~ dj~ aircraft serial#: 3025

SPEAR AIR, Wilkesboro, NC

Airframe Log Entry Date: January 15th, 2013 Aircraft Reg#: N997GC Model: Challenger 601 Serial#: 3025

- Performed engine and airframe preservation runs once a month from May 6, 2012 to January 15, 2013 as per the GE CF34-1A and Bombardier Maintenance Manuals.

Signed: ~ dj""~ Roger Spears, A&P 3631699

Date: Work Order:

RELIABLE JET MAINTENANCE, LLC. AIRFRAME LoG ENTRY

December 5, 2012 12-10768

Aircraft Reg#: N997GC Aircraft Serial#: 3025

561-417-3834

Total Time: NOT AVAILABLE Total Cycles: NOT AV AlLABLE

Performed tbe foUowiog Maintenance: 1. Complied with top charge of main battery p/n 40178-26 s/n 1160871AW Saft CMM24-32~5

and CL-601 MM24-33~. This aircraft bas been inspected/repaired in accordance with current Federal Aviation Regulations and tbe manufacture ' maintenance manual and is approved for return to service.

\;

··~ RELIABLEJETMAINTENANCt:,LLC. 561-417-3834 - ----- _... AIRFRAME LoG ENTRY

Date: September 13,2013 Aircraft Reg#: N997GC Work Order: 13-11494 Aircraft Serial#: 3025 Total Time: Total Cydes:

Performed the foUowing Maintenance: I. Performed engine runs 08/01/13,08/14/13, and 08130/13, lAW CL-601 MM 71-00-00. 2. Performed APU runs on 08/01/13,08/14/13, and 08/30113, lAW CL-601 MM 49-10-00. 3. Powered up avionics systems 08/01/13,08/14/13, and 08130/13. 4. Removed failed Signal Data Computer pin 476-675-120 s/n 285. 1nstalled serviceable Signal Data

Computer pin 476-675-120 s/n 293. Performed • Automatic Power Reserve Operational Test' lAW CL-601 MM 71-00-00 with no discrepancies noted. Performed Ops check of the engine instrument panel ref: CL~I MM 77-11-QO with no discrepancies noted.

5. Serviced the main and nose tires JAW CL-601 MM 12-10-32. 6. Serviced the engine oiler with four quarts of2380 oil lAW CL-601 MM 12-10-79. 7. ServicedtheADG ejection jack pump IAWCL-601 MM 12-12-24. 8. Serviced the#2 engine JOG JAW CL-601 MM 12-11-24. 9. Serviced the 021AW CL-601 MM 12-10-35. I 0. Serviced the# I & #3 hydraulic systems lAW CL-60 I MM 12-10-29. II. Serviced the #I hydraulic accumulator lAW CL-601 MM 12-10-29.

This aircraft bas been Inspected/repaired in rdan wltb current Federal Aviation Regulations and tbe manufacturer's maintenance m pi~ proved for return to service.

Thomas Cragg --''--"--"--'-$-'--. ........, L ____ _ For

Reliable Jet Maintenance, LLC. CRS# LCPR02SG Created By: TC

:~ R ELIABLE JET MAINTENANCE, LLC. 561-417-3834 ..... / AIRFRAME LOG ENTRY

Date: July 29, 2013 Aircraft Reg#: N997GC Work Order: 12-10853 Aircraft Serial#: 3025

Total Time: Total Cycles:

Performed the following Maintenance: 1. Powered up avionics bi-weekly from 2/26/ 13 to 5/29/ 13. 2. Powered up avionics on 6/ 12/ 13, 6/26113 & 7/ 11 / 13. 3. Performed engine runs bi-weekly from 2/26/ 13 to 5/29/13 lAW CL-601 MM 71-00-00. 4. Performed engine runs on 6/12/13, 6/26/ 13 & 7/ ll / 13 lAW CL-601 MM 71-00-00. 5 Performed APU runs bi-weekly from 2/26/13 to 5/29/ 13 lAW CL-60 I MM 49-l 0-00. 6: Performed APU run on 6/ 12/ 13, 6/26113 & 7/ll / 131AW CL-601 MM 71-00-00. 7. Performed top charge on main battery p/n 40178-26 s/n 11 6087 lAW CMM 24-32-05 .

This aircraft has been inspected/repaired in accordance with current Federal A~iation Regulations and the manufacturer's maintenan anual and · approved for return to serv•ce.

HH1GC Cl-ii1l1

Accomplished the following tasks

1 Ran aircraft engines for incoming inspection.

DATE September 20, 2013 TOTAL TIME 9583.35

ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT I ENGINE WAS PERFORMED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION.

SIGNED

George Glen A&P 2730175

LOGBOOK ENTRY: N997GC CANADAIR C600-2A12 SIN 3025 A/C TT: 9583.85 C!W FAR.91.411 & 91.413 RVSM AIR DATA SYSTEM AND TRANSPONDER ACCURACY CHECK VERIFYING SYSTEM MEETS 1/A/W CANADAIR CHALLENGER MM PSP601-2 34-13-00 PGS 202-206 REV DATEMA Y 05,2010 RVSM TOLERANCES AND MEETS REQUIREMENTS FOR CONTINUED OPERATIONS IN RVSM AIRSPACE. I CERTIFY THAT THE ALTIMETER AND TRANSPONDER TESTS REQUIRED BY FAR 91.411 AND 91.413 HAVE BEEN PERFORMED AND IS APPROVED FOR RETURN TO SERVICE. PERTINENT DETAILS OF THIS TEST IS ON FILE AT THIS REPAIR STATION UNDER: W.O.# 121313 DATE: JAN.15, 2014

SIGNATURE tfYJ1_~ _(3 · ~ INS~ TROPIC RADIO INC. 2695 N.W. 56th ST. HANGER 53-A FT.LAUDERDALE FL. 33309 FAA APPROVED REPAIR STATION# RZ4R510M FT.LAUDERDALE EXECUTIVE AIRPORT* ARCHER RAMP* TELEPHONE # 954-776-4030 #1 PILOTS ADC PIN 7000700-637 SIN 07037571 TESTED TO 50000 Ff #2 CO-PILOTS ADC PIN 7000700-637 SIN 84125844 TESTED TO 50000 Ff #1 PILOT ALTIMETER PIN 4016341-904 SIN 80101692 TESTED TO 50000 Ff #2 COPILOT ALTIMETER PIN 4016341-904 SIN 89125844 TESTED TO 50000 Ff STANDBY ALTIMETER PIN 8047/10 SIN 9143B TESTED TO 50000 Ff # 1 TRANSPONDER PIN 066-01143-2101 SIN M123003 # 2 TRANSPONDER PIN 066-01143-2101 SIN 4064

,

(

CHECK CURRENT DUE LIST FOR DUE nME CHANGES

J~tor SKY HIGH AIR L.L.C. Work card No.: 34.420

Serial No.: 3025 Model: CL-601

~egNo.: N997GC Workorder No.:

Date A/C HRS AFL APH

Due At 20-JUN-2010

Accomplished II o ,_\ ~ - "t I I I I I I

TECHNIOAN SIGNATURE:11t. ~ • ~ "' :ULfL~ ,.N\ wo H , 21 Jt .2 KIND OF CERTIFICATE & NO.;.:· r-_"'--=.~__:>::.__10_ .. _;_ ·•---------

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.:..· ----------------

1345106 RIGKT TRANSPONDER

REASON REMOVED: I B TIME EXPIRED :JFAILURE B~ORN a~OANER B SCHEDUUNG CONV

(CHECK ONE) - MOD/UPGRADE ~SERVICE ENGINE CHANGE TIRE CHANGE SWAP/TRBlf SHOOT D DAMAGED _O uNKNOWN

If removed PIN & SIN information is incorrect please provide details below.

REMOVED P/N 066-01143-0301 II I S/N 4064 II I LABOR-HRS

INSTALLED P/N I I S/N I l PART COST$

INSTALLED TSN MOS INSTALLED TSO MOS TIME SINCE MOS WARRANlY TIME MOS

HRS HRS REPAIR HRS REMAINING

HRS

LOGS LOGS LOGS LOGS

ITECH: I IINSP:I

REM~ :==========================================================================~

INITIAL ll-IE SERVICE TASKS BELOW WHICH WERE ACCOMPLISHED DURING CHANGE. IF TASKS WERE NOT ACCOMPUSHED, RECORD TIME ACCRUED SINCE TASK WAS LAST ACCOMPUSHED OR CHECK CONTINUE TIME (CT).

#>345116 MANDATORY

FUNcnONAL TEST RIGHT TRANSPONDER -FAR91.413

RECORD DATE OF CAliBRATION Q.l__j~ / tf

LABOR-HRS TIME CONTINUE HRS.THS ACCRUED TIME

AMM 3+5+00 RE~ : ~==--~~~~===========-~~~==~~~==============~~----=-~~====~==-NOTE: 1. FOLLOWING INSTALLATION OR MAINTENANCE ON AN ATC TRANSPONDER WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, ll-IE INTEGRATED SYSTEM MUST BE TESTED, INSPECTED AND FOUND TO COMPLY Will-I PARAGRAPH (C), APPENDIX E OF PART 43.

2. FREQUENCY MAY DIFFER AS LAID DOWN BY ll-IE APPROPRIATE REGULATORY AUll-IORITY.

BOMBARDIER® AND CHAU.ENGER® ARE TRADEMARKS OF BOMBARDIER, INC.

