CESCOM 10 - Aircraft Status Report...CESCOM 10 - Aircraft Status Report Tracking Rate Average Daily...

CESCOM 10 - Aircraft Status Report

Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:

Aircraft Serial: 525A-0200 Unit: Reg No: N200FT

10:33PM09-May-2016

Part Number

Part Serial No

Item Code Description C/W Time 1 TBO 1

Drawing # / Task # City Mod Lvl C/W Time 2 TBO 2Position

Remains

RemainsTSO 2

TSO 1

Maintenance Inspections

DUE 1

DUE 2

Adj.

+ or -

5-12-01 INSPECTION DOCUMENT 1 (INTERVAL 1A)

COU

04-Jun-2015MTH

38513003551HRS 127.4

3128LDG

5-12-02 INSPECTION DOCUMENT 2 (INTERVAL 1C)

SMF

31-Jul-20161207-Jul-2015MTH 2 m 22 d

3571.8HRS

3141LDG

B262201 WEIGHT CHECK PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 2 (INTERVAL 1C)

10633

Y-96496

CABIN

5-12-02

SMF 31-Jul-20161207-Jul-2015MTH 2 m 22 d

3571.8HRS

3141LDG

B262201 WEIGHT CHECK PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 2 (INTERVAL 1C)

A352TS

W746327

COCKPIT

5-12-02

SMF 31-Jul-20161207-Jul-2015MTH 2 m 22 d

3571.8HRS

3141LDG

5-12-03 INSPECTION DOCUMENT 3 (INTERVAL 2C) N/A


SMF

3617-Jul-2015MTH

3584.1HRS

3152LDG

A323101 RESTORATION (HYDROSTATIC TEST) PNEUMATIC BLOWDOWN/EMERGENCY BRAKE BOTTLE : INSPECTION DOCUMENT 4

(INTERVAL 3C)

40005320-2

7304

SMF 31-Oct-20173631-Oct-2014MTH 17 m 22 d

5-12-05 INSPECTION DOCUMENT 5 (INTERVAL 5C) 60MTH

HRS

LDG

B262002 HYDROSTATIC TEST FIRE EXTINGUISHER BOTTLE : INSPECTION DOCUMENT 5 (INTERVAL 5C)

30401102-2 -

9912048-6

60937B1

LEFT ENGINE LFPB 01-Dec-20186026-Feb-2014MTH 30 m 22 d

3385.63HRS

3014LDG

B262002 HYDROSTATIC TEST FIRE EXTINGUISHER BOTTLE : INSPECTION DOCUMENT 5 (INTERVAL 5C)

30401102-2

49522B1

RIGHT ENGINE 01-Feb-20186014-Mar-2013MTH 20 m 23 d

3036.27HRS

2728LDG


LFPB

7225-Feb-2010MTH

2137.02HRS

1960LDG

A262201 SPECIAL DETAILED INSPECTION PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 6 (INTERVAL 6C)

10633

Y-96496

CABIN 31-Jan-20177201-Jan-2011MTH 8 m 22 d

A262201 SPECIAL DETAILED INSPECTION PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 6 (INTERVAL 6C)

A352TS

W746327

COCKPIT SCK 28-Feb-20227225-Feb-2016MTH 69 m 19 d

5-12-07 INSPECTION DOCUMENT 7 (INTERVAL 12C) 14413-Mar-2004MTH

0HRS

0LDG

B262202 HYDROSTATIC TEST PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 7 (INTERVAL 12C)

10633

Y-96496

CABIN 31-Jan-202314401-Jan-2011MTH 80 m 22 d

B262202 HYDROSTATIC TEST PORTABLE FIRE EXTINGUISHER : INSPECTION DOCUMENT 7 (INTERVAL 12C)

A352TS

W746327

COCKPIT SCK 29-Feb-202814425-Feb-2016MTH 141 m 20 d

5-12-08 INSPECTION DOCUMENT 8 (INTERVAL 1A/2C)

COU

31-Mar-20172405-Mar-2015MTH 10 m 22 d

3822.73003522.7HRS 99.1

3102LDG

of 70NOTE: Item Codes in italics show pre-migration CESCOM item codes and position (provided for cross-reference). Remains calculated from Print

Date for calendar items.


Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016

Description C/W Time 1 TBO 1

Drawing # / Task # City Mod Lvl C/W Time 2 TBO 2

Remains


Remains

TSO 1

TSO 2

Item Code Part Number

Part Serial NoPosition

DUE 1

DUE 2

Adj.

+ or -


SMF

30-Apr-20193614-Apr-2016MTH 35 m 21 d

4872.312003672.3HRS 1148.7

3244LDG


SMF

30-Apr-20193614-Apr-2016MTH 35 m 21 d

4872.312003672.3HRS 1148.7

3244LDG

5-12-12 INSPECTION DOCUMENT 12 (14 CFR 91.207)

SMF

1207-Jul-2015MTH

3571.8HRS

3141LDG

A256002 DETAILED INSPECTION ELT TRANSMITTER : INSPECTION DOCUMENT 12 (14 CFR 91.207)

453-5000

02485

SMF 31-Jul-20161207-Jul-2015MTH 2 m 22 d

3571.8HRS

3141LDG

B256003 OPERATIONAL CHECK ELT TRANSMITTER EMERGENCY LOCATOR BEACON SYSTEM: INSPECTION DOCUMENT 12 (14 CFR

91.207)

453-5000

02485

SMF 31-Jul-20161207-Jul-2015MTH 2 m 22 d

3571.8HRS

3141LDG

5-12-13 INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

SCK 2415-Feb-2016MTH

3669.2HRS

3240LDG

341060 FUNCTIONAL CHECK RVSM SKIN WAVINESS: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

341066 CALIBRATION TEST AIR DATA COMPUTER FAR 91.411: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

822-1109-004

18F9D

LEFT SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

341068 CALIBRATION TEST AIR DATA COMPUTER FAR 91.411: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

822-1109-004

1CMHX

RIGHT SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

341074 CALIBRATION TEST ALTIMETER/AIRSPEED INDICATOR FAR 91.411: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND

RVSM)

WL102AMS6

AL533

STANDBY SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

B341001 FUNCTIONAL CHECK PITOT-STATIC SYSTEM: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

LEFT SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

B341001 FUNCTIONAL CHECK PITOT STATIC SYSTEM: INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM)

RIGHT SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

B345001 CALIBRATION TEST TRANSPONDER NO. 1 TRANSPONDER FAR 91.413 (EXCEPT PHILLIPINES CERTIFIED AIRPLANES):

INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM

011-00455-30

84405538

NO. 1 SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

B345001 CALIBRATION TEST TRANSPONDER NO. 2 TRANSPONDER FAR 91.413 (EXCEPT PHILLIPINES CERTIFIED AIRPLANES):

INSPECTION DOCUMENT 13 (CFR 91.411, 91.413, AND RVSM

011-00455-30

84405545

NO. 2 SCK 28-Feb-20182415-Feb-2016MTH 21 m 19 d

5-12-14 INSPECTION DOCUMENT 14 A/R06-May-2007MTH

1260HRS

A324103 SPECIAL DETAILED INSPECTION WHEEL ASSEMBLY LANDING GEAR WHEELS (NDI): INSPECTION DOCUMENT 14

3-1601-3

1343

LEFT MAIN GEAR KISM T/C08-May-2015MTH

3546.2HRS

3120LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


3-1418/6342110-2

6109

NOSE LANDING GEAR T/CDAYS


3-1601-3

1372

RIGHT MAIN GEAR KISM T/C08-May-2015MTH

3546.2HRS

3120LDG

5-12-17 INSPECTION DOCUMENT 17

SMF

1214-Apr-2016MTH

1003672.3HRS

3244LDG

D243201 CAPACITY CHECK BATTERY NICKEL-CADMIUM BATTERY FUNCTIONAL CHECK (NOTE: THE INSPECTION INTERVAL CAN BE

ADJUSTED AFTER THE AVERAGE BATTERY WATER DECREASE PER CELL IS FOUND : INSPECTION DOCUMENT 17

30978-002

10503120

SMF 30-Apr-20171214-Apr-2016MTH 11 m 21 d

3772.31003672.3HRS 48.7

3244LDG


LFPB

A/R09-Aug-2012MTH

2942.13HRS

2636LDG

5-12-19 INSPECTION DOCUMENT 19 A/R13-Mar-2004MTH

5-12-21 INSPECTION DOCUMENT 21 (INTERVAL 2A/2C) 31-Aug-20162411-Aug-2014MTH 3 m 22 d

4049.16003449.1HRS 325.5

3062LDG

5-12-24 INSPECTION DOCUMENT 24 (INTERVAL1A/1C)

SMF

31-Jul-20161207-Jul-2015MTH 2 m 22 d

3871.83003571.8HRS 148.2

3141LDG

5-12-25 INSPECTION DOCUMENT 25 13-Mar-2004MTH

400040000HRS 276.4


SMF

31-Oct-2016614-Apr-2016MTH 5 m 22 d

3672.3HRS

3244LDG

5-12-MA INSPECTION DOCUMENT MA (CHAPTER 4)

SMF

14-Apr-2016MTH

3972.33003672.3HRS 248.7

3244LDG

5-12-MC INSPECTION DOCUMENT MC (CHAPTER 4)

COU

05-Mar-2015MTH

4722.712003522.7HRS 999.1

3102LDG

5-12-MD INSPECTION DOCUMENT MD (CHAPTER 4)

LFPB

04-May-2011MTH

3961.3814252536.38HRS 237.78

2314LDG

5-12-ME INSPECTION DOCUMENT ME (CHAPTER 4) 13-Mar-2004MTH

500050000LDG 1696

5-12-MF INSPECTION DOCUMENT MF (CHAPTER 4)

LFPB

04-May-2011MTH

5086.3825502536.38HRS 1362.78

2314LDG

5-12-MG INSPECTION DOCUMENT MG (CHAPTER 4) 04-Jan-2012MTH

5594.1828002794.18HRS 1870.58

2507LDG

5-12-MH INSPECTION DOCUMENT MH (CHAPTER 4) 27-May-2013MTH

6198.2831003098.28HRS 2474.68

2782LDG

5-12-MI INSPECTION DOCUMENT MI (CHAPTER 4) 13-Mar-2004MTH

495049500HRS 1226.4

5-12-MJ INSPECTION DOCUMENT MJ (CHAPTER 4) 13-Mar-2004MTH

500050000HRS 1276.4




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

5-12-MK INSPECTION DOCUMENT MK (CHAPTER 4) 13-Mar-2004MTH

505050500HRS 1326.4

5-12-ML INSPECTION DOCUMENT ML (CHAPTER 4) 13-Mar-2004MTH

505050500HRS 1326.4

5-12-MM INSPECTION DOCUMENT MM (CHAPTER 4) 13-Mar-2004MTH

600060000HRS 2276.4

A545001 INSPECT FORWARD AND AFT ENGINE MOUNT CHANNELS, INBOARD AND OUTBOARD FLANGES (AIRPLANES 0300 AND ON):

INSPECTION DOCUMENT MM (CHAPTER 4)

N/R13-Mar-2004MTH

5-12-MP INSPECTION DOCUMENT MP (CHAPTER 4) 13-Mar-2004MTH

862886280HRS 4904.4

052001 FJ44 CHECK 1

E1

UNK

14-Apr-2015MTH

3840.93003540.9HRS 117.3

3112LDG

052001 FJ44 CHECK 1

E2

UNK

06-Apr-2015MTH

3840.93003540.9HRS 117.3

3112LDG

052002 FJ44 CHECK 2

E1

UNK

14-Apr-2015MTH

4140.96003540.9HRS 417.3

3112LDG

052002 FJ44 CHECK 2

E2

UNK

06-Apr-2015MTH

4140.96003540.9HRS 417.3

3112LDG

723021 VISUALLY INSPECT THE INSTALLED SPINNER

E1

UNK

14-Apr-2015MTH

4140.96003540.9HRS 417.3

3112LDG

723021 VISUALLY INSPECT THE INSTALLED SPINNER

E2

UNK

06-Apr-2015MTH

4140.96003540.9HRS 417.3

3112LDG

753010 INSPECT ACCELERATION BLEED SYSTEM

E2

UNK

06-Apr-2015MTH

4140.96003540.9HRS 417.3

3112LDG

052003 FJ44 CHECK 3

E1

03-Nov-2008MTH

13541.3120001754.72HRS 9817.7-213.42

1626LDG

052003 FJ44 CHECK 3

E2

03-Nov-2008MTH

13657.9120001871.32HRS 9934.3-213.42

1706LDG

052004 FJ44 CHECK 4

E1

UNK

14-Apr-2015MTH

15541.28120003540.9HRS 11817.68.38

3112LDG

052004 FJ44 CHECK 4

E2

UNK

06-Apr-2015MTH

15541.28120003540.9HRS 11817.68.38

3112LDG

052005 FJ44 CHECK 5

E1

13-Mar-2004MTH

5540.91200017.3HRS 1817.3-6476.4

052005 FJ44 CHECK 5

E2

13-Mar-2004MTH

5657.512000133.9HRS 1933.9-6476.4

052006 FJ44 CHECK 6

E1

13-Mar-2004MTH

7541.31200017.3HRS 3817.7-4476

052006 FJ44 CHECK 6

E2

13-Mar-2004MTH

7657.912000133.9HRS 3934.3-4476

052007 FJ44 CHECK 7

E1

13-Mar-2004MTH

9541.31200017.3HRS 5817.7-2476




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

052007 FJ44 CHECK 7

E2

13-Mar-2004MTH

9657.912000133.9HRS 5934.3-2476

052008 FJ44 CHECK 8

E1

13-Mar-2004MTH

11541.31200017.3HRS 7817.7-476

052008 FJ44 CHECK 8

E2

13-Mar-2004MTH

11657.912000133.9HRS 7934.3-476

351005 RESTORATION (HYDROSTATIC TEST) OXYGEN CYLINDER (DOT3HT1850 OR DOT3FC1850 OR ANY CYLINDER MANUFACTURED

UNDER DOT-E-8162)-OXYGEN BOTTLE AND REGULATOR ASSEMBLY

176274-50

2552-14503

COU 31-Jan-20206014-Jan-2015MTH 44 m 22 d

351006 RESTORATION (HYDROSTATIC TEST) OXYGEN BOTTLE (DOT3AA)-OXYGEN BOTTLE AND REGULATOR ASSEMBLY

5500-L6W-BEF23A

ST56602

PORTABLE EDDL 31-Aug-20186001-Aug-2013MTH 27 m 22 d

351006 RESTORATION (HYDROSTATIC TEST) OXYGEN CYLINDER (DOT3AA)-OXYGEN BOTTLE AND REGULATOR ASSEMBLY

EDDL 31-Aug-20186009-Aug-2013MTH 27 m 22 d

3186.08HRS

2841LDG

551010 INSPECT VERTICAL FIN FOR CRACKS AROUND FASTENERS,MAIN SPAR CAP AT UPPERMOST ATTACHMENT HOLE #1

045501 13-Mar-2004MTH

15000150000HRS 11276.4

551020 INSPECT VERTICAL FIN FOR CRACKS AROUND FASTENERS,REAR SPAR CAP AT UPPERMOST ATTACHMENT HOLE #1

045502 13-Mar-2004MTH

11250112500HRS 7526.4

571010 INSPECT LEFT WING FRONT SPAR , WS 88.50

045701

13-Mar-2004MTH

12000120000HRS 8276.4

571015 INSPECT RIGHT WING FRONT SPAR, WS 88.50

045701

13-Mar-2004MTH

12000120000HRS 8276.4

571020 INSPECT LEFT WING MAIN SPAR, WS 61.50

045702

13-Mar-2004MTH

12500125000HRS 8776.4

571025 INSPECT RIGHT WING MAIN SPAR, WS 61.50

045702

13-Mar-2004MTH

12500125000HRS 8776.4


045703

13-Mar-2004MTH

12000120000HRS 8276.4


045703

13-Mar-2004MTH

12000120000HRS 8276.4


045704

13-Mar-2004MTH

12000120000HRS 8276.4


045704

13-Mar-2004MTH

12000120000HRS 8276.4

571050 INSPECT LEFT WING MAIN SPAR, WS 171.00 (INBOARD)

045705

13-Mar-2004MTH

13000130000HRS 9276.4

571055 INSPECT RIGHT WING MAIN SPAR, WS 171.00 (INBOARD)

045705

13-Mar-2004MTH

13000130000HRS 9276.4

571060 INSPECT LEFT WING REAR SPAR, WS 136.65

045706

13-Mar-2004MTH

13000130000HRS 9276.4

571065 INSPECT RIGHT WING REAR SPAR, WS 136.65

045706

13-Mar-2004MTH

13000130000HRS 9276.4

571070 INSPECT LEFT WING REAR SPAR, WS 154.00

045707

13-Mar-2004MTH

13000130000HRS 9276.4

571075 INSPECT RIGHT WING REAR SPAR, WS 154.00

045707

13-Mar-2004MTH

13000130000HRS 9276.4

571080 INSPECT LEFT WING MAIN SPAR SPLICE, WS 111.00

045708

13-Mar-2004MTH

12000120000HRS 8276.4




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

571085 INSPECT RIGHT WING MAIN SPAR SPLICE, WS 111.00

045708

13-Mar-2004MTH

12000120000HRS 8276.4

571090 INSPECT LEFT WING REAR SPAR SPLICE, WS 111.00

045709

13-Mar-2004MTH

12000120000HRS 8276.4

571095 INSPECT RIGHT WING REAR SPAR SPLICE, WS 111.00

045709

13-Mar-2004MTH

12000120000HRS 8276.4

571100 INSPECT LEFT WING FRONT STRINGER SPLICE, WS 111.00

045710 13-Mar-2004MTH

12000120000HRS 8276.4

571105 INSPECT RIGHT WING FRONT STRINGER SPLICE, WS 111.00

045710 13-Mar-2004MTH

12000120000HRS 8276.4

712085 INSPECT LEFT ENGINE FORWARD ENGINE MOUNT AFT CHANNEL WEB

047103 13-Mar-2004MTH

15000150000HRS 11276.4

712090 INSPECT RIGHT ENGINE FORWARD ENGINE MOUNT AFT CHANNEL WEB

047103 13-Mar-2004MTH

15000150000HRS 11276.4

712095 INSPECT LEFT ENGINE FORWARD ENGINE MOUNT FORWARD CHANNEL WEB

047104 13-Mar-2004MTH

12000120000HRS 8276.4

712100 INSPECT RIGHT ENGINE FORWARD ENGINE MOUNT FORWARD CHANNEL WEB

047104 13-Mar-2004MTH

12000120000HRS 8276.4

712105 INSPECT LEFT ENGINE AFT ENGINE MOUNT

047107

13-Mar-2004MTH

15000150000HRS 11276.4

712110 INSPECT RIGHT ENGINE AFT ENGINE MOUNT

047107

13-Mar-2004MTH

15000150000HRS 11276.4

714005 INSPECT LEFT ENGINE FORWARD ENGINE BEAM AFT UPPER ANGLE COMMON TO AFT WEB, BL 34.90

047101 13-Mar-2004MTH

862886280HRS 4904.4

714010 INSPECT RIGHT ENGINE FORWARD ENGINE BEAM AFT UPPER ANGLE COMMON TO AFT WEB, BL 34.90

047101 13-Mar-2004MTH

862886280HRS 4904.4

714015 INSPECT LEFT ENGINE FORWARD ENGINE BEAM AFT WEB UPPER EDGE, BL 26.56

047102 13-Mar-2004MTH

15000150000HRS 11276.4

714020 INSPECT RIGHT ENGINE FORWARD ENGINE BEAM AFT WEB UPPER EDGE, BL 26.56

047102 13-Mar-2004MTH

15000150000HRS 11276.4

714035 INSPECT LEFT ENGINE FORWARD ENGINE BEAM AT ATTACHMENT TO FUSELAGE

047105 13-Mar-2004MTH

15000150000HRS 11276.4

714040 INSPECT RIGHT ENGINE FORWARD ENGINE BEAM AT ATTACHMENT TO FUSELAGE

047105 13-Mar-2004MTH

15000150000HRS 11276.4

714045 INSPECT LEFT ENGINE AFT ENGINE BEAM AT ATTACHMENT TO FUSELAGE

047106 13-Mar-2004MTH

15000150000HRS 11276.4

714050 INSPECT RIGHT ENGINE AFT ENGINE BEAM AT ATTACHMENT TO FUSELAGE

13-Mar-2004MTH

15000150000HRS 11276.4




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Components

DUE 1

DUE 2

Adj.

+ or -

211001 PRESSURE SHUTOFF VALVE

5253-00-1

1237

LEFT

ICT

0O/C10-Aug-2014MTH

03448.1HRS

03061LDG

211001 PRESSURE SHUTOFF VALVE

5253-00-1

1446

RIGHT

ICT

0O/C10-Aug-2014MTH

03448.1HRS

03061LDG

211002 VARIABLE VALVE

2601-21

0813

LEFT

0O/C13-Mar-2004MTH

211002 VARIABLE VALVE

2601-21

0815

RIGHT

0O/C13-Mar-2004MTH

211003 PRESSURE HEAT EXCHANGER

10840A

843

0O/C13-Mar-2004MTH

211005 EMERGENCY PRESSURE SHUTOFF VALVE

2601-23

0432

9912422-2

0O/C13-Mar-2004MTH

212001 BAGGAGE COMPARTMENT BLOWER

0113-12

0785

0O/C13-Mar-2004MTH

212003 (STO29) TEMPERATURE SWITCH

1173T42-1

341

0O/C13-Mar-2004MTH

212302 WINDSHIELD AIR BLOWER MOTOR

7003-200

0977

0O/C13-Mar-2004MTH

213001 PRIMARY OUTFLOW VALVE

52771-316

K897A

9912409-20 LFPB

98O/C25-Feb-2010MTH

30392137.02HRS

41960LDG

213002 SECONDARY OUTFLOW VALVE

52772-116

1025

9912409-15

0O/C13-Mar-2004MTH

213003 PRESSURE CONTROLLER

52770-116

1842

9912409-13

0O/C13-Mar-2004MTH

213005 DIFFERENTIAL PRESSURE INDICATOR

C668511-0106

22580

3001J73

0O/C13-Mar-2004MTH

213008 MANUAL PRESSURE SWITCH

52773-001

1463

9912409-4

0O/C13-Mar-2004MTH

215000AFT BLOWER MOTOR AFT EVAPORATOR

1133210-7

1747

SMF

0O/C17-Jul-2015MTH

03584.1HRS

03152LDG

215000FWD BLOWER MOTOR FWD EVAPORATOR

1260185-1

SN-UNKNOWN

0O/C13-Mar-2004MTH

215001 FORWARD EVAPORATOR

1134300-3

262

9912583-9

0O/C13-Mar-2004MTH

215002 AFT EVAPORATOR

1134820-15

1155

9912583-10 SMF

0O/C17-Jul-2015MTH

03584.1HRS

03152LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

215003 VAPOR CYCLE COMPRESSOR DRIVE MOTOR

1134146-1

746A

LFPB

003-Apr-2012MTH

02844.6HRS

02557LDG

4851030001851ACH 2454.5

215005 CONDENSOR ASSEMBLY

1134620-3

310

9912583-7

0O/C13-Mar-2004MTH

215007 RECEIVER DRYER ASSEMBLY

1134275-1

SN-UNKNOWN

9912583-3 SMF

0A/R17-Jul-2015MTH

03584.1HRS

03152LDG

215008 COMPRESSOR ASSEMBLY

1134130-5

733

LFPB

12O/C16-Jun-2010MTH

02238.03HRS

02057LDG

215009 AXIAL BLOWER VANE

1250435-5

3750

0O/C14-Dec-2012MTH

03007.88HRS

02702LDG

215010 AIR CONDITIONING FLIGHT HOURMETER

1250703-3

SN-UNKNOWN

0O/C13-Mar-2004MTH

215011 COMPRESSOR DRIVE BELT

225L100

SN-UNKNOWN

LFPB

0O/C16-Jun-2010MTH

02238.03HRS

02057LDG

215012 VAPOR CYCLE COMPRESSOR DRIVE MOTOR BRUSHES

1251171-6

NSN

LFPB

010-Oct-2013MTH

03248.52HRS

02893LDG

267905002179ACH 282.5

215060 COMPRESSOR DRIVE

1134610-1

321

215004

0O/C13-Mar-2004MTH

216001 RAM AIR MODULATING VALVE

27241287-15

8AR35E

LSZH

0O/C20-Jan-2011MTH

02464.67HRS

02258LDG

216002 TEMPERATURE CONTROLLER

1E58-7

1AW17

0O/C13-Mar-2004MTH

216003 (TC007) SENSOR

27221274

9AW310

AFT 9912085-3

0O/C13-Mar-2004MTH

216003 (UT006) SENSOR

27221274

10AW340

FORWARD 9912085-3

0O/C13-Mar-2004MTH

221002 SERVO MOUNT

622-5735-021

18YWD

AILERON

0O/C13-Mar-2004MTH

221002 SERVO MOUNT

622-5735-022

13F5H

ELEVATOR

0O/C13-Mar-2004MTH

221002 SERVO MOUNT

622-5735-022

18TKN

RUDDER

0O/C13-Mar-2004MTH

221003 SERVO

822-1168-002

1BXWT

AILERON SVO-3000

0O/C13-Mar-2004MTH

221003 SERVO

822-1168-001

1C6VC

ELEVATOR SVO-3000

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

221003 SERVO

822-1168-001

128TF

RUDDER SVO-3000

0O/C13-Mar-2004MTH

221004 AUTOPILOT PANEL

622-6208-223

1BT9K

0O/C13-Mar-2004MTH

231007 COMM 2 ANTENNA

17-40-02W

0848

BOTTOM

0O/C28-Jun-2005MTH

0483HRS

231007 COMM 1 ANTENNA

18-50-01

1167

TOP

LFPB

0O/C21-May-2014MTH

03430.87HRS

03055LDG

235001 AUDIO AMPLIFIER

5636-1

1136

LEFT S3100-63

44O/C03-Nov-2008MTH

1358.41737.42HRS

1626LDG

235001 AUDIO AMPLIFIER

5636-1

1206

RIGHT S3100-63

0O/C01-Feb-2013MTH

03023.72HRS

02719LDG

237003 CVR MICROPHONE

S055-0065-00

000247279

0O/C13-Mar-2004MTH

237004 CVR IMPACT SWITCH

6895D2-X-5-5

4382

0O/C13-Mar-2004MTH

243001 BATTERY TEMP INDICATOR

1229-1

3030

0O/C13-Mar-2004MTH

243003 GENERATOR CONTROL UNIT

51525-001F

Y3402

LEFT

LFPB

O/C24-Mar-2014MTH

3413.47HRS

3040LDG

243003 GENERATOR CONTROL UNIT

51525-001F

Y3401

RIGHT

LFPB

O/C24-Mar-2014MTH

3413.47HRS

3040LDG

243004 BATTERY TEMP MONITOR

1529-1-1

4035

0O/C13-Mar-2004MTH

243006 GENERATOR LOAD AMMETER

C662501-0107

J23577

LEFT

0O/C13-Mar-2004MTH

243006 GENERATOR LOAD AMMETER

C662501-0107

K23977

RIGHT

0O/C13-Mar-2004MTH

243007 BATTERY

30978-002

10503120

9914058-6 COU

2O/C04-Jun-2015MTH

24.53551HRS

3128LDG

243008 BATTERY RELAY

A931F

50488

0O/C13-Mar-2004MTH

243011 DC POWER VOLTMETER

C662502-0101

D21212

0O/C30-Jul-2004MTH

0149HRS

245003 IGNITOR CONTROL P.C.B.

6318322-4

SN-UNKNOWN

LEFT

0O/C13-Mar-2004MTH

245003 IGNITOR CONTROL P.C.B.

6318322-4

SN-UNKNOWN

RIGHT

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

245011 FUEL FLOW P.C.B

85-230-2

0314107A

0O/C13-Mar-2004MTH

245020 OVERVOLTAGE DETECTOR

1645-1-3

3326

0O/C13-Mar-2004MTH

25-CUS-001 MEDAIRE FIRST AID KIT

P8-02-0004-209

000357

COU

30-Nov-20170DUE17-Mar-2015MTH 18 m 21 d

0DUE3524.4HRS

0DUE3104LDG

DUE

Expiration Date: 30-Nov-2017

256001 ELT TRANSMITTER

453-5000

02485

C406-2

O/C03-Nov-2008MTH

1737.42HRS

1626LDG

256002 ELT BEACON BATTERY PACK

452-0133

N/A

LFPB

01-Jan-201746006-May-2012MTH 7 m 23 d

02874.35HRS

02580LDG

256003 REMOTE SWITCH

452-0010

SN-UNKNOWN

0O/C13-Mar-2004MTH

256004 ELT ANTENNA

110-328-01

3783

0O/C13-Mar-2004MTH

256006 LIFE VEST

P01074-103

12072040053

CO-PILOT

01-Aug-20170DUE26-Feb-2014MTH 14 m 23 d

0DUE3385.63HRS

0DUE3014LDG

DUE

Expiration Date: 01-Aug-2017

256006 LIFE VEST

P01074-103

13103380019

NO. 1

19-Nov-20180DUE26-Feb-2014MTH 30 m 10 d

0DUE3385.63HRS

0DUE3014LDG

DUE


256006 LIFE VEST

P01074-103

13103380016

NO. 2

19-Nov-20180DUE26-Feb-2014MTH 30 m 10 d

0DUE3385.63HRS

0DUE3014LDG

DUE


256006 LIFE VEST

P01074-103

13103380017

NO. 3

19-Nov-20180DUE26-Feb-2014MTH 30 m 10 d

0DUE3385.63HRS

0DUE3014LDG

DUE


256006 LIFE VEST

P01074-103

13103380018

NO. 4

19-Nov-20180DUE26-Feb-2014MTH 30 m 10 d

0DUE3385.63HRS

0DUE3014LDG

DUE


256006 LIFE VEST

P01074-103

267701

NO. 5

01-Mar-20180DUE26-Feb-2014MTH 21 m 20 d

0DUE3385.63HRS

0DUE3014LDG

DUE

Expiration Date: 01-Mar-2018

256006 LIFE VEST

P01074-103

254253

NO. 6

01-Mar-20180DUE26-Feb-2014MTH 21 m 20 d

0DUE3385.63HRS

0DUE3014LDG

DUE

Expiration Date: 01-Mar-2018




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

256006 LIFE VEST

P01074-103

13103380028

PILOT

19-Nov-20180DUE26-Feb-2014MTH 30 m 10 d

0DUE3385.63HRS

0DUE3014LDG

DUE

256006A CREW LIFE VEST

P01074-103

13103380028

PILOT

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006B CREW LIFE VEST

P01074-103

12072040053

COPILOT

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006C PASSENGER LIFE VEST

P01074-103

13103380019

NO. 1

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006D PASSENGER LIFE VEST

P01074-103

13103380016

NO. 2

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006E PASSENGER LIFE VEST

P01074-103

13103380017

NO. 3

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006F PASSENGER LIFE VEST

P01074-103

13103380018

NO. 4

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

256006G PASSENGER LIFE VEST

P01074-103

254253

NO. 6

LFPB

O/C26-Feb-2014MTH

3385.63HRS

3014LDG

256006H PASSENGER LIFE VEST

P01074-103

267701

NO. 5

LFPB

O/C26-Feb-2014MTH

3385.63HRS

3014LDG

256007 GPS DIGITAL INTERFACE UNIT

453-6500

02917

0O/C13-Mar-2004MTH

261001 FIRE DETECTOR SENSOR

3001-212-1004/455-9

204861

LEFT 9912416-1

0O/C13-Mar-2004MTH

261001 FIRE DETECTOR SENSOR

3001-212-1004/455-9

4461XL2

RIGHT 9912416-1

0O/C13-Mar-2004MTH

262001 FIRE EXTINGUISHER BOTTLE

30401102-2 -

9912048-6

60937B1

LEFT ENGINE

LFPB

0O/C26-Feb-2014MTH

03385.63HRS

03014LDG

262001 FIRE EXTINGUISHER BOTTLE

30401102-2

49522B1

RIGHT ENGINE 9912048-6

0O/C14-Mar-2013MTH

03036.27HRS

02728LDG

262003 PORTABLE FIRE EXTINGUISHER

10633

Y-96496

CABIN

O/C17-Mar-2015MTH

262003 PORTABLE FIRE EXTINGUISHER

A352TS

W746327

COCKPIT

0O/C13-Mar-2004MTH

262010 FIRE EXTINGUISHER CARTRIDGE

13085-5

BATCH

ESD13H501-001

LEFT ENGINE NO.1

LFPB

01-Aug-20197226-Feb-2014MTH 38 m 23 d

3385.63HRS

3014LDG

Manufacture Date: 01-Jan-2012




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


13085-5

BATCH

ESD13H501-001

LEFT ENGINE NO.2

LFPB

01-Aug-20197226-Feb-2014MTH 38 m 23 d

3385.63HRS

3014LDG



13083-5

ESD13A459-001

RIGHT ENGINE NO.1

31-Jan-20197214-Mar-2013MTH 32 m 22 d

3036.27HRS

2728LDG



13083-5

ESD13A459-001

RIGHT ENGINE NO.2

31-Jan-20197214-Mar-2013MTH 32 m 22 d

3036.27HRS

2728LDG


272001 RUDDER BIAS VALVE

5307-1

1466C

0O/C05-Nov-2012MTH

02982.18HRS

02677LDG

273001 SHAKER CONTROL

201

5824

0O/C13-Mar-2004MTH

273002 ELEVATOR TRIM SERVO

44430-3548

T872

0O/C13-Mar-2004MTH

275001 SHUTOFF VALVE

4083-1

372

0O/C13-Mar-2004MTH

275002 FLAP ACTUATOR

1542000-7

1547

LEFT 9912365-5

0O/C13-Mar-2004MTH

275002 FLAP ACTUATOR

1542000-7

1546

RIGHT 9912365-5

0O/C13-Mar-2004MTH

276001 SPEED BRAKE ACTUATOR

1542100-5

1520

LEFT 9912375-4

0O/C13-Mar-2004MTH

276001 SPEED BRAKE ACTUATOR

1542100-5

1524

RIGHT 9912375-4

0O/C13-Mar-2004MTH

281001 SURGE TANK FLOAT VALVE

35C10D

2867

LEFT 9912016-2

0O/C13-Mar-2004MTH

281001 SURGE TANK FLOAT VALVE

35C10D

2860

RIGHT 9912016-2

0O/C13-Mar-2004MTH

282001 FUEL BOOST PUMP

1C7-13

1C713

LEFT 9912017-4

0O/C13-Mar-2004MTH

282001 FUEL BOOST PUMP

1C7-13

3AW53

RIGHT 9912017-4

0O/C13-Mar-2004MTH

282002 EJECTOR FUEL AFT PUMP

RG45310

B9098

LEFT 9912190-2

0O/C13-Mar-2004MTH

282002 EJECTOR FUEL AFT PUMP

RG45310

B9085

RIGHT 9912190-2

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

282003 SOLENOID VALVE

527700-103

0378

LEFT 9914470-3

0O/C13-Mar-2004MTH


527700-103

0394

RIGHT 9914470-3

0O/C13-Mar-2004MTH

282004 FUEL MOTOR VALVE

AV24B1507

1340

LEFT 9912014-3

0O/C13-Mar-2004MTH

282004 FUEL MOTOR VALVE

EM9014-3

1486

RIGHT 9912014-3

0O/C13-Mar-2004MTH

282005 EJECTOR FUEL FORWARD PUMP

RG45310

B9087

LEFT 9912190-2

0O/C13-Mar-2004MTH

282005 EJECTOR FUEL FORWARD PUMP

RG45310

B9083

RIGHT 9912190-2

0O/C13-Mar-2004MTH

282006 TRANSFER VALVE

ZSV57

308057

9914103-6

0O/C13-Mar-2004MTH

284001 #5 FUEL PROBE

10664T05Y00

0913

LEFT 9912589-5

0O/C13-Mar-2004MTH


10664T05Y00

0906

RIGHT 9912589-5

0O/C13-Mar-2004MTH


10664T06Y00

0957

LEFT 9912589-6

0O/C13-Mar-2004MTH


10664T06Y00

0875

RIGHT 9912589-6

0O/C13-Mar-2004MTH

284003 FUEL QUANTITY SIGNAL CONDITIONER

10663B01Y02

03080712

9912589-9

0O/C13-Mar-2004MTH


10664T03Y00

0917

LEFT 9912589-3

0O/C13-Mar-2004MTH


10664T03Y00

0885

RIGHT 9912589-3

0O/C13-Mar-2004MTH

284005 #4 INBOARD FUEL PROBE

10664T04Y00

1150

LEFT 9912589-4

0O/C13-Mar-2004MTH

284005 #4 INBOARD FUEL PROBE

10664T04Y00

1357

RIGHT 9912589-4

0O/C13-Mar-2004MTH


10664T02Y00

0844

LEFT 9912589-2

0O/C13-Mar-2004MTH


10664T02Y00

0928

RIGHT 9912589-2

0O/C13-Mar-2004MTH


10664T01Y00

0911

LEFT 9912589-1

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


10664T01Y00

0931

RIGHT 9912589-1

0O/C13-Mar-2004MTH

284009 #4 OUTBOARD FUEL PROBE

10664T04Y00

1359

LEFT 9912589-4

0O/C13-Mar-2004MTH

284009 #4 OUTBOARD FUEL PROBE

10664T04Y00

1358

RIGHT 9912589-4

0O/C13-Mar-2004MTH

291002 HYDRAULIC PUMP

24195-LAC

369

LEFT 9912062-6

0O/C13-Mar-2004MTH

291002 HYDRAULIC PUMP

24195-LAC

446

RIGHT 9912062-6

0O/C13-Mar-2004MTH

291005 HYDRAULIC RESERVOIR ASSEMBLY

6317001-59

SN-UNKNOWN

0O/C13-Mar-2004MTH

291006 LOADING VALVE

4134-4

632

9912423-39

0O/C13-Mar-2004MTH

291007 PRESSURE SWITCH GAUGE

GPP1250-301 -

9912373-6

1028310

LFPB

0O/C31-Jan-2014MTH

03375.98HRS

03006LDG

291008 HYDRAULIC MANIFOLD ASSY

8184-12

740

9912423-40

0O/C13-Mar-2004MTH

291009 RELIEF VALVE

2576-2 -

9912423-46

106A

LFPB

O/C12-Aug-2012MTH

2946.45HRS

2640LDG


AV24B1388-2

AA190438

LEFT 9912400-4 LFPB

0O/C09-Aug-2012MTH

02942.13HRS

02636LDG


AV24B1388-2

T91428

RIGHT 9912400-4 LFPB

0O/C09-Aug-2012MTH

02942.13HRS

02636LDG

291011 FLOW SWITCH VALVE

V10F14

863

LEFT 9912194-2

0O/C13-Mar-2004MTH

291011 FLOW SWITCH VALVE

V10F14

993

RIGHT 9912194-2

0O/C13-Mar-2004MTH

291012 SPEEDBRAKE DUMP VALVE

4082-6

359

9912423-33

0O/C13-Mar-2004MTH

291014 GEAR VALVE

4051-3

361

9912423-35

0O/C13-Mar-2004MTH

291016 SPEEDBRAKE CHECK VALVE

9505-1

710

LEFT 9912423-31

0O/C13-Mar-2004MTH

291016 SPEEDBRAKE CHECK VALVE

9505-1

711

RIGHT 9912423-31

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

291017 THERMAL RELIEF VALVE

2577-1

356

9912423-32

0O/C13-Mar-2004MTH

291018 PNUEMATIC DUMP VALVE

9503-2

363

9912423-34

0O/C13-Mar-2004MTH

291019 ATTENUATOR VALVE

4107-3

360

LEFT 9912423-28

0O/C13-Mar-2004MTH

291019 ATTENUATOR VALVE

4107-4

361

RIGHT 9912423-27

0O/C13-Mar-2004MTH

291020 SPEED BRAKE VALVE

4052-3

358

9912423-30

0O/C13-Mar-2004MTH

291021 FLAP VALVE

4052-4

361

9912423-29

0O/C13-Mar-2004MTH

291150 LANDING GEAR VALVE

9504-1

351

291015

0O/C13-Mar-2004MTH

301001 ISOLATION VALVE

2602-36

1030

9912403-2

0O/C13-Mar-2004MTH

301002 PRESSURE SWITCH

1106P55-1

2586A

LEFT

0O/C13-Mar-2004MTH


1106P55-1

2627A

RIGHT

0O/C13-Mar-2004MTH

301003 PRESS REGULATOR VALVE

1962-00-9

2017

LEFT 9912495-5

0O/C13-Mar-2004MTH

301003 PRESS REGULATOR VALVE

1962-00-9

2065

RIGHT 9912495-5

0O/C13-Mar-2004MTH

301004 TEMPERATURE SWITCH

1173T42-4

2160

LEFT

0O/C13-Mar-2004MTH

301004 TEMPERATURE SWITCH

1173T42-4

2343

RIGHT

0O/C13-Mar-2004MTH


3D2353-06

N03560

LEFT

0O/C13-Mar-2004MTH


3D2353-06

N20391

RIGHT

0O/C13-Mar-2004MTH

301006 HORIZONTAL STABILIZER BOOT

P29S4D5244-15

NCV2290

LEFT

SMF

0O/C20-Sep-2015MTH

03622.7HRS

3197LDG

301006 HORIZONTAL STABILIZER BOOT

29S4D5244-16

MATZ970

RIGHT

1O/C04-Aug-2009MTH

01964.5HRS

01796LDG

302001 PRESS REG VALVE

5285-00-3

0648

LEFT

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

302001 PRESS REG VALVE

5285-00-3

0448

RIGHT

0O/C13-Mar-2004MTH

302002 INLET TEMP SWITCH

1173T0759

2235

LEFT

0O/C13-Mar-2004MTH

302002 INLET TEMP SWITCH

1173T0759

2190

RIGHT

0O/C13-Mar-2004MTH

303002 TUBE PITOT

PH502

1916610

LEFT

0O/C05-Nov-2012MTH

02982.18HRS

02677LDG

303002 TUBE PITOT

PH502

1867006

RIGHT

0O/C05-Nov-2012MTH

02982.18HRS

02677LDG

304001 B/A TEMP MONITOR

1169-1

3498

0O/C13-Mar-2004MTH

304002 HEAT EXCHANGER

10653A

1474

9912041-3

0O/C13-Mar-2004MTH

304003 PRESSURE REGULATING CHECK VALVE

27221274

2083

0O/C13-Mar-2004MTH

304004 FLOORBOARD TF006 SENSOR

27221274

10AW317

AFT 9912085-3

0O/C13-Mar-2004MTH

304004 T/C TT002 SENSOR

27221274

12AV607

FORWARD 9912085-3

0O/C13-Mar-2004MTH

304005 TEMP CONTROLLER

1E58-1

6AW91

9912085-6

0O/C13-Mar-2004MTH

304006 TEMP CONTROL VALVE

27241287

8AW73

9912085-1

0O/C13-Mar-2004MTH

304007 ALCOHOL PUMP ASSY

476411E

SN-UNKNOWN

0O/C13-Mar-2004MTH

304008 W/S BLEED AIR VALVE

1403-25

3414

LEFT BYLB50168

0O/C13-Mar-2004MTH

304008 W/S BLEED AIR VALVE

1403-25

3404

RIGHT BYLB50168

0O/C13-Mar-2004MTH


1115P25

4916AB

0O/C14-Dec-2012MTH

03007.88HRS

02702LDG

304010 PITOT STATIC CURRENT SENSOR

76250-1

5184

LEFT

0O/C13-Mar-2004MTH

304010 PITOT STATIC CURRENT SENSOR

76250-1

5200

RIGHT

0O/C13-Mar-2004MTH

312001 DIGITAL CLOCK

M877A5V

14824

LEFT

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

312001 DIGITAL CLOCK

M877A5V

14905

RIGHT

0O/C13-Mar-2004MTH

313001 FLIGHT HOUR METER

C664503-0104

SN-UNKNOWN

85071

0O/C13-Mar-2004MTH

315001 CABIN ALT SWITCH

GB300NA161

0329533

9910095-6

0O/C13-Mar-2004MTH

315002 MASTER ANNUNCIATOR

9912586-2

586000237

315003 9912586-2

0O/C13-Mar-2004MTH

321001 (AND ATTACHING HARDWARE) LANDING GEAR

6341200-9

11

LEFT MAIN

0O/C13-Mar-2004MTH

321001 (AND ATTACHING HARDWARE) LANDING GEAR

6341200-2

SN-UNKNOWN

RIGHT MAIN

0O/C13-Mar-2004MTH

321003 TRUNNION

6341221-5

SN-UNKNOWN

LEFT MAIN GEAR

013-Mar-2004MTH

399910399910LDG 36687

321003 TRUNNION

6341221-6

SN-UNKNOWN

RIGHT MAIN GEAR

321004

013-Mar-2004MTH

399910399910LDG 36687

321004 FORK PISTON ASSEMBLY

6342200-4

SN-UNKNOWN

013-Mar-2004MTH

125000125000LDG 9196

321005 OLEO ASSEMBLY

6341201-1

48

LEFT MAIN GEAR

013-Mar-2004MTH

280750280750LDG 24771

321005 OLEO ASSEMBLY

6341201-1

47

RIGHT MAIN GEAR

013-Mar-2004MTH

280750280750LDG 24771

321007 TRAILING LINK AND AXLE ASSEMBLY

6341241-3

24162952

LEFT

ICT

010-Aug-2014MTH

03448.1HRS

447270416663061LDG 41423

321007 TRAILING LINK AND AXLE ASSEMBLY

6341241-4

24008184

RIGHT

ICT

010-Aug-2014MTH

03448.1HRS

447270416663061LDG 41423

321011 OLEO ASSEMBLY LOWER BARREL

6341135-3

SN-UNKNOWN

LEFT MAIN GEAR

321011L

013-Mar-2004MTH

162240162240LDG 12920

321011 OLEO ASSEMBLY LOWER BARREL

6341135-3

SN-UNKNOWN

RIGHT MAIN GEAR

321011R

013-Mar-2004MTH

162240162240LDG 12920

321012 OLEO ASSEMBLY UPPER BEARING ASSEMBLY

6341133-9

SN-UNKNOWN

LEFT MAIN GEAR

321012L

013-Mar-2004MTH

197130197130LDG 16409

321012 OLEO ASSEMBLY UPPER BEARING ASSEMBLY

6390037-5

25361762R

RIGHT MAIN GEAR

321012R

SMF

014-Apr-2016MTH

03672.3HRS

229570197133244LDG 19653

322001 NOSE LANDING GEAR SHIMMY DAMPER

6343001-10

638-10X

LFPB

O/C20-Dec-2013MTH

3329HRS

2966LDG

322002 NOSE LANDING GEAR STRUT ASSY(AND ATTACHING HARDWARE) ASSEMBLY

6342200-3

203

013-Mar-2004MTH

225000225000LDG 19196




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

322003 NOSE LANDING GEAR FORK

5542300-1

SN-UNKNOWN

0O/C13-Mar-2004MTH

322005 NOSE LANDING GEAR ASSEMBLY

6342200-5

SN-UNKNOWN

0O/C13-Mar-2004MTH

323001 SIDE BRACE ACTUATOR

1556700-3

0414

LEFT MAIN GEAR 9912573-2

013-Mar-2004MTH

416660416660LDG 38362

323001 SIDE BRACE ACTUATOR

1556700-3

0417

RIGHT MAIN GEAR 9912573-2

013-Mar-2004MTH

416660416660LDG 38362

323002 UPLOCK

6327504-6

709

LEFT MAIN GEAR

0O/C13-Mar-2004MTH

323002 UPLOCK

6327504-6

SN-UNKNOWN

RIGHT MAIN GEAR

0O/C13-Mar-2004MTH

323004 NOSE GEAR ACTUATOR ASSEMBLY

9912370-5

1343

LFPB

002-Oct-2011MTH

02705.25HRS

9938075002438LDG 6634

323005 NOSE LANDING GEAR UPLOCK ACTUATOR

6327504-7

333

0O/C13-Mar-2004MTH

323006 HYD-SHUTTLE VALVE

98312

0385

0O/C13-Mar-2004MTH

323020 PNEUMATIC BLOWDOWN/EMERGENCY BRAKE BOTTLE

40005320-2

7304

9912368-2 SMF

31-Aug-203428817-Jul-2015MTH 219 m 22 d

3584.1HRS

3152LDG

Manufacture Date: 31-Aug-2010

323021 EMERGENCY GEAR BOTTLE GAUGE

18225901

021341

0O/C13-Mar-2004MTH

324001 WHEEL ASSEMBLY

3-1601-3

1343

LEFT MAIN GEAR 9912743-6 KISM

0O/C08-May-2015MTH

03546.2HRS

03120LDG


3-1601-3

1372

RIGHT MAIN GEAR 9912743-6 KISM

0O/C08-May-2015MTH

03546.2HRS

03120LDG


3-1418/6342110-2

6109

NOSE LANDING GEAR

LFPB

O/C18-Jan-2012MTH

2807.35HRS

2520LDG

324003 TIRE

277K28-1 -

9912576-1

42752234

LEFT MAIN GEAR

SMF

0O/C14-Apr-2016MTH

03672.3HRS

03244LDG

324003 TIRE

277K28-1 -

9912576-1

42752358

RIGHT MAIN GEAR

KISM

0O/C08-May-2015MTH

03546.2HRS

03120LDG

324004 NOSE LANDING GEAR TIRE

184F68-1

92930374

LFPB

0O/C18-Jan-2012MTH

02807.35HRS

02520LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

324005 BRAKE ASSEMBLY

2-1651-1 -

9912743-5

0116

LEFT MAIN GEAR

KISM

1O/C08-May-2015MTH

03546.2HRS

03120LDG

324005 BRAKE ASSEMBLY

2-1651-1 -

9912743-5

0765

RIGHT MAIN GEAR

KISM

1O/C08-May-2015MTH

03546.2HRS

03120LDG

324007 SHUTTLE VALVE

211-121

SN-UNKNOWN

LEFT

0O/C13-Mar-2004MTH

324007 SHUTTLE VALVE

211-121

SN-UNKNOWN

RIGHT

0O/C13-Mar-2004MTH

324101 BRAKE ANTISKID VALVE

38-861-1

150

9912575-4 SMF

5O/C17-Jul-2015MTH

03584.1HRS

03152LDG

324102 ANTISKID TRANSDUCER

40-955

6621

LEFT 9912305-2

0O/C13-Mar-2004MTH

324102 ANTISKID TRANSDUCER

40-955

6619

RIGHT 9912305-2

0O/C13-Mar-2004MTH

324103 DIGITAL BOX

142-031-1

311

9912575-3

0O/C13-Mar-2004MTH

324104 BRAKE PRESSURE SWITCH

GPP1250-77

0316214

0O/C13-Mar-2004MTH

324105 PARKING BRAKE VALVE

95853

0858A

9912388-1

0O/C13-Mar-2004MTH

324106 HYDRAULIC PUMP MOTOR

MP50B1

2700

0O/C13-Mar-2004MTH

324107 BRAKE ANTISKID ACCUMULATOR

57C57663

0002T

0O/C13-Mar-2004MTH

324108 LOW PRESSURE SWITCH

GPP1250-29

0340797

9912373-1

0O/C13-Mar-2004MTH

324109 BRAKE PRESSURE PUMP

640929

1683

9912364-2

0O/C13-Mar-2004MTH

324110 EMERGENCY BRAKE VALVE

878208-03

V350

9912387-3

0O/C13-Mar-2004MTH

324111 FAULT DISPLAY UNIT

42-92750

1371A

9912305-9

0O/C13-Mar-2004MTH

324113 RELIEF VALVE

1785-1

788

0O/C13-Mar-2004MTH

326001 UPLOCK SWITCH

65-430087

SN-UNKNOWN

LEFT MAIN GEAR

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


65-430087

SN-UNKNOWN

NOSE LANDING GEAR

0O/C13-Mar-2004MTH


65-430087

SN-UNKNOWN

RIGHT MAIN GEAR

0O/C13-Mar-2004MTH

331001 LIGHT DIMMER

273-1

0336160

CENTER

0O/C13-Mar-2004MTH

331001 LIGHT DIMMER

273-1

0336170

LEFT

0O/C13-Mar-2004MTH

331001 LIGHT DIMMER

273-1

208260002

RIGHT

13O/C06-Nov-2009MTH

02061.1HRS

01876LDG

331002 ELECTRICAL PANEL INVERTER

EM2044-1

4116A

0O/C13-Mar-2004MTH

332001 FORWARD LEFT INVERTER

AL750PS

21235

L1

0O/C13-Mar-2004MTH

332001 MID FORWARD INVERTER

AL750PS

20282

L2

0O/C13-Mar-2004MTH

332001 MID LEFT INVERTER

AL750PS

21064

L3

0O/C13-Mar-2004MTH

332001 AFT MID INVERTER

AL750PS

21077

L4

0O/C13-Mar-2004MTH

332001 AFT LEFT INVERTER

AL750PS

20287

L5

0O/C13-Mar-2004MTH

332001 FORWARD RIGHT INVERTER

AL750PS

21062

R1

0O/C13-Mar-2004MTH

332001 MID FORWARD INVERTER

AL750PS

18217

R2

0O/C13-Mar-2004MTH

332001 MID RIGHT INVERTER

AL750PS

20455

R3

0O/C13-Mar-2004MTH

332001 AFT MID INVERTER

AL750PS

22031

R4

0O/C13-Mar-2004MTH

332001 AFT RIGHT INVERTER

AL750PS

22043

R5

0O/C13-Mar-2004MTH

334001 GROUND RECOGNITION RED LIGHT

90033-13

014678

0O/C13-Mar-2004MTH

334003 COLLISION LIGHT POWER SUPPLY

04-1502-1408

20342

LEFT

0O/C13-Mar-2004MTH

334003 COLLISION LIGHT POWER SUPPLY

04-1502-1408

20321

RIGHT

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

334004 LANDING LAMP HOUSING

50033025-1

1443

LEFT

0O/C13-Mar-2004MTH

334004 LANDING LAMP HOUSING

50033025-1

1396

RIGHT

0O/C13-Mar-2004MTH

334005 COLLISION LIGHT ASSEMBLY

03-1302-003

20993

LEFT

0O/C13-Mar-2004MTH

334005 COLLISION LIGHT ASSEMBLY

03-1302-0004

21053

RIGHT

0O/C13-Mar-2004MTH

335000 EMERGENCY EXIT LIGHT BATTERY

CBS28-1

3053M

LEFT

SMF

O/C14-Apr-2016MTH

3672.3HRS

3244LDG

2382.2ACH

335001 EMERGENCY EXIT LIGHT BATTERY

CBS28-1

3678M

NO. 2

SMF

O/C26-Oct-2015MTH

3641.5HRS

3212LDG

341001 AIR DATA COMPUTER

822-1109-004

18F9D

LEFT ADC-3000 LFPB

0O/C24-Feb-2012MTH

02823.85HRS

02535LDG

341001 AIR DATA COMPUTER

822-1109-004

1CMHX

RIGHT ADC-3000

0O/C13-Mar-2004MTH

341002 ALTIMETER/AIRSPEED INDICATOR

WL102AMS6

AL533

STANDBY

LFPB

O/C21-May-2014MTH

3430.87HRS

3055LDG

341004 AOA COMPUTER

C-13206-1

298

0O/C13-Mar-2004MTH

341006 AOA INDICATOR

C12405-1

83011

0O/C13-Mar-2004MTH

341007 AOA SENSOR

C-12717-1

1231

0O/C13-Mar-2004MTH

341008 BAROMETRIC SWITCH

GBC300-156

0331200

0O/C13-Mar-2004MTH

341010 RADIO ALT ANTENNA

S67-2002

27715

AFT

0O/C13-Mar-2004MTH

341010 RADIO ALT ANTENNA

S67-2002

27716

FORWARD

0O/C13-Mar-2004MTH

341011 RADIO ALTIMETER TRANSMITTER

822-0615-022

1BT8K

0O/C13-Mar-2004MTH

341030 TEMPERATURE PROBE SENSOR

0129G

A50596

0O/C13-Mar-2004MTH

341101 IAPS CARD CAGE

822-1459-001

1BKMY

ICC-3001

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

341102 IO PROCESSOR CARD

822-1130-151

144GT

LEFT ICO-3000

0O/C13-Mar-2004MTH

341102 IO PROCESSOR CARD

822-1130-151

18BGB

RIGHT IOC-3000

0O/C13-Mar-2004MTH

341103 CONFIGURATION CONTROL STRAPPING UNIT

822-1363-002

191MC

NO. 1

0O/C13-Mar-2004MTH

341103 CONFIGURATION CONTROL STRAPPING UNIT

822-1363-002

191MF

NO. 2

0O/C13-Mar-2004MTH

342002 AHRS COMPUTER

822-1110-002

1C7KG

LEFT AHC-3000 SMF

O/C26-Oct-2015MTH

3641.5HRS

3212LDG

342002 AHRS COMPUTER

822-1110-002

26P3G

RIGHT AHC-3000 SMF

0O/C26-Oct-2015MTH

03641.5HRS

03212LDG

342003 HSI INDICATOR

2855-01-1

MB7813

RIGHT S3100-303

0O/C13-Mar-2004MTH

342005 FLIGHT GUIDANCE COMPUTER

822-1108-122

1C9XN

LEFT FGC-3000

0O/C13-Mar-2004MTH

342005 FLIGHT GUIDANCE COMPUTER

822-1108-122

1CYDM

RIGHT FGC-3000

0O/C13-Mar-2004MTH

342006 FLUX DETECTION UNIT

822-1193-001

29597

LEFT FDU-3000

0O/C13-Mar-2004MTH

342006 FLUX DETECTION UNIT

822-1193-001

25459

RIGHT FDU-3000

0O/C13-Mar-2004MTH

342007 EXTERNAL COMPENSATION UNIT

822-1200-003

1BNYX

LEFT ECU-3000

0O/C13-Mar-2004MTH

342007 EXTERNAL COMPENSATION UNIT

822-1200-003

18M3X

RIGHT ECU-3000

0O/C13-Mar-2004MTH

342008 IAPS POWER SUPPLY

822-1137-001

1BMJB

LEFT PWR-3000

0O/C13-Mar-2004MTH

342008 IAPS POWER SUPPLY

822-1137-001

1BMJF

RIGHT PWR-3000

0O/C13-Mar-2004MTH

342009 ENVIROMENTAL CONTROL

822-1167-001

1BMXC

IEC-3001

0O/C13-Mar-2004MTH

342010 OPERATION CONFIGURATION MODULE

822-1484-201

1BTPR

LEFT OCM-3100

0O/C13-Mar-2004MTH

342010 OPERATION CONFIGURATION MODULE

822-1484-201

1C3UB

RIGHT OCM-3100

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

342030 STANDBY GYRO

501-1568-56 -

AI-300AE

5024

LFPB

0O/C10-Oct-2013MTH

03248.52HRS

02893LDG

342031 STANDBY GYRO POWER SUPPLY

501-1682-01 -

PS-834

1106

LFPB

O/C12-Nov-2013MTH

3288.37HRS

2928LDG

342301 MODE SELECTOR

622-6209-019

18T6D

LEFT MSP-85

0O/C13-Mar-2004MTH

342301 MODE SELECTOR

622-6209-019

18G1L

RIGHT MSP-85

0O/C13-Mar-2004MTH

342302 ADAPTIVE FLT DISPLAY

822-1084-208

18NYX

CENTER

0O/C13-Mar-2004MTH

342302 ADAPTIVE FLT DISPLAY

822-1084-208

1GVBD

LEFT

0O/C13-Mar-2004MTH

342302 MULTI-FUNCTION FLT DISPLAY

822-1084-208

1G66R

RIGHT

COU

0O/C09-Jan-2015MTH

03499.4HRS

03088LDG

342303 COURSE PANEL

822-1281-002

3PCN

CKP-3000

O/C21-Nov-2007MTH

1385.08HRS

1335LDG

342304 DISPLAY CONTROL PANEL

822-1134-102

1BLGR

LEFT DCP-3000

0O/C13-Mar-2004MTH

342304 DISPLAY CONTROL PANEL

822-1134-102

1BT1V

RIGHT DCP-3000

0O/C13-Mar-2004MTH

342305 COURSE/HEADING PANEL

822-1279-002

13CJV

CHP-3000

0O/C13-Mar-2004MTH

343000 MARKER BEACON RECEIVER

066-01044-0001

1917

KMR-675

0O/C13-Mar-2004MTH

343001 MARKER BEACON ANTENNA

31-10-01

4626

0O/C13-Mar-2004MTH

343002 DUAL GLIDESCOPE COUPLER

82-70-01

1443

0O/C13-Mar-2004MTH

343003 GLIDESCOPE ANTENNA

RGS10-48

9183

0O/C13-Mar-2004MTH

344001 EGPWS COMPUTER

965-1206-011

2159

MARK(V111)HONEYW

ELL

0O/C13-Mar-2004MTH

344002 RADAR TRANSCEIVER

822-1050-004

1C2XV

RTA-800

0O/C13-Mar-2004MTH

345001 DME 1 ANTENNA

DMNI50-2-2

88434

FORWARD

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

345001B DME ANTENNA

DMNI50-2-2

89308

NO. 2

0O/C13-Mar-2004MTH

345002 DME 2 TRANSCEIVER

622-6263-003

1BLWW

RIGHT

0O/C13-Mar-2004MTH

345002B DME TRANSCEIVER

622-6263-003

12796

NO. 1

0O/C07-Jul-2009MTH

01912.43HRS

01759LDG

345003 DME INDICATOR

622-7318-001

1423R

RIGHT

0O/C13-Mar-2004MTH

345003L DME INDICATOR

622-7318-001

1NHMK

NO. 1

COU

0O/C09-Jan-2015MTH

03499.4HRS

03088LDG

345005 NAVIGATION ANTENNA

22-37-101

3253

LEFT C598505-0303

0O/C13-Mar-2004MTH

345005 NAVIGATION ANTENNA

22-37-101

3252

RIGHT C598505-0303

0O/C13-Mar-2004MTH

345020 ADF 1 ANTENNA

071-1234-02

KA44B-A92775

TOP

LFPB

0O/C21-May-2014MTH

03430.87HRS

03055LDG

345040 TRANSPONDER 2 ANTENNA

DMNI50-2-2

88431

AFT 85226

0O/C13-Mar-2004MTH

345040 TRANSPONDER 1 ANTENNA

DMNI50-2-2

89292

FORWARD 85226

0O/C13-Mar-2004MTH

345040 -DIVERSITY TRANSPONDER ANTENNA

DMNI50-2-2

89293

LEFT TOP

0O/C13-Mar-2004MTH

345040 -DIVERSITY TRANSPONDER ANTENNA

DMNI50-2-2

89328

RIGHT TOP

0O/C13-Mar-2004MTH

345041 TRANSPONDER

011-00455-30

84405538

NO. 1 GTX-330D

0O/C13-Mar-2004MTH

345041 TRANSPONDER

011-00455-30

84405545

NO. 2 GTX-330D GARMIN

0O/C13-Mar-2004MTH

345049 FMS NAV COMPUTER

2116-40-1110

472

S3100-259/UNSIL SMF

O/C26-Oct-2015MTH

3641.5HRS

3212LDG

345050 GPS FMS DISPLAY

1117-1-104

3593

S3100-241

0O/C13-Mar-2004MTH

345051 GPS FMS ANTENNA

10706

8359

NO. 1

0O/C13-Mar-2004MTH


010-10040-02

60009103

NO. 2

0O/C24-Jan-2008MTH

01418HRS

01383LDG


011-00147-00

60006081

NO. 3 GA 56

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

345052 FMS CONFIGURATION MODULE

11921

5054

0O/C13-Mar-2004MTH

345053 GNS COM/NAV/GPS UNIT

011-00835-10

46400285

NO. 1 GNS-530A SMF

O/C14-Apr-2016MTH

3672.3HRS

3244LDG

2382.2ACH

345053 GNS COM/NAV/GPS UNIT

011-00835-10

46400278

NO. 2 GNS-530A SMF

O/C14-Apr-2016MTH

3672.3HRS

3244LDG

2382.2ACH

345062 TCAS ANTENNA

805-10003-001

SN-UNKNOWN

TOP

0O/C13-Mar-2004MTH

345063 HP SKYWATCH PROCESSOR

805-11900-002

80063

TRC-899

0O/C13-Mar-2004MTH

345110 ADF RECEIVER

066-01072-0007

77694

NO. 1

345021

0O/C13-Mar-2004MTH

350006 OXYGEN CYLINDER

176274-50

2552-14503

PURITAN/DOT-E8162-1

850

LFPB

30-Nov-202018025-Feb-2010MTH 54 m 21 d

02137.02HRS

01960LDG

Manufacture Date: 30-Nov-2005

350007 OXYGEN PRESSURE GAUGE

C668512-0101

J23378

MD-97

0O/C13-Mar-2004MTH

350010 OXYGEN BOTTLE

5500-L6W-BEF23A

ST56602

PORTABLE

EDDL

0O/C09-Aug-2013MTH

03186.08HRS

02841LDG

351001 OXYGEN 3 POSITION VALVE

P21007

1541

0O/C13-Mar-2004MTH

351002 OXYGEN MASK

MC10-16-101 -

9914067-41

SE27692

COPILOT

LFPB

01-Jul-201907217-Jul-2013MTH 37 m 22 d

03156.48HRS

02822LDG

351002 OXYGEN MASK

MC10-16-101 -

9914067-41

86378

PILOT

SMF

31-Aug-202117220-Sep-2015MTH 63 m 22 d

3622.7HRS

3197LDG

351003 OXYGEN PRESSURE SWITCH

P24032

0806

0O/C13-Mar-2004MTH

351007 CABIN EMERGENCY OXYGEN BOTTLE

5500L6W-BEF23A

ST56602

CABIN

EDDL

0O/C09-Aug-2013MTH

03186.08HRS

02841LDG

351008 PROTECTIVE BREATHING EQUIPMENT PBE

15-40F-11

27302-026

CABIN

LFPB

01-Jul-20191712025-Dec-2010MTH 37 m 22 d-24

02455.5HRS

02250LDG

361001 PRECOOL TEMPERATURE SENSOR

27431501-10

6AW40

LEFT 9912584-3

0O/C13-Mar-2004MTH

361001 PRECOOL TEMPERATURE SENSOR

27431501-10

6AW41

RIGHT 9912584-3

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

361002 B/A PRECOOLER ASSEMBLY

8161-2

S4883T1293

LEFT 9914402-4 SMF

30-Apr-2025010814-Apr-2016MTH 107 m 21 d

7172.3035003672.3HRS 3448.7

03244LDG

361002 B/A PRECOOLER ASSEMBLY

8161-2

S4883T1300

RIGHT 9914402-4 SMF

30-Apr-2025010814-Apr-2016MTH 107 m 21 d

7172.3035003672.3HRS 3448.7

03244LDG

361003 MODULATING VALVE

1H139-2

9AW32

LEFT

0O/C13-Mar-2004MTH

361003 MODULATING VALVE

1H139-2

9AW30

RIGHT 9912584-2

0O/C13-Mar-2004MTH


P18M30

3396

0O/C13-Mar-2004MTH

361006 OVERTEMPERATURE SWITCH

1173T181-2

4141

LEFT 9914149-2

0O/C13-Mar-2004MTH

361006 OVERTEMPERATURE SWITCH

1173T181-2

4145

RIGHT 9914149-2

0O/C13-Mar-2004MTH

361007 B/A PRESSURE REGULATOR

1H75-18

9AW69

9912510-1

0O/C13-Mar-2004MTH

522001 INFLATABLE DOOR SEAL

S15501-4

N/A

9912075-4 LFPB

O/C25-Feb-2010MTH

2137.02HRS

1960LDG

522002 SECONDARY SEAL

551230-96

SN-UNKNOWN

LFPB

O/C25-Feb-2010MTH

2137.02HRS

1960LDG

531000 TRUNNION SUPPORT FITTING

5513056-7

SN-UNKNOWN

LEFT

013-Mar-2004MTH

225000225000LDG 19196

531000 TRUNNION SUPPORT FITTING

5513056-8

SN-UNKNOWN

RIGHT

013-Mar-2004MTH

225000225000LDG 19196

531001 NOSE LANDING GEAR ACTUATOR FITTING

6511105-1

SN-UNKNOWN

013-Mar-2004MTH

239000239000LDG 20596

561001 WINDSHIELD

P00042-1

542

LEFT 9912064-15

0O/C13-Mar-2004MTH

561001 WINDSHIELD

93200-16

1106

RIGHT 9912064-16

0O/C13-Mar-2004MTH

561002 CABIN DOOR WINDOW

93105-8

9504

L1 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9747

L2 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9754

L3 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9735

L4 9912207-8

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

561002 CABIN WINDOW

93105-8

9734

L5 9912207-8

0O/C13-Mar-2004MTH


93105-8

9737

L6 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9571

R1 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9750

R2 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9752

R3 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9753

R4 9912207-8

0O/C13-Mar-2004MTH

561002 CABIN WINDOW

93105-8

9755

R5 9912207-8

0O/C13-Mar-2004MTH


93105-8

9757

R6 9912207-8

0O/C13-Mar-2004MTH

561003 PILOT SIDE WINDOW

6311263-1

0415

LEFT

0O/C13-Mar-2004MTH

561004 CO-PILOT SIDE WINDOW

6311263-2

0430

RIGHT

0O/C13-Mar-2004MTH

571000 AFT TRUNNION ATTACH FITTING

6321070-9

SN-UNKNOWN

LEFT

013-Mar-2004MTH

204800204800LDG 17176

571000 AFT TRUNNION ATTACH FITTING

6321070-10

SN-UNKNOWN

RIGHT

013-Mar-2004MTH

204800204800LDG 17176

571001 FORWARD TRUNNION ATTACH FITTING

6321060-9

SN-UNKNOWN

LEFT

013-Mar-2004MTH

204800204800LDG 17176

571001 FORWARD TRUNNION ATTACH FITTING

6321060-10

SN-UNKNOWN

RIGHT

013-Mar-2004MTH

204800204800LDG 17176

571002 SIDE BRACE FITTING

6321080-1

SN-UNKNOWN

LEFT

013-Mar-2004MTH

350000350000LDG 31696

571002 SIDE BRACE FITTING

6321080-2

SN-UNKNOWN

RIGHT

013-Mar-2004MTH

350000350000LDG 31696

712001 ISOLATOR MOUNT

LM601SA5

3741

LEFT ENGINE

FORWARD BOTTOM

9912410-3

13-Mar-2004MTH

8000080000HRS 4276.4


LM601SA5

3746

LEFT ENGINE

FORWARD TOP

9912410-3

13-Mar-2004MTH

8000080000HRS 4276.4


LM601SA5

3463

RIGHT ENGINE

FORWARD BOTTOM

9912410-3

10-Oct-2013MTH

11248.523248.5280003248.52HRS 7524.92

2893LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


LM601SA5

3429

RIGHT ENGINE

FORWARD TOP

9912410-3

10-Oct-2013MTH

11248.523248.5280003248.52HRS 7524.92

2893LDG


LM601SA4

LK1361

LEFT ENGINE AFT 9912410-2

013-Mar-2004MTH

8000080000HRS 4276.4


LM601SA4

LK1242

RIGHT ENGINE AFT 9912410-2

11510-Oct-2013MTH

11248.523248.5280003248.52HRS 7524.92

28932893LDG

71EN1 ENGINE

60500

126265

NO. 1 FJ44-2C ICT

E/C24-Apr-2015MTH

3523.63540.9HRS

30983112LDG

71EN2 ENGINE

60500

126266

NO. 2 FJ44-2C KITC

E/C24-Apr-2015MTH

34073540.9HRS

30183112LDG

720001 FAN ROTOR

65502

AU00458

E1

013-Mar-2004MTH

1001401000014LDG 6710

720001 FAN ROTOR

65502

AU00461

E2

LFPB

013-Mar-2004MTH

1009401000094LDG 6790

720002 IP COMPRESSOR ROTOR

61968

AU01804

E1

013-Mar-2004MTH

80140800014LDG 4710

720002 IP COMPRESSOR ROTOR

61968

AU01801

E2

013-Mar-2004MTH

80940800094LDG 4790

720003 COMPLETE LP SHAFT ASSEMBLY

64257

RX1SN13782

E1

0O/C13-Mar-2004MTH

720003 COMPLETE LP SHAFT ASSEMBLY

64257

RX1SN13818

E2

0O/C13-Mar-2004MTH

720004 HIGH PRESSURE SHAFT

118924

RX14RT2943

E1

UNK

0O/C14-Apr-2015MTH

03540.9HRS

03112LDG

720004 HIGH PRESSURE SHAFT

118924

RX14RT2926

E2

UNK

0O/C06-Apr-2015MTH

03540.9HRS

03112LDG

720006 DIFFUSER CASE ASSEMBLY

67894

AU01721

E1

0O/C13-Mar-2004MTH

720006 DIFFUSER CASE ASSEMBLY

67894

AU01903

E2

0O/C13-Mar-2004MTH

720007 1ST LP TURBINE NOZZLE

115315

AU01770

E1

UNK

O/C06-Aug-2014MTH

3465.4HRS

3075LDG

720007 1ST LP TURBINE NOZZLE

70217

AU02008

E2

0O/C13-Mar-2004MTH

720008 ACCESSORY DRIVE GEARBOX ASSEMBLY

120746

WL01900

E1

UNK

O/C14-Apr-2015MTH

3851.63540.9HRS

21263112LDG

720008 ACCESSORY DRIVE GEARBOX ASSEMBLY

120746

WL01949

E2

UNK

O/C06-Apr-2015MTH

3747.33540.9HRS

34943112LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

721902 NUT RETAINER, AXIAL COMPRESSOR

45785

JDM00346

E1

0O/C24-Dec-2007MTH

01418.13HRS

01361LDG

721902 NUT RETAINER, AXIAL COMPRESSOR

45785

JDM00303

E2

0-24-Dec-2007MTH

01534.73HRS

01441LDG

722010 IP (STAGE 1 & 2) VANE ASSEMBLY

115570

AU00383

E1

UNK

O/C14-Apr-2015MTH

2584.93540.9HRS

20953112LDG

722010 IP (STAGE 1 & 2) VANE ASSEMBLY

115570

AU20368

E2

O/C02-Aug-2013MTH

03265.85HRS

02893LDG

723037 FAN STATOR VANE ASSEMBLY

116640

AU01322

E1

UNK

O/C14-Apr-2015MTH

2005.13540.9HRS

16263112LDG

723037 FAN STATOR VANE ASSEMBLY

116640

AU01313

E2

O/C02-Aug-2013MTH

1977.83265.85HRS

18432893LDG

724035 HP TURBINE COMBUSTER ASSEMBLY

61702

GD300B

E1

UNK

O/C14-Apr-2015MTH

2025.43540.9HRS

24703112LDG

724035 HP TURBINE COMBUSTER ASSEMBLY

61702

GD025B

E2

UNK

O/C06-Apr-2015MTH

20173540.9HRS

15883112LDG

725016 NOZZLE, 2ND LP TURBINE HOUSING ASSEMBLY

56310

GD177A

E1

UNK

O/C06-Aug-2014MTH

3537.13465.4HRS

32333075LDG

725016 NOZZLE, 2ND LP TURBINE HOUSING ASSEMBLY

56310

AU01758

E2

UNK

O/C06-Apr-2015MTH

6999.33540.9HRS

45793112LDG

725101 HP COMPRESSOR ROTOR

123509

HW15242

E1

UNK

14-Apr-2015MTH

35003540.9HRS

8052306080003112LDG 4748

725101 HP COMPRESSOR ROTOR

123509

HW14892

E2

UNK

06-Apr-2015MTH

3751.53540.9HRS

6057305560003112LDG 2753

725103 HP TURBINE DISK

59387

RRL7LD13577

E1

03-Nov-2008MTH

1762.221754.72HRS

8136149080001626LDG 4832

725103 HP TURBINE DISK

59387

RRL7LD11271

E2

03-Nov-2008MTH

1679.171871.32HRS

8391131580001706LDG 5087

725501 1ST LP TURBINE DISK

55531

RRL7S03118

E1

UNK

06-Aug-2014MTH

1485.23465.4HRS

12219856100003075LDG 8915

725501 1ST LP TURBINE DISK

55531

RRL7S3164

E2

013-Mar-2004MTH

1009401000094LDG 6790

725502 2ND LP TURBINE DISK

55534

RRL7S02952

E1

UNK

06-Aug-2014MTH

1485.23465.4HRS

12219856100003075LDG 8915

725502 2ND LP TURBINE DISK

55534

RRL7S3325

E2

013-Mar-2004MTH

1009401000094LDG 6790

730002 FUEL NOZZLE ASSEMBLY

50817

BBC1BBC1277

E1

4O/C22-Feb-2008MTH

01476.88HRS

01421LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

730002 FUEL NOZZLE ASSEMBLY

50817

BCC-1BUP1970

E2

0O/C27-May-2013MTH

03232.18HRS

02861LDG

730003 SEAL AND FUEL SLINGER

55608

AU21493

E1

UNK

O/C14-Apr-2015MTH

3540.9HRS

3112LDG

730003 SEAL AND FUEL SLINGER

55608

AU21099

E2

O/C02-Aug-2013MTH

3265.85HRS

2893LDG

730010 FUEL PRESSURE SWITCH

1103P0448

6117

E1

0O/C13-Mar-2004MTH

730010 FUEL PRESSURE SWITCH

1103P0448

5980

E2

0O/C13-Mar-2004MTH

731046 FUEL MANIFOLD ASSEMBLY

56544

AU00873

E2

O/C02-Aug-2013MTH

2049.233265.85HRS

14282893LDG

732101 INTEGRATED FUEL CONTROL UNIT

67985

RF13444065

E1

SMF

14514-Apr-2016MTH

4017.33696.540003713.8HRS 293.7

32783292LDG

732101 INTEGRATED FUEL CONTROL UNIT

67985

RF13444084

E2

SMF

14514-Apr-2016MTH

4133.93579.940003713.8HRS 410.3

31983292LDG

732301 FUEL FILTER ELECTRICAL INDICATOR

57847

GE0991

E1

UNK

O/C14-Apr-2015MTH

3540.9HRS

3112LDG

732301 FUEL FILTER ELECTRICAL INDICATOR

57847

GE0348

E2

UNK

O/C06-Apr-2015MTH

3540.9HRS

3112LDG

733001 FUEL FLOW TRANSMITTER

1573-4

1579

E1

0O/C13-Mar-2004MTH

733001 FUEL FLOW TRANSMITTER

1573-4

1565

E2

0O/C13-Mar-2004MTH

741001 IGNITION EXCITER

CH92007

CK0300567

E1 INBOARD

0O/C13-Mar-2004MTH


CH92007

CK0300834

E1 OUTBOARD

0O/C13-Mar-2004MTH


CH92007-1

CK0300558

E2 INBOARD

0O/C13-Mar-2004MTH


CH92007-1

CK0300701

E2 OUTBOARD

0O/C13-Mar-2004MTH

741002 SHORT IGNITER LEAD

53279

SN-UNKNOWN

E1

0O/C13-Mar-2004MTH

741002 SHORT IGNITER LEAD

53279

SN-UNKNOWN

E2

0O/C13-Mar-2004MTH

741003 LONG IGNITER LEAD

53221

SN-UNKNOWN

E1

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

741003 LONG IGNITER LEAD

53221

SN-UNKNOWN

E2

0O/C13-Mar-2004MTH

741004 IGNITOR

68032

CK-1300482

E1 INBOARD

0O/C27-May-2013MTH

03115.58HRS

02781LDG

741004 IGNITOR

68032

CK1402688

E1 OUTBOARD

UNK

0O/C14-Apr-2015MTH

03540.9HRS

03112LDG

741004 IGNITOR

68032

CK-1300495

E2 INBOARD

0O/C27-May-2013MTH

03232.18HRS

02861LDG

741004 IGNITOR

68032

CK-1300490

E2 OUTBOARD

0O/C27-May-2013MTH

03232.18HRS

02861LDG

753020 HP COMPRESSOR COVER ASSY

65593

AU02241

E1

0O/C13-Mar-2004MTH

753020 HP COMPRESSOR COVER ASSY

65593

AU02235

E2

0O/C13-Mar-2004MTH

771001 N1 SPEED PICKUP

70722

YYV032

E1

0O/C13-Mar-2004MTH


70722

YYV029

E2

0O/C13-Mar-2004MTH


70721

YYV011

E1

0O/C13-Mar-2004MTH


70721

YYV010

E2

0O/C13-Mar-2004MTH

772001 ITT PROBE

62141

YYF009099

E1 NO. 1

0O/C13-Mar-2004MTH

772001 ITT PROBE

62141

YYF009105

E2 NO. 1

0O/C13-Mar-2004MTH

772020 ITT PROBE

62141

YYF009100

E1 NO. 2

0O/C13-Mar-2004MTH

772020 ITT PROBE

62141

YYF009106

E2 NO. 2

0O/C13-Mar-2004MTH

772030 ITT PROBE

62141

YYF009101

E1 NO. 3

0O/C13-Mar-2004MTH

772030 ITT PROBE

62141

YYF009107

E2 NO. 3

0O/C13-Mar-2004MTH

772040 ITT PROBE

62141

YYF009102

E1 NO. 4

0O/C13-Mar-2004MTH

772040 ITT PROBE

62141

YYF009108

E2 NO. 4

0O/C13-Mar-2004MTH




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

772050 ITT PROBE

62141

YYF009103

E1 NO. 5

0O/C13-Mar-2004MTH

772050 ITT PROBE

62141

YYF009109

E2 NO. 5

0O/C13-Mar-2004MTH

772060 ITT PROBE

62141

YYF009104

E1 NO. 6

0O/C13-Mar-2004MTH

772060 ITT PROBE

62141

YYF009110

E2 NO. 6

0O/C13-Mar-2004MTH

774001 N1 STANDBY INDICATOR

10645N01R02

B0196A

E1

LFPB

0O/C05-Mar-2012MTH

02845.07HRS

02536LDG

774020 CONCENTRATOR UNIT

822-1278-004

18XNB

E1 FORWARD

0O/C13-Mar-2004MTH


822-1278-004

18WXL

E2 FORWARD

0O/C13-Mar-2004MTH


822-1278-004

18YHJ

E1 AFT

0O/C13-Mar-2004MTH


822-1278-004

193RY

E2 AFT

0O/C13-Mar-2004MTH

774040 N1 COMPUTER

PN

SN-UNKNOWN

E1

0O/C13-Mar-2004MTH

783000 T/R DEPLOY SWITCH

602EN602-6

SN-UNKNOWN

LEFT

0O/C13-Mar-2004MTH

783000 T/R DEPLOY SWITCH

602EN602-6

SN-UNKNOWN

RIGHT

0O/C13-Mar-2004MTH

783001 T/R STOW SWITCH

602EN602-6

SN-UNKNOWN

LEFT

0O/C13-Mar-2004MTH

783001 T/R STOW SWITCH

602EN602-6

SN-UNKNOWN

RIGHT

0O/C13-Mar-2004MTH

783003 ATTENUATOR ACTUATOR

6317105-13

753

LEFT

0O/C13-Mar-2004MTH

783003 ATTENUATOR ACTUATOR

6317105-13

735

RIGHT

0O/C13-Mar-2004MTH

792201 LUBE OIL COOLER

59857

FC0741

E1

0O/C13-Mar-2004MTH

792201 LUBE OIL COOLER

59857

FC0750

E2

0O/C13-Mar-2004MTH

792401 LUBE AND SCAVENGE PUMP

110487

WL01583

E1

UNK

014-Apr-2015MTH

8540.9050003540.9HRS 4817.3

03112LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Components

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

792401 LUBE AND SCAVENGE PUMP

110487

WL01584

E2

UNK

006-Apr-2015MTH

8540.9050003540.9HRS 4817.3

03112LDG

793002 OIL PRESSURE SWITCH

S1103P89-3

1651

E1

0O/C13-Mar-2004MTH

793002 OIL PRESSURE SWITCH

S1103P89-3

1652

E2

0O/C13-Mar-2004MTH

793003 OIL PRESSURE TRANSMITTER

APTE-304-200G

683410601

E1

0O/C13-Mar-2004MTH

793003 OIL PRESSURE TRANSMITTER

APTE-304-200G

68341474

E2

0O/C13-Mar-2004MTH

801101 STARTER GENERATOR

300SGL129Q -

9912125-2

2961XL2

LEFT ENGINE

LFPB

020-Dec-2013MTH

4329010003329HRS 605.4

02966LDG

801101 STARTER GENERATOR

300SGL129Q

7786XL2

RIGHT ENGINE

801101R

9912125-2 LFPB

009-Jun-2012MTH

3893.55010002893.55HRS 169.95

02595LDG




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Service Bulletins

DUE 1

DUE 2

Adj.

+ or -

SL CIL-99-03 R1 MISCELLANEOUS - CORROSION PREVENTION AND CONTROL PROGRAM (CPCP)

RECOMMENDEDLFPB -26-Feb-2014MTH Complete

3385.63HRS

3014LDG

COMPLIED WITH - SL CIL-99-03 R1 "INSPECTION CORROSION PREVENTION AND CONTROL PROGRAM"

COMPLIED WITH.

MOC :

SL 525A-02-01 TRANSMITTAL OF ROCKWELL COLLINS OPERATOR'S GUIDE (3RD EDITION) ADDENDUM #1

INFORMATIONAL -

MOC :

SL 525A-99-01 R4 CESCOM PRICES (THIS SL CANCELS SL525A-99-01 R3 AND PREVIOUS)

INFORMATIONAL -

MOC :

SL 525A-99-02 R1 TRANSMITTAL OF CESSNA'S CERTIFICATION REQUIREMENTS FOR PORTABLE ELECTRONIC DEVICE USAGE

INFORMATIONAL -

MOC :

SL 525A-99-03 MISCELLANEOUS - CESSNA PART NUMBER SUFFIXES FOR REMANUFACTURED PARTS

INFORMATIONAL A/R

- INFORMATION ABOUT PN SUFFIXES. (SBR4811/PP0912/11/)MOC :

SL 525A-99-04 MISCELLANEOUS - CESSNA SERVICE DOCUMENT CHANGE NOTIFICATION

INFORMATIONAL A/R

- INFORMATION ABOUT SERVICE DOCUMENT CHANGE NOTIFICATION. (SBR4811/PP091211/)MOC :

SL CIL-03-01 CERTIFICATION REQUIREMENTS - SUPPLEMENTAL TYPE CERTIFICATE (STC)

INFORMATIONAL -

MOC :

SL CIL-99-04 MISCELLANEOUS - INCREMENTAL LIBRARY UPDATES FOR CESVIEW

INFORMATIONAL -

MOC :

SL 525A-03-01 R1 SUPPLEMENTAL TYPE CERTIFICATION (STC) (THIS SL IS REPLACED BY CIL-03-01, DATED JUNE 3, 2013)

INFORMATIONAL -

MOC :

SL 525A-05-02 PRECOOLER LIFE LIMIT

INFORMATIONAL

-

MOC :

SB FJ44-05-002 UNSERVICEABLE PARTS - NOTIFICATION

INFORMATIONAL

E1

-

MOC :

SB FJ44-05-002 UNSERVICEABLE PARTS - NOTIFICATION

INFORMATIONAL

E2

-

MOC :

SB 525A-11-04 GEAR EXTEND SPEED REDUCTION

MANDATORY

A/R Complete

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL CIL-99-01 R1 USE OF CORROSION INHIBITING COMPOUNDS

INFORMATIONAL

-

MOC :

SL CIL-99-01 R2 USE OF CORROSION INHIBITING COMPOUNDS

INFORMATIONAL

-

MOC :

SL CIL-99-02 MISCELLANEOUS - AVOID OPERATIONS ON RUNWAYS TREATED WITH RUNWAY DE-ICE (RDI) FLUIDS. AIRCRAFT WASHING

RECOMMENDED AFTER EXPOSURE TO RDI FLUIDS

RECOMMENDED -MTH

MOC :

SL CIL-20-01 R2 STANDARD PRACTICES - CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

INFORMATIONAL -

MOC :

SL 525A-20-01 R9 CESSNA CERTIFICATION OF NONDESTRUCTIVE TESTING FACILITIES/PERSONNEL

INFORMATIONAL A/R

- INFORMATION INFORMATIONAL REFERENCE. (SLR0111/AC070111/LR200111)MOC :

CIL 21-01 AIR CONDITIONING - COMPRESSOR MOTOR BRUSH LIFE LIMIT

- N/A

NOT APPLICABLE - N/A BY MODEL. ONLY 525A-CJ1. (SBR0412/PP230312/)MOC :

SB 525A-21-05 TEMPERATURE SENSOR RELOCATION

OPTIONAL

A/R

MOC :

SB 525A-21-06 AIR CONDITIONING - AFT EVAPORATOR DRAIN HOSE IMPROVEMENT

DISCRETIONARY A/R

- OPEN TO BE C/W IN CASE THE MIXTURE FROM THE AFT EVAPORATOR WATER DRAIN, LEAKS

ONTO THE CARPET. NO WARRANTY COVERAGE. KIT COST - $236.00 USD. LABOUR - 8MH.

(SBR44/D171110/A241110)

MOC :

SAIB CE-10-49 R1 SAIB-DRAIN MAST HEATER A/R

- INFORMATION TRANSMIT INFORMATION TO THE CREW AND CONTRACTED PART 145.

(ADR01/140111/A040211)

MOC :

SL 525A-21-01 PRESSURIZATION CONTROL ADJUSTMENT/TEST PROCEDURE IMPROVEMENT

INFORMATIONAL -

MOC :

SB 525A-23-02 COCKPIT VOICE RECORDER MODIFICATION

RECOMMENDED

- N/A

NOT APPLICABLEMOC :

SB 525A-23-03 GARMIN RADIO MODIFICATION

RECOMMENDED

-13-Mar-2004MTH N/A

NOT APPLICABLEMOC :

SB 525A-23-04 HONEYWELL KY-196A/KY-196B DUAL VHF COMMUNICATION SYSTEM UPGRADE

RECOMMENDED - N/A

NOT APPLICABLEMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-23-05 GARMIN RADIO REPLACEMENT

OPTIONAL

- N/A

NOT APPLICABLEMOC :

SB 525A-23-06 GARMIN TRANSPONDER REPLACEMENT

RECOMMENDED

- N/A

NOT APPLICABLEMOC :

SB 525A-23-07 GARMIN GTX330/330D TRANSPONDER SOFTWARE VERSION 3.03 UPGRADE

MANDATORY 6MTH N/A

NOT APPLICABLEMOC :

SB 525A-23-08 R1 RADIO TUNING UNIT (RTU) UPDATE

MANDATORY

A/RMTH N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A PER S/NMOC :

SL 525A-23-01 R1 TRANSMITTAL OF GARMIN SERVICE BULLETIN 0218, NEW SOFTWARE VERSION 3.00 (MAIN) FOR 400/500 SERIES UNITS AND

3.00(GPS) FOR 400/500 SERIES UNITS

OPTIONAL -

MOC :

SB 525A-24-02 AFT CABIN WIRE BUNDLE PROTECTION

RECOMMENDED

- N/A

NOT APPLICABLEMOC :

SB 525A-24-03 AVIONICS EMERGENCY BUS RELAY IMPROVEMENT

DISCRETIONARY

A/R

MOC :

SB 525A-24-05 CIRCUIT BREAKER PANEL HARDWARE IMPROVEMENT

MANDATORY

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 348 TO 386. (SBR16/D290408/A070708)MOC :

SB 525A-24-06 GENERATOR CONTROL UNIT WIRE BUNDLE ROUTING

MANDATORY

LFPB

-10-Oct-2013MTH Complete

3248.52HRS

2893LDG

COMPLIED WITHMOC :

SL 525A-24-01 STARTER/GENERATOR WIRE ROUTING INSPECTION/CORRECTION

RECOMMENDED -

MOC :

SL 525A-24-02 WIRE BUNDLE INSPECTION

RECOMMENDED

A/R N/A

NOT APPLICABLE - NO SIDE FACING SEAT INSTALLED.MOC :

SB 525A-25-01 R1 B&D CABIN DISPLAY IMPROVEMENT

OPTIONAL

-

MOC :

SB 525A-25-02 FLUSHING TOILET INSTALLATION

OPTIONAL

-

MOC :

SB 525A-25-03 EMERGENCY LOCATOR TRANSMITTER (ELT) WIRING MODIFICATION

OPTIONAL -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-25-04 R1 THREE FREQUENCY EMERGENCY LOCATOR TRANSMITTER (ELT)WITH NAVIGATION INTERFACE INSTALLATION

OPTIONAL A/R N/A

NOT APPLICABLE - A/C COMPLIANT WITH EASA REGULATIONS. THREE FREQUENCY EMERGENCY

LOCATOR TRANSMITTER ARTEX C406-2 INSTALLED (P/N 453-5000). (SBR25/D211010/A251010)

MOC :

SB 525A-25-05 R1 GLARESHIELD LEATHER STRIP INSTALLATION

OPTIONAL

-

MOC :

SB 525A-25-06 AFT CABIN INSULATION MODIFICATION

OPTIONAL

-

MOC :

SB 525A-25-07 AIRCELL ANTENA INSTALLATION IMPROVEMENT

OPTIONAL

-

MOC :

SB 525A-25-08 PASSENGER SEAT GEAR AND BACKREST LATCH PIN REPLACEMENT

OPTIONAL -22-Feb-2007MTH Complete

1188HRS

COMPLIED WITHMOC :

SB 525A-25-09 CABIN BRIEFER WIRING IMPROVEMENT

RECOMMENDED

A/R N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A PER AIRCRAFT S/NMOC :

SB CIB-25-01 EQUIPMENT/FURNISHINGS - PASSENGER SEAT QUICK RELEASE PIN INSTALLATION

OPTIONAL -

MOC :

SL 525A-25-01 EQUIPMENT/FURNISHINGS - TRANSMITTAL OF PACIFIC SCIENTIFIC AEROSPACE SERVICE BULLETINSB 25-1111432,

INFORMATION REGARDING THE POTENTIAL FAILURE OF THE GUARDED ROTARYBUCKLE PLASTIC HANDLE

MANDATORY A/R26-Feb-2008MTH Complete

1459.58HRS

1421LDG

COMPLIED WITH - COMPLIED BY CCESCMOC :

SL 525A-25-02 INSPECTION OF THE BACKREST LATCH PLATES

MANDATORY

LFPB

A/R30-Jul-2010MTH Complete

2318.02HRS

2121LDG

COMPLIED WITHMOC :

SL 525A-25-03 EQUIPMENT/FURNISHINGS - TRANSMITTAL OF B/E AEROSPACE SERVICE BULLETIN 2524.565-25-01 REPLACEMENT OF SWIVEL

ASSEMBLY

MANDATORY A/RMTH N/A

NOT APPLICABLE - BY SERIAL NUMBER APPLICABLE TO SERIAL NUMBERS -0440,-0447,-0451,-0455

THRU -0457 ONLY. (SBR42/A291010)

MOC :

SB 525A-26-02 FIRE BOTTLE IDENTIFICATION SLEEVE INSTALLATION

MANDATORY

- Complete

COMPLIED WITHMOC :

SL 525A-26-01 ENGINE FIRE PROTECTION SENSOR LOOP INSPECTION

MANDATORY

30DAYS

15HRS

MOC :

SB 525A-27-01 R3 STEEP APPROACH CERTIFICATION

OPTIONAL

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-27-03 R1 FLAP OVERRIDE SWITCH INSTALLATION

RECOMMENDED

- N/A

NOT APPLICABLEMOC :

SB 525A-27-04 AILERON CABLE AND FAIRLEAD TUBE REPLACEMENT

RECOMMENDED

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 1-125. (SBR16/D240409/A210509)MOC :

SB 525A-27-07 ELEVATOR TRIM POINTER IMPROVEMENT

OPTIONAL

-

MOC :

SB 525A-27-08 RUDDER BIAS SIMPLIFICATION

OPTIONAL

A/R

MOC :

SB 525A-27-09 ELEVATOR TRIM POINTER ASSEMBLY IMPROVEMENT

OPTIONAL

LFPB

A/RMTH

MOC :

SB 525A-27-10 INSPECTION OF TAILCONE WIRE BUNDLE

RECOMMENDED

LFPB

A/R25-Feb-2010MTH Complete

2137.02HRS

1960LDG

COMPLIED WITHMOC :

SB 525A-27-12 AILERON CONTROL SYSTEM MODIFICATION

DISCRETIONARY

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 0300 THRU -0304 AND -0306 THRU -0408

(SBR31/D020908/A040908)

MOC :

SB 525A-27-13 R1 VERTICAL STABILIZER CABLE FAIRLEAD INSTALLATION

MANDATORY

EDDL

A/R09-Aug-2013MTH Complete

3186.08HRS

2841LDG

COMPLIED WITHMOC :

ASL 525A-27-02 BRAKES PUSHROD INSPECTION

MANDATORY

30DAYS N/A

25HRS

NOT APPLICABLEMOC :

SL 525A-27-01 ELEVATOR ELECTRIC TRIM TAB ACTUATOR MOUNT INSPECTION

RECOMMENDED -

MOC :

SL 525A-27-03 RUDDER BIAS PNEUMATIC LINE CLAMP INSPECTION

RECOMMENDED

-

MOC :

SL 525A-27-05 FLIGHT CONTROLS - FLAP PUSHROD SAFETY WIRE INSPECTION

RECOMMENDED -26-Feb-2008MTH Complete

1459.58HRS

1421LDG

COMPLIED WITH - COMPLIED AT CCESCMOC :

SL 525A-27-06 AILERON CABLE GUARD REPLACEMENT

MANDATORY

-MTH

MOC :

SB 525A-28-01 REPLACEMENT OF WING FUEL FILLER

DISCRETIONARY

- N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 1-19.MOC :

SB 525A-28-02 FUEL BOOST PUMP ANNUNCIATION IMPROVEMENT

DISCRETIONARY

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-28-03 WING FUEL BOOST PUMP WIRE ROUTING IMPROVEMENT

MANDATORY

- N/A

NOT APPLICABLEMOC :

SB 525A-28-04 FIREWALL SHUTOFF VALVE REPLACEMENT AND FIREWALL SHUTOFF VALVE BRACKET MODIFICATION

OPTIONAL A/R

MOC :

SB CIB-28-01 FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT

RECOMMENDED

-MTH

MOC :

SL 525A-28-01 WING BOOST PUMP WIRE ROUTING INSPECTION

MANDATORY


1459.58HRS

1421LDG


SL 525A-28-02 FUEL LINE CLEARANCE IMPROVEMENT

MANDATORY

A/R30-Apr-2009DAYS Complete

1850.78HRS

1711LDG

COMPLIED WITH - PERFORMED NO DEFECT FOUNDMOC :

SB 525A-29-01 SOLENOID LOADING VALVE REPLACEMENT

RECOMMENDED

-

MOC :

SB 525A-29-02 FLAP HYDRAULIC SYSTEM RESTRICTOR RELOCATION

MANDATORY

3MTH

150HRS

MOC :

SB 525A-29-03 TAILCONE HYDRAULIC TUBE IMPROVEMENT

RECOMMENDED

-

MOC :

SB 525A-29-04 R1 HYDRAULIC RELIEF VALVE INLET NUT INSPECTION/REPLACEMENT

MANDATORY -03-Nov-2008MTH Complete

1737.42HRS

1626LDG

COMPLIED WITH - RELIEF VALVE REMOVED AND INSPECTED - NO DEFECT FOUNDMOC :

SB 525A-29-04 R2 HYDRAULIC RELIEF VALVE INLET NUT INSPECTION/REPLACEMENT

CANCELLED A/R N/A

NOT APPLICABLE - TERMINATED REV 02 CANCELS THIS SB. REV 01 HAS BEEN COMPLIED ON 03/11/08.

(SBR09/D040309/A210509)

MOC :

SB 525A-29-06 R1 HYDRAULIC POWER - HYDRAULIC RELIEF VALVE STAKING IMPROVEMENT

MANDATORYLFPB A/R12-Aug-2012MTH Complete

2946.45HRS

2640LDG

COMPLIED WITH - OPEN TO BE RE-EVALUATED BEFORE 1200FH OR 3YEARS FROM THE JUN 6/2011.

LABOUR 1+2MH. (SBR2411/PP070711/) CW WO-12-158 - SB 525A-29-06 R1 COMPLETED

MOC :

SB 525A-29-07 HYDRAULIC POWER - STAINLESS STEEL TUBE ASSEMBLY INSTALLATION

OPTIONALICT A/R10-Aug-2014MTH Complete

3448.1HRS

3061LDG

COMPLIED WITHMOC :

SL 525A-29-01 MAIN HYDRAULIC RESERVOIR RELIEF VALVE MODIFICATION

RECOMMENDED -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL 525A-29-02 HYDRAULIC RELIEF VALVE INLET NUT TORQUE INSPECTION

RECOMMENDED A/R N/A

NOT APPLICABLE - BY EFFECTIVITY SN -200 NOT CONCERNEDMOC :

SL CIL-30-01 R1 ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES

INFORMATIONAL -

MOC :

SL CIL-30-01 ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES

INFORMATIONALLFPB -14-Mar-2013MTH Complete

3036.27HRS

2728LDG

COMPLIED WITH - CIL-30-01 PARA 5 ¿APPROVED DE-ICING PROGRAM UPDATES¿ COMPLIED WITH.MOC :

SL 525A-30-01 R12 ICE AND RAIN PROTECTION - APPROVED DEICING PROGRAM UPDATES

INFORMATIONAL -

- INFORMATION ACKNOWLEDGED. FLIGHT OPERATIONS MANAGER AND CJ2 FLIGHT CREW

INFORMED. (SBR4411/PP071111/)

MOC :

SB 525A-31-01 LOW BRAKE PRESSURE ANNUNCIATION & MASTER CAUTION IMPROVEMENT

RECOMMENDED -

MOC :

SB 525A-31-02 FLIGHT LEVEL 180 SELECT SWITCH ACTIVATION

OPTIONAL

-

MOC :

SL 525A-31-01 TRANSMITTAL OF ROCKWELL COLLINS SERVICE BULLETIN 12 REVISION 2, AFD-3010 ADAPTIVE FLIGHT DISPLAY

MANDATORY 60DAYS

50HRS

MOC :

SL 525A-31-02 COCKPIT SWITCH INSPECTION

RECOMMENDED

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 301 AND ON

SBR51/D241207/A070108

MOC :

SL 525A-31-05 TRANSMITTAL OF L-3 COMMUNICATIONS ALERT BULLETINNO. CESSNA SB 001


NOT APPLICABLE - BY S/N OF A/C. (SBR36A11/PP071111/LR101111)MOC :

SL 525A-31-06 INDICATING/RECORDING SYSTEMS - INDICATING/RECORDING - ARES SOFTWARE UPDATE

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N 475-477. (SBR4711/PP170212/LR200212)MOC :

SB 525A-32-01 R1 EMERGENCY GEAR RELEASE BRACKET CLEARANCE IMPROVEMENT

RECOMMENDED -

MOC :

SB 525A-32-02 BRAKE SYSTEM IMPROVEMENTS

RECOMMENDED

-

MOC :

SB 525A-32-03 R1 BRAKE TUBE IMPROVEMENT

RECOMMENDED

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-32-03 BRAKE TUBE IMPROVEMENT

RECOMMENDED

A/R

MOC :

SB 525A-32-04 BRAKE HIGH PRESSURE SWITCH IMPROVEMENT

RECOMMENDED

-

MOC :

SB 525A-32-05 R1 BRAKE METERING/ANTISKID VALVE REPLACEMENT

RECOMMENDED

-

MOC :

SB 525A-32-07 BEARING REPLACEMENT

MANDATORY

- Complete

COMPLIED WITHMOC :

SB 525A-32-08 ANTISKID CONTROL UNIT INSPECTION/REPLACEMENT

MANDATORY

A/R N/A

NOT APPLICABLE - BY SERIAL NUMBER EFFECTIVITY: MODEL 525A (CJ2) SERIAL NUMBERS -0211 THRU

-0244

MOC :

SB 525A-32-10 R1 MAIN LANDING GEAR ACTUATOR EXTEND HOSE IMPROVEMENT

RECOMMENDED A/R N/A

NOT APPLICABLE - NO ACTION REQUIRED ORIGINAL SB COMPLIED WITH AT CCESC ON 26 FEBRUARY

2008. NO ADDITIONAL REQUIREMENTS AT REV 1 (SBR05/D02022009/A210509)

MOC :

SB 525A-32-10 MAIN LANDING GEAR ACTUATOR EXTEND HOSE IMPROVEMENT

RECOMMENDED A/R26-Feb-2008MTH Complete

1459.58HRS

1421LDG


SB 525A-32-11 BRAKE HYDRAULIC AND PNEUMATIC TUBE IMPROVEMENT

MANDATORY

A/R16-Nov-2006MTH Complete

COMPLIED WITHMOC :

SB 525A-32-12 R1 IMPROVEMENT TO THE PUSHROD ASSEMBLY ON THE MAIN LANDING-GEAR DOOR

MANDATORY A/R Complete

COMPLIED WITH - PREVIOUSLY PREVIOUSLY COMPLIED WITH ORIGINAL SB.

(SBR044/D051208/A150509)

MOC :

SB 525A-32-12 IMPROVEMENT TO THE PUSHROD ASSEMBLY ON THE MAIN LANDING GEAR DOOR

MANDATORY A/R21-Sep-2007DAYS Complete

1333.08HRS

1296LDG

COMPLIED WITHMOC :

CIL 99-01 MISCELLANEOUS - USE OF CORROSION INHIBITING COMPOUNDS

-

- INFORMATIONAL. (SBR0312/PP200112/)MOC :

ASL 525A-32-11 MAIN LANDING GEAR DOOR PUSHROD INSPECTION

MANDATORY

A/R28-Sep-2006DAYS Complete

1039HRS

COMPLIED WITHMOC :

SL CIL-32-01 LANDING GEAR - IMPROVED NOSE WHEEL GREASE SEAL

INFORMATIONAL

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL CIL-32-03 NLG UPLOCK ROLLER BRACKET INSPECTION

RECOMMENDED

MTH

3822.02300HRS 98.42

MOC :

SL CIL-32-04 WIRELESS TIRE PRESSURE MONITORING SYSTEM INSTALLATION

INFORMATIONAL -

MOC :

SL 525A-32-01 TRANSMITTAL OF BFGOODRICH SERVICE LETTER SL 1866 LANDING GEAR - MAIN AND NOSE WHEELS APPROVED CLEANERS

FOR ALUMINUM WHEEL ASSEMBLIES

INFORMATIONAL -

MOC :

SL 525A-32-02 TRANSMITTAL OF BFGOODRICH SERVICE LETTER SL 1878, EFFECT OF DISINFECTANT ON WHEEL AND BRAKE ASSEMBLIES

INFORMATIONAL -

MOC :

SL 525A-32-03 HYDRAULIC TUBE INSPECTION

RECOMMENDED

-

MOC :

SL 525A-32-04 NOSE LANDING GEAR TIRE INSPECTION

MANDATORY

25LDG

MOC :

SL 525A-32-05 TRANSMITTAL OF GOODRICH SERVICE LETTER 1919, LANDING GEAR- MAIN WHEEL- APPLY RTV TO WHEEL BASE ASSEMBLY

INFORMATIONAL -

MOC :

SL 525A-32-08 R1 NOSE LANDING GEAR ICE PROTECTION BOOT INSTALLATION

OPTIONAL -

MOC :

SL 525A-32-09 TRANSMITTAL OF GOODRICH SERVICE BULLETIN 3-1601-32-2 LANDING GEAR - MAIN WHEEL - P/N 3-1601-2 - CESSNA CJ2 -

INTRODUCTION OF NEW SIDE RIM

INFORMATIONALLFPB A/RMTH

MOC :

SL 525A-32-10 MAIN LANDING GEAR SIMULATOR TEST BOX

INFORMATIONAL

A/R

MOC :

SL 525A-32-12 TRANSMITTAL OF GOODRICH SERVICE LETTER 2056

RECOMMENDED


1459.58HRS

1421LDG

COMPLIED WITH - S/O 119935MOC :

SL 525A-32-13 MAIN LANDING GEAR DOOR PUSHROD SAFETY WIRE INSPECTION

RECOMMENDED -16-Apr-2008MTH N/A

NOT APPLICABLE - BY EFFECTIVITY ONLY APPLICABLE TO A/C S/N 341 TO 358.

(SBR08/D160408/A210408)

MOC :

SL 525A-32-14 AUXILIARY BRAKE TUBE INSPECTION

RECOMMENDED

A/R26-May-2008MTH Complete

1566.67HRS

1504LDG

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL 525A-32-15 TRANSMITTAL OF GOODRICH SERVICE LETTER SL2060, LANDING GEAR - MAIN WHEEL ASSEMBLY - INTRODUCTION OF AN

IMPROVED OPTIONAL THERMAL RELIEF PLUG ASSEMBLY

INFORMATIONALLFPB A/R29-Jan-2010MTH Complete

2127HRS

1952LDG

COMPLIED WITH - C/W BY CCESC ON MAIN WHEEL ASSY P/N : 3-1601-2, S/N : 0447 ON OCTOBER 02ND

2009 AT 2028:34 FH AND 1853 CY (SEE S/O 121625). C/W BY CCESC ON MAIN WHEEL ASSY P/N :

3-1601-2, S/N : 0496 ON JANUARY 29TH 2010 AT 2127:00 FH AND 1952 CY (SEE S/O 122061).

MOC :

SL 525A-32-17 R2 EMERGENCY GEAR RELEASE INSPECTION

MANDATORY


2478.17HRS

2268LDG

COMPLIED WITHMOC :

SL 525A-32-18 LANDING GEAR- TRANSMITTAL OF GOODRICH SERVICE BULLETIN 2-1651-32-2, LANDING GEAR- BRAKE ASSEMBLY-

REPLACEMENT OF BLEEDER SCREWS AND BLEEDER FITTINGS WITH BLEEDER PLUGS

MANDATORY -14-Mar-2013MTH Complete

3036.27HRS

2728LDG


SB 525A-33-01 AISLE LIGHTING CIRCUIT BREAKER INSTALLATION

RECOMMENDED

-

MOC :

SB 525A-33-02 WING TIP ANTICOLLISION LIGHT MODIFICATION

RECOMMENDED

-

MOC :

SB 525A-33-03 CHART LIGHT MODIFICATION

OPTIONAL

-

MOC :

ASL 525A-33-01 R1 TRANSMITTAL OF BIRK SERVICE BULLETIN SB25-01, INTERIOR LIGHT LAMP SOCKET REPLACEMENT

MANDATORY A/R Complete

COMPLIED WITHMOC :

ASL 525A-33-01 TRANSMITTAL OF BIRK SERVICE BULLETIN SB25-01, INTERIOR LIGHT LAMP SOCKET REPLACEMENT

MANDATORY A/R

MOC :

SL CIL-33-01 TRANSMITTAL OF RADIANT POWER CORP. SB-RPC-001, PROCEDURE TO REPLACE OBSOLETE CONNECTOR ASSEMBLY FOR

CBS28 EMERGENCY BATTERY

INFORMATIONAL -

MOC :

SL 525A-33-02 NAVIGATION/ANTI-COLLISION LIGHT SCREW INSPECTION/ REPLACEMENT

RECOMMENDED A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N -0417, -0439 THRU -0440, -0442 THRU -0460.

(SBR29/A111110)

MOC :

SB 525A-34-01 R1 REDUCED VERTICAL SEPARATION MINIMUM (RVSM) OPERATION MODIFICATION

OPTIONAL -13-Mar-2004MTH Complete

COMPLIED WITH - AT MANUFACTUREMOC :

SB 525A-34-02 FLIGHT GUIDANCE COMPUTER (FGC)-3000 MOD 1

RECOMMENDED

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-34-03 UNIVERSAL AVIONICS FLAT PANEL CONTROL DISPLAY UNIT UPGRADE TO MOD 8

MANDATORY -

MOC :

SB 525A-34-04 FLIGHT GUIDANCE COMPUTER VOR IMPROVEMENT

RECOMMENDED

-

MOC :

SB 525A-34-06 SKYWATCH HP TRANSMITTER/RECEIVER COMPUTER INSTALLATION

OPTIONAL -

MOC :

SB 525A-34-07 ADAPTIVE FLIGHT DISPLAY UPGRADE

RECOMMENDED

-

MOC :

SB 525A-34-09 ATTITUDE INDICATOR AND HORIZONTAL SITUATION INDICATOR MODIFICATION

RECOMMENDED -

MOC :

SB 525A-34-10 R1 GDL-49 ECHO FLIGHT TRANSCEIVER INSTALLATION

OPTIONAL

-

MOC :

SB 525A-34-11 RADIO ALTIMETER CONVERTER UPGRADE

DISCRETIONARY

-

MOC :

SB 525A-34-14 GARMIN GNS-530A RADIOS/FMS & GTX-330D TRANSPONDER INSTALLATION

OPTIONAL -

MOC :

SB 525A-34-15 MST-67A DIVERSITY TRANSPONDER INSTALLATION

OPTIONAL

-

MOC :

SB 525A-34-16 NAVIGATION - GARMIN GTX-330D TRANSPONDER INSTALLATION UPGRADE

- N/A

NOT APPLICABLE - GARMIN GTX-330D TRANSPONDER ALREADY INSTALLEDMOC :

SB 525A-34-17 GARMIN GTX-330(D) TRANSPONDER SOFTWARE UPGRADE TO 4.01

OPTIONAL A/R07-Aug-2007MTH Complete

1286.58HRS

1227LDG

COMPLIED WITH - TRANSPONDER UPGRADE TO 4.01MOC :

SB 525A-34-18 UNIVERSAL UNS-1K SOFTWARE UPGRADE TO 604.7

OPTIONAL

A/R N/A

NOT APPLICABLE - N/A BY P/N INSTALLED. COMPUTER NAV FMS, P/N : S3100-259/UNS1LMOC :

SB 525A-34-19 R1 NAVIGATION - TERRAIN AWARENESS WARNING SYSTEM (TAWS) UPGRADE TO SOFTWARE LEVEL 1.13

- N/A

NOT APPLICABLE - BY EFFECTIVITY TAWS 8000 NOT INSTALLED ON C525A-200;

SBR04/D280107/A310107

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-34-19 NAVIGATION - TERRAIN AWARENESS WARNING SYSTEM (TAWS) UPGRADE TO SOFTWARE LEVEL 1.13

OPTIONAL - N/A

NOT APPLICABLE - BY EFFECTIVITY TAWS 8000 NOT INSTALLED ON C525A-200 (30-11-2007).MOC :

SB 525A-34-20 R1 FILE SERVER INSTALLATION AND MULTIFUNCTION DISPLAY (MFD) UPDATE FOR CHARTS AND XM SATELLITE WEATHER

OPTIONAL A/R

MOC :

SB 525A-34-20 R2 FILE SERVER INSTALLATION AND MULTIFUNCTION DISPLAY (MFD) UPDATE FOR CHARTS AND XM SATELLITE WEATHER

OPTIONAL A/R

MOC :

SB 525A-34-22 GPS-4000S RECEIVER IMPROVEMENT

MANDATORY

A/RDAYS

MOC :

SB 525A-34-26 DIVERSITY ANTENNA INSTALLATION FOR ENHANCED SURVEILLANCE TRANSPONDERS

OPTIONAL A/R

MOC :

SB 525A-34-29 CABIN DISPLAY ARINC 429 BUS MODIFICATION

DISCRETIONARY

A/R

MOC :

SB 525A-34-30 XM WEATHER -002 CONFIGURATION MOD

RECOMMENDED

A/R

MOC :

SB 525A-34-31 V-SPEED ENABLE AND SOFTWARE UPGRADE

RECOMMENDED

A/R N/A


SB 525A-34-32 CURSOR CONTROL PANEL (CCP) HARDWARE UPGRADE TO MOD LEVEL 1

DISCRETIONARY A/R N/A

NOT APPLICABLE - ONLY APPLICABLE FROM S/N 0300 TO 0347.MOC :

SB 525A-34-33 ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) AUDIO INHIBIT WIRE INSTALLATION

MANDATORY - N/A


SB 525A-34-35 R1 NAVIGATION - DBU¿5000 DATABASE UNIT (FLASH MEMORY) SOFTWARE DATABASE LOADER

OPTIONAL A/R N/A

NOT APPLICABLE - THIS SB IS NOT APPLICABLE TO OUR MODEL. ONLY FOR SERIAL NUMBERS: -0300

THRU -0416, -0418 THRU -0438. (SBR1411/AC080611/LR120611)

MOC :

SB 525A-34-36 R2 COLLINS FMS-3000 WIDE AREA AUGMENTATION SYSTEM (WAAS) WITH FMS 4.0 SOFTWARE

RECOMMENDED -MTH

MOC :

SB 525A-34-39 NAVIGATION - TDR-94D TRANSPONDER UPGRADE

OPTIONAL

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-34-40 NAVIGATION - HONEYWELL TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM II (TCAS II) VERSION 7.1 SOFTWARE

UPDATE

OPTIONAL -

MOC :

SB 525A-34-41 NAVIGATION - AUTOMATIC DEPENDENT SURVEILLANCE BROADCAST (ADS-B) OUT TRANSPONDER INSTALLATION

OPTIONAL -

MOC :

CTI 81-15 CTI 81-15

NATIONAL

REQUIREMENT


2137HRS

1960LDG

COMPLIED WITHMOC :

ASL 525A-34-01 FLAT PANEL CONTROL DISPLAY UNIT INVERTER CIRCUITRY INTEGRITY TEST

MANDATORY - N/A

NOT APPLICABLEMOC :

SB CIB-34-02 GPS-4000S SOFTWARE UPDATE

RECOMMENDED

-

MOC :

SB CIB-34-04 ROCKWELL COLLINS ADAPTIVE FLIGHT DISPLAY UPGRADE

OPTIONAL

-

MOC :

SL CIL-34-04 TDR-94/94D TRANSPONDER ALL-CALL

INFORMATIONAL

-

MOC :

SL 525A-34-02 R1 GNS-XLS FMS MOD 7 SOFTWARE UPGRADE

RECOMMENDED

-

MOC :

SL 525A-34-03 TRANSMITTAL OF HONEYWELL SERVICE BULLETIN KN 40-7 NAV CONVERTER

RECOMMENDED -

MOC :

SL 525A-34-04 TRANSMITTAL OF ROCKWELL COLLINS OPERATOR BULLETIN OPSB 0034-03, FLIGHT DIRECTOR ANOMALY: FAILURE TO

PROVIDE PROPER GUIDANCE

INFORMATIONAL -

MOC :

SL 525A-34-07 TRANSMITTAL OF GARMIN SERVICE ALERT DIRECT-TO-WAYPOINT SELECTION SERVICE ALERT: 050721-00

INFORMATIONAL -

MOC :

SL 525A-34-08 R1 UNS-1ESP FMS CAPACITOR UPGRADE

MANDATORY

A/R N/A

NOT APPLICABLE - BY EFFECTIVITY SN -200 NOT CONCERNED BY SL EFFECTIVITYMOC :

SL 525A-34-10 TRANSMITTAL OF HONEYWELL INSTALLATION BULLETIN 531 FOR MST-67A TRANSPONDERS

INFORMATIONAL A/R

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL 525A-34-11 TRANSMITTAL OF L-3 COMMUNICATIONS AVIONICS SYSTEMS’ SERVICE LETTER SL-230 (REV. A)

INFORMATIONAL A/R

MOC :

SL 525A-34-13 CONFIGURATION FOR AUSTRALIA, SINGAPORE FIR, AND HONG KONG ADS-B OUT

OPTIONAL -

MOC :

ASL 525A-35-01 R1 OXYGEN MASK INSTALLATION VERIFICATION

MANDATORY

- Complete

COMPLIED WITHMOC :

SL CIL-35-01 TRANSMITTAL OF BE AEROSPACE SERVICE BULLETIN 118077-35-01

MANDATORYLFPB -26-Feb-2014MTH Complete

3385.63HRS

3014LDG

COMPLIED WITH - SL CIL-35-01 ?OXYGEN ? TRANSMITTAL OF BE AEROSPACE SB 118077-35-01?

COMPLIED WITH.

MOC :

SL CIL-35-05 OXYGEN - TRANSMITTAL OF ZODIAC AEROSPACE SB MCF-SBU-35-001

MANDATORY -MTH N/A

3669.2HRS

3240LDG

NOT APPLICABLE - NOT APPLICABLEMOC :

SL 525A-35-02 R1 TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240

MANDATORY -13-May-2013MTH Complete

3078.22HRS

2765LDG

COMPLIED WITH - LETTER "I" WRITTEN ON THE BUSHING OF INFLATABLE HARNESS - S/O 125704.MOC :

SL 525A-35-02 R2 OXYGEN - TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240


3078.22HRS

2765LDG


SL 525A-35-02 OXYGEN - TRANSMITTAL OF INTERTECHNIQUE SERVICE BULLETIN MXH-35-240


3078.22HRS

2765LDG


SB 525A-36-01 FAN BYPASS PORT MOD

RECOMMENDED

-

MOC :

SB 525A-36-04 PNEUMATIC - MOISTURE TRAP INSTALLATION

OPTIONAL

A/R

- OPEN TBD. (SBR22)MOC :

SB 525A-38-01 PILOT'S RELIEF TUBE IMPROVEMENT

OPTIONAL

-

MOC :

SB 525A-52-01 CABIN ENTRANCE DOOR THRESHOLD STEP CLOSEOUT IMPROVEMENT

RECOMMENDED -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-52-02 R1 IMPROVEMENT FOR THE CABIN ENTRY STEPS

OPTIONAL

A/R

MOC :

SB 525A-52-03 CABIN ENTRY DOOR HANDLE POSITION SWITCH INSTALLATION

OPTIONAL A/R

MOC :

ASL 525A-52-01 EMERGENCY DOOR INSPECTION

MANDATORY

30DAYS N/A

30HRS

NOT APPLICABLE - DOCUMENT 10 C/W ON 22 FEBRUARY 2007 (30-11-2007).MOC :

SL CIL-52-01 DOORS - EMERGENCY DOOR INSPECTION

MANDATORY

-14-Mar-2013MTH Complete

3036.27HRS

2728LDG


SB 525A-53-01 R1 FUSELAGE - DISABLE THE COCKPIT MOUNTED RELIEF TUBE(S)

MANDATORY - N/A

NOT APPLICABLE - BY EFFECTIVITY COCKPIT RELIEF TUBE NOT INSTALLED ON C525A-200.MOC :

ASL 525A-53-04 R1 RELIEF TUBE CORROSION

MANDATORY

BF/F N/A

NOT APPLICABLE - EQUIPMENT NOT INSTALLEDMOC :

ASL 525A-53-04 RELIEF TUBE CORROSION

MANDATORY

A/R12-Dec-2006MTH N/A

1139HRS

NOT APPLICABLEMOC :

ASL 525A-53-05 R3 RELIEF TUBE CORROSION INSPECTION

MANDATORY

A/R30-Nov-2007DAYS N/A

NOT APPLICABLE - BY EFFECTIVITY COCKPIT RELIEF TUBE NOT INSTALLED ON C525A-200.MOC :

ASL 525A-53-05 R6 RELIEF TUBE CORROSION INSPECTION

MANDATORY

A/R N/A

NOT APPLICABLE - EQUIPMENT NOT INSTALLEDMOC :

SL 525A-53-01 LIGHTNING DIVERTER STRIP INSTALLATION/REPAIR PROCEDURE CHANGE (RADOME)

INFORMATIONAL -

MOC :

SL 525A-53-02 TAILCONE DRAIN HOLE INSPECTION

RECOMMENDED

-

MOC :

SL 525A-53-09 INTERCOSTAL DRAINAGE PATH INSPECTION

RECOMMENDED


2137HRS

1960LDG

COMPLIED WITHMOC :

SL 525A-53-10 UPPER TAILCONE SKIN INSPECTION

MANDATORY

A/R20-Jan-2011MTH Complete

2464.67HRS

2258LDG

COMPLIED WITH - PERFORMED SL525A-53-10MOC :

SB 525A-54-01 R1 FIREWALL BOX

RECOMMENDED

LFPB

A/R09-Aug-2012MTH

2942.13HRS

2636LDG

- CW MJ-WO-12-119 R05MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB 525A-54-02 NACELLES/PYLONS - FORWARD ENGINE BEAM INSPECTION ACCESS PANEL INSTALLATION

OPTIONAL -

MOC :

SL CIL-54-01 NACELLES/PYLONS - ACCESS PANEL SEALANT INSPECTION

RECOMMENDED

-

MOC :

SL 525A-55-01 HORIZONTAL STABILIZER RIB INSPECTION

MANDATORY

A/RMTH N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A PER S/NMOC :

SB 525A-57-01 CNTR WING NOISE REDCTN IMPROVES A/R22-Feb-2007MTH Complete

1188HRS

COMPLIED WITH - PARTIALLY AT MFGMOC :

SB 525A-57-02 KEEL FITTING INSPECTION

MANDATORY

-MTH N/A

NOT APPLICABLE - BY SERIAL NUMBERMOC :

SL 525A-57-01 ACCESS DOOR DRAINAGE IMPROVEMENT

RECOMMENDED

-

MOC :

SB 525A-71-01 R1 ENGINE DIFFUSER DRAIN RE-INCORPORATION

MANDATORY

-

MOC :

SB 525A-71-02 R1 UPPER ENGINE COWL SUPPORT MODIFICATION

OPTIONAL

-

MOC :

SB 525A-71-04 R2 PT2/TT2 SENSOR INSTALLATION IMPROVEMENT

RECOMMENDED

A/R N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A PER AIRCRAFT S/NMOC :

SB 525A-71-06 COWL STIFFENER INSTALLATION

MANDATORY

- N/A

NOT APPLICABLE - - PER S/N EFFECTIVITYMOC :

SL CIL-71-02 TRANSMITTAL OF WILLIAMS INTERNATIONAL FJ44 SERVICE BULLETIN FJ44-72-128, ENGINE - SPLIT INNER RING BALL BEARING

- REPLACE

MANDATORYLEFT ENGINE -MTH

MOC :

SL CIL-71-02 TRANSMITTAL OF WILLIAMS INTERNATIONAL FJ44 SERVICE BULLETIN FJ44-72-128,ENGINE - SPLIT INNER RING BALL BEARING

- REPLACE

MANDATORYRIGHT ENGINE -MTH

MOC :

SL 525A-71-01 TRANSMITTAL OF WILLIAMS INTERNATIONAL SERVICE BULLETIN FJ44-72-062R3, ENGINE - GEARBOX INSPECTION

MANDATORY A/R N/A

NOT APPLICABLE - BY EFFECTIVITY SN -200 NOT CONCERNED BY SL EFFECTIVITYMOC :

SL 525A-71-02 DESALINIZATION RINSE - REMOVE BLEED CAP REQUIREMENT

INFORMATIONAL -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SL 525A-71-03 R1 POWER PLANT - FUEL AND HYDRAULIC HOSE REPLACEMENT

MANDATORY

-

MOC :

SL 525A-71-03 R2 POWERPLANT - FUEL AND HYDRAULIC HOSE REPLACEMENT

MANDATORY

-

MOC :

SL 525A-71-03 POWER PLANT - FUEL AND HYDRAULIC HOSE REPLACEMENT

MANDATORY

-

MOC :

SB FJ44-71-002 ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION

MANDATORY

E1

- N/A

NOT APPLICABLE - SUPERSEDED N/A BY ENG S/N. (SBR1111/AC240311/LR300311).MOC :

SB FJ44-71-002 ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION

MANDATORY

E2

- N/A

NOT APPLICABLE - SUPERSEDED N/A BY ENG S/N. (SBR1111/AC240311/LR300311).MOC :

SB FJ44-71-002 R2 ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION

MANDATORY

E1

- N/A

NOT APPLICABLE - N/A BY ENG S/N. (SBR /AC /LR030711).MOC :

SB FJ44-71-002 R2 ENGINE - HP COMPRESSOR - BORESCOPE INSPECTION

MANDATORY

E2

- N/A

NOT APPLICABLE - N/A BY ENG S/N. (SBR /AC /LR030711).MOC :

SB FJ44-72-042 R6 INSTALL REAR MOUNT SLEEVE

OPTIONAL

E1

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 501, 1001 – 1072. (SBR3211/120811/LR200811)MOC :

SB FJ44-72-042 R6 INSTALL REAR MOUNT SLEEVE

OPTIONAL

E2

A/R N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 501, 1001 – 1072. (SBR3211/120811/LR200811)MOC :

SB FJ44-72-042R4 INSTALL REAR MOUNT SLEEVE

OPTIONAL

E1

- N/A

NOT APPLICABLE - SUPERSEDED BY R6. NOT APPLICABLE BY SERIAL NUMBER.

(SBR11/AC240311/LR240311

MOC :

SB FJ44-72-042R4 INSTALL REAR MOUNT SLEEVE

OPTIONAL

E2

- N/A

NOT APPLICABLE - SUPERSEDED BY R6. NOT APPLICABLE BY SERIAL NUMBER.

(SBR11/AC240311/LR240311)

MOC :

SB FJ44-72-043 INSTALL DIFFUSER/BYPASS DUCT FUEL TUBES

E1

-

MOC :

SB FJ44-72-043 INSTALL DIFFUSER/BYPASS DUCT FUEL TUBES

E2

-

MOC :

SB FJ44-72-047 REWORK REAR MOUNT SLEEVE

N/A BY SERIAL

NUMBER

E1

- N/A

NOT APPLICABLE - BY SERIAL NUMBER ONLY APPLICABLE TO ENG S/N 1019, 1048, 1954, 1059-1069,

1066, 1071-1090 (LR-D030908)

MOC :

SB FJ44-72-047 REWORK REAR MOUNT SLEEVE

N/A BY SERIAL

NUMBER

E2

- N/A

NOT APPLICABLE - BY SERIAL NUMBER ONLY APPLICABLE TO ENG S/N 1019, 1048, 1954, 1059-1069,

1066, 1071-1090 (LR-D030908)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-048 LOCKWIRE NO.1 BEARING RETAINING NUT

RECOMMENDED

E1

-

MOC :

SB FJ44-72-048 LOCKWIRE NO.1 BEARING RETAINING NUT

RECOMMENDED

E2

-

MOC :

SB FJ44-72-049 REPLACE BLEED VALVE SHAFT

SUPERSEDED

E1

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY SB FJ44-72-063 R2.MOC :

SB FJ44-72-049 REPLACE BLEED VALVE SHAFT

SUPERSEDED

E2

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY SB FJ44-72-063 R2.MOC :

SB FJ44-72-051 R3 REWORK NAMEPLATE

RECOMMENDED

E1

- N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 1001 - 1143. (SBR3211/PP120811/)MOC :

SB FJ44-72-051 R3 REWORK NAMEPLATE

RECOMMENDED

E2

- N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 1001 - 1143. (SBR3211/PP120811/)MOC :

SB FJ44-72-051R1 REWORK NAMEPLATE

RECOMMENDED

E1

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY R3(SBR3211/PP120811/)MOC :

SB FJ44-72-051R1 REWORK NAMEPLATE

RECOMMENDED

E2

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY R3(SBR3211/PP120811/)MOC :

SB FJ44-72-054 R4 ENGINE - GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE1 - N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 1001-1143, 126001-126080. (SBR3211/PP1208117)MOC :

SB FJ44-72-054 R4 ENGINE - GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE2 - N/A

NOT APPLICABLE - ONLY APPLICABLE S/N 1001-1143, 126001-126080. (SBR3211/PP1208117)MOC :

SB FJ44-72-054 R6 GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE1 -

MOC :

SB FJ44-72-054 R6 GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE2 -

MOC :

SB FJ44-72-054R1 GEARBOX ASSEMBLY-INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE1 - N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY REV 2. ONLY APPLICABLE TO ENGINE S/N'S - 1001

TO 1143 AND 126001-126080.

MOC :

SB FJ44-72-054R1 GEARBOX ASSEMBLY-INCORPORATE NEW FUEL PUMP ADAPTER

RECOMMENDEDE2 - N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY REV 2. ONLY APPLICABLE TO ENGINE S/N'S - 1001

TO 1143 AND 126001-126080.

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-054 ENGINE - GEARBOX ASSEMBLY - INCORPORATE NEW FUEL PUMP ADAPTER

OPTIONALE1 -

MOC :

SB FJ44-72-055R1 REPLACE SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER

E1 -

MOC :

SB FJ44-72-055R1 REPLACE SEAL & BEARING RETAINER HOUSING AND LP REAR BEARING SEAL RETAINER

E2 -

MOC :

SB FJ44-72-058R2 BREATHER TUB-SERVICE ISLAND PORT-CAPPING

RECOMMENDED

E1

-03-Nov-2008MTH Complete

1754.72HRS

1626LDG

COMPLIED WITHMOC :

SB FJ44-72-058R2 BREATHER TUB-SERVICE ISLAND PORT-CAPPING

RECOMMENDED

E2

-03-Nov-2008MTH Complete

1871.32HRS

1706LDG

COMPLIED WITHMOC :

SB FJ44-72-062 R3 ENGINE - GEARBOX - INSPECTION

MANDATORY

E1

- N/A

NOT APPLICABLE - N/A BY ENGINE S/N INSTALLED: 126265MOC :

SB FJ44-72-062 R3 ENGINE - GEARBOX - INSPECTION

MANDATORY

E2

- N/A

NOT APPLICABLE - N/A BY ENGINE S/N INSTALLED: 126266MOC :

SB FJ44-72-063 R3 ENGINE - IP BLEED VALVE - REPLACE

RECOMMENDED

E1

-06-Jan-2014MTH N/A

3360.98HRS

2979LDG

NOT APPLICABLEMOC :

SB FJ44-72-063 R3 ENGINE - IP BLEED VALVE - REPLACE

RECOMMENDED

E2

-06-Jan-2014MTH N/A

3361.02HRS

2980LDG

NOT APPLICABLEMOC :

SB FJ44-72-063R1 ENGINE - IP BLEED VALVE - REPLACE

SUPERSEDED

E1

A/R N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY REV 2. (ORIGINAL DISPATCH

SBR036/D130908/A170908)

MOC :

SB FJ44-72-063R1 ENGINE - IP BLEED VALVE - REPLACE

SUPERSEDED

E2

A/R N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY REV 2. (ORIGINAL DISPATCH

SBR036/D130908/A170908)

MOC :

SB FJ44-72-064 ENGINE - 1ST REDUCTION BEVEL GEAR BEARING SUPPORT - REWORK OR REPLACE

RECOMMENDEDE1 A/R06-Jan-2014MTH N/A

3360.98HRS

2979LDG

NOT APPLICABLE - N/A DUE TO SB CANCELLED, NO LONGER AVAILABLEMOC :

SB FJ44-72-066 R5 ENGINE - CARBON RING SEAL AND BEARING HOUSING - REPLACE

RECOMMENDEDE1 -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-066 R5 ENGINE - CARBON RING SEAL AND BEARING HOUSING - REPLACE

RECOMMENDEDE2 -

MOC :

SB FJ44-72-066 R6 CARBON RING SEAL AND BEARING HOUSING - REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-72-066 R6 CARBON RING SEAL AND BEARING HOUSING - REPLACE

RECOMMENDED

E2

-

MOC :

SB FJ44-72-066 ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE

RECOMMENDEDE1 A/R03-Nov-2008MTH Complete

1754.72HRS

1626LDG

COMPLIED WITHMOC :

SB FJ44-72-066 ENGINE - HOUSING, CARBON RING SEAL AND BEARING (NO. 3 BEARING RETAINER) - REPLACE

RECOMMENDEDE2 A/R03-Nov-2008MTH Complete

1871.32HRS

1706LDG

COMPLIED WITHMOC :

SB FJ44-72-068 R3 ENGINE - UPGRADE GEARBOX (4K MAGSEAL) TO SPRING LOADED CONFIGURATION

OPTIONALE1 - N/A

NOT APPLICABLE - N/A BY S/N. ONLY APPLICABLE TO ENG S/N 1001-1143, 126001-126235.

(SBR1111/AC240311/LR300311)

MOC :


OPTIONALE2 - N/A

NOT APPLICABLE - N/A BY S/N. ONLY APPLICABLE TO ENG S/N 1001-1143, 126001-126235.

(SBR1111/AC240311/LR300311)

MOC :

SB FJ44-72-068 UPGRADE GEARBOX (4K MAGSEAL) TO SPRING LOADED CONFIGURATION

SUPERSEDEDE1 -

MOC :

SB FJ44-72-070 R2 ENGINE- UPGRADE GEARBOX (4K SPRING-LOADED) TO IMPROVED CONFIGURATION

OPTIONALE1 A/R

- OPEN OPTIONAL - NOT COVERED BY JSSI. TO BE RE-EVALUATED BEFORE CHECK 4 OR GEARBOX

CHANGE. INCLUDED AS TEMP OP ON CHECK 4. ONLY CAN BE PERFORMED AT WILLIAMS INT.

FACILITIES. (SBR03/D040210/A070210)

MOC :

SB FJ44-72-070 R2 ENGINE- UPGRADE GEARBOX (4K SPRING-LOADED) TO IMPROVED CONFIGURATION

OPTIONALE2 A/R

- OPEN OPTIONAL - NOT COVERED BY JSSI. TO BE RE-EVALUATED BEFORE CHECK 4 OR GEARBOX

CHANGE. INCLUDED AS TEMP OP ON CHECK 4. ONLY CAN BE PERFORMED AT WILLIAMS INT.

FACILITIES. (SBR03/D040210/A070210)

MOC :

SB FJ44-72-075 R1 ENGINE - GEARBOX P/N 78823 - INSPECTION

MANDATORY

E1

- N/A

NOT APPLICABLE - BY SERIAL NUMBER ONLY APPLICABLE TO ENG. S/N 1088.

(SBR03/D021110/A081110)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-075 R1 ENGINE - GEARBOX P/N 78823 - INSPECTION

MANDATORY

E2

- N/A

NOT APPLICABLE - BY SERIAL NUMBER ONLY APPLICABLE TO ENG. S/N 1088.

(SBR03/D021110/A081110)

MOC :

SB FJ44-72-077 R4 IP COMPRESSOR STATOR (STAGE 1-2) - REWORK

OPTIONAL

E1

UNK

-14-Apr-2015MTH Complete

3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-077 R4 IP COMPRESSOR STATOR (STAGE 1-2) - REWORK

OPTIONAL

E2

UNK

-02-Aug-2013MTH Complete

3148.87HRS

2799LDG

COMPLIED WITHMOC :

SB FJ44-72-079 R2 ENGINE - MPI - TIME EXTENSION FOR TAP ENGINES

INFORMATIONAL

E1

- N/A

NOT APPLICABLE - ENGINE NOT ENROLLED TO TOTAL ASSURANCE PROGRAM.

(SBR27/D021110/A081110)

MOC :

SB FJ44-72-079 R2 ENGINE - MPI - TIME EXTENSION FOR TAP ENGINES

INFORMATIONAL

E2

- N/A

NOT APPLICABLE - ENGINE NOT ENROLLED TO TOTAL ASSURANCE PROGRAM.

(SBR27/D021110/A081110)

MOC :

SB FJ44-72-080 R1 ENGINE - 2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE

RECOMMENDEDE1 -

MOC :

SB FJ44-72-080 R1 ENGINE - 2ND REDUCTION BEVEL GEAR BALL BEARING (GEARBOX ASSEMBLY) - REPLACE

RECOMMENDEDE2 -

MOC :

SB FJ44-72-085 R5 ENGINE – IP BLEED VALVE – REPLACE

E1

UNK


3465.4HRS

3075LDG

COMPLIED WITHMOC :

SB FJ44-72-085 R6 IP BLEED VALVE - REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-72-085 R6 IP BLEED VALVE - REPLACE

RECOMMENDED

E2

UNK


3265.47HRS

2893LDG

COMPLIED WITHMOC :

SB FJ44-72-085 ENGINE - IP BLEED VALVE - REPLACE

RECOMMENDED

E1

- N/A

NOT APPLICABLE - SUPERSEDED BY REVISION 1.MOC :

SB FJ44-72-086 R3 ENGINE – BLEED VALVE SHAFT – REPLACE

RECOMMENDED

E1

- N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A BY ENGINE SN INSTALLED: 126265.

(SBR27/D091210/A301210)

MOC :

SB FJ44-72-086 R3 ENGINE – BLEED VALVE SHAFT – REPLACE

RECOMMENDED

E2

- N/A

NOT APPLICABLE - BY SERIAL NUMBER N/A BY ENGINE SN INSTALLED: 126266.

(SBR27/D091210/A301210)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -


OPTIONALE1 -

MOC :


OPTIONALE2 -

MOC :

SB FJ44-72-104 ENGINE - UPGRADE GEARBOX (4K MAGSEAL) TO SPRING LOADED CONFIGURATION

OPTIONALE1 -

MOC :

SB FJ44-72-105 R2 UPGRADE GEARBOX (4K SPRING LOADED) TO IMPROVED CONFIGURATION

OPTIONALE1 UNK -14-Apr-2015MTH Complete

3540.9HRS

3112LDG

COMPLIED WITHMOC :


OPTIONALE2 UNK -06-Apr-2015MTH Complete

3540.9HRS

3112LDG

COMPLIED WITHMOC :


OPTIONALE1 -

MOC :


OPTIONALE2 -

MOC :

SB FJ44-72-107 R1 2ND REDUCTION PINION BEARING HOUSING - REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-72-107 R1 2ND REDUCTION PINION BEARING HOUSING - REPLACE

RECOMMENDED

E2

-

MOC :

SB FJ44-72-108 R1 ACCESSORY DRIVE SHAFT - REPLACE

RECOMMENDED

E1

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-108 R1 ACCESSORY DRIVE SHAFT - REPLACE

RECOMMENDED

E2

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-109 ENGINE - 1ST REDUCTION BEVEL GEAR BALL BEARING - REPLACE

RECOMMENDEDE1 UNK -14-Apr-2015MTH Complete

3540.9HRS

3112LDG

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-109 ENGINE - 1ST REDUCTION BEVEL GEAR BALL BEARING - REPLACE

RECOMMENDEDE2 UNK -06-Apr-2015MTH Complete

3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-119 HP COMPRESSOR ROTOR - REWORK

RECOMMENDED

E1

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-119 HP COMPRESSOR ROTOR - REWORK

RECOMMENDED

E2

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-123 R1 CANCELLED - INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE

CANCELLEDE1 -

MOC :

SB FJ44-72-123 R1 CANCELLED - INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE

CANCELLEDE2 -

MOC :

SB FJ44-72-123 INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE

MANDATORYE1 -

MOC :

SB FJ44-72-123 INNER GUIDED ROLLER BEARING (NO. 3 BEARING) - REPLACE

MANDATORYE2 -

MOC :

SB FJ44-72-126 HP SHAFT - REPLACE

MANDATORY

E1

-

MOC :

SB FJ44-72-126 HP SHAFT - REPLACE

MANDATORY

E2

-

MOC :

SB FJ44-72-129 REPLACE INNER GUIDED ROLLER BEARING (NO. 3 BEARING)

MANDATORYE1 -

MOC :

SB FJ44-72-129 REPLACE INNER GUIDED ROLLER BEARING (NO. 3 BEARING)

MANDATORYE2 -

MOC :

SB FJ44-72-130 HP COMPRESSOR ROTOR - INSPECTION

RECOMMENDED

E1

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-72-130 HP COMPRESSOR ROTOR - INSPECTION

RECOMMENDED

E2

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-72-134 1ST LP TURBINE NOZZLE HEATSHIELD HOUSING ASSEMBLY - REPLACE

RECOMMENDEDE1 -

MOC :

SB FJ44-72-134 1ST LP TURBINE NOZZLE HEATSHIELD HOUSING ASSEMBLY - REPLACE

RECOMMENDEDE2 -

MOC :

SB FJ44-72-140 GEARBOX HOUSING ASSEMBLY - INSPECTION

MANDATORY

E1

7541.3DUEHRS 3817.7

DUE

MOC :

SB FJ44-72-140 GEARBOX HOUSING ASSEMBLY - INSPECTION

MANDATORY

E2

7657.9DUEHRS 3934.3

DUE

MOC :

SB FJ44-72-143 BLEED VALVE SHAFT - REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-72-143 BLEED VALVE SHAFT - REPLACE

RECOMMENDED

E2

-

MOC :

SL 525A-73-01 6355003-6 ORIFICE AND AS5174-0404 UNION INSPECTION

RECOMMENDED A/R N/A

NOT APPLICABLE - ONLY APPLICABLE TO A/C S/N -0385 THRU -0391 (SBR16/D240409/A210509)MOC :

SL 525A-73-02 TRANSMITTAL OF WILLIAMS INTERNATIONAL SERVICE BULLETINFJ44-73-034, ENGINE AND FUEL CONTROL - FADEC

SOFTWARE UPLOAD OF CP294.03.01

RECOMMENDED A/RDAYS N/A

NOT APPLICABLE - BY SERIAL NUMBER APPLICABLE TO AIRCRAFT -0300 THRU -0460.MOC :

SB FJ44-73-016R1 FCU-REMOVE, REWORK, INSTALL PRESSURIZATION VALVE & PUMP SHAFT

MANDATORY &

PART 135 AUDIT

ITEM

E1 -

MOC :

SB FJ44-73-016R1 FCU-REMOVE, REWORK, INSTALL PRESSURIZATION VALVE & PUMP SHAFT

MANDATORY &

PART 135 AUDIT

ITEM

E2 -

MOC :

SB FJ44-73-018 R3 REPLACE INTEGRATED FUEL CONTROL UNIT

RECOMMENDED

E1

- N/A

NOT APPLICABLE - ONLY APPLICABLE SN1001 – 1143, 126001 – 126037, 501. (SBR3211/PP230312/)MOC :

SB FJ44-73-018 R3 REPLACE INTEGRATED FUEL CONTROL UNIT

RECOMMENDED

E2

- N/A

NOT APPLICABLE - ONLY APPLICABLE SN1001 – 1143, 126001 – 126037, 501. (SBR3211/PP230312/)MOC :

SB FJ44-73-018 R4 INTEGRATED FUEL CONTROL UNIT - REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-73-018 R4 INTEGRATED FUEL CONTROL UNIT - REPLACE

RECOMMENDED

E2

-

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

SB FJ44-73-018 R5 ENGINE FUEL AND CONTROL - INTEGRATED FUEL CONTROL UNIT - REPLACE

RECOMMENDEDE1 -

MOC :

SB FJ44-73-018 R5 ENGINE FUEL AND CONTROL - INTEGRATED FUEL CONTROL UNIT - REPLACE

RECOMMENDEDE2 -

MOC :

SB 525A-74-01 ENGINE IGNITION PRINTED CIRCUIT BOARD (PCB) REPLACEMENT

MANDATORY -

MOC :

SB FJ44-74-004 REPLACE 90 DEGREE IGNITION BRACKET

RECOMMENDED

E1

-

MOC :

SB FJ44-74-004 REPLACE 90 DEGREE IGNITION BRACKET

RECOMMENDED

E2

-

MOC :

SB 525A-76-02 FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) INTERFACE PCB IMPROVEMENT

MANDATORY A/R N/A

NOT APPLICABLE - BY SERIAL NUMBER ONLY APPLICABLE TO A/C S/N 300-371.MOC :

SB 525A-76-03 ENGINE CONTROLS - REMOVAL OF TRIM BOX WIRING

OPTIONAL

A/R

- OPEN COST BENEFIT ANALYSES. (SBR1911/PP050711/)MOC :

SB 525A-76-04 ENGINE CONTROLS - FADEC CONNECTOR WASHER REMOVAL

RECOMMENDED

A/R N/A

NOT APPLICABLE - BY SERIAL NUMBER APPLICABLE TO S/N:300 THRU 0478. (SBR40/D221110/A291110)MOC :

SL 525A-76-01 R1 ENGINE SYNCHRONIZER CONTROLLER INSPECTION

RECOMMENDED

-

MOC :

SB FJ44-77-005 REPLACE ITT JUMPER HARNESS ASSEMBLY

E1

-

MOC :

SB FJ44-77-005 REPLACE ITT JUMPER HARNESS ASSEMBLY

E2

-

MOC :

SB 525A-78-01 ENGINE EXHAUST NOZZLE DEFLECTOR TAB INSTALLATION

DISCRETIONARY

-

MOC :

SB 525A-78-02 R1 THRUST ATTENUATOR PADDLE IMPROVEMENT

MANDATORY

LSZH


2329.5HRS

2132LDG

COMPLIED WITH - COMPLIED WITH AT CCESC ON THE 11/08/10. COMPLIANCE WITH THIS SB IS THE

TERMINATING ACTION FOR THE LATEST REVISION OF ASL525A-78-01 (SBR08/D200210/A030310)

MOC :

SB 525A-78-02 THRUST ATTENUATOR PADDLE IMPROVEMENT

MANDATORY

LSZH


2329.5HRS

2132LDG

COMPLIED WITHMOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains

Service Bulletins

Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

ASL 525A-78-01 R1 THRUST ATTENUATOR PADDLE INSPECTION

MANDATORY

LSZH


2329.5HRS

2132LDG

COMPLIED WITH - COMPONENT REPLACEMENT C/W SB525A-78-02 R01- THRUST ATTENUATOR

PADDLE IMPROVEMENT, WHICH CONSTITUTES TERMINATING ACTION FOR SL525A-78-01

MOC :

ASL 525A-78-01 THRUST ATTENUATOR PADDLE INSPECTION

MANDATORY

LSZH


2329.5HRS

2132LDG

COMPLIED WITH - COMPONENT REPLACEMENTMOC :

SB 525A-79-01 TRANSMITER ORIFICE REPLACEMENT

MANDATORY

-21-Jan-2005MTH Complete

COMPLIED WITHMOC :

SB 525A-79-02 R1 ENGINE OIL BREATHER TUBE MODIFICATION

DISCRETIONARY

A/R03-Nov-2008MTH Complete

1737.42HRS

1626LDG

COMPLIED WITHMOC :

SB FJ44-79-007 R4 ENGINE - LUBE PUMP - REWORK TO P/N 110487

RECOMMENDED

E1

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-79-007 R4 ENGINE - LUBE PUMP - REWORK TO P/N 110487

RECOMMENDED

E2

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-79-011 R4 MAGNETIC SELF-CLOSING VALVE - REPLACE

MANDATORY

E1

UNK


3540.9HRS

3112LDG

COMPLIED WITHMOC :

SB FJ44-79-011 R4 MAGNETIC SELF-CLOSING VALVE - REPLACE

MANDATORY

E2

UNK


3265.47HRS

2893LDG

COMPLIED WITHMOC :

SB FJ44-79-012 LUBE OIL COOLER - REWORK OR REPLACE

RECOMMENDED

E1

-

MOC :

SB FJ44-79-012 LUBE OIL COOLER - REWORK OR REPLACE

RECOMMENDED

E2

-

MOC :

SB FJ44-79-015 OIL - LUBE AND SCAVENGE PUMP ASSEMBLY - TIME EXTENSION OF TIME BETWEEN OVERHAUL (TBO) FOR TOTAL

ASSURANCE PROGRAM (TAP)

RECOMMENDEDE1 -

MOC :

SB FJ44-79-015 OIL - LUBE AND SCAVENGE PUMP ASSEMBLY - TIME EXTENSION OF TIME BETWEEN OVERHAUL (TBO) FOR TOTAL

ASSURANCE PROGRAM (TAP)

RECOMMENDEDE2 -

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016

Part Number

Part Serial No



Remains

RemainsTSO 2

TSO 1

Airworthiness Directives

DUE 1

DUE 2

Adj.

+ or -

EASA 2007-0156 APPLIANCE AD - COMMUNICATION COMM UNITS & TRANSPONDERS MODIFICATION /REPLACEMENT

- N/A

NOT APPLICABLE - BY COMMUNICATION UNIT AND TRANSPONDER INSTALLED (GLOBAL NAVIGATION

SYSTEM GARMIN INSTALLED & TRANSPONDER GARMIN GTX330D)

MOC :

FAA 1998-25-02 APPLIANCE AD - BFGOODRICH SKYWATCH SKY497

MANDATORY

A/R13-Mar-2004MTH N/A

NOT APPLICABLEMOC :

FAA 2002-20-09 APPLIANCE AD - COLLINS AFD-3010 AFD UNITS

MANDATORY

A/R13-Mar-2004MTH Complete

COMPLIED WITHMOC :

FAA 2004-08-15 APPLIANCE AD - TAWS 8000 TERRAIN AWARENESS

MANDATORY

A/R22-May-2004MTH N/A

56HRS

NOT APPLICABLEMOC :

FAA 2006-16-18 APPLIANCE AD - SANDEL AVIONICS INCORPORATED MODEL ST3400 TERRAIN AWARENESS WARNING SYSTEM/RADIO

MAGNETIC INDICATOR(TAWS/RMI)

MANDATORY A/R N/A

NOT APPLICABLE - TAWS NOT INSTALLED. HONEYWELL MARL VIII INSTALLED.SUPERSEDED BY FAA

VAD 2006-16-18 R1

MOC :

TCCA CF-2009-44 APPLIANCE AD - EMERGENCY LOCATOR TRANSMITTER - POTENTIAL FAILURE TO TRANSMIT THE REQUIRED 406 MHZ CODED

SIGNAL

- N/A

NOT APPLICABLE - NOT APPLICABLE BY ELT UNIT P/N INSTALLED ( P/N 453-5000)MOC :

FAA 2008-02-06 TO DETECT AND CORRECT DEFECTIVE GARMIN GSM 85 SERVO GEARBOX UNITS

MANDATORY - N/A

NOT APPLICABLE - GARMIN GSM 85 SERVO GEARBOX NOT INSTALLED ON C525A.MOC :

EASA 2005-0021 HONEYWELL RCZ-83() AND RCZ-85() COMMUNICATION UNITS-

SUPERSEDED A/R19-Oct-2005MTH Complete

COMPLIED WITH - SUPERSEDED BY EASA AD 2007-0156MOC :

EASA 2006-0334 R1 APPLIANCE AD - COMMUNICATIONS - THALES COMMUNICATIONS VHF DATA RADIO - MODIFICATION - THALES

COMMUNICATIONS

-08-May-2013MTH N/A

NOT APPLICABLE - BY

VHF MANUFACTURER

INSTALLED (HONEYWELL)

MOC :

EASA 2014-0088 (1) REMOVE THE TEAM CVR P/N AP71232101 OR P/N AP71231101, AS APPLICABLE, FROM THE AIRCRAFT AND, DEPENDING ON

OPERATIONAL REGULATIONS, INSTALL A SERVICEABLE CVR IN ACCORDANCE WITH APPROVED AIRCRAFT MODIFICATION

INSTRUCTIONS

MANDATORY

-24-Apr-2014MTH N/A

NOT APPLICABLE - BY COCKPIT VOICE RECORDER P/N INSTALLEDMOC :

EASA 2014-0088 (2) DO NOT INSTALL ON ANY AIRCRAFT A TEAM CVR P/N AP71232101 OR P/N AP71231101, AS REQUIRED BY PARAGRAPH (2.1) OR

(2.2) OF THIS AD, AS APPLICABLE

MANDATORY

-24-Apr-2014MTH N/A





Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

EASA 2014-0088 COMMUNICATIONS - COCKPIT VOICE RECORDER - REPLACEMENT

MANDATORY -24-Apr-2014MTH N/A


FAA 2013-18-09 APPLIANCE AD - EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING DISCREPANCIES - HONEYWELL ASCA INC

(SUPERSEDED BY FAA AD 2014-17-02)

MANDATORY -30-Sep-2013DAYS N/A

NOT APPLICABLE - BY ELT TRANSMITTER UNIT P/N INSTALLED (P/N 453-5000)MOC :

EASA 2010-0152 APPLIANCE AD - OXYGEN MASK REGULATOR - MODIFICATION - INTERTECHNIQUE

MANDATORY A/R N/A

NOT APPLICABLE - BY PART NUMBER N/A BY OXYGEN MASK P/N INSTALLED P/N MC10-16-101.

(ADR30/D300710/A030810)

MOC :

EASA 2011-0093 APPLIANCE AD - EQUIPMENT / FURNISHINGS – EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA – MODIFICATION /

REPLACEMENT - CHELTON LIMITED

SUPERSEDED A/RMTH N/A

NOT APPLICABLE - SUPERSEDED SUPERSEEDED BY EASA AD 2011-0103 (LR)MOC :

EASA 2011-0094 APPLIANCE AD - EQUIPMENT AND FURNISHING – LIFE JACKET VACUUM BAG – MODIFICATION - AERAZUR

MANDATORY 6MTH N/A

NOT APPLICABLE - NOT APPLICABLE BY P/N (ADR21/AC070611/LR080611)MOC :

EASA 2011-0103 APPLIANCE AD - EQUIPMENT / FURNISHINGS - EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA - MODIFICATION /

REPLACEMENT - CHELTON LIMITED


NOT APPLICABLE - ONLY APPLICABLE TO CHELTON (COBHAM) ANTENNAS P/N 21-41. P/N INSTALLED

110-328-01. (ADR23/AC140611/LR200611)

MOC :

EASA 2012-0038 APPLIANCE AD - EQUIPMENT & FURNISHINGS - PASSENGER SEAT BACKREST LINK - INSPECTION / REPLACEMENT - SICMA

AERO SEAT

5MTH N/A

900HRS

NOT APPLICABLE - N/A TO PASSENGER SEAT INSTALLED P/N 63195XX. (ADR1112/PP220312/LR250312)MOC :

EASA 2013-0020 R1 APPLIANCE AD - EQUIPMENT & FURNISHINGS - SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSPECTION / REPLACEMENT

MANDATORY -05-Apr-2013MTH Complete

3049.55HRS

2743LDG

COMPLIED WITH - PC/W BY EASA VAD 2013-0020 PERFORMEDMOC :

EASA 2014-0125 (1) AMEND THE AFM OF AFFECTED AIRCRAFT TO INCORPORATE TEMPORARY CPI SIU OPERATING PROCEDURES BY INSERTING

A COPY OF APPENDIX 1 OF THIS AD (OR ITS TEXT) INTO THE APPLICABLE NORMAL PROCEDURES SECTION OF THE AFM

MANDATORY

-20-May-2014MTH N/A

NOT APPLICABLE - BY ANY ELT INSTALLEDMOC :

EASA 2014-0125 (2) ACCOMPLISH THE COMPLETE START-UP PROCEDURE/APPLICABLE START-UP PROCEDURE/SHUTDOWN PROCEDURE

MANDATORY

-20-May-2014MTH N/A


EASA 2014-0125 (3) COMPLIANCE WITH THE REQUIREMENTS OF PARAGRAPH (2) OF THIS AD

MANDATORY

-20-May-2014MTH N/A





Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

EASA 2014-0125 (4) REPLACE THE CPI SIU HAVING P/N 503-24 OR P/N 503-24-2 OR P/N 503-24-6 WITH AN IMPROVED UNIT P/N 503-24G OR P/N

503-24-2G OR P/N 503-24-6G IN ACCORDANCE WITH THE APPLICABLE AIRCRAFT DESIGN APPROVAL HOLDER SERVICE

INSTRUCTIONS AND, CONCURRENTLY, REMOVE THE TEMPORARY AFM PROCEDURE AS REQUIRED BY PARAGRAPH (2) OF

THIS AD

-

MOC :

EASA 2014-0125 (5) MODIFICATION OF AN AIRCRAFT AS REQUIRED BY PARAGRAPH (4) OF THIS AD CONSTITUTES TERMINATING ACTION FOR

ACCOMPLISHMENT OF THE PROCEDURES AS REQUIRED BY PARAGRAPH (2) OF THIS AD

MANDATORY

-20-May-2014MTH N/A


EASA 2014-0125 (6) FROM THE EFFECTIVE DATE OF THIS AD, INSTALLATION ON AN AIRCRAFT OF AN HR SMITH (TECHNICAL DEVELOPMENTS) CPI

SYSTEM SERIES 15-503-134-1 EQUIPPED WITH BRU P/N 503-21-1 AND SIU P/N 503-24 OR P/N 503-24-2 OR P/N 503-24-6 IS

ALLOWED, PROVIDED THE AIRCRAFT IS OPERATED IN COMPLIANCE WITH THE PROCEDURES AS REQUIRED BY THIS AD

MANDATORY

-20-May-2014MTH N/A


EASA 2014-0125 (7) AFTER REPLACEMENT OF THE CPI SIU ON AN AIRCRAFT AS REQUIRED BY PARAGRAPH (4) OF THIS AD, DO NOT INSTALL AN

SIU P/N 503-24 OR P/N 503-24-2 OR P/N 503-24-6 ON THE CPI SYSTEM OF THAT AIRCRAFT

MANDATORY

-20-May-2014MTH N/A


EASA 2014-0125 EQUIPMENT / FURNISHINGS - CRASH POSITION INDICATOR SYSTEM - REPLACEMENT; AIRCRAFT FLIGHT MANUAL -

AMENDMENT

MANDATORY -20-May-2014MTH N/A


FAA 1974-08-09 R3 LAVATORY PAPER OR LINEN WASTE RECEPTACLE FIRE PREVENTION

MANDATORY - N/A

NOT APPLICABLE - A/C DON'T HAVE LAVATORIES EQUIPPED WITH PAPER OR LINEN WASTE

RECEPTACLES. (ADR0812/PP090312/LR140312)

MOC :

FAA 2010-02-06 APPLIANCE AD - SICMA AERO SEAT 90XX AND 92XX SERIES PASSENGER SEATS

-08-May-2013MTH N/A

NOT APPLICABLE - BY TYPE

INSTALLED

MOC :

FAA 2011-07-05 APPLIANCE AD - SICMA AERO SEAT INSTALLED ON VARIOUS TRANSPORT CATEGORY AIRPLANES

A/R N/A

NOT APPLICABLE - N/A TO PASSENGER SEAT INSTALLED P/N 6319545-X. (ADR14/AC180411/LR200411)MOC :

FAA 2011-21-05 APPLIANCE AD - AVIOINTERIORS S.P.A. PASSENGER SEATS 12M()()-()()()()()()

MANDATORY -08-May-2013MTH N/A

NOT APPLICABLE - BY

PASSENGER SEAT

INSTALLED

MOC :

FAA 2011-21-08 APPLIANCE AD - SICMA AERO SEAT 88XX, 89XX, 90XX, 91XX, 92XX, 93XX, 95XX, AND 96XX SERIES PASSENGER SEAT

ASSEMBLIES

- N/A

NOT APPLICABLE - N/A BY P/N. ONLY APPLICABLE SICMA SEATS. P/N 4711371 AND 63195XX

INSTALLED. (ADR4311/PP021111/LR041111)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

FAA 2011-23-06 APPLIANCE AD - SICMA AERO SEAT PASSENGER SEAT ASSEMBLIES

- N/A

NOT APPLICABLE - ONLY APPLICABLE SICMA AERO SEAT PASSENGER. N/A BY MODEL. AMP

MANUFACTURER SEATS INSTALLED.SUPERSEDED BY AD2012-08-07

MOC :

FAA 2012-08-07 APPLIANCE AD - SICMA AERO SEAT PASSENGER SEAT ASSEMBLIES

- N/A

NOT APPLICABLE - ONLY APPLICABLE SICMA AERO SEAT PASSENGER. N/A BY MODEL. AMP

MANUFACTURER SEATS INSTALLED. (ADR1712/PP020512/LR120512)

MOC :

FAA 2015-10-02 (G) GENERAL VISUAL INSPECTION FOR CRACKING OF SEAT BACKREST LINKS HAVING PART NUMBER (P/N) 90-000200-104-1, P/N

90-000200-104-2, P/N 90-000202-104-1 AND P/N 90-000202-104-2

MANDATORY

SMF -07-Jul-2015MTH N/A

3571.8HRS

3141LDG

NOT APPLICABLE - COMPLIED WITH AD2015-10-02 EFFECTIVE ON JUNE 12, 2015 BY INSPECTING

AIRCRAFT. FOUND ZODIAC SEATS FRANCE PASSENGER SEATS NOT INSTALLED. NO FURTHER

ACTION REQUIRED.

MOC :

FAA 2015-10-02 (H) CORRECTIVE ACTIONS - CRACKING IS FOUND ON THE LINK

MANDATORY


3571.8HRS

3141LDG



ACTION REQUIRED.

MOC :

FAA 2015-10-02 (I) REPLACE ALL SEAT BACKREST LINKS, HAVING P/N 90-000200-104-1, P/N 90-000200-104-2, P/N 90-000202-104-1 AND P/N

90-000202-104-2, WITH NEW LINKS

MANDATORY


3571.8HRS

3141LDG



ACTION REQUIRED.

MOC :

FAA 2015-10-02 APPLIANCE AD - EQUIPMENT/FURNISHINGS - ZODIAC SEATS FRANCE - INSPECTION/REPLACEMENT

MANDATORYSMF -07-Jul-2015MTH N/A

3571.8HRS

3141LDG



ACTION REQUIRED.

MOC :

TCCA CF-2013-25 APPLIANCE AD - EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATION DISCREPANCIES

MANDATORY -20-Aug-2013DAYS N/A

NOT APPLICABLE - BY ELT TRANSMITTER UNIT PIN INSTALLED (PIN 453-5000).MOC :

EASA 2009-0251-E APPLIANCE/EMERGENCY AD - FIRE PROTECTION - PORTABLE FIRE EXTINGUISHERS - IDENTIFICATION / REPLACEMENT- FIRE

FIGHTING ENTERPRISES LIMITED

MANDATORY -08-May-2013DAYS N/A

NOT APPLICABLE - BY

PORTABLE FIRE

EXTINGUISHER P/N

INSTALLED ( P/N

A352TS & 892480)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

EASA 2009-0262 R1 APPLIANCE AD - FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/REPLACEMENT - FIRE FIGHTING

ENTERPRISES LIMITED

- N/A

NOT APPLICABLE - N/A BY FIRE EXTINGUISHERS MODELS (A352TS) INSTALLED.

(ADR04/D290110/A040210)

MOC :

EASA 2009-0262 APPLIANCE AD - FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION/REPLACEMENT - FIRE FIGHTING

ENTERPRISES LIMITED

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY EASA AD 2009-0262R1.MOC :

EASA 2009-0278 APPLIANCE AD - EASA - FIRE PROTECTION - PORTABLE HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION / REPLACEMENT

- SICLI

- N/A

NOT APPLICABLE - N/A BY FIRE EXTINGUISHER MODEL INSTALLEDMOC :

EASA 2010-0062 R1 APPLIANCE AD - HALON 1211 FIRE EXTINGUISHERS -IDENTIFICATION/REPLACEMENT - FIRE FIGHTING ENTERPRISES LIMITED

- N/A

NOT APPLICABLE - N/A BY FIRE EXTINGUISHER P/N INSTALLED. (ADR20/D270510/A280510)MOC :

EASA 2010-0062 APPLIANCE AD - FIRE PROTECTION - HALON 1211 FIRE EXTINGUISHERS - IDENTIFICATION / REPLACEMENT - FIRE FIGHTING

ENTERPRISES LIMITED

- N/A

NOT APPLICABLE - SUPERSEDED BY EASA VAD 2010-0062 R1MOC :

EASA 2012-0037 APPLIANCE AD - FIRE PROTECTION - HAND OPERATED FIRE EXTINGUISHER - MODIFICATION - KIDDE GRAVINER (A HAMILTON

SUNDSTRAND COMPANY)

6MTH N/A

NOT APPLICABLE - N/A BY FIRE EXTINGUISHER P/N INSTALLED. (ADR1112/PP220312/LR260312)MOC :

FAA 2005-17-11 PREVENT INCORRECT INSTALLATION OF WIRES TO THE ENGINE FIRE EXTINGUISHER BOTTLES

MANDATORY - Complete

COMPLIED WITH - PREVIOUSLY BY SB525A¿26¿02 PERFORMED 16 MAY 2005MOC :

FAA 2010-01-03 APPLIANCE AD - IDENTIFY AND REMOVE FROM SERVICE ALL AFFECTED FIRE EXTINGUISHERS AND REPLACE WITH

SERVICABLE UNITS

MANDATORY A/R N/A

NOT APPLICABLE - N/A BY HALON PORTABLE FIRE EXTINGUISHER INSTALLED (AMEREX MODEL

A352TS). (ADR01/D080110/A140110)

MOC :

FAA 2010-04-16 APPLIANCE AD - SICLI HALON 1211 PORTABLE FIRE EXTINGUISHERS AS INSTALLED ON VARIOUS AIRPLANES AND

ROTORCRAFT

- N/A

NOT APPLICABLE - N/A BY P/N PORTABLE FIRE EXTINGUISHER INSTALLED - AMEREX P/N A352TS.

(ADR08/D260210/A270210)

MOC :

FAA 2012-17-01 APPLIANCE AD - GOODYEAR AVIATION TIRES - N/A

NOT APPLICABLE - BY MANUFACTURER (MLG) AND BY PN (NLG). SEE Q-PULSE.MOC :

EASA 2008-0159 MODE-S TRANSPONDER (MST-67A) - MODIFICATION / REPLACEMENT

A/R N/A

NOT APPLICABLE - BY PART NUMBER MST67-A NOT INSTALLED. (ADR34/D290808/A290808)MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

EASA 2009-0097 APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER - CHECK / MODIFICATION - ROCKWELL COLLINS INC.

-08-May-2013MTH N/A

NOT APPLICABLE - SUPERSEDED BY

EASA AD 2010-0067

MOC :

EASA 2009-0173 R1 APPLIANCE AD - NAVIGATION – MODE S TRANSPONDER – MODIFICATION / REPLACEMENT - ROCKWELL COLLINS INC.

- N/A

NOT APPLICABLE - N/A BY TRANSPONDER PN INSTALLED (P/N 011-00455-30). (ADR40/D111010/A141010)MOC :

EASA 2009-0173 APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER - MODIFICATION/REPLACEMENT - ROCKWELL COLLINS

SUPERSEDED -08-May-2013MTH N/A

NOT APPLICABLE - SUPERSEDED BY

EASA AD 2009-0713

R1

MOC :

EASA 2009-0200 APPLIANCE AD - NAVIGATION - NARCO AVIONICS INC AT-150 MODE A/C TRANSPONDER -CHECK/MODIFICATION (VSB AT150

NO. 6, VAD 2004-08-16)

-08-May-2013MTH N/A

NOT APPLICABLE - TO EQUIPMENT

INSTALLED : GARMIN

GTX330D

MOC :

EASA 2010-0003 R1 APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER AIRCRAFT TYPE MODE STRAPPING - CHECK / MODIFICATION -

ROCKWELL COLLINS INC.

- N/A

NOT APPLICABLE - N/A BY TRANSPONDER MODEL (GARMIN) INSTALLED. (ADR02/D150110/A210110)MOC :

EASA 2010-0003 APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER AIRCRAFT TYPE MODE STRAPPING -CHECK / MODIFICATION

- N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY EASA AD 2010-0003R1. (ADR01/D020210/A140110)MOC :

EASA 2010-0067 APPLIANCE AD - NAVIGATION - MODE S TRANSPONDER - CHECK / MODIFICATION - ROCKWELL COLLINS INC.

MANDATORY A/R N/A

NOT APPLICABLE - NOT APPLICABLE TO EQUIPMENT INSTALLED: GARMIN GTX330D.MOC :

EASA 2010-0204 APPLIANCE AD - NAVIGATION SYSTEMS – MODE-S TRANSPONDER – MODIFICATION / REPLACEMENT - ROCKWELL-COLLINS

INC.

- N/A

NOT APPLICABLE - N/A BY TRANSPONDER PN 011-00455-30 INSTALLED. (ADR40/D111010/A141010);

(ADR23/AC200611/LR210611)

MOC :

EASA 2011-0043 APPLIANCE AD - NAVIGATION SYSTEMS – MODE-S TRANSPONDER CONTROL PANELS – MODIFICATION - GABLES

ENGINEERING INC.

-08-May-2013MTH N/A

NOT APPLICABLE - BY TRANSPONDER

MODEL GARMIN

INSTALLED

MOC :

EASA 2011-0239 APPLIANCE AD - NAVIGATION - RADIO ALTIMETER INDICATOR - MODIFICATION - SMS (TRADING AS COBHAM AVIONICS),

FORMERLY NEC AERO.

- N/A

NOT APPLICABLE - BY PN. WL102AMS6 INSTALLED. (AD0212/PP190112/LR030212)MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

FAA 2005-01-19 GTX330/330D SOFTWARE UPGRADE

MANDATORY

-20-Jun-2007MTH N/A

NOT APPLICABLE - NOT APPLICABLE BY SOFTWARE VERSION INSTALLEDMOC :

FAA 2006-16-18 R1 APPLIANCE AD - SANDEL ST3400 TAWS/RMI PLACARD

AIRWORTHINESS

A/R N/A

NOT APPLICABLE - TAWS NOT INSTALLED. HONEYWELL MARK VIII INSTALLED

(SBR24/D270608/A070708 )

MOC :

FAA 2009-05-05 TO PREVENT CERTAIN CONDITIONS FROM EXISTING WHEN PFDS DISPLAY INCORRECT ATTITUDE, ALTITUDE, AND AIRSPEED

INFORMATION

-DAYS N/A

NOT APPLICABLE - BY PART NUMBER COLLINS AVIONIC PFD'S INSTALLED. P/N - 822-1084-208.

(ADR09/D030309/A070509)

MOC :

FAA 2009-05-08 APPLIANCE AD - TRIMBLE OR FREEFLIGHT SYSTEMS 2101 I/O APPROACH PLUS POSITIONAING SYSTEM (GPS) NAVIGATION

SYSTEM (2101 I/O APPROACH PLUS SYSTEM)

MANDATORY A/R08-May-2013MTH N/A

NOT APPLICABLE - BY GPS

MANUFACTURER INSTALLED

(GARMIN)

MOC :

FAA 2009-08-01 APPLIANCE AD - NAVIGATION - HONEYWELL NZ-2000 NAVIGATION COMPUTERS AND IC-800 INTEGRATED AVIONICS

COMPUTERS - INDENTIFICATION/MODIFICATION

MANDATORY -08-May-2013DAYS N/A

NOT APPLICABLE - BY

FMS MANUFACTURER

INSTALLEDS ( UNIVERSAL

AVIONICS)

MOC :

FAA 2010-07-02 APPLIANCE AD - PERFORM A ONE-TIME GENERAL VISUAL INSPECTION OF THE MODIFICATION PLATE FOR THE HONEYWELL

PRIMUS II NV-850 NAVIGATION RECEIVER MODULE (NRM)

MANDATORY A/R08-May-2013MTH N/A

NOT APPLICABLE - BY INU

NOT INSTALLED

MOC :

FAA 2010-09-04 APPLIANCE AD - HONEYWELL INTERNATIONAL INC., PRIMUS EPIC AND PRIMUS APEX FLIGHT MANAGEMENT SYSTEMS.

- N/A

NOT APPLICABLE - NOT APPLICABLE BY FMS MANUFACTURER INSTALLEDS ( UNIVERSAL AVIONICS)MOC :

FAA 2012-02-08 APPLIANCE AD - AVIATION COMMUNICATIONS & SURVEILLANCE SYSTEMS (ACSS) TRAFFIC ALERT AND COLLISION

AVOIDANCE SYSTEM (TCAS) UNITS

- N/A

NOT APPLICABLE - NA BY P/N. TCAS P/N 805-11900-002 MANUFACTURED BY BF GOODRICH INSTALLED.

(ADR0612/PP150212/LR200212)

MOC :

FAA 2012-14-15 APPLIANCE AD - HONEYWELL INTERNATIONAL, INC. KGS200 MERCURY² SYSTEM SOFTWARE PROBLEM

MANDATORY - N/A

NOT APPLICABLE - BY MANUFACTURER - GARMIN GNS UNIT INSTALLED.MOC :

FAA 2012-26-15 R1 AIR DATA PRESSURE TRANSDUCERS, AS INSTALLED IN AIR DATA COMPUTERS (ADC), AIR DATA MODULES (ADM), AIR DATA

ATTITUDE HEADING REFERENCE SYSTEMS (ADAHRS), AND DIGITAL AIR DATA COMPUTERS (DADC)

MANDATORY -MTH

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

FAA 2012-26-15 APPLIANCE AD - HONEYWELL INTERNATIONAL INC. AIR DATA PRESSURE TRANSDUCERS REPLACEMENT

MANDATORY -10-Jan-2013DAYS N/A

NOT APPLICABLE - BY ADC PART NUMBER INSTALLED (P/N 822-1109-004)MOC :

FAA 2014-05-27 APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. TPR-720 AND TPR-900 MODE S TRANSPONDERS - TEST AND

CALIBRATION

MANDATORY -07-Apr-2014MTH N/A

NOT APPLICABLE - (G) (1) - NOT APPLICABLE BY TRANSPONDER P/N INSTALLED (P/N 011-00455-30).(G)

(2) - FOR INFORMATION.

MOC :

FAA 2014-18-01 APPLIANCE AD - NAVIGATION - ROCKWELL COLLINS, INC. MODE S TRANSPONDERS - INSPECTION / MODIFICATION

MANDATORY -MTH

MOC :

FAA 2015-10-51-E APPLIANCE/EMERGENCY AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO

LIMITATIONS SECTION OF THE AFM OR AFMS.


3571.8HRS

3141LDG

NOT APPLICABLE - COMPLIED WITH AD2015-10-51 DATED "EFFECTIVE UPON RECEIPT" BY INSPECTION

OF AIRCRAFT. FOUND AFFECTED EQUIPMENT NOT INSTALLED. AD IS NOT APPLICABLE PER

PARAGRAPH (C). NO FURTHER

MAINTENANCE ACTION REQUIRED.

MOC :

FAA 2015-10-51 APPLIANCE AD - AVIDYNE INTEGRATED FLIGHT DISPLAY (IFD)- INCORPORATE OPERATIONAL LIMITATIONS INTO LIMITATIONS

SECTION OF THE AFM OR AFMS


3571.8HRS

3141LDG

NOT APPLICABLE - COMPLIED WITH AD2015-10-51 EFFECTIVE ON JULY 1, 2015 BY INSPECTING

AIRCRAFT. FOUND AVIDYNE CORPORATION INTEGRATED FLIGHT DISPLAYS NOT INSTALLED. NO

FURTHER ACTION REQUIRED.

MOC :

EASA 2011-0090 R1 APPLIANCE AD - OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS – IDENTIFICATION / REPLACEMENT -

INTERTECHNIQUE (PART OF ZODIAC AEROSPACE), EROS

-13-May-2013MTH Complete

3078.22HRS

2765LDG

COMPLIED WITH - LETTER "I" WRITTEN ON THE BUSHING OF INFLATABLE HARNESS - S/O 125704MOC :

EASA 2011-0090 APPLIANCE AD - OXYGEN – OXYGEN MASK REGULATOR INFLATABLE HARNESS – IDENTIFICATION / REPLACEMENT -

INTERTECHNIQUE (PART OF ZODIAC AEROSPACE), EROS

MANDATORY 24MTH N/A

NOT APPLICABLE - SUPERSEDED SUPERSEDED BY REV 01. N/A BY OXYGEN MASKS REGULATOR S/N

INSTALLED: PILOT MASK S/N 116840; CO-PILOT MASK S/N 94444. (ADR20/AC070611/LR130611;

ADR21/AC070611/LR140611)

MOC :

EASA 2012-0254 (1) INSPECT/CHECK OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT OXYGEN MASK REGULATOR TO INDENTIFY THE P/N AND S/N

MANDATORY

-05-Dec-2012DAYS Complete

COMPLIED WITH - INSPECTION PERFORMED IN ACCORDANCE WITH MAINTENANCE RECORD AND

FOUND P/N MC10-16-101. SUPERSEDED BY EASA AD 2012-0254 R1

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

EASA 2012-0254

(2.1)

REPLACE OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT AFFECTED OXYGEN MASK REGULATOR

MANDATORY

-05-Dec-2012MTH N/A

NOT APPLICABLE - BY P/N FLIGHT CREW OXYGEN MASK REGULATOR INSTALLED (P/N MC10-16-101

INSTALLED). SUPERSEDED BY EASA AD 2012-0254 R1

MOC :

EASA 2012-0254 R1

(1)

INSPECT OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT EACH FLIGHT CREW OXYGEN MASK REGULATOR TO IDENTIFY THE P/N AND S/N

MANDATORY

-04-Jan-2013DAYS Complete

COMPLIED WITH - INSPECTION PERFORMED IN ACCORDANCE WITH MAINTENANCE RECORD AND

FOUND P/N MC10-16-101

MOC :

EASA 2012-0254 R1

(2.1)

REPLACE OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT EACH AFFECTED FLIGHT CREW OXYGEN MASK REGULATOR WITH A SERVICEABLE PART

MANDATORY

-04-Jan-2013DAYS N/A

NOT APPLICABLE - BY P/N FLIGHT CREW OXYGEN MASK REGULATOR INSTALLED (P/N MC10-16-101

INSTALLED)

MOC :

EASA 2012-0254 R1 APPLIANCE AD - OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT

MANDATORY -04-Jan-2013MTH N/A

NOT APPLICABLEMOC :

EASA 2012-0254 APPLIANCE AD - OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR -IDENTIFICATION / OPERATIONAL PROCEDURE /

REPLACEMENT

MANDATORY -05-Dec-2012MTH N/A

NOT APPLICABLE - SUPERSEDED BY EASA AD 2012-0254 R1MOC :

FAA 2007-26-11 INTERTECHNIQUE ZODIAC AIRCRAFT SYSTEMS, OXYGEN RESERVE CYLINDERS

A/R N/A

NOT APPLICABLE - OXYGEN CYLINDER MANUFACTURED BY B/E AEROSPACE (AQQUIRED PURITAN

BENNETT)

MOC :

FAA 2009-21-10 R1 APPLIANCE AD - FAA - AVOX SYSTEMS AND B/E AEROSPACE OXYGEN CYLINDER ASSEMBLIES VENDOR AD

LFPB -25-Feb-2010MTH N/A

2137.02HRS

1960LDG

NOT APPLICABLE - N/A BY OXYGEN CYLINDER P/N 176274-50 INSTALLED. (ADR03/D250110/A290110)MOC :

FAA 2009-21-10 INSPECT TO DETERMINE THE SERIAL NUMBER OF THE OXYGEN CYLINDER ASSEMBLIES INSTALLED IN THE AIRPLANE

LFPB -25-Feb-2010MTH N/A

2137.02HRS

1960LDG

NOT APPLICABLE - N/A BY OXYGEN CYLINDER P/N 176274-50 INSTALLED. SUPERSEDED BY FAA AD

2009-21-10 R1

MOC :

FAA 2010-11-05 APPLIANCE AD - INSPECT FOR AND REMOVE SUBSTANDARD OXYGEN CYLINDERS FROM AIRPLANE


NOT APPLICABLE - N/A BY OXYGEN CYLINDERS P/N AND S/N INSTALLED.MOC :

FAA 2011-01-09 APPLIANCE AD - B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE) UNITS HAVING PART NUMBER (P/N) 119003-11

N/A N/A

NOT APPLICABLE - ONLY APPLICABLE TO P/N 119003-11. P/N INSTALLED IS 15-40F-11.

(ADR01/120111/A160111)

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

FAA 2011-04-09 OXYGEN GENERATOR DEACTIVATION - N/A

NOT APPLICABLE - SUPERSEDED BY AD2012-11-09 (PP290612/LR05/07/2012). NO CHEMICAL OXYGEN

GENERATOR INSTALLED. (ADR10/AC160311/LR200311).

MOC :

FAA 2011-14-08 APPLIANCE AD - B/E AEROSPACE, CONTINUOUS FLOW PASSENGER OXYGEN MASK ASSEMBLY

SMF A/R07-Jul-2015MTH Complete

3571.8HRS

3141LDG

COMPLIED WITH - COMPLIED WITH AD2011-14-08 EFFECTIVE ON AUGUST 19, 2011 BY

ACCOMPLISHING THE B/E AEROSPACE SERVICE BULLETIN 174080-35-04, REV 000, DATED SEPTEMBER

6, 2010.

TRANS.

MOC :

FAA 2012-11-09 OXYGEN SYSTEM RESTORATION - N/A

NOT APPLICABLE - A/C WITHOUT CHEMICAL OXYGEN GENERATOR INSTALLED.

THIS AD SUPERSEDES AD 2011-04-09. (PP/LR050712)

MOC :

FAA 2015-08-07

PARA (G)

INSPECT THE INFLATABLE HARNESS FITTED TO EACH FLIGHTCREW OXYGEN MASK REGULATOR TO DETERMINE IF THE

INFLATABLE HARNESS IS INSTALLED WITH A PART NUMBER AND A BATCH NUMBER IDENTIFIED IN APPENDIX I OF ZODIAC

AEROSPACE SERVICE BULLETIN MXH-35-240, REVISION 7, DATED SEPTEMBER 1, 2011

MANDATORY

SMF -07-Jul-2015MTH Complete

3571.8HRS

3141LDG

COMPLIED WITH - COMPLIED WITH AD2015-08-07 EFFECTIVE ON JUNE 16, 2015 BY INSPECTING THE

CREW OXYGEN MASKS PER THE ZODIAC AEROSPACE SERVICE BULLETIN MXH-35-240, REVISION 7,

DATED SEPTEMBER 1,

2011. FOUND BOTH CREW OXYGEN MASKS WERE SERVICEABLE.

MOC :

FAA 2015-08-07

PARA (H)

REPLACE THE INFLATABLE HARNESS IDENTIFIED IN PAPRGRAPH G WITH A NEW OR RE-IDENTIFIED HARNESSES

MANDATORY

SMF -07-Jul-2015MTH Complete

3571.8HRS

3141LDG



DATED SEPTEMBER 1,


MOC :

FAA 2015-08-07 APPLIANCE AD - OXYGEN - ZODIAC AEROTECHNICS (FORMERLY INTERTECHNIQUE AIRCRAFT SYSTEMS) FLIGHTCREW

OXYGEN MASK REGULATORS - INSPECTION / REPLACEMENT OF INFLATABLE HARNESSES

MANDATORYSMF -07-Jul-2015MTH Complete

3571.8HRS

3141LDG



DATED SEPTEMBER 1,


MOC :

FAA 2015-23-09

PARA (G)

INSPECT EACH FLIGHTCREW OXYGEN MASK REGULATOR TO IDENTIFY THE PART NUMBER AND SERIAL NUMBER

MANDATORY

SCK -MTH N/A

3668HRS

3239LDG

NOT APPLICABLE - AD DOES NOT APPLY DUE TO PART NUMBER/SERIAL NUMBER OF OXYGEN MASKS

ARE NOT LISTED IN ZODIAC AEROSPACE S/B MCF-SBU-35-001, REV 1, DATED DECEMBER 3, 2012.

MOC :




Tracking Rate

Average Daily

UtilizationHours

Events/

Landings

Last Actual

Date

AIRCRAFT .483723.6 3304 30-Apr-2016

ENG 1 .483706.3 3290 30-Apr-2016

ENG 2 .483589.7 3210 30-Apr-2016

AIR COND .172396.5 30-Apr-2016

J & J AVIATION

525A - CJ2

13-Mar-2004

Aircraft Model:

Owner:

Airworthiness:

Print Date:


10:33PM09-May-2016



Remains


Remains

TSO 1

TSO 2



DUE 1

DUE 2

Adj.

+ or -

FAA 2015-23-09

PARA (H)(1)

REPLACE EACH AFFECTED FLIGHTCREW OXYGEN MASK WITH A PART IDENTIFIED IN PARAGRAPH (H)(1)(I) OR (H)(1)(II).

MANDATORY

SCK -MTH N/A

3668HRS

3239LDG



MOC :

FAA 2015-23-09

PARA (H)(2)(I)

REVISE THE EMERGENCY PROCEDURES SECTION OF THE AIRPLANE FLIGHT MANUAL (AFM) BY INSERTING THE STATEMENT

PROVIDED IN FIGURE 1

MANDATORY

SCK -MTH N/A

3668HRS

3239LDG



MOC :

FAA 2015-23-09

PARA (H)(2)(II)

FABRICATE AND INSTALL A PLACARD ON THE FLIGHTCREW OXYGEN MASK CONTAINER THAT STATES: "USE SELECTOR ON

100% OR EMERGENCY ONLY."

MANDATORY

SCK -MTH N/A

3668HRS

3239LDG



MOC :

FAA 2015-23-09

PARA (I)

REGULATOR REPLACEMENT

MANDATORY

SCK

-27-Jan-2016MTH N/A

3668HRS

3239LDG



MOC :

FAA 2015-23-09 OXYGEN - ZODIAC AEROTECHNICS (FORMERLY INTERTECHNIQUE AIRCRAFT SYSTEMS) FLIGHT CREW OXYGEN MASK

REGULATORS - INSPECTION / REPLACEMENT OF OXYGEN MASK REGULATORS

MANDATORYSCK -27-Jan-2016MTH N/A

3668HRS

3239LDG



MOC :

FAA 2008-03-10 INSPECT THE LOWER WING SKIN STRUCTURE, FORWARD WING SPAR, LOWER FUSELAGE SKIN, FAIRINGS, AND THE

EXTERNAL FAIRING FRAMES FOR CORROSION; REPAIR ANY DAMAGE FOUND; APPLY A CORROSION INHIBITIVE SEALANT TO

THE FUSELAGE FAIRINGS BEFORE REINSTALLING; AND DISABLE THE COCKPIT MOUNTED PILOT RELIEF TUBE

AIRWORTHINESS A/R N/A

NOT APPLICABLE - AIRCRAFT NOT EQUIPPED WITH COCKPIT RELIEF TUBE (ADR06/D130208/A180208)MOC :

FAA 2010-12-01 DETECT AND CORRECT LOOSE AND DAMAGED FASTENERS, AND CRACKS IN THRUST ATTENUATOR PADDLES

MANDATORYLSZH A/R11-Aug-2010MTH Complete

2329.5HRS

2132LDG


FAA 2009-24-13 DETECT AND CORRECT LOOSE AND DAMAGED FASTENERS AND CRACKS IN THE THRUST ATTENUATOR PADDLES -

SUPERSEDED BY AD 2010-12-01

SUPERSEDEDLSZH A/R11-Aug-2010DAYS Complete

2329.5HRS

2132LDG




CESCOM 10 - Aircraft Status Report...CESCOM 10 - Aircraft Status Report Tracking Rate Average Daily...

Documents

Transcript of CESCOM 10 - Aircraft Status Report...CESCOM 10 - Aircraft Status Report Tracking Rate Average Daily...