripped of all paint, inspected, then filled and . . ' , •.:.-,; .>"Ai- S|

L . . • • • . ' • • ' • • • • '-^m' ' • ' '.•'. : ':''--i"-'i™ji

' •' . • ^.••-•'•••W->>g3Jl

DATE

19

TOTALTIME INSERVICE

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

Certified Repair Station: CRS H5GRO5OO14235 Oak Sprinas Road, Haaerstown, MD 21742 f301) 733-7604

Installing onto vertical stabilizer. 1 each new hinge p/n 0831106-4 was also installed

6 - Both ailerons were inspected and found both of the control push/pull rods withslight bend, 2 each new control push/pull rods p/n 502501B-1 were installed.7 - Elevator bell crank pivot Bait was tound bent. Bolt was removed and bell crankinspected. Ho defects found. Bell1 crank was re-installed with 1 each new bolt p/n ftH4-

8 - The horizontal a vertical stabilizers, elevators, rudder, and ailerons were allre-painted to match using U-Tech white.

additional weight to bring them to 'within normal limits. Control surfaces were re-checked after the addition of weight and found to be within normal limits. The rudderwas vhecked and found to be within normal limits and required no additional balancing.10 - The horizontal and vertical stabilizers, elevators, rudder, and ailerons were re-

11 - The elevator system, rudder system, and aileron system were all checked and 'adjusted for proper cable tensions and control surface travels, systems were adjustedto bring them to within manufacturers specifications.12 - Conducted a po-sC maintenance flight check and made minor adjustments as

This aircraft is approved for return to service in respect to work performed. All work

instructions and current federal aviation regulations. See above work order 10905178for further details.

Sianed: Tracev L. Pottat-^3^^-— 7 ~~^~~ S*^

FAR Approved Repair Station H5GR0500

5B5=S££~mTT .tr**-* - •'—-•* ~-" '

Prr^'^j;

TOTALTIME INSERVICE

REFERENCE OF MAJOR REPAIRS AND MAJOR. AERATIONS

FAA FORM ACA-337 EY DATH, OR TO THS V/ORK ORDER BY NUMBER'. AtoVTHE'-Xl

Hagerstown. Aircraft. Services,, ...Inc.i-jJCertified Repair Station: CRS H5GRQ5OO ' - , : ; ;•;' •;

Id235 Oak Springs Road, Hagerstown. MD 21742. (301) ,733-;76Q-4; •

DJVTE 3/2/10 HOBSS 30S0.1 Ji./FT!C 6013.1 W/0* •0905178-:.^H% 6240X__ _t^KE CESSN.&. MODEL 340ft._: . _ '_ '_ ;_5/H; 34QR0437.I have inspected this aircraft and found it td be safe^xor^aferry flight from Hagerstown MD. (KHC .) to Winchester V&;0(Rfor maintenance. (Annual Inspection Expired) See wort'order^,0905178 for pertinent details. ' ' • • - . " • :, •"' •V'"1-!':'

T o ' - _ _ _ 7 - z

OF WINCHESTER, INC.615AIRPORT ROAD #109 - WINCHESTER, VA 22602

(540)678-1661

5/20/2010 N6240X Cessna 340A S/N0437 Tach: 3050.6

Opened ail cowlings and access panels, and cleaned and inspected aircraft in accordance with approved checklist per14 CFR 43 app. D. Lubricated all pulleys, hinges, bell cranks, and rod ends. 'Tested all lights for proper operation.Set ail tire pressures. Cleaned and lubricated landing gear struts, Inspected battery and box and charged battery.Replaced left wingtip static wick. Re-set loose entry door hinge pin. Replaced missing external power doorfastener. Replaced leaking fuel line from left nacelân^-Qeaaed^^s^t^^Êto^salve.seals. Replaced

pressure scat hose in forward bag;9910011-1. Repacked allsides after overhaul by Apeemergency modes. ELÊS

t,

replacement due May SG13.'manuals.AD's 00-01due @3250 hours.100 heater hours or 24 mon

* v^ ^ * \ >ty i

:%TT-%Î certify that this aircraft has been inspectesfm^ccoraance TVIairworthy condition.