23-DEC-2013

Return completed copy via email to [email protected] > INDICATES DUE ITEMS

© CAMP SYSTEMS 1 of 2 Total Pages = __ _, Initial __

CHECK CURRENT DUE UST FOR DUE nME CHANGES

t~' SKY HIGH AIR L.L.C. Work card No.: 349066

Serial No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.:


Due At 26-JUL-2010

Accomplished I 0\-I.S-t '1 1 I I I I I

TECHNICIAN SIGNA1URE:111_ uJ-L ~ " ~4 KIND OF CERTIFICATE & N0.·)2_ =t!ft2..S {O .N} tV o.:lt I 1.1 St3

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.-· ---------------

>349066 CAUBRATE STANDBY ALnMETER

INSP L.ABOR-HRS

HRS.lliS

~~= --------------------------------------------------------------------------------------------------------------------------------

BOMBARDIER® AND CHAllENGER® ARE TRADEMARKS OF BOMBARDIER, INC.

23-DEC-2013


© CAMP SYSTEMS 1 of 2 Total Pages= __ _, Initial __

CHECK CURRENT DUE UST FOR DUE TIME CHANGES

~Operator SKY HIGH AIR L.L.C. Work card No.: 34.020

Serial No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.:


Due At 20-JUN-2010

Accomplished II Ol - \5'""1'f l I I I I I

TECHNIOAN SIGNAlU~~ ();_' ~ KIND OF CERTIFICATE & NO.:...!:' f<_-=-..:.~-!:...:.IL..=;5oJ....L!:I0:::..!.01_n__W_O_':iJ___:J.:::..~..:..I_3_t.:J __

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.:...· ----------------

1341021 PILOT ALTIMETER GENERIC NO REF

REASON REMOVED: I B~ME EXPIRED (CHECK ONE) MOD/UPGRADE

8 FAIWRE

SERVICE B~ORN

ENGINE CHANGE

a lOANER

TIRE CHANGE

~t:j~EDUUNGCONV SWAP{TRBLE SHOOT D DAMAGED O uNKNOWN


REMOVED P/N 4016341-904 II S/N 80101692 II I L.ABOR-HRS

INSTALLED P/N I I S/N I I PART COST$

INSTALLED TSN MOS INSTALLED TSO MOS TIME SINCE MOS WARRANlY TIME MOS


HRS

LOGS LOGS LOGS LOGS

TTEcH:T TINSP:I

REM~ : ==========================================================================~

INITIAL THE SERVICE TASKS BELOW WHICH WERE ACCOMPLISHED DURING CHANGE. IF TASKS WERE NOT ACCOMPliSHED, RECORD TIME ACCRUED SINCE TASK WAS LAST ACCOMPLISHED OR CHECK CONTINUE TIME (CT).

INSP LABOR-HRS TIME CONTINUE HRS.THS ACCRUED TIME

#>341031 MANDATORY

AMM 34-11-00

CAUBRATE PILOT ALTIMETER -RECORD DATE OF CAUBRATION -FAR91.411

RECORD DATE OF CAliBRATION

RE~:~~~~~~==~~~~~~~~~~~~==~~~~~~~~~==~==~~~~~~~~ NOTE: 1. FOLLOWING INSTALLATION OR MAINTENANCE ON THE AUTOMATIC PRESSURE ALTITUDE REPORTING SYSTEM OF THE ATC TRANSPONDER WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, THE INTEGRATED SYSTEM MUST BE TESTED, INSPECTED AND FOUND TO COMPLY WITH PARAGRAPH (C), APPENDIX E OF PART 43.

2. EXCEPT FOR THE USE OF SYSTEM DRAIN AND ALTERNATE STATIC PRESSURE VALVES, FOLLOWING ANY OPENING AND CLOSING OF THE STATIC PRESSURE SYSTEM, THAT SYSTEM MUST BE TESTED AND INSPECTED AND FOUND TO COMPLY WITH PARAGRAPH (A), APPENDICES E AND F, OF PART 43.

3. FREQUENCY MAY DIFFER AS LAID DOWN BY THE APPROPRIATE REGULATORY AUTHORITY.

BOMBARDIER® AND CHAI..l.ENGER® ARE TRADEMARKS OF BOMBARDIER, INC.

23-DEC-2013 © CAMP SYSTEMS 1 of 2 Return completed copy via email to [email protected] > INDICATES DUE ITEMS

Total Pages = __ _,Initial __ _


Operator: SKY HIGH AIR L.L.C. Work card No.: 34.021


~egNo.: N997GC Workorder No.:


Due At 20-JUN-2010

Accomplished lo '-•5"-1'{ I I I I I I

TECHNICIAN SIGNATUREpYit~ a-. ~ KIND OF CERTIACATE &. NO .. f.-~ lO.It-1 I.A.)t/"~f I ). I 3 J 3

INSPECTED BY:------------------KIND OF CERTIACATE &. NO.-· ----------------

341026 COPILOT ENCODING ALTIMETER GENERIC NO REF

REASON REMOVED: I B~ME EXPIRED 2~MLURE :-]woRN a~OANER ']SCHEDUUNG CONV

(DiECK ONE) _ MOD/UPGRADE SERVICE 0 ENGINE OiANGE TIREOiANGE CJswAP/TRBl.E SHOOT O DAMAGED O uNKNOWN


REMOVED P/N 4016341-904 II I S/N 89125844 II I LABOR-HRS


INSTALLED TSN MOS INSTALLED TSO MOS TIME SINCE MOS WARRANTY TIME MOS


HRS

LOGS LOGS LOGS LOGS

ITECH: I IINSP:I

REM~: ==========================================================================~

INmAl TiiE SERVICE TASKS BELOW WHIOi WERE ACCOMPUSHED DURING CHANGE. IF TASKS WERE NOT ACCOMPUSHED, RECORD TIME ACCRUED SINCE TASK WAS LAST ACCOMPUSHED OR CHECK CONTINUE TIME (CT).

#>341036 MANDATORY

AMM34-11-()()

CAUBRATE COPILOT ENCODING ALTIMETER -RECORD DATE OF CAUBRATION -FAR91.411 0 I • Is, I ~

RECORD DATE OF CALIBRATION ~. t l

INSP LABOR-HRS TIME CONTINUE HRS.THS ACCRUED TIME

REMARKS: NOTE: 1. FO~LL=O=WI----.N=G _,IN-..SI""ALLA==-..TI..-O"""N=O'""R=M=AI-=-NTEN":"'"=AN_,CE.....,.O=N""'lli.....-E =AUTO-==M=ATI ........ C=PR'""ESSU..,...._,RE--:=AL-..TITU=-..DE=:=-RE_,PO____.R_,TI..-N'""G'""SYSTE.......,"'""M==oO':'F Tli::=:E=A'""T'""c '"""TRA:=-N'""SPO:=-N.__D_,ER==~ WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, TliE INTEGRATED SYSTEM MUST BE TESTED, INSPECTED AND FOUND TO COMPLY WITH PARAGRAPH (C), APPENDIX E OF PART 43.

2. EXCEPT FOR TiiE USE OF SYSTEM DRAIN AND ALTERNATE STATIC PRESSURE VALVES, FOLLOWING ANY OPENING AND CLOSING OF TliE STATIC PRESSURE SYSTEM, TiiAT SYSTEM MUST BE TESTED AND INSPECTED AND FOUND TO COMPLY WITH PARAGRAPH (A), APPENDICES E AND F, OF PART 43.

3. FREQUENCY MAY DIFFER AS LAID DOWN BY TliE APPROPRIATE REGULATORY AUTHORITY.

BOMBARDIER® AND OiALLENGER® ARE TRADEMARKS OF BOMBARDIER. INC.

23-DEC-2013 Return completed copy via email to [email protected] >INDICATES DUE ITEMS

© CAMP SYSTEMS 1 of 2 Total Pages = __ _, Initial __ _


Operator: SKY HIGH AIR L.LC. Work card No.: 34.060


~eg No.: N997GC Workorder No.:


Due At 20-JUN-2010

Accomplished l()l-\ S-•'f I I I I I I

TECHNICIANSIGNATURE0Y\ ~h_, Qt- . ~ A~~~ wo#t~l3l~ KIND OF CERTIFICATE & NO.;....· ,_f<.-_-_._ T ____ t/\f _________ _

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.;....· ----------------

#>341067 AIRWORTHINESS

AMM3+13-()()

FUNCTIONAL TEST NO. 1 ADC (34-13-00-101)

RECORD DATE OF CALIBRATION ~ ( $1 '2.0 ( If

REMARKS :

I TECH INSP LABOR-HRS

HRS.THS

@ __ _

NOTE: 1. FO~Ll=O=WI~NG=I-N=S"[""'ALLA~..,:n=O=N=O=R=M=AI=NTE.....,..N=AN=CE==O=N=TH=E=A=liT~OM=A=:Tl=C=PRESSU~~RE~Al=TITU~=DE~RE-PO~RTI-NG-SYSTI:--M-0-F=TH=E-A-:n=C~-~~~~

TRANSPONDER WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, THE INTEGRATED SYS[EM MUST BE TES[ED, INSPECTED, AND FOUND TO COMPLY WI:nH PARAGRAPH (C), APPENDIX E, OF PART 43.

2. EXCEPT FOR THE USE OF SYS[EM DRAIN AND AlTERNATE STATIC PRESSURE VALVES, FOLLOWING ANY OPENING AND Q.OSING OF THE STATIC PRESSURE SYS[EM, THAT SYSTI:M MUST BE TES[ED AND INSPECTED AND FOUND TO COMPLY WI:nH PARAGRAPH (A), APPENDICES E AND F, OF PART 43.


