N708AA Aircraft Specifications

Transcription

1 N708AA Aircraft Specifications GENERAL INFORMATION Model No. B Manufacturer Line No Registration No. N708AA Date of Manufacture Manufacturer Boeing Selcal DGEK Serial No Configuration AEI Cargo Mod. Variable No. QB805 Status CVG OPERATIOL WEIGHTS Max Taxi Weight 195,500 lb Max Zero Fuel Weight 155,000 lb Max Takeoff Weight 195,000 lb Operating Empty Weight 94,050 lb Max Landing Weight 164,000 lb Fuel Capacity 54,000 lb TIME/CYCLE DATA - FUSELAGE All data as of: Total Hours C Check Interval 3000 Hrs / 24 months Total Cycles Last C Check C Next C Check Hrs / Total Hours Remaining to Next C Ck 2368 Hrs / 9 months Total Cycles LANDING GEAR Part Number Serial Number Time since Overhaul Nose BB Hrs / 41 months Left H Hrs/ 17 months Right E Hrs/ 17 months Last Overhaul Interval Time Remaining Nose Hrs/120 months Hrs / 79 months Left Hrs/120 months Hrs / 103 months Right Hrs/120 months Hrs / 103 months AUXILIARY POWER UNIT Part No. Serial No. GTCP85-98C P-15464C TIME / CYCLES DATA - ENGINE Serial No. Engine Type Total Time / Cycles Remaining to Limit Limiting Item JT8D-9A Hrs / Cyc 3495 Cyc C4 Due: 07/20/14 SB JT8D-9A Hrs / Cyc 2148 Cyc T1 Due: 01/24/14 SB JT8D-9A Hrs / Cyc 3812 Cyc T1 / T2 Due: 11/18/14 SB 6431

2 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:14 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 708 Sub Location: #1 Status: SERVICEABLE Time On A/C: FHRS = 62,482:01 CYCS = 34,542 Date = 01/12/2012 Utilization Rates/Day >> FHRS:3.9 CYCS:3.0 (Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR 61,956:10 525:51-88, JT8D-9A CYC 34, , NO LIMITS ENGINE, JT8D CAL 03/07/2011 0Y10M 5D - 3, POS: #1 GRN No.> FHR INSTALLED 1,792:34-11, /24/ CYC WITH 1, ,000 9,645 10, ,355 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 2Y 7M18D - 4, FOR: L/L BBDUAP7390 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 4,283:06 16,000 11,884 4,116 16, /02/ CYC WITH 3, ,000 8,316 10,684 19, ,116 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y 5M 6D - 3, FOR: O/H BBDUAU1572 POS: OLY GRN No.> DUE >> DUE >> FHR INSTALLED 4,283:06 30,000 23,533 6, /26/ CYC WITH 3, ,000 14,682 5, ,467 FHR COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y 5M 6D - 3, FOR: L/L BBDUAJ4116 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 17,779 12, /26/ CYC WITH 3, ,000 16,493 3, ,507 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y 5M 6D - 1, FOR: L/L R91407 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 12,811 17, /09/ CYC WITH 3, ,000 10,787 9, ,213 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y 5M 6D - 1, FOR: L/L BBDUAJ8438 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 12,959 17, /25/ CYC WITH 3, ,000 10,831 9, ,169 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y 5M 6D - 1, FOR: L/L P59870 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 14,303 15, /20/ CYC WITH 3, ,000 9,291 10, ,709 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y 5M 6D - 3, FOR: L/L BENCAP5654 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 4,283:06 30,000 4,283 25, /19/ CYC WITH 3, ,000 3,816 16, ,184 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y 5M 6D - 2, FOR: L/L BENCAW9553 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 4,283 25, /19/ CYC WITH 3, ,000 3,816 16, ,184 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y 5M 6D - 1, FOR: L/L BENCAW4482 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,283:06 30,000 4,283 25, /19/ CYC WITH 3, ,000 3,816 16, ,184 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y 5M 6D - 2, FOR: L/L BENCAW9524 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,303 15, /20/ CYC WITH 4, ,000 9,291 10, ,709 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BENCAP1462 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,303 15, /20/ CYC WITH 4, ,000 9,291 10, ,709 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BENCAP5493 POS: OLY GRN No.> DUE >>