Peter Eshleman A&P559112401IA

pressure seal boots P/Nexhaust systems both

j rH V J

Veaf-DêcationlSi both normal and, -J-O. X\^

f— \"i'J I"S I \_i. i j ail ™_^.erv^ce an(^ maintenance

h

ja in 50 hours. Part Ftest, due again @

year or 100 hours.

d was found in

DATE

19

A. D.NUMBER

TOTALTIME INSERVICE

AIRWORTHINESS DIRECTIVES i -, 1'ACHRONOLOGICAL LISTING OF COMPLIANCE AKD METHOD OF COMPLIANCE ' I

OF WINCHESTER, INC.— 615A1RPORTROAD#109 • WINCHESTER, VA 22602

(540)678-1661

_ 6/2/20J1 N6240X Cessna 340A S/N 0437 Tach: 3096.2

— Opened all cowlings and access panels, and cleaned and inspected aircraft in accordance with approved'chevSS!_ 14 CFR 43 app. D. Lubricated all pulleys, hinges, bell cranks, and rod ends. Inspected brakes. Tested ,alUij

proper operation. Set all tire pressures. Cleaned and lubricated landing gear .struts Inspected" Cleaned pressure outflow valve seals. Tested landing— tested in accordance with FAR 91.207d,_ with applicable Cessna service^afST^^Bi'

inspection, due again in SOJlQufi

and emergencyaccomplished in acc' ^

* H "* f^VOKftum

System, C/W3perSBAl'65

DATEAfRWORTHINISS DIRECTIVES

.CHRONOtgGlCAlMJSTING OF _COMPLjANCE^AH.D,METHOD. OI; .COMPLIANCE.

TO'STATION'UMOER-THE

' ' '

DATE

19-

TOTALTIME INSERVICE

MANUFACTURERS MANDATORY SERVICE i.tuUrTINSCHRONOLOGICAL LISTING OF COMPLIANCE AND METHOD';,;.OJvCO

«*~^ DESCRIPTION OF SERVICE WORK PERFORMED **** . ' '.. '\';^-.\:.

Confirmed intermittent autopilot problem, the engage switch would not stay in ttie.-on'.:If the switch were physically held in the on position, the system would otherwise ,'wor, ^Removed the C-S31A AP Controller, pn 41090-112S sn 174-9, and accessed tJie Trim;'1-DTsccwinec®Test switches and rang out wires. Found that the Disconnect switch was dirty., CTeMed^aiglf

exercised switch. Reinstalled tJie controller and tested system, Function Test OK.'Reconoenttest flight prior to IFR use. ... . . . . ™»

THE AIRCRAFT, AIRFRAHE, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED 'ABOVE :WA5- REPWlAND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION'. AGENCY^AND^STAPPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THISi>REPWRSTATION UNDER THE ABOVE WORf; &RDER.

DATE

CAPITAL AVIATION INST. 4 AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391KLOG1D#7892 3S-Od:ober-2011 'WO# 41846 CA11 HOBBS1S6.6N6240X S/N340A0437 CESSNA 340A

installed new 02 capillary line, PN C166011r0108 from bott]e to bulkhead, leak checked good,serviced 02 to 1300 psi IAW Cessna service manual. Removed aircraft clock, replaced battery,reset and reinstalled. Repaired-aft tail ;cbne~ by hortz stab, removed broken & loose plastic,fabricated & installed repair doublers from T3-2029 .025 aluminum, treated and primed area, topcoated with appropriate resin filler and surface protection..During troubleshooting of

prassurizafion leaxs found scat duct under'heater leaking, replaced'with new scat duct,adjusted duct going to ram air valve fwd of heater, cleaned both pressure drain valves in floorof pilot & copilot areas, resealed RH'wing root pass.through, for;throw;!e,cables, adjusted DV

window and 3 upper S 1 lower .cabin 'door "lock,pins' in door frame,; cleaned!* lubricated rearbulkhead cable seals. During troubleshooting of.'freon. AC'system fourid, RH .evaporator .leaking,removed RH evaporator PN HES1300-3 SN ,17715SS'fdr repair per .'customers request, freon systemdeactivated at this time, no further action 'taken. , ' . • ' . , . . - . ' ' . . , - . - • ' , ' " ' . ' . ' , , .

THE AIRCRAFT, AIRFRAME, AIRCRAFT ENGENE;'' PROPELLER, OR APPLIANCE IDENTIFIED 'ABOVEjWAS REPAIREDAND INSPECTED IN ACCORDANCE WITH .CURRENT 'REGULATIONS. OR THE FEDERAL AVIATION AGENCY'AND ISAPPROVED FOR. RETURN TO SERVICE/ PERTTNENT DETAILS""OP THE-REPAIR ARE: pfj,FILE-AT THIS' REPAIRSTATION UNDER THE _AS«VE WORK ORDER.

SOWERS

• • • • • • • • ;•:/ . • ' • ' • ' - - ' • ' • . n

: . . ' • . • . - . • • ' . . . . , • . • • ; 'a" ' . . ' . . . • • ' • . . . D

• - -' . ' n1 - a

•a.nD

. nnaana

Addition of Required— Exch an g fed for OptionalRemoval of Required— Exchanged for Optional

Addition of Optional EquipmentRemoval of Optional EquipmentAddition of Required— Exchanged for OptionalRemoval of Required— Exchanged for Optional

Addition of Optional EquipmentRemoval of Optional EquipmentAddition of Required— Exchanged for OptionalRemoval of Ra quired— Exchanged for Optional

Addition of Optional EquipmentRemoval of Optional EquipmentAddition of Required— Exchanged for OplionafRemoval of Required— Exchanged for Optional

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DATE

1?

CAPITAL AVIATION INST. * AVIONICS 10660 AVIATION LANE MANASSAS, VA 20110 OY1R391KLOG IW7789 29-August-2011 WO#4184G CA11 AC TT3120.SN6240X S/N340A0437 CESSNA 340A

THE ALTIMETER, TRANSPONDER, STATIC, AND ALTITUDE REPORTING SYSTB1S HAVE SEEN TESTED ASBY PAR'S 91.411 AND 91.413 AND MEET THE REQUIRHilENTS OF FAR PART 43 APPENDIX E AND F-.

ALTIMETERCS): TESTED TO 30,000 FTADC P-l: P/N 011-00332-10 S/N 20605524ALT *1: P/N 15035-01102 S/N 174233ASPEN PFD: P/N A-O5-110-00 S/N 2535COPILOTS ST5Y ALT: P/N 43300-6123 S/N 1561TRANSPONDER #1: P/N 011-OO45S-00 . S/N 84131177TRANSPONDER *2: p/N 622-2092-001 S/N 5440DATA CORRESPONDENCE WAS TESTED TO 30,000 FT

THE AIRCRAFT. AIRFRAME, AIRCRAFT ENGINE, PROPELLER, OR APPLIANCE IDENTIFIED ABOVE WAS 'REPAIRED]AND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION AGENCY' AND' l£-APPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THIS REPAIR*"-;-STATION UNDER THE ABOVE WORK ORDER. . . - X \ .-"-*

CRS OY1R391K bfiStlE TOUART

1

"CAPITAL AVIATION INST. «, AVIONICS lowo AVIATION LANE MANASSAS, VA 20110 OWOHK-LOGEW8549 17-Juty-2012 WO#43081 CA11N6240X S/N340A0437 CESSNA 340A •

ART—161A WX Radar R/ i, pn -r~.-,-~,i ri/c-t-Mn •Fimr-i—ion "CesT OK. • ' • , • - •'--ijSjfej

THE ATRCKAM. ftj-n-rujvnc, AIRCRAFTAND

STATION UNDER THE_ABOVE

/6

tfoOF WINCHESTER, INC.

DATE: 7-9-12 HOBBS: 3169.7 TTAJF:1. INSPECT AIRCRAFT LAW CHECKLIST PER 14 CFR 43 APP, ,D.

2. OPEN ALL ACCESS PANELS AND LUBRICATE ALL PULLEYS, HINGE POINTS, BELLCRANKS, & RODENDS.3. LUBRICATE MAIN & NOSE LANDING GEAR & PREFORM RETRACT TEST IN NORMAL & EMERG. MODE.4. TEST ALL LIGHTS, SERVICE BATTERY WITH DISTILLED H20, & CHARGE.5. TESTED ELTIAW FAR 91.207d. INSTALL NEW BATTERY. DUE: NOVI4.6. RESEAL LH LANDING GEAR STRUT AND SERVICE WITH 56061N2.7. GREASE LH & NLG WHEEL BEARINGS, SERVICE ALL TIRES WO PROPER PRESSURE.

•' . ' f - *iiS^5» -5, .8. CHECK RH AND LH FULL FLAP TRAVEL, BOTH 45 DEJ^^T™^--^ ^' 9. REMOVE BIRDS NEST FROM HORIZONJAL^^^ÔTJC ____

10. TIGHTEN FWD JAMB NUT ON

11. RECONNECT CAPICITOR / VIBR^^MC^re^rfrajTROnL.12. REMOVE SHIMMY DAMPERÎ^^gj^^^Ê^^Sif E^RINGJJI13. STOP DRILL CRACKS: LH IsffepQBRjbH W^^J^Sl14. SEAL SMALL TEAR IN CABBIN D®R;S§A^^f ^TiT15. FOR AD COMPLIANCE SF "™J^'"~ ~16. TIGHTEN LH BAGGAGE DUOK4M

17. INSTALL CLAMP ON ELEVATOR CA ._ . ^w^pc^. jj/ff ^\^&- ,- ^ ^18. REMOVE STRIPED SCREWS FROM LH¥lP.TONK?A^19. SERVICE A/C WITH 1#R134-A. ^\' *~^'~~^-f—~~^_ }I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSP)ECTED_jnÂCCJÂNCE " ^WITH AN ANNUAL INSPECTION AND DETERMINED TO BE IN"A1RWORTHY CONDITION.CHRIS M. COLLINS A&P/IA 44870861 .^^^^^^ 1

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d-g airways, inc. 3-18-2002

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