23-DEC-2013 © CAMP SYSTEMS 1 of 2 Total Pages = __ _, Initial __ Return completed copy via email to [email protected]

>INDICATES DUE ITEMS




""'eg No. : N997GC Workorder No.:

Date NCHRS AFL APH

Due At 20-JUN-2010

Accomplished II o 1 -1 s- ' 'i1 I I I I I

TECHNICIAN SIGNATURE~ ~ • ~ (<. -=l4-t<S (J.)o# l ~ 13 13 KIND OF CERTIFICATE & NO. ·;,.__ ____ Jo_ht _________ _

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.-· ----------------

1341061 NO. 1 AIR DATA COMPUTER AMM34-13-()()

REASON REMOVED: I B~ME EXPIRED (OiECK ONE) _ MOD/UPGRADE

a~~LURE SERVICE

B~ORN ENGINE CHANGE

s~OANER TIRE CHANGE

a~EDUUNG CONV

SWAP[TRBI.E SHOOT O DAMAGED O uNKNOWN

If removed PIN & SIN information is incorrect please provide details below_

REMOVED P/N 7000700-637 II S/N 97037571 II I LABOR-HRS

INSTALLED P/N I J S/N I I PART COST$



HRS

LOGS LOGS LOGS LOGS

lTECH: I IINsPJ

REMAA~: ==========================================================================~

INITIAL THE SERVICE TASKS BELOW WH!Oi WERE ACCOMPliSHED DURING CHANGE. IF TASKS WERE NOT ACCOMPLISHED, RECORD TIME ACCRUED SINCE TASK WAS LAST ACCOMPliSHED OR CHECK CONTINUE TIME (CT).

#>341066 MANDATORY

CAUBRATE NO. 1 AIR DATA COMPUTER -RECORD DATE OF CAUBRATION -FAR91.411

RECORD DATE OF CALIBRATION

GENERIC NO REF

BOMBARDIER® AND CHALLENGER® ARE TRADEMARKS OF BOMBARDIER, INC.

23-DEC-2013 Return completed copy via email to [email protected] > INDICATES DUE ITEMS

© CAMP SYSTEMS

LABOR-HRS TIME CONTINUE HRS.THS ACCRUED TIME

1 of 2 Total Pages= __ __, Initial __


~~or. SKY HIGH AIR L.L.C. Work card No.: 34.061

Senal No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.:


Due At 19-JUN-2010

Accomplished lo\ _, 5- l ~ I I I I I I

TECHNICIAN SIGNAlURE:_% __ ~---~---~-------KIND OF CERTIFICATE & NO.· fJ.__ ~R$ #'AJ 'v.,;()'#- f 2.t 3 { t INSPECTED BY:------------------KIND OF CERTIFICATE & NO.;....· ----------------

1341063 NO. 2 AIR DATA COMPUTER AMM34-13-()()

REASON REMOVED: I P TIME EXPIRED ,_.,

r---; SCHEDUUNG CONV a~MlURE U WORN a~OANER O swAP{TRBlE SHOOT n DAMAGED (CHECK ONE) ;] MOD/UPGRADE SERVICE :]ENGINE CHANGE TIRE CHANGE O uNKNOWN


REMOVED P/N 700070o-637 II I S/N 84120798 II I LABOR-HRS




HRS

LOGS LOGS LOGS LOGS

'TECH: I IINSP:I

REM~ :==========================================================================~

INmAL TiiE SERVICE TASKS BELOW WHICH WERE ACCOMPUSHED DURING CHANGE. IF TASKS WERE NOT ACCOMPUSHED, RECORD TIME ACCRUED SINCE TASK WAS LAST ACCOMPUSHED OR CHECK CONTINUE TIME ccn.

#>341069 MANDATORY

CAUBRATE NO. 2 AIR DATA COMPUTER - RECORD DATE OF CAUBRATION -FAR91.411

RECORD DATE OF CAUBRATION

TECH INSP LABOR-HRS TIME CONTINUE HRS.THS ACCRUED TIME

~----0 GENERIC NO REF RE~ : ~~~~-=~~==========================~====~====~==~~~~~==~====~


23-DEC-2013


© CAMP SYSTEMS 1 of 2 Total Pages= __ __. Initial __




~teg No.: N997GC Workorder No.:


Due At 20-JUN-2010

Accomplished I tHIS . 20\ 'fl I I I I I

TECHNICIAN SIGNAlURE~ @.. ~k KIND OF CERTIFICATE & NO.·

INSPECTED BY:------------------KIND OF CERTIFICATE & NO.;....· ----------------

#>341070 AIRWORTHINESS

AMM34-13-oo

FUNCTIONAL TEST NO. 2 ADC (34-13-00-101)

RECORDDATEOFCALIBRATION ~~ l 'f

I TEOi INSP LABOR-HRS

HRS.llfS

@ __ _

REMARKS : NOTE: 1. FO~u.-o""'WI""'"'"N~G ':"'IN~ST:~All.A""'"""""":TI::"O:""N-O:""R"":M~AI~NTE~N'"'"AN":'"CE::"""O':"'N"::TH~E ""Atro~O':"'M""'ATI~C":'PR:":ESSU:""":'"":RE"::""Al"":TTTU~"::DE~RE~PO~R~TI~N~G"=SYSTE~=M"'""':"O':"'F TH~E""A:':::T:":'C~~~=~~ TRANSPONDER WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, THE INTEGRATED SYST:EM MUST BE TEST:ED, INSPECTED, AND FOUND TO COMPLY WITH PARAGRAPH (C), APPENDIX E, OF PART 43.

2. EXCEPT FOR THE USE OF SYSTEM DRAIN AND ALTERNATE STATIC PRESSURE VALVES, FOlLOWING ANY OPENING AND CLOSING OF THE STATIC PRESSURE SYST:EM, THAT SYST:EM MUST BE TEST:ED AND INSPECTED AND FOUND TO COMPLY WITH PARAGRAPH (A), APPENDICES E AND F, OF PART 43.

BOMBARDIER® AND CHAU.ENGER® ARE TRADEMARKS OF BOMBARDIER, INC.

23-DEC-2013 © CAMP SYSTEMS 1 of 2 Return completed copy via email to [email protected] >INDICATES DUE ITEMS

Total Pages = __ ___. Initial __ _


~· SKY HIGH AIR L.L.C. Work card No.: 34.100

Senal No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.:


Due At 20-JUN-2010

Accomplished II 0\ II S II «f I I I I I I l '

TECHNICIAN SIGNA lURE~ , 0 • Clu.:-~ ... KIND OF CERTIFICATE & NO. ·

INSPECTED BY:------------------ KIND OF CERTIFICATE & NO.:....· ---------------

>341111 MANDATORY

PRESSURE LEAK TEST PITOT /STATIC AND TEMPERATURE SENSING SYSTEMS

TEO! INSP LABOR-HRS

HRS.lliS

~~ = --------------------------------------------------------------------------AMM 34-11-00

BOMBARDIER® AND CHAllENGER® ARE lRADEMARKS OF BOMBARDIER, INC.

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© CAMP SYSTEMS 1 of 2 Total Pages = __ _, Initial __


Operator: SKY HIGH AIR LL.C. Work Card No. : 34.420

Serial No.: 3025 Model: CL-601 ,,eg No.: N997GC Workorder No.:

Date A/C HRS AFL APH Due At 20-JUN-2010

Accomplished I O\ - l~- l'tl I I I I

TECHNICIAN SIGNAlURE:~ k}.. {)u_,_k n ~~ /'1 t' l ~ Wo#-1 ' J .3 I.:;> KIND OF CERTIFICATE & NO.~·~~~--t.-==-.::.0___::....__ __ ____:_<-=-_ ___::....___

INSPECTED BY:------------------ KIND OF CERTIFICATE & NO.:...· ---------------

1345101 LEFT TRANSPONDER

REASON REMOVED: I B~ME EXPIRED (CHECK ONE) MOD/UPGRADE

a FAILURE

SERVICE

B WORN

ENGINE OIANGE

a .LOANER

TIRE OIANGE

R SCHEDUUNG CONV

SWAP{TRBLE SHOOT n DAMAGED D uN KNOWN


REMOVED P/N 066-01143-0301 II I 5/N 2238 If I LABOR-HRS

INSTALLED P/N I () IDfD - 0 l 14' ~ ,. n '3n I I S/N I J'YI• ~3oo:3 l PART COST$

INSTALLED TSN MOS INSTALLED TSO M05 TIME SINCE MOS WARRANTY TIME MOS


HRS

LOGS LOGS LOGS LOGS

ITECH: I tMP;J IINSP:I

REM~ :=========================================================================-

INITIAL lliE SERVICE TASKS BELOW WHICH WERE ACCOMPLISHED DURING CHANGE. IF TASKS WERE NOT ACCOMPLISHED, RECORD TIME ACCRUED SINCE TASK WAS LAST' ACCOMPLISHED OR CHECK CONTINUE TIME (CT).

#>345111 MANDATORY

FUNcnONAL TEST LEFT TRANSPONDER ·FAR91.413

RECORD DATE OF CALIBRATION (2L_j~ 20~

TEOi INSP LABOR-HRS TIME COtfTINUE HRS.THS ACCRUED TIME

~-----0 AMM 34-54-00

RE~ : ----==~~~-------=-=====------~--==~==~~------~--====~-------=====~ NOTE; 1. FOLLOWING INSTALLATION OR MAINTENANCE ON AN ATC TRANSPONDER WHERE DATA CORRESPONDENCE ERROR COULD BE INTRODUCED, lliE INTEGRATED SYSTEM MUST BE TESTED, INSPECTED AND FOUND TO COM PL. Y Willi PARAGRAPH (C), APPENDIX E OF PART 43.

2. FREQUENCY MAY DIFFER AS LAID DOWN BY lliE APPROPRIATE REGULATORY AUlliORITY.

BARDIER® AND OIAUENGER® ARE TRADEMARKS OF BOMBARDIER. INC.

23-DEC-2013


© CAMP SYSTEMS 1 of 2 Total Pages= __ _. Initial __

- -TROPIC RADIO INC.

w

1!6 2695 NW 56TH ST. HANGER 53-A ~ BILL TO

FT. LAUDERDALE FL. 33309 ,·. ,· . "' )e II v I, I

ADDRESS

FAA APPROVED REPAIR STATION I IJ~ I• ~4R510~ - CITY ' SlATE ZIP CODE

\/Y) J /.._

.0.# -. ,"") I ...., PHONE: 954-776-4030 USER TEL . NO -

INVOICE DATE' TIME PHONE WHEN READY lOADER WRITTEN BY ADDRESS CITY AND STATE

A.M. P.M. MAKE ANI MODEL YEAR SE ~lA NUMBER AtG.liJUMBER AIR( RAFT HOURS CUSTOMER ORDER NO . 0 WARRANT AUTHORIZATION

... ~ ·, I 0 CASH i~/ ./fl Vo' J / V I I I r..:::rr L.... v. ,,. - 0 CHARGE

I rEM REPAIR JRDER INS'"RI rtONS A TION TAKEN ( HARC iES

, / . Lf I 5 ).r::v../v;. ul! rf})( I ~ r -.

. ... \ ~) t 4 I)~' 7/.::J.j I "'r~• J ' . , ./~/ 'f

u t"rv~(J/· - rr; I I itt-_~)

~ ~~ '-1· ~ 1~ ' ev.-- ',;'pi v I ~· l L . I . . ~

', ..... ~I f ' I ,, ) ' 'I 'I J PJAv '" ON't [ ,, -r .. .. . _. - ~.., -., t

~LM }./~' 1

~·I VI_., • r:.(<l ( : a ( ~ t/ d , - ..:.::.~{r-. \""'C. :-v

':Vr- C,_;;AJr,,J£~ ..0£ I J/'.1 /.L.I I

) . . . t .. -.!_.[l(Clr-'"J t..:.._ ... , /U.t i? ':J {;I h ~ ' ·I

. II

l...O ll ~L.-t t.J/)., '((,.A"" •; t.::/;-1/ . , The atrcraft. airframe . aircraft engme. propeller or appliance The only warr1n1•es apply1ng 10 ll"'tS Pfir1h) are those •h,ch may be offered by the manufacturer The ~ll•ng dealer h~eby e•pressly d•scla•ms all warranl•e5 . eiH'ltr eapress or •rnphed •nclud•ng any •mphed 'dent1f1ed above wasJepair&d and inspected in accordance with warrant1es or merchantab•l•ty or fitness for a par1•tutar purpou and ne•lrler assumn nor authonzes •ny other person to assume I of •t any ilabll•ty 10 connechon w•ltlttlt sa le ol ttl•s part( s) and! or s.erv•ce Buy.w s~/1

current regulations of the Federal Av18l10n Admimstration and not~ enlilltd to recover !ro m the s.ell•ng dealer any cons@Qut:ll,al damages damages to property damages lor toss ol1.1se. loss ol t•me. lou ol proht or •ncome 01 any ottler •nC•denllal damage

is approved for return to seryice

, '.JJ

ITEM PART NO . OTY . COST TOTAL CUSTOMER P 0 NO . . SIGNED DATE

1\1....1 f ., .... I hereby authorize the above repa11 work 10 be done along wilh the necessary malarial , and hereby grant you and/or your em- , ' ' f.J ~

I ployees permission to operate and fly the airplane herein de- . .., .... , , I I I 1 I LABOR I scribed for the purpose of testing and/or inspect1on An express

' -11' ~/ mechanics lien is hereby acknowledged on above airplane lo - ' PARTS secure the amount of repairs lhereto TROPIC RADIO is not J / .. responsible for loss or damage to plane or articles lefl in planes

~ 14 ,~ ( I .J - •J"j in case of lire, theft . or any olher cause beyond our control. I V ,/ SHIPPING

X J I 7tJJ.),_;),,, ""l'

~ ' SUPPLIES ~"~ CUSTOMER SIGNATURE __, /,v •'/ t l I SUBLET REPAIRS SUBLET

'3iA '/tJ ?ol U> 1 TAX

TOTAL I

) ) TOTAL PARTS ) rc.TR ~ 'r.f' f0610 , ACCRUING FINANCE CHARGE OF 1.8% PER MONTH ASSESSED ON ALL ACCOUNTS OVER 30 DAYS

TROPIC RADIO INC •

w

>-A 1!!' BILL TO - . I I) .)J.. '- J\ .. h J)t: /' IJ I I

II qly

r.f\.1-\. .A.rr.KVV nu KnrA.tK ~!A. liON ADDRESS - /'r, -€if;

~ f"fJI I J t;._ I .' ~

. RZ4R510M - CITY StATE - ZIP CODE

1 I

~ .~ ~( .) i ' ) • ... , . ' .... ,

PHONE: 954-776-4030 .0.# I~ 1.3 . .....'\ USER TEL. NO~

I .:;:) ~ t - ) . 1 .. I I

INVOI,CE OATf! .,. TIME PHONE WHEN READY 'ORDER WAITT~N BY ADDRESS CITY AND STATE / - 1 _, I A .M . I '

P.M. r MAKE AN, MODEL YEAR SEI IAl Nl IURI=R REn -ri!TJMJJER AIRCRAFT HOURS cus· MER ORDER NO. 0 WARRANT AUTHORIZATION

i I I') I \ • '[)-~

'7t c :-- ::> ey l J OCASH

-...I 11 I ' )"') 5' ;V, ' . <_.,, .vrd l-h-... ..)''' ... ' ( -- i L. '" .. L 0 CHARGE .

; I'EM REPAIR JRQEj; INSTAL riONS ACTI N AKEN < HAA( ES

/. ~- ;, } /. {{ ...

I ' \ , .... , { ' r- r /I " \_ ~ . -...

I .. ' -· ' .

-~)· ,, yl ~,-; I . ; b.<f.' I

I . ( , ... ....

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• ../ i IIJ A,/ ' ~.)t/..1 I • I 'fiC I

I I tf :i;, l .! v1v;-JII f",, . ~ rv.,; .... - ' ~ .f.

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' ' . ~~-- - ,} .., ' -., -...,.-· ' { .~.. ... , i< /"t e .

' ·~ ~.!· ) ;(}a,, I I I

The ~i_rcralt , airframe, aircraft engine, propeller or appliance The onty warrantift applying to lhtt p8r1(1) ere thOH whteh may be offered by the manufacturer TM Mll•ng <Seater n.reby e.cprenty d•aclattnl all wa~ran11es . ttlhet eapress Of unphed. includang any tmphed 1denhlled above was .repaired and inspected In accordance wilh watrantltl or merchAntability or fttnnt for a parttcu .. r purpote and nttlhtr anumn nor lv1hOfiZts •ny other person 10 assume tot tlany lt~btltty tnconneCiton w•th theule of lh•l part! I) and/or MNIGe BIJ'Ietlhalt

curran! regulations of the Federal Avlallon Admlnlslrallon and not be tnt illtd to recover lrom the a.elhng dealer eny consi'Qut:"li tl damages damagtn 10 property oamages for ton of us.e. ross olltml. tos.s of ptol•t or •nc.ome or any other •nctc:Jtnhal damage

is approved lor return to aervice.

' r ITEM PART NO. OTY . COST TOTAL CUSTOMER P 0 . NO.

SIGNED If I DATE ,¥ ,t.. - - t J.) 'i I 0 ~4~ ,..., f /,"' .---/l IG, f'\.

I hereby authorize the above repair work lo be done along wilh h ~

lhe necessary material, and hereby gran! you and/or your em-f I ' J I f I - (0'-{ ! 1/;: ~ t~ Lj ployees permission to operale and fly lhe airplane herein de- L.J,..J I • ' I \ .Jf , '/N LABOR

ocrlbed lor the purpose of teallng and/or inspeclion. An e•press

--i.ij 4 t\(_ u,.~. /-;O .., "'"?. ·~,I I

mechanics lien ia hereby acknowledged on above airplane 1o . J '7 ', I PARTS aacure the amount of repairs !hereto TROPIC RADIO Is not I -responsible lor lo .. or damage to plane or artlclea left In planes I

~

... ,;., I f ',.~f4 ... - ,ct ,, (.. I I .J ., ' , in case of lire, {haft, or any other cause beyond our control . • ~

-, SHIPPING .,

-:(' I /-·' syPPUes ') X ..... ""'- \..

;! ,)• I J , I .) ' I 'I .'

CUSTOMER SIGNATURE --· -- I) ( :.-./,\ 'I ..... ./ SUBLET REPAIRS I \ f - f SUBLET ' .. - -

J,l I I I ?oY· , /1 () - J • ' 1 .... j I ,.., , It I TAX . TOTAL

"\. t I TOTAL PARTS -~

-, • •N "r Y .a,..,..,... ... ""'"".,..-·-----·-·-

TROPIC RADIO INC .

N

1}r .tO~) NW )0 ___ 1SJ.liANl.ThK )3-A ~ BILL TO

/ -·~;.· (.. /) ' .. . ~y ./.;,.~ \I I II ..,

FT. LAUDERDALE FL. 33309 . . ..

ADDRESS ,;E . FAA APPROVED REPAIR STATION -., I I· '

RZ4R510M - CITY SlATE ZIP CODE ! -

} IY) I •fl. \...,.) /..:,C. I ... ( ) r PHONE: 954-776-4030 TEL . NO

.0.# I ,'1 I'; USER - · ) , ,..... , I ~

I I I INVOICE DATE TIME PHONE WHEN READY lOADER WRITTEN BY ADDRESS CITY AND STATE

l ~ -: . . ' A.M . P.M .

MAKE ANI MODEL YEAR SE ~IAL NUMBER R~G. NUMBEA AIRC RAFT HOURS CUSTOMER ORDER NO. 0 WARRANT AUTHORIZATION

. "\ l .... . I· ' -· ... .. 0 CASH '•. '# ) \ (,.'~ t,.-· ;V ·) . c t") . "'

,,I I "" r { r_,.' • ' \... . ' . -' I ' I~ I .. . 'l • 0 CHARGE ... ' • '

ITEM REPAIR )RIJEI INSIRL liONS ACTION_ TAKEN C:HARC: iES . I

"? ) t:::J .. ~..k:t(J I I

I >J IAJ I A r - . ' ' ' ""'

. I ' ( . d f ·f , ·'

1/tC-. r( t (. c ', ., J '- . I(~J) /I v

f .. .. I .. ·,' r) '~ v I I 0i I I

(. . ... ,.. 'L '~ .. !1' - ,

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r ·,N, .. i· .

' I

_/. ' . •• ~ r I l .~ I

r __

'

.~. - ' ,~..A ,It, , ,.:f;rl> ~

r

The aircrall. airframe. aircrall engine. propeller or appliance The only warranfin applying to lhtl p.n(s) ~re thOM wh•ch may be orttred by I he m1nulac1urer The wurng de•ler h.,eby t.tepreuly drsclarms 111 WIIHIInl•es. •riner eapress or unphed. includrng any tmpl•ed Identified above was.repalred and inspected In accordance with wananues or merchantability or ftlnns for a panrcular purpoM and nerener assumes nor authOrlln any olner person to assume fOf tl any lrabtllly tn connect ton wrtntne u leof tnrs panls)andlor aervrce Buyl'f shall

current regulations ot the Federal Aviat ion Administration and not be entrlltd to recOYet from the Mllrng de111er any conseque;,t• ll damaQel damages to property cum•ges for loss of us.e. lou of lime. lou of prolrt or rncome or any other mcioenhal damage

is approved tor return to service.

'.: ., ITEM PART NO. OTY. COST TOTAL CUSTOMER P.O. NO. I

SIGNED DATE ~ ;-j,.J .

I I,~ ,"),. . J ~ -1 J "{ I 'i '' ..1

,, I hereby authorize the above repair work to be done along with ·" the necessary material. and hereby grant you and/or your em- I f.; J I /,v I - I 'I l ~ fJ I lf' - '1 .. ~ "' LABOR ployeea permlsalon to operate and tly the airplane herein de- .. I i ~

acribed tor the purpose ot testing and/or inspection. An ••press . ·I ) ._,/ --, mechanica lien it hereby acknowledged on above airplane to I i'\ - 7 I PARTS aecure the amount of repairs thereto TROPIC RADIO is not - j J '""

responalble lor lou or damage to plane or articles left In planes ~. /~ (\ (

I f-1 In case of lire, theft, or eny other cause beyond our control. i I • SHIPPING • \ (" - I ..:.Jr 1-(;1 • 1 ) ) X J I I f

.~,'"r '- .. Slrfli'I?LIES CUSTOMER SIGNATURE

,II r 4. ' ( :-. /~v I I -- ) .; SUBLET REPAIRS ~ SUBLET

-(· P/tJ 9-ot ' . ' • t l ,,

I I I TAX ... ... l . '"\., TOTAL

1' \ TOTAL PARTS () • - .. -

1. Approving National Aviation 2. Authority/Country AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number.

FAA/UNITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 2QNVA0001001001 4. Organization Name and Address:

Duncan Aviation/Lincoln Ai art/Lincoln NE 68524 JGVR194F Oescription:

MODES TRANSPONDER

13. Remarks:

8. Part Number.

066..01143-2101

Customer: SMART PARTS INC Discrepancy: Quote repair and 0/H price.

9. Eligibility: •

N/A

5. Wor1< Order/Contract/Invoice Number.

2QNVA 10. Quantity: 11. Seriai/Bat<:h Number 12. Status/Work:

1 M123003 Overhauled

Preliminary Findings: Bench checked and found unit inoperative. Troubleshot and found burnt power supply board #2 and failed transistor on power supply #1 . Unit has SB 1 installed but not marked on modification plate.

Corrective Action: Disassembled. Replaced defective parts. Installed service bulletin MST67 A-34-56 to upgrade to latest software. Marked off SB 1. Overhauled. Unit function tested per BENDIX MST 67 A Mode S Transponder Component Maintenance Manual with Illustrated Parts List, Revision 5, dated 08/12/2011.

This transponder meets all requirements of FAR Part 43 Appendix F.

Duncan Aviation certifies that the work specified in Blocks 12 and 13 was performed I.A.W. EASA Implementation Rule part 145 approval, and with respect to that work, the aircraft component is considered ready for release to service under EASA approval number EASA.145.4392. Certificate Number JGVR 194F. All EASAIFAA Airworthiness Directives are the responsibility of the installer. No current U.S. Airworthiness Directives apply. Technician: Scott A Griess This document constitutes a signed copy of the work order Approval for return to service See attached parts list

19.18114 CFR 43.9 Return to Service 181 Other regulations specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was acex>mplished in ac:Cordance with Title 14,

oo\,\>'•;i·?·':H·>'i<":·rcode of Federal Regulations, part 43 and in respect to that work, the items are

DUNCAN 011519

21. ApprovaVCertiftcale No.:

JGVR194F 23. Date (m/d/y):

Jan 10 2014

Where the user/installer performs worX in accordance with the national regLDations of an airworthiness authority cftfferent than the aitworthiness authority of the country specified in Block 1, it is essential at the user/installer ensures that his/her airworthiness authortty accepts parts/components/assembfies from the airworthiness authority of the country specified in Block 1.

tatements in blocks 14 and 19 do not constiMe installations certification. In all cases. aircraft maintenance records must contain an installation certification issued in accordance with the national

regulations by the userRnstaner beforv the aircran may be nown.

FAA Form 8130-3 *6-01 • Installer must cross-check eligibility with applicable technical data. NSN-0052.00.012·9005

art Number ~07-00161-0000

057-05287-0104 057-05335-0004 122-01901-0104 122-01902-0104 200-08420-0000

Part Description TRANSISTOR SOFTWARE MOD TAG DECAL PGRMD IC PGRMD IC POWER SUPPLY #2 ASSY

Parts List

Serial Number

NA2

3. Form Tracking Number:

2QNVA0001001001

Quantity 1.000 1.000 1.000 1.000 1.000 1.000

Page 2 of2

1. Approving National Aviation Authority/Country

FAA/UNITED STATES 4. Organization Name and Address:

2. AUTHORIZED RELEASE CERTIFICATE FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG

5. Work Order/ContracUinvoice Number.

Duncan Aviation/Lincoln Airport/Lincoln NE 68524 JGVR194F 2QNVA ~tem: 7. Description: 8. Part Number. 9. Eligibility: • 10. Quantity: 11. Serial/Batch Number 12. Status/Wor1<:

r/ MODES 066-01143-2101 N/A 1 M123003 Overhauled TRANSPONDER

13. Remari<s:

Customer: SMART PARTS INC * Discrepancy: Quote repair and 0/H price.

Preliminary Findings: Bench checked and found unit inoperative. Troubleshot and found burnt power supply board #2 and failed transistor on power supply #1 . Unit has SB 1 installed but not marked on modification plate.

Corrective Action : Disassembled. Replaced defective parts. Installed service bulletin MST67 A-34-56 to upgrade to latest software. Marked off SB 1. Overhauled. Unit function tested per BENDIX MST 67 A Mode S Transponder Component Maintenance Manual with Illustrated Parts List, Revision 5, dated 08/12/2011 .

This transponder meets all requirements of FAR Part 43 Appendix F.

Duncan Aviation certifies that the work specified in Blocks 12 and 13 was performed I.A.W. EASA Implementation Rule part 145 approval , and with respect to that work, the aircraft component is considered ready for release to service under EASA approval number EASA.145.4392. Certificate Number JGVR 194F. All EASAIFAA Airworthiness Directives are the responsibility of the installer. No current U.S. Airworthiness Directives apply. Technician: Scott A Griess This document constitutes a signed copy of the work order Approval for return to service See attached parts list

14. Certifies the items identified above were manufactured on confinmily to:

0 Approved design data and are in a condition for safe operation.

0 Non-approved design data specified in Block 13.

15. Authorized Signature: 16. Approval Authorization No.;

17. Name (Type or Printed): 18. Date (mldly):

19. ~ 14 CFR 43.9 Return to Service~ Other regulations specified in Block 13

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

20. Authorized Signature:

~~ 22. Name (Type or Printed):

Dustin C Johnson

DUNCAN 0 11519

21. Approval/Certificate No.:

JGVR194F 23. Date (m/d/y):

Jan 10, 2014 User/Installer Responsibilities

It is important to understand that the existence of this document alone does not automatically constitute authority to install the partlcomponenUassembly.

Where the user/installer performs work in acoordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

Statements in blocks 14 and 19 do not constitute installations certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown. FAA Form 8130-3 *6-01 ) • Installer must cross-check eligibility with applicable technical data. NSN-0052-00-012-9005

FAALNK Page 1 of2

.,art Number rOO 7-00161-0000

057-05287-0104 057-05335-0004 122-01901-0104 122-01902-0104 200-08420-0000

Part Description TRANSISTOR SOFTWARE MOD TAG DECAL PGRMD IC PGRMD IC POWER SUPPLY #2 ASSY

Parts List

Serial Number

NA2

3. Form Tracking Number:

2QNVA0001 001001

Quantity 1.000 1.000 1.000 1.000 1.000 1.000

Page 2 of2


1 Ran aircraft engines tor preservation

DATE February 22, 2014 TOTAL TIME 9583.35

ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT I ENGINE WAS PERFORMED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRA TTON.

SIGNED I~ George Glen A&P 2730175 I

i '

Accomplished the following Tasks 1/A/W CL-601 MM 1. 058280; 6 MONTH~NSPECTij>N. ./ ./

242114; 12-20-00-320; 34922o; 243061; 239656

2. 056300- 12 MONTHS INSPECTION. / I 1 / / .. / / / I . / / / /

~203; 240301; 242113; 242121; 243061; 259106; 259116: 2~11; 28-21-21-205; 262076; 262081; 262086; 262091; 7 · / / / 7 ,. _, /" I' / / r 7 /

262099; 269003; 275096; 275101; 275106; 275111; 275116; 275121 ' 5126; 275131; 321023; 321028; 33:1000; 335009; / / I' / {_ _ / / - ;- / /

339008; 339009; 341106; 342196; 349223; 349992; 491181; 53-10-11-228; 57-()().()0..203-1; 51-o0-00-203-2; 51-3o-oD-213-1; / (

57-30-00-213-2; 761103

3. 050320 • 2~0NTHS IN~ECTION. / / / / / / C54-00-801-1; CU-00-801-2; C51-00-802-2; C51-oo-802·1; 55-50-00-213; 55-tf0.00.212; 55-50-00-211; 55-30-00-209;

, ,. "// /, _ ,/ I ~1~20~522001;522006;555091;520216;346211;346216;291184;291183;259015;

/ r .., 291185; 315131; 242115

4. 056330 • 36 MONTHS INSPECTION. / / / / / / / ~; ~5-00-812; ~13; ~50-00-219; 55-5().00..218; 56-60-00-217; 55-50-00-216;

, -' r I / I 55-50-00-215; 55-lS0-00-214; 359001; 359003; 359(1(}8; 359:107

5. -48 MONljiS INSPECTI_9N. 7 / / / ,. _J _ ! / 23-6o-oo-203; ~2-00-803; C!3-00-814; C!3-00-815; C55-00-801; C55-00-804; C55-00-806j C55-00-810; C~11

/ , / /' . C51-00-810-~ C57-00-811J.1; ~5-00-609-2; C55-01J.809-1

8. 058340 • 60 MONTHS INSPECTION. - / / / / I ////// /

20-40-00-202;_2CJ..40.00;-203; 240301; 242105£_242113; 242121; 243061; 259106; 259116; 259311; 259402~25H04; --.....__...- / r , / "' / ' / _., / r ,

2594111; 259<109; 259412; 28-21-21-205; 2620~6; 262076; 262031; 262081; 262036j,262086; 262091; 262099; / / .., / r · . / /' /' / _ , / r

269003; 2~29; 27.::; 275101; 275106; 275111; 2751.16; 275121; 275126; 276131; 28-1~203; 28-11J.21-206; / / / / . / / /" / , /

281036; 281()41; 28 8; 284221; 28!S046; 30-11-D6-2CU-1; 30-11-08-2CU-2; 32-43-18-223; 32Q~; 321023; 321028; ._, / / . / / / / / / ;" ,r I

335006;335009;339008;339009;341106;349223;349992;359028;491181;52-20-00-209;52-30-00-210; ,..- ,..- r' . , r' / I ,. /

53-00-00-204; 53-10-00-205; 53-10-00-206; 53-10-00-207; 53-10-00-208; 53-10-00-209; 53-10-00-210; 53-10-00-211; "' · ,..- ._, ,- r /" ,. (

53-10-00-2.12; 53-10-00-213; 53-10-1!;9-214; 53-10-00-215; 53-10-00-216; 53-10-00-217; 53-10-00-218;, 53-10-0().219; ~ , / , / / ~ ,

~10.00.220; 53-10.11·228; 53-10.11-230; 5J.31J.00..222; 53-10-00-225; 5U0-11-221; 632068; 632113; 532177;

~202-1; ~2o2-2; ~10:00..203; ~1'o:io-204: 56:ao-«;;.210; 51-00-00-203-~; 57-00-00-203-Z;

57~~1; 51~2CU-2; 57-1o.oO.i0s.1: 51-10-00-zOs-2: 5T-1~206-1; s1.1o:oo.208-2; 57-1~7-1; / ,.. ., - ,.- / ,

51-1~207-2; 57·10-00-208-1; 51-10-00-208-2; 57-10-00-209-1; 57-10-00-209-2; 57·2~211J.1; 51-20-01J.211J.2; -- ,.- . /" . ·-~ /" 51-20-00-211-1; 57-20-00-211-2; 51-30-00-213-1; 51-30-00-213-2; 51-4IJ.00-217-1; 57-«HJJ-217-2; 57-4IJ.00-21B-1;

/ / · ,- r . ,.- ....- _, :fT..fO.(J(J.218-2; :fT..fO.(J(J.219-1; 67-4lJ.00-219-2; 51-40-00-220.1; 51-40-00-220.2; 57-40-00-221-1; 57-40-01J.221-2;

,r / (' . / ,. /' / ,/" ~ 51-50-00-222-1; 57·50-00-222-2; 761103; C52-0IJ.801; C52-0IJ.802; C52-0IJ.B04; C52-00-805; C52-00-806; C!J3-00.B01;

/ , / / - .; ....... / ---7-C53-00-B02; C53-0<»(U; C53-00-B/ 05; C53-00-806; C!3-00-807; C53-01J.808; C53-00-809; C53-00-810; C53-00-811; .,.. / . ,. / / , , r C5~2; ~13; C~17; C53-00-8)8; C53-0,l?-81f: C53-00412J; ~22j.P53-p0-8~ C53-00-8~

C!i3-tJO..IU5; C53-0IJ.826; C53-00-827; C54-00-802-1; Ctu-00-1102-~ CSS-00-802; C55-00-803; C55-00-807; C55-00-808; --~ ~-,- · ,/" / . - / / / / C51-00-801; C51-00-803-1; C57-00-803-2; C51-00-8CU-1; C57-00-BCU-2; C57-00-805-1; C51-00-805-2; C57-00-808-1;

, r ,. <" ,.. -- - -C51-IJ0.806.2; C57-00-1107-1; C51-oo-807-2; C57-oo-808-1; C57-00-8DB-2; C57-00-809-1; C51-00-809-2; C57-oo-811·1; ,.. , /" /" , - .- , , C51-00-811·2; C51-oo-812-1; C51-oo-812·2; C51-00-813-1; C51-00-813-2; C57-D0-814-1; C57-00-814-2; C57-00-815-1; ,. ,. ,. .,.. .... / /" ,. Cts7~11S-2; Cts7~1fl-1; Cl17-«HH1tl-il; C:IT-oo-817•1; Cl1T-oo-ll17•2i c:JT-oo-818-1; C57-00-81B-2; C57-0IJ.819-1i

r ., t"" / / C57-00-819-2; C57-00-820; C71-00-801; C71-0Q-802; C 1-00-803; C78-00-801

7. 056010-100 HRs TASK. ITEMS COMPLIED WITH

243048; 273901; 792030 {#. 1 ); 792030 {#.2)

Stand Alone Items

8. 259003 Removed & replaced ELT battery PIN OFF: 452-0133, SIN OFF: nla ;SIN ON: 360584-077

9. 242103 Removed & replaced ADG up lock squib PIN OFF: 0550468, SIN OFF: 137;SIN ON: 506-511

10. 239651 Removed & replaced CVR ULD battery PIN OFF: DIK 120, SIN OFF: DU46978;SIN ON: DU27952

11. 532161 Check Intercostal I cleat FS 421-544

12. 577051 Visual check left lower center wing plank water drain holes periphery

13. 499020 APU - Visual check magnetic drain plug

14. 329021 Removed & replaced left MLG assembly with customer supply, UG that was restored by Jet Harbor CRS # WK4R625M

on 06127111. (Restoration was verify by Pollard Spares DOM: Mark Eubanks A&P # 522924150) & (Inspected by Advance

Aviation Technologies CRS # GQRR443L) PIN OFF: 601-85082-5, SIN ON: DEC030183100-

PIN ON: 6100-217, SIN ON: DEC027-83. Gear was installed with 9476 Cycles

15. 321044 Removed & replaced with customer supply left MLG side stay actuator that was restored by Jet Harbor CRS# N56K026B

on 06127111. (Verified by Pollard Spares DOM: Mark Eubanks A&P # 522924150) & (Inspected by Advantage Aviation

Technologies. CRS # GQRR443L) Actuator PIN: 600-85001-85, SIN OFF: DRG4785179-0- SIN ON: DCL205191

Actuator has 9476 Cycles. Next restoration Due 0612021

16. 321045 Removed & replaced with customer supplied right MLG side stay actuator that was restored by

Jet Harbor CRS# N56K026B on 06127111 (Verified by Pollard Spares DOM: Mark Eubanks A&P # 522924150) &

(Inspected by Advantage Aviation Technologies. CRS # GQRR443L) Actuator PIN: 600-85001-85, SIN OFF: DEC97182100-

SIN ON: DCL001-87. Actuator has 9476 Cycles. Next restoration Due 0612021

17. 329026 Removed & replaced right MLG assembly with customer supplied UG that was previously restored on 06127111 by

Jet Harbor CRS# WK4R625M (Inspected by Advantage Aviation CRS# GQRR443L on 11105/13) PIN OFF: 601-85082-6,

SIN OFF: DEC026183100- PIN ON: 6100-2, SIN ON: DEC-024-083. Installed UG has 9476 cycles

18. 322011 Removed & replaced NLG retraction actuator that was inspected by Advantage Aviation Technologies

CRS # GQRR443L on 11115113 under WO# LG33161. PIN ON: 104471003, SIN ON: DEC27-81

COMPLIED WITH THE FOLLOWING ADs:

1~!!lJfiifiii~ragraph(F)(1) Revise cracking of the wing anti-ice piccolo ducks the normal and abnormal

procedures sections of the applicable Canadair

~lA!fn.:li!QjloaL)_ :.QJZ!£<tivate all chemical oxygen generators in the lavatories until the generator oxygen supply is

expended. NIA due 02 generators not installed.

o spect for cracking of backrest link. N/A due to PIN seats installed --'"""!"·--~.t)!l.j

c::...::.~~=~'"-'""'-~!lllvent the in-line flow indicators of the oxygen mask assembly from fracturing & separating.

S~~~,__...,."""""'"~ect the ADG power feeder harness to determine the wire type

~~~-_prevent TCAS units from dropping tracks, which could compromise separation of air traffic.

NIA due to PIN installed.

~~~!~~1!2jNo~. Jl• ngine - Visually inspect & Eddy Current Inspect I Replace stage 5 LPT &I or 6

(PCW by Standard Aero on 10-19-2006.@ TSN:8823.4hrs and CSN:5619).

. Next Due A TC:5227(ENC:5983) .

3 . 1 1 No. 2 Engine - Visual Inspection fan blade of the fan blade abradable rub strip for wear

Next Due ATC:5227(ENC:5789) .

33. Aerospace protective breathing equipment (PBE). NIA due PIN mask installed.

king on the upper & lower web of the engine support beam

;;:~~~~~~~ ht inboard elevator flutter damper. NIA due to PIN installed

ight outboard elevator flutter damper NIA due PIN installed.

?immw;;;i~~~~· t aileron flutter damper. Next Due 1-31-1519883.35 hrs.

Discrepancies

41. Removed & replaced UH Flap seal (outboard flap, inboard section). PIN: 600-14532-7

42. Removed & replaced RIH NA V light. PIN: 1524

43. Removed & replaced reservoir filling line T-fitting (AFT equipment bay). PIN OFF: MS 21905D6; PIN ON: MS 21905DL

44. Removed & replaced ground strap on left inboard horizontal stab. Trailing. PIN: MS25083-6DD5

45. Removed & reinstalled horizontal stab actuator after repair by Ontic Engineering & MFG. INC CRS# OE6R225J

PIN: 21207-008; SIN: Y2017

46. Removed & replaced No 3A Hydraulic pump motor PIN: 62613- SIN OFF: RE1017; SIN ON: RJ1542

47. Removed & replaced upper tail NAV light. PIN: S2371-201

48. Removed corrosion, cleaned area, prepped & primed on UH AFT wing to fuselage panel

49. Removed corrosion, cleaned area, prepped & primed on RIH AFT wing to fuselage panel

50. Removed corrosion, cleaned area, prepped & primed multiple areas on UH upper wing

51. Removed corrosion, cleaned area, prepped & primed multiple areas on RIH upper wing

52. Removed & replaced RIH pylon logo light. PIN: 4713

53. Removed & replaced NLG with customer supply landing gear (That was previously restored by

Jet Harbor INC CSR # N56R0268 on Jun 27 2011) PIN OFF: 7300-15, SIN OFF: DEC005-78-00R

PIN ON: 7300-3, SIN ON: DCL35-01

54. Removed & replaced UH MLG with customer supply landing gear (That was previously restored by

Jet Harbor INC CSR # N56R0268 on Jun 27 2011) PIN OFF: 601-85082-5, SIN OFF: DEC030/83100

PIN ON: 6100-217, SIN ON: DEC027-83

55. Removed & replaced RIH MLG with customer supply landing gear (That was previously restored by

Jet Harbor INC CSR # N56R026B on Jun 27 2011) PIN OFF: 601-85082-6, SIN OFF: DEC026/83100

PIN ON: 6100-2, SIN ON: DEC024-83

56. Removed & replaced No.1 MLG tire PIN: 256K43-3, SIN OFF: 81527001, SIN ON: 32233317

57. Removed & replaced No.2 MLG tire PIN: 256K43-3, SIN ON: 32273290

58. Removed & replaced No.3 MLG tire PIN: 256K43-3, SIN OFF: 71707071, SIN ON: 32353320

59. Removed & replaced No.4 MLG tire PIN: 256X43-3, SIN OFF: 81667033, SIN ON: 32283303

60. Removed & replaced (6) cabin reading lamps PIN: 1308

61. Removed & replaced lav overhead dome light. PIN: 1308

62. Removed & replaced No.1 & No.2 nose landing gear tires.

No. 1 Tire PIN: 184F23-2, SIN ON: 22293250

No. 2 Tire PIN: 184F23-2, SIN ON: 22413257

63. Removed & replaced RIH engine cowling latch. PIN: 228-50201-264

64. Serviced UH Main landing gear strut.

65. Serviced RIH Main landing gear strut.

66. Serviced Nose landing gear strut.

67. Removed & replaced LGCU with customer supplied unit. PIN: 600-50969-9, SIN: OFF: 168, SIN ON: 438.

68. Removed & replaced IRU with customer supply IRU. PIN: 4G1066AD003, SIN OFF: 123, SIN ON: 083

69. Removed & replaced C/8 panel bezels (x2) PIN: 601A50924-3, (+2) PIN: 601A50924-5

70. Removed & replaced the following# 1 HF components (3): HF control PIN: 071-1274-02, SIN OFF: P1275, SIN ON: 5146

HF Control adapter PIN: 071-1268-01, SIN ON: 1954

HF Bridging Amplifier PIN: 071-0019-00, SIN ON: 4200

71 . Removed & replaced CVR control. PIN: 93-A151-20, SIN OFF: 76347- SIN ON: 72334

72. Removed & replaced INU fan filter. PIN: 26000790-101GF,SIN ON: LOT# 070104

73. Installed new life vest (x 6) PIN: P01074-101:SIN: 896664 ,896637, 006380,006475,006108 & 896600(exp. 0111012019).

74. Removed & replaced with customer supply INU fan PIN: 021392, SIN ON: KY3445

75. Removed & replaced with customer supplied AD/ (Repair) . PIN: 7000466-905, SIN OFF: 82051571,0N: 82041501.

76. Removed & replaced the following components from# 2 ADF: Receiver PIN: 622-2362-001,SIN OFF: 15246, SIN ON:7058.

Antenna PIN: 622-3710-001, SIN ON: 3233.

77. Removed & replaced ADF receiver# 1 PIN: 622-2362-001, SIN ON: 6123

78. Removed & replaced Flap Control Unit PIN OFF: 8-341-02, SIN OFF: 61- PIN ON: 8-341-06 SIN ON: 319

79. Removed & replaced TCAS processor. PIN: 066-50000-2120, SIN OFF: 1683,0N: 1785.

80. Removed & replaced with customer supplied item (Overhauled) # 2 Comms control head.

PIN: 822-1120-005, SIN OFF: 19327,SIN ON: 12867.

81. Removed & replaced# 1 Nav control head. PIN: 622-6521-013, SIN OFF:19483,SIN:ON: 18112.

82. Removed & replaced # 1 Nav receiver. PIN: 622-6137-201, SIN OFF: 4398,SIN ON: 9381.

83. Removed & replaced (Tested)# 2 TCAS/VS/. PIN: 066-50001-1001, SIN OFF: 1557, SIN ON: 1350.

ITEM COMPLIED WITH BY OUTSIDE COMPANIES

Jet Harbor Inc. SCR# WK4R625M

84. 321081 Restoration of UH MLG assembly was C/W by Jet Harbor Inc. on June 27, 2011 (Restoration verified by Pollard Spares

LLC, Director of Maintenance: Mark Eubanks A&P: 522924154 on 1111512013) Gear has 9476 cycles.

Next restoration due 0612021

85. 321086 Restoration of RIH MLG assembly was CIW by Jet Harbor Inc. on June 27, 2011 (Restoration verified by Pollard Spares

LLC, Director of maintenance: Mark Eubanks A&P: 522924154 on 1111 512013) Gear has 9476 cycles.

Next restoration due 0612021

86. 322081 Restoration of NLG assemby was CIW by Jet Harbor Inc, on June 27th 2011 (Restoration was verified by Pollard Spares, Ll

DOM A&P # 522924150 on 1111512013) & (Inspected by Advantage Aviation Technologies CRS # GQRR443L on 10125113)

NLG has 9476 Cycles. Next restoration due 0612021

87. (F1) omplied by Jet Harbor Inc. (Verified by Pollard Spares LLC. DOM Mark Eubanks A&P # 522924150

on 1111 512013)

Advantage Aviation Technologies. LLC. SCR # GQRR443L

88. 321071 Detailed inspection of left MLG was done by Advantage Aviation Technologies , LLC, on 10-25-2013

Gear has 9476 cycles.

89. 321076 Detailed inspection of right MLG was done by Advantage Aviation Technologies , LLC, on 10-25-2013

Gear has 9476 cycles.

90. 322071 Detailed inspection of the NLG was done by Advantage Aviation Technologies , LLC, on 10-25-2013

under WO# LG331612

Tropic Radio Inc. CRS # RZ4R510M

91. 341069 Calibrated No.2 Air data computer. Date of calibration 01115114.

92. 345116 Functional test right transponder. Date of calibration 01115114

93. 349066 Calibrate standby altimeter. Date of calibration 01115114

94. 341031 Calibrate pilot altimeter. Date of calibration 01115114

95. 341036 Calibrate copilot encoding altimeter. Date of calibration 01115114

96. 341067 Funtional test No. 1 ADC. Date of calibration 0111512014

97. 341066 Calibrate No. 1 Air data computer. Date of calibration 0111512014

98. 341070 Funtional test to No. 2 ADC. Date of calibration 01115114

99. 341111 Pressure leak test pilot I static & temparature sensing systems

100. 345111 Functional test left transporder. Date of calibration 0111512014

Other Vendors

101. 351061 Restore pilot 02 Mask assembly. COMPLIED BY AMERON GLOBAL PRODUCT SUPPORT, CRS: OWR461N,

COMPLY DATE 10108113.

Removed & replaced oxygen mask PIN OFF: MC10-13-03, SIN OFF:25840; SIN ON: 96179

102. 351066 Restore copilot 02 Mask assembly. COMPLIED BY LAURENCE WALTER AEROSPACE SOLUTIONS LLC,

CRS: 2LWR432B

DATE February 26, 2014 TOTAL TIME 9583.35

ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT I ENGINE WAS PERFORMED IN ACCORDANCE WITH MAJESTIC JET FALCON 10 AAIP AND CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED.

SIGNED ~ George Glen- A&P # 2730175

I.

Accomollshed the following tasks

1 Ran aircraft engines for preservation

DATE March 1, 2014

r. 3026

TOTAL TIME 9584.65

ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT I ENGINE WAS PE~F=ORMED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION.

SlGNED


Challenger 601 AFTT: 9583.35

SIN 3025 LANDINGS: 5152

N997GC March 7. 2014

1. Replaced cabin and cockpit carpet with AlP Charlie, Gobi Beige 2215 wool carpet. Roll #0408312, Invoice #CF108787, Test ID #6260, Project #SP0256WI-Q-F09999 from Aircraft Interior Products dated 11/26/13.

2. Recovered one (1) 3 place divan with Donghia Fabric: Item #B 10221 009 Paddington, color Ash. Flame treated by Applikators Plus. Certificate #SA0056183, Test Report# 51246 dated 02/25/14.

The above materials meet the requirements of F.A.R. 25.853 (a) With respect to the work perform , t aircraft is approved for return to service.

Mike Schmitzer·L.-L.S~~L:t~2a~~~--A&P 3454326 PRO Aircraft Interiors, nc. Pompano Beach, FL 33060

----------------------------~-----------------end __________________________________________ __

'WO<l(DIYWIQYE P.L IPE )f_o/I)lrrlOJf

Registration Number I Aircraft Type Serial Number 1 Landings Total Time

N997GC I CL-601 3025 I 5154 9584.65


1 Removed & replaced stab aug computer. P/N: 4031475-805, S/N OFF: 82010240,5/N ON: 81040185

2 Removed and replaced APU fuel pump with customer supplied pumpP/N:600-62966-21.S/N:ON 122M,OFF:574.

3 Removed & replaced No. 3A pump, P/N: 63108-06, S/N OFF: 2207798- S/N ON: 255759

4 Removed & replaced No. 3A pump motor, P/N: 62613, S/N OFF: RJ1542- S/N ON: YA334

5 Removed & replaced L/H windshield new windshield. P/N OFF: 600-33030-2, S/N OFF: 10095

P/N ON: 158700-59, S/N ON: 12163

6 Removed and replaced APU fuel filter P/N:7511283

7 Removed and replaced APU oil filter P/N:WF335135

8 Removed & replaced No. 3A pump line with customer supplied line. P/N: AE4186G0210-000

9 Removed & replaced L/H coalescer bag. P/N: 21BC112

10 Removed & replaced R/H coalescer bag. P/N: 21BC112

11 Removed & replaced R/H taxi light. P/N: 4587

For further details see WO 14-

DATE April 2, 201 TOTAL TIME 9584.65

ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT I ENGINE WAS PERFORMED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED.

SIGNED

George Glen A&P 2730175 I

\ • j

EXECUTIVE JET

DESIGNS INC. (561) 577-3729

LOGBOOK SUPPLEMENT

Make: Canadair Model: Challenger CL-600-2A12

Serial #: 3025

Base colors: Matterhorn White DuPont

Stripes (3): Silver, Blue, and Gold DuPont

June 11, 2014

Reg #: N997GC

The aircraft was stripped and painted in the above colors. Flight controls were not removed. All work was

performed in accordance ~ith .m~facturer's specifications.

~ ~~~ · ~3=57~4=86=3~--------------------Carlos Lugo ~ ' ~ A&P License Number

Processed by: JESSL YN CLEMENTE

pPerator: SKY HIGH AIR L.L.C. Work card No.: 12·2G-OG-320

erial No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.: /11.-036

Date A/CHRS AA.. APH

Due At

Accomplished 61if/l~ 9560·2- Sl5b I I

lEO<NIOAN SIG"?Jlf#~ KINDDFCEiffiFICATl'. No.·Lf/2~/j INSPEcrED BY:_, • .,..LV'--I~J.'--'~"""-::.__...:::::::.,...~"""'"---f--------KIND OF CERTIFicATE & No.·...f£.= f g& ftJ 5 ~ V V

12-2Q-OD-320 OPTJONAL

LUBRICATION OF THE SERVIONG DOOR LOCKS

I TEOi LABOR-HRS

INSP · HRS.lliS

P1L- __

~M~: --------~~~~~~~--~--------------------------------------~~---

DMBARDIERl AND CHAilfNGERl ARE TRADEMARKS OF BOMBARDIER. INC..

17-JUN-2014 Return completed copy via email to [email protected]

© CAMP SYSTEMS 1 of 2 Total Pages-__ _, Initial __ •


{0

\,.Operator: SKY HIGH AIR L.L.C. Work card No.: 24.150

erial No.: 3025 Model: CL-601 1eg No.: N997GC Workorder No.: /4 - CJ3-(.


Due At

Accomplished b /17-1/.y q.s:zc )..- .5/Sb I I

1

KIND OF CERTIACATE & NO.· ~ f u 6 'J-«..t S'"

KINDOFCERTIFICATE&NO.· ~p l(, ~tf 2.,{, V

242114 . CHECK AIR DRIVEN GENERATOR SYSTEM OIL LEVEL AND FOR OIL LEAKAGE

I TEOi INSP LABOR-HRS

HRS.THS

~~=--------------------------------------------------------------------------AMM 24-23-QO

---- __ ... -

JOI'I!li\RDIERl ANI> OIAUENGERi. ARE TRADEMARKS Of BOMBARDIER, INC.


© CAMP SYSTEMS 1 of 2 Total Pages= __ _, Initial __


CHECK CURRENT DUE UST FOR DUE TlME CHANGES

! Operator: SKY HIGH AIR LLC. Work Card No.: 24.230

) Serial No.: 3025 Model: CL-601 Reg No.: N997GC Workorder No.: J4 - o3~.

Date NCHRS AFL APH

Due At 07-JUL-2014 -

Accomplished b l!gfr'ct .-qB5b· 2. 51S"'b I

>243051 CAPAaTY TEST/ELECTROLYTE CHECK NO.1 MAIN BATTERY I 1('4 D (24-33-00-212) (REF. CMM/PSP 608/608A 24-30-99 OR ~ - -- - -- -- ----24-32·05, AS APPUCABLE; CHECK, PERIODIC CHECK) .

~:~~---~~~==~~~~~~==~~~~~~-~~~~~~==~~==~~ CA.:? ~~C- i)1f)\)r-~ Prul?F t>l' E~~~ AMM2+3Hl0

1101'41JMDIERt M D CJWlEitGERL ARE TRADEMARKS OF BOMBARDIER, lftC.

26-JUN-2014

Retum completed copy via email to [email protected] > INDICATES DUE ITEMS

© CAMP SYSTEMS 2 of 3 Total Pages = __ _. Initial __


Operator: SKY HIGH AIR L.l.C. Work Card No.: 239656

erial No.: 3025 Model: Cl-601 eg No.: N997GC Workorder No.: I Lj- D 3 (17


Due At

Accomplished ()(p Jg. d )'--1 8f56l .:z; sro6

KIND OF CERTIACATE & NO.· ,4--Zf 4 ' (p J' 2..--£L <e INSPECfEDBY:-----------------KINDOFCERTIACATE&NO.;....· ---------------

239656 RJNCTIONAL DiECK CVR ULO BATTERY

REMARKS : f?-&.r\a.c~ \)v,e t\&\. od a.olq

HBARDIERl NIO OIAI.l.EftGERl liRE TRAOB1ARK5 Of 80MBARDIER. lllC.


© CAMP SYSTEMS

LABOR-HRS . TEOi INSP HRS.THS

lfJJJ(_ ··-----

1 of 1 Total Pages= __ _. Initial __


L Operator: SKY HIGH AIR L.LC. Work Card No.: 349220

Serial No.: 3025 Model: CL-601 eg No.: N997GC Workorder No.: 14 - ().3(-.


Due At -

Accomplished 6 ?)...j-1 v Cft;;l3~·z ::;,~b

TECHNICIAN SIGNAllJRf:;._· ___,7:l£hrl-f-.:J....:lifs(IL-!!.l..<.!:::.r_~-------- KIND OF CERTIACATE &. NO •. :_· ....:./I..:....LJI.:....~__:::::;):..._7:....:~=[J~/--'A~UL_-_____ _

INSPECTED BY:-----------------KIND OF CERTIFICATE & NO.:_· ---------------

349220 CAPAOTY TEST/ELECTROLYTE CHECK NO. 1 INS BATTERY

RfMARKS : ~\Li(_O~\ h ~ h<!i£0, e<c\ 'i:O I <f

I TECH INSP LABOR~HRS

HRS.TIIS

--14----t4:nJJF:::.;- 1-c~<£~ -ffv P/aoe ct' /z;-r/P~;/._. _____ _ _ _ _

IIOHBAADIERL AIID Q!Al.l£NGERi. ARE TRADEMARJCS Of BOMBARDIER, INC.


© CAMP SYSTEMS 1 of 2 Total Pages - ---' Initial

I ..... , ............. tf997GC I



DATE June 23, 2014

l ~Jiumber 3025

TOTAL TIME

! ·~·~ ~;Jllne I 5156 9586.2

9586.2


SIGNED {~ George Glen A&P 2730175

3025

1 Ran aircraft engines for preservati

DATE TOTAL TIME 9586.2

ALL MAINTENANCE PERFORMED ON THIS IRCRAFT I ENGINE WAS PERFORMED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FEDERA AVIATION ADMINISTRATION.

SIGNED


WO!Rj:cDWJ([YE P.LIPE }lo/J}lr[JO:N

· Rllgliltlllllon NumiMir Alrcnlll Type 8eNI Number ......... TOiall'lme r-H - r 1 ·' 1 I N997GC CL-601 3025 5156 9586.~ Accomplished the following tasks


DATE August 12, 2014 TOTAL TIME 9586.2


SIGNED !i/1iJl.Lc-George Glen A&P 2730175 I

~ dj~ aircraft serial#: 3025

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