3 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:14 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 708 Sub Location: Status: SERVICEABLE Time On A/C: FHRS = CYCS = Date = Utilization Rates/Day >> FHRS: CYCS: Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR INSTALLED 6,037:23 30,000 14,303 15, /20/ CYC WITH 4, ,000 9,291 10, ,709 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BBDUAU5069 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,304 15, /20/ CYC WITH 4, ,000 9,291 10, ,709 CYC TURBINE DISK,T1 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BKLBCU1398 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,303 15, /25/ CYC WITH 4, ,000 9,291 6, ,709 CYC TURBINE DISK,T2 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BLDLCB2921 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,303 15, /25/ CYC WITH 4, ,000 9,291 6, ,709 CYC TURBINE DISK,T3 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BKDLCC0473 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,037:23 30,000 14,303 15, /20/ CYC WITH 4, ,000 9,291 10, ,709 CYC TURBINE DISK,T4 CAL ASSEMBLY 9Y 5M18D - 3, FOR: L/L BLDLCM7958 POS: OLY GRN No.> DUE >> *** END OF REPORT ***

4 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 708 Sub Location: #2 Status: SERVICEABLE Time On A/C: FHRS = 62,482:01 CYCS = 34,542 Date = 01/12/2012 Utilization Rates/Day >> FHRS:3.9 CYCS:3.0 (Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR 61,057:48 1,424:13-50, , JT8D-9A CYC 33, , , ,208 - NO LIMITS ENGINE, JT8D CAL 01/11/2010 2Y 0M 1D - 2, , POS: #2 GRN No.> FHR INSTALLED 1,424:13-10, /27/ CYC WITH 1, ,000 6,167 13, ,833 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 2Y 0M 2D - 3, FOR: L/L BBDUAT8861 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 16,000 13,371 2,629 16, /16/ CYC WITH 3, ,000 12,535 6,465 19, ,629 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAU9246 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAY3601 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAY0389 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAY1364 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAY7296 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BENCAP2476 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BENCAR5724 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 3,661 26, /10/ CYC WITH 3, ,000 3,208 16, ,792 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y10M18D - 2, FOR: L/L BENCAW3348 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BENCAR6694 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BENCAR8857 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BENCAR7550 POS: OLY GRN No.> DUE >>

5 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 708 Sub Location: Status: SERVICEABLE Time On A/C: FHRS = CYCS = Date = Utilization Rates/Day >> FHRS: CYCS: Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR INSTALLED 3,661:00 30,000 13,371 16, /04/ CYC WITH 3, ,000 12,535 7, ,465 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BBDUAY1726 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 17,215 12, /01/ CYC WITH 3, ,000 17,840 2, ,160 CYC TURBINE DISK,T1 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L S42637 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /12/ CYC WITH 3, ,000 12,535 3, ,465 CYC TURBINE DISK,T2 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BLDLCG7208 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 13,371 16, /12/ CYC WITH 3, ,000 12,535 3, ,465 CYC TURBINE DISK,T3 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L BLDLCC0662 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,661:00 30,000 20,215 9, /19/ CYC WITH 3, ,000 13,132 6, ,868 CYC TURBINE DISK,T4 CAL ASSEMBLY 5Y11M 9D - 2, FOR: L/L P87399 POS: OLY GRN No.> DUE >> *** END OF REPORT ***

6 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 708 Sub Location: #3 Status: SERVICEABLE Time On A/C: FHRS = 62,482:01 CYCS = 34,542 Date = 01/12/2012 Utilization Rates/Day >> FHRS:3.9 CYCS:3.0 (Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR 58,535:36 3,946:25-66, , JT8D-9A CYC 30, , , ,646 - NO LIMITS ENGINE, JT8D CAL 01/21/2007 4Y11M22D - 1, , POS: #3 GRN No.> FHR 61,359:02 1,122: , ,740-10/18/ CYC 33, , ,000 7,108 12,892-4, ,072-12,892 CYC COMPRESSOR DISK, C1 CAL 05/17/2010 1Y 7M26D - 4, , ,842 - FOR: L/L BBDUAP7387 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 23,342 6, /13/ CYC WITH 3, ,000 14,549 5, ,658 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L N87863 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 22,395 7, /14/ CYC WITH 3, ,000 13,614 6, ,605 FHR COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BBDUAJ3827 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 16,590 13, /29/ CYC WITH 3, ,000 14,560 5, ,440 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L S58523 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 16,742 13, /29/ CYC WITH 3, ,000 13,648 6, ,352 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BBDUAT0172 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 16,742 13, /29/ CYC WITH 3, ,000 13,648 6, ,352 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BBDUAR9784 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 5,070 24, /15/ CYC WITH 3, ,904 13,507 5, ,397 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAJ8516 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 13,717 16, /12/ CYC WITH 3, ,000 10,041 9, ,959 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAN0164 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 3,946 26, /15/ CYC WITH 3, ,000 3,646 16, ,354 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAX2530 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 11,892 18, /20/ CYC WITH 3, ,000 9,841 10, ,159 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAM2944 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 10,400 19, /18/ CYC WITH 3, ,000 9,665 10, ,335 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAM8039 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 22,332 7, /18/ CYC WITH 3, ,000 15,599 4, ,401 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BENCAK5867 POS: OLY GRN No.> DUE >>

7 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 15:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-9A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 708 Sub Location: Status: SERVICEABLE Time On A/C: FHRS = CYCS = Date = Utilization Rates/Day >> FHRS: CYCS: Forecast) RCN / CCI PART # / DESC CON INSTALLATION DATA SAFE LIFE CONTROLS OVERHAUL CONTROLS SHOP VISIT CONTROLS DUE DATA FOR # SERIAL NO. / POSITION TRL A/C DATA TSI LIMIT TSN RMNG LIMIT TSO RMNG LIMIT TSV RMNG FIRST DUE FHR INSTALLED 3,946:25 30,000 19,630 10, /26/ CYC WITH 3, ,000 16,034 3, ,966 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L R49856 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 16,180 13, /09/ CYC WITH 3, ,000 16,176 3, ,824 CYC TURBINE DISK,T1 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BKLBB17349 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 16,180 13, /09/ CYC WITH 3, ,000 16,176 3, ,824 CYC TURBINE DISK,T2 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BLDLBC9343 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 11,443 18, /14/ CYC WITH 3, ,000 9,601 6, ,399 CYC TURBINE DISK,T3 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L P79299 POS: OLY GRN No.> DUE >> FHR INSTALLED 3,946:25 30,000 13,609 16, /16/ CYC WITH 3, ,000 10,858 9, ,142 CYC TURBINE DISK,T4 CAL ASSEMBLY 5Y 0M14D - 1, FOR: L/L BLDLB21603 POS: OLY GRN No.> DUE >> *** END OF REPORT ***

8 CCIA Major Alterations (B727 acft) N708AA As of: 25-Mar-10 extracted from 337 forms and other sources Only currently installed alterations are listed. MA X-Ref (may be Item applicable) Subject Document 1 See American Airlines modification list for previously installed modifications 2 Fed Ex Stage 3 STC ST00350AT & SA5839NM 3 Cargo mod & interior - AEI AEI STC SA1797SO & SA1798SO 4 GPS antenna tripler Cotney EDM Mode "S" antenna doubler removal and re-installation Cotney EDM BM * Ventura 9G barrier STC ST00848LA Lower cargo smoke detector 7 BM by Holingsead STC ST00399LA-D 8 BM * Modification of fwd lav by Aero Design Services Drawing BB BM * Library cabinet Aero Analytics Drawing Altair ZFW weight increase STC ST00076SE 11 Altair MTGW weight increase STC ST00077SE 12 BM * Altair floor loading without reinforcement? STC 00731SE SIE STC ST00779LA (part of 13 BM * Vertical side restraints AEI P to F conversion) 14 Splitter locks SIE STC ST00778LA (part of AEI P to F conversion) 15 Floor beam SIE STC 00770LA (part of AEI P to F conversion) ASM EO IS&S DADC system for RVSM (STC ST009957SC) 17 EGPWS by EMTEQ STC ST2995AT 18 BM R0 Cargo door safety system AEI SB 04-02, MA BM R0 Remove eyebrow windows & install plates CCIA BM & STC ST01704SE 20 BM * Aux Fuel Tank Removal 708, ORDER 99CCAL-011M-1D Reactivate TCAS OHM , MM , 21 BM R0* 708,713,715,427 WD AEI Door Hinge Fail-Safe AD BM Hinge AA

9 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 1 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, TO PREVENT FATIGUE CRACKS OF INS DOC: AD THE FRONT SPAR WEB OF THE W/C: (a) CENTER SECTION OF THE WINGS B INS DOC: AD W/C: (a)(1) LAST 11/10/ ,098:47 32, WO: 4678 ITEM: 12 NEXT 35, MINIMUM CHECK: C INT> 3,000 INS DOC: AD W/C: (a)(2) INS DOC: AD W/C: (D)2(I) MOD DOC: SB MA : PE T 60, TO PREVENT FATIGUE CRACKING OF INS N/A THE FUSELAGE SKIN AND BONDED DOUBLER AREA ABOVE THE ENTRY DOORWAY. MOD DOC: SB MA : PE T 60, TO PREVENT DEGRADATION OF INS DOC: AD REV#: 1 STRUCTURAL CAPABILITIES W/C: SB MOD DOC: AD MA : TO DETECT AND CORRECT CRACKING INS DOC: AD OF THE REAR SPAR WEB, WHICH W/C: (a)(2) LAST 11/16/ ,098:47 32, COULD PERMIT FUEL LEAKAGE INTO WO: 4678 ITEM: 13 THE AIRFLOW MULTIPLIER NEXT 35, MINIMUM CHECK: C INT> 3,000 MOD DOC: SB-57A0182 MA : PE T 60, TO PREVENT FAILURE OF THE INS DOC: AD BEARING SUPPORT FITTING OF THE W/C: (A) FORWARD TRUNNION INS DOC: AD W/C: (e)/(f) LAST 01/08/ ,864:57 33, WO: 5593 ITEM: 12 NEXT 01/08/ , MINIMUM CHECK: C INT> 10 Y 12,000 MOD DOC: AD MA : PC 01/18/ ,355:00 26, FIND AND FIX CORROSION OR INS DOC: AD REV#: 1 CRACKING IN HINGE PINS OF HORIZ W/C: (e)PRT3 STAB S/B727-55A0090 WO: 3542 ITEM: 4 INS DOC: AD W/C: (e)PRT4 LAST 11/13/ ,096:06 32, NEXT 11/13/ ,096:06 MINIMUM CHECK: C INT> 96 M 12,000

10 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 2 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT DETACHMENT OF THE INS DOC: AD SHOULDER RESTRAINT HARNESS OF W/C: SU 02/12/2007 THE ATTENDANT OR OBSERVER SEAT FROM ITS MOUNTING BRACKET MOD DOC: AD MA : FIND AND FIX CRACKING OF UPPER INS DOC: AD REV#: 1 CHORD OR REAR SPAR OF THE WINGS W/C: (A) LAST 03/21/ ,833:37 30, SB WO: 3542 ITEM: 5 NEXT 34, MINIMUM CHECK: C INT> 4, TO REPAIR CRACKING IN THE LOWER INS DOC: AD SKIN PANEL AT LOWER ROW OF W/C: KLH PE T 55, FASTENERS OF LAP JOINTS MINIMUM CHECK: C INT> 55,000 INS DOC: AD W/C: H LOW INS DOC: AD W/C: INT HJ PE T 35, MINIMUM CHECK: C INT> 35,000 INS DOC: AD W/C: LOW JKH INS DOC: AD W/C: MED H INS DOC: AD W/C: MED HJK INS DOC: AD W/C: MED L INS DOC: AD W/C: MOD H PE T 48, MINIMUM CHECK: C INT> 48, TO PREVENT CRACKING OF ELEVATOR INS N/A REV#: 1 HINGE SUPPORT RIBS S/B727-55A091 MOD DOC: AD MA : TM 01/11/ TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF MAIN DECK CARGO DOOR HINGE W/C: (A) PC 05/22/ ,843:11 28, OR FAILURE OF CARGO DOOR SYSTEM WO: 2552 ITEM: 85 INS DOC: AD W/C: (E) TM 04/15/ ,833:37 30, WO: 3542 ITEM: 98 FAA GRANTED 8 MO. EXTENSION TO AD INS DOC: AD W/C: A

11 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 3 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF MAIN DECK CARGO DOOR HINGE W/C: (B)&(F) PC 05/22/ ,843:11 28, OR FAILURE OF CARGO DOOR SYSTEM WO: 2552 ITEM: TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF MAIN DECK CARGO DOOR HINGE W/C: OR FAILURE OF CARGO DOOR SYSTEM INS DOC: AD W/C: (A) INS DOC: AD W/C: B,E&F INSPECTION OF WIRE BUNDLE FOR INS DOC: AD CHAFFING AT STANDBY HYD W/C: TM 01/02/ ,349:48 27, RESERVOIR AREA INSPECTION AND IF NECESSARY INS DOC: AD REPLACEMENT OF TITEFLEX HOSES W/C: TM 05/23/ ,843:11 28, TO PREVENT FAILURE OF A HOSE WO: 2552 ITEM: 90 WHEN EXPOSED TO FIRE. MOD DOC: AD MA : CW 05/30/ ,842:01 28, TO PREVENT INCAPACITATION OF INS DOC: AD FLIGHTCREW DUE TO LACK OF W/C: CW 05/29/ ,842:01 28, OXYGEN - TABLE 2 - FIGURE TO PREVENT HIGH-VELOCITY INS DOC: AD SEPARATION OF A BARREL, PISTON, W/C: OR END CAP FROM A HYDRAULIC ACCUMULATOR To prevent undesirable and INS N/A potentially dangerous pitch TM 06/02/2003 oscillations during coupled instrument landing system To prevent undetected cracking INS N/A of the H-11 bolts TM 03/07/ TO ENSURE ADEQUATE ELECTRICAL INS DOC: AB-29A67 BONDING BETWEEN THE PENETRATION W/C: ASB29A67 TM 06/03/2003 FITTINGS OF THE HYDRAULIC HEAT EXCHANGER AND THE REAR SPARS OF

12 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 4 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF THE WING AND FUEL LEAKS IN W/C: (G) CW 05/15/ ,898:06 29, THE AIRPLANE DUE TO STRESS CORROSION CRACKING OF THE WING INS DOC: AD W/C: (H)(1) CW 05/06/ ,863:05 30, COMPLETED ON >> WO: 3542 ITEM: 6 INS DOC: AD W/C: (h)(2) LAST 11/10/ ,801:48 33, WO: 4678 ITEM: 125 NEXT 11/10/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD W/C: (h)(3) LAST 11/13/ ,098:47 32, WO: 4678 ITEM: 126 NEXT 11/13/2012 MINIMUM CHECK: A INT> 48 M INS DOC: AD W/C: (h)(4) LAST 11/10/ ,801:48 33, WO: 4678 ITEM: 127 NEXT 11/10/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD W/C: (h)(5) LAST 11/13/ ,098:47 32, WO: 4678 ITEM: 128 NEXT 11/13/2012 MINIMUM CHECK: A INT> 48 M FATIGUE CRACKING OF THE ATTACH INS DOC: AD FITTINGS OF FOREFLAP CARRIAGE W/C: (f)1&2 LAST 12/14/ ,864:57 33, OF THE WINGS WO: 5593 ITEM: 83 NEXT 34, MINIMUM CHECK: A INT> 1,000 INS DOC: AD W/C: (h)&(m) CW 12/02/ ,096:06 32, COMPLETED ON >> WO: 4678 ITEM: TO PREVENT FATIGUE CRACKING OF INS DOC: AD THE FORWARD SUPPORT FITTING OF W/C: LAST 12/22/ ,864:57 33, THE #1 & #3 ENGINES WO: 5593 ITEM: 13 NEXT 12/22/ ,864:57 MINIMUM CHECK: C INT> 24 M 3,000 INS DOC: AD W/C: (j) CW 01/23/ ,679:22 30, INS DOC: AD W/C: (m) LAST 01/12/ ,864:57 33, WO: 5593 ITEM: 14 NEXT 01/12/ , MINIMUM CHECK: A INT> 24 M 3,000 INS DOC: AD W/C: AMC PE T 01/12/ , MINIMUM CHECK: A INT> 2 Y 2,500

13 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 5 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT FATIGUE CRACKING OF INS DOC: AD THE FORWARD SUPPORT FITTING OF W/C: AMC THE #1 & #3 ENGINES INS DOC: AD W/C: AMOC INS DOC: AD W/C: (g)AMOC TM 12/02/ ,022:19 32, TO DETECT CRACKS IN THE FRAMES, INS DOC: AD WHICH COULD RESULT IN CRACKS IN W/C: (G) PE T 40, THE SKIN PANELS AND RAPID MINIMUM CHECK: A INT> 3,500 DECOMPRESSION OF THE AIRCRAFT To prohibit the resetting of a INS N/A tripped circuit breaker for a TM 11/10/2005 fuel pump TO PREVENT LOSS OF STRUCTURAL INS DOC: AD INTERITY OF FWD ENTRY DOORWAY W/C: (f) DUE TO CRACKING AT BS INS DOC: AD W/C: (h) INS DOC: AD W/C: (h)r INS DOC: AD W/C: (j) PE T 34, MINIMUM CHECK: C INT> 4,500 INS DOC: AD W/C: (j)r MOD DOC: SB MA : PE T 60, TO PREVENT EXCESSIVE VIBRATION INS DOC: AD OF THE OUTBOARD AILERON BALANCE W/C: (g)(1) LAST 11/05/ ,792:44 33, TAB AND RUDDER TAB. WO: 4678 ITEM: 14 NEXT 11/05/ ,792:44 MINIMUM CHECK: C INT> 24 M 8,000 INS DOC: AD W/C: (g)(2) LAST 10/01/ ,385:12 34, WO: 5593 ITEM: 15 NEXT 07/01/ ,585:12 MINIMUM CHECK: C INT> 9 M 3,200 INS DOC: AD W/C: (G)(1)I CW 01/11/ ,425:54 31, INS DOC: AD W/C: (G)(2)I CW 04/20/ ,780:02 31,065.00

14 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 6 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** Shoulder restraint harness of INS N/A the attendant or observer seat detaching from the mounting bracket. MOD DOC: AD MA : TM 01/03/ TO DETECT AND CORRECT CHAFING INS DOC: AD OF THE FUEL BOOST PUMP W/C: (L) PE T 46, ELECTRICAL WIRING AND LEAKAGE MINIMUM CHECK: A INT> 15,000 OF FUEL INTO THE CONDUIT AND TO No Reason Entered For The Following Change(s): INS DOC: AD W/C: (L)INT CW 03/31/ ,731:08 31, INS DOC: AD W/C: (M) CW 06/08/ ,891:36 31, TO DECTECT AND CORRECT CRACKS INS DOC: AD IN THE SKIN, DOUBLER AND BEAR W/C: (g) STRAP AT THE HINGE CUTOUTS OF WO: 4678 ITEM: 16 THE FWD ENTRY DOOR INS DOC: AD W/C: (i)dvi LAST 11/20/ ,096:06 32, NEXT 35, MINIMUM CHECK: C INT> 3,000 INS DOC: AD W/C: (i)HFEC LAST 11/20/ ,096:06 32, NEXT 52, MINIMUM CHECK: C INT> 20,000 MOD DOC: AD MA : PE T 60, TO DETECT AND CORRECT A CRACKED INS DOC: AD PRESSURE BULKHEAD WEB, WHICH W/C: (F) PE T 40, COULD RESULT IN RAPID MINIMUM CHECK: C INT> 3,500 DECOMPRESSION OF THE AIRPLANE INS DOC: AD W/C: (F)(1) TO DETECT AND CORRECT FATIGUE INS DOC: AD CRACKS OF THE CROWN SKIN W/C: (F) PE T 66, MINIMUM CHECK: C INT> 3, TO PREVENT THE POTENTIAL FOR INS DOC: AD IGNITION SOURCES INSIDE FUEL W/C: (G) TM 12/12/ ,098:47 32, TANKS CAUSED BY LATENT FAILURES, ALTERATIONS, REPAIRS INS DOC: AD W/C: (H) PE T 03/28/2014 MINIMUM CHECK: A INT> 72 M

15 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 7 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT THE POTENTIAL FOR IGNITION SOURCES INSIDE FUEL TANKS CAUSED BY LATENT FAILURES, ALTERATIONS, REPAIRS TO PREVENT A FRACTURED SIDE INS DOC: AD STRUT, WHICH COULD RESULT IN W/C: (F) LAST 12/09/ ,098:47 32, COLLAPSE OF THE MLG WO: 4678 ITEM: 17 NEXT 12/09/2018 MINIMUM CHECK: C INT> 120 M INS DOC: AD W/C: (G) LAST 12/09/ ,098:47 32, WO: 4678 ITEM: 18 NEXT 12/09/2018 MINIMUM CHECK: C INT> 120 M TO DETECT AND CORRECT CRACKING INS DOC: AD IN THE VINYL INTERLAYER OR W/C: (f) #2 LAST 10/23/ ,410:42 34, DAMAGE TO THE STRUCTURAL INNER NEXT 10/23/ ,910:42 GLASS PANES OF THE FLIGHT DECK MINIMUM CHECK: C INT> 36 M 7,500 INS DOC: AD W/C: (f)#2 I CW 11/10/ ,096:06 32, COMPLETED ON >> WO: 4678 ITEM: 19 INS DOC: AD W/C: (f)4/5 INS DOC: AD W/C: (f)4/5I WO: 4678 ITEM: 20 MOD DOC: AD MA : TM 12/09/ ,098:47 32, To prevent cracking of the INS DOC: AD elevator rear spar at the tab W/C: (f) hinge locations INS DOC: AD W/C: (i) INS DOC: AD W/C: (n) INS DOC: AD W/C: (q) TM 10/16/ ,745:31 33, To detect and correct damage to INS DOC: AD the aft attachement lugs of the W/C: (f) PE T 12/24/ ,235:29 37, elevator quadrant support MINIMUM CHECK: C INT> 30 M 4,000 3,000 assembly that could lead to the INS DOC: AD W/C: (f)i CW 06/24/ ,235:29 34, INS DOC: AD W/C: Pt 3

16 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 8 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** To detect and correct damage to the aft attachement lugs of the elevator quadrant support assembly that could lead to the To ensure that insulation INS DOC: AD blankets constructed of AN-26 W/C: (f) are removed from the fuselage To prevent an electrical fault INS DOC: AD in the fuel pump system W/C: (f) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M INS DOC: AD W/C: (g) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M INS DOC: AD W/C: (h) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M TO detect and correct cracking INS DOC: AD of the LH/RH side web posts & W/C: (f) shear ties of the kickload beam. INS DOC: AD W/C: (f)int PE T 64,872:39 35, MINIMUM CHECK: C INT> 4,000 3,000 INS DOC: AD W/C: (f)INT To detect and correct failure INS DOC: AD of the engine fuel suction feed W/C: (f) PE T 04/16/ ,059:19 of the fuel system MINIMUM CHECK: C INT> 36 M 7,000 INS DOC: AD W/C: (f)int CW 04/16/ ,057:52 34, To detect and correct cracking INS DOC: AD in the aft pressure bulkhead W/C: (g)(1) web, which could adversely affect the structural integrity INS DOC: AD W/C: (g)(1)I PE T 37, MINIMUM CHECK: A INT> 3,500 INS DOC: AD W/C: (g)(2) INS DOC: AD W/C: (g)(2)I

17 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 9 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** To detect and correct scribe INS DOC: AD lines which can develop into W/C: (g) PE T 03/01/2013 fatigue cracks in the skin MINIMUM CHECK: A INT> 24 M INS DOC: AD W/C: INS DOC: AD W/C: a INS DOC: AD W/C: b INS DOC: AD W/C: c To provide the flight crew with INS N/A more complete procedures if all TM 09/12/1969 generators are lost To prevent possible stabilizer INS N/A flutter from mismatch of the PC 06/24/1981 elevator balance panel aft hinges in bays 2 and TO PREVENT RUPTURE OF ENGINE INS N/A FUEL FEED HOSE ASSEMBILES REWORK THRUST REVERSER INS N/A MAIN LANDING GEAR LOCK INS DOC: AD REV#: 3 INSPECTION W/C: C-115 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C INS DOC: AD W/C: C LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C INS DOC: AD W/C: C-123 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C

18 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 10 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** MAIN LANDING GEAR LOCK INS DOC: AD REV#: 3 INSPECTION W/C: C LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C TO ASSURE THE FLIGHT CREW HAS INS N/A POSITIVE WARNING WHEN THE L/E PC 11/17/1982 DEVICES ARE NOT EXTENDED FOR TAKEOFF TO PREVENT IN FLIGHT FIRES INS N/A PC 10/21/ LEADING EDGE SLAT ACTUATOR ASSY INS DOC: AD SB W/C: INS DOC: AD W/C: (A) TO PREVENT UNDETECTED PROLONGED INS N/A ENGINE STARTER PC 06/12/ TO ASSURE ADEQUATE LAVATORY INS N/A FIRE PROTECTION PC 06/15/ RAM AIR DUCT CORROSION INSP PER INS DOC: AD REV#: 1 PARA "B" VISUALLY INSPECT UPPER W/C: A1 LAST 11/10/ ,098:47 32, WALL OF AIR CONDITIONING RAM WO: 4678 ITEM: 34 AIR PLENUM CHAMBER IAW PART II NEXT 11/10/ ,098:47 MINIMUM CHECK: C INT> 48 M 8, TO REPLACE SEALED NEEDLE INS DOC: AD BEARINGS IN THE DOWNLOCK OUTER W/C: LH PE T 12/13/2020 LINK OF THE STRUT UPPER SEGMENT MINIMUM CHECK: A INT> 10 Y INS DOC: AD W/C: RH PE T 12/13/2020 MINIMUM CHECK: A INT> 10 Y

19 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 11 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** To eliminate the possibility of INS N/A a chemical reaction between TM 07/16/2007 atmospheric oxygen and volatile gases from the tire inner liner TO PREVENT MLG DOOR RELEASE INS N/A LEVER FROM MOVING TO THE DOOR PC 04/07/1988 OPEN POSITION DURING FLIGHT TO PREVENT MAIN LANDING GEAR INS N/A FAILURE TO EXTEND PROPERLY AS A RESULT OF STRUCTURAL FAILURE IN THE LOCK SYSTEM ENSURE STRUCTURE INTEGRITY OF INS DOC: AD WING UPPER SURFACE STRINGER S/B W/C: (A)(3) A159 INS DOC: AD W/C: (B)(1) INS DOC: AD W/C: (B)(2) LAST 03/29/ ,833:37 30, NEXT 41, MINIMUM CHECK: C INT> 11,000 MOD DOC: SB-57A159 MA : PE T 60, MAIN LANDING GEAR ACTUATOR INS DOC: AD JAMMING S/B W/C: PC 10/29/ TAKE-OFF WARNING SYS INS DOC: AD W/C: E INS DOC: AD W/C: N LAST 11/04/ ,432:59 34, WO: 5593 ITEM: 91 NEXT 62,632:59 MINIMUM CHECK: A INT> TO PREVENT FAILURE OF MLG INS N/A SUPPORT LINK SHAFT PC 02/07/ FAILURE OF THE MLG TO EXTEND AS INS N/A A RESULT OF LOOSENING OF THE PC 02/07/1990 SELF-LOCKING NUT AT THE ATTACHMENT OF THE DOWNLOCK FWD

20 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 12 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT BINDING OF THE INS N/A AILERON CONTROL WHEEL CAUSED BY PC 02/07/1990 INTERL DAMAGE IN THE AILERON POWER CONTROL UNIT TO PREVENT ENGINE SEPARATION INS N/A TM 03/07/ TO PREVENT NOSE AND MLG FAILURE INS N/A TO EXTEND PROPERLY DUE TO PC 01/01/1991 DISCONNECT OF LG CONTROL SELECTOR VALVE ACTUATOR ARM Takeoff configuration nuisance INS N/A warnings when taxi operations PC 01/01/ TO PREVENT STRUCTURAL FAILURE - INS N/A AGING AIRCRAFT MOD DOC: AD MA : MOD DOC: AD MA : PC 01/01/1991 MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60,000.00

21 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 13 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE - MOD DOC: AD AGING AIRCRAFT MA : MOD DOC: AD MA : MOD DOC: AD MA : MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : MOD DOC: AD MA : TM 12/18/2000 MOD DOC: AD MA : MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : TM 04/07/ ,833:37 30, MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : TM 05/19/2003 MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PC 01/01/ INBOARD TRAINING EDGE FLAPS INS DOC: AD INBOARD TRACK S/B & W/C: A1b(1) LAST 10/23/ ,410:42 34, WO: 4678 ITEM: 122 NEXT 04/23/ , MINIMUM CHECK: C INT> 18 M 3,000 INS DOC: AD W/C: A1b(2)

22 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 14 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** INBOARD TRAINING EDGE FLAPS INS DOC: AD INBOARD TRACK S/B & W/C: A1c LAST 10/23/ ,410:42 34, NEXT 04/23/ , MINIMUM CHECK: A INT> 18 M 3,000 MOD DOC: SB MA : PE T 60, BODY STATION 1183, PRESSURE INS DOC: AD BULKHEAD WEB S/B A0171 W/C: C INS DOC: AD W/C: G LAST 11/10/ ,098:47 32, WO: 4678 ITEM: 35 NEXT 35, MINIMUM CHECK: C INT> 3,500 MOD DOC: SB-53A0171 MA : PE T 60, AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF1 LAST 11/30/ ,096:06 32, MODEL 727 NEXT 11/30/2018 MINIMUM CHECK: C INT> 120 M W/C: C OF1 LAST 12/13/ ,864:57 33, WO: 5593 ITEM: 36 NEXT 12/13/2020 MINIMUM CHECK: C INT> 120 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 43 MINIMUM CHECK: C INT> 18 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 44 MINIMUM CHECK: C INT> 18 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 45 MINIMUM CHECK: C INT> 18 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 46 MINIMUM CHECK: C INT> 18 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 47 MINIMUM CHECK: C INT> 18 M W/C: C OF6 PE T 01/27/2012 WO: 4678 ITEM: 48 MINIMUM CHECK: C INT> 18 M W/C: C OF1 W/C: C OF1

23 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 15 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF4 LAST 01/26/ ,864:57 33, MODEL 727 WO: 5593 ITEM: 37 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 38 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 03/23/ ,833:37 30, WO: 3542 ITEM: 28 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF4 LAST 03/23/ ,833:37 30, WO: 3542 ITEM: 29 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF1 PE T 01/27/2012 WO: 4678 ITEM: 49 MINIMUM CHECK: C INT> 18 M W/C: C OF3 LAST 04/14/ ,833:37 30, NEXT 04/14/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF3 LAST 03/23/ ,833:37 30, NEXT 03/23/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF3 LAST 04/14/ ,833:37 30, NEXT 04/14/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF2 LAST 03/22/ ,833:37 30, NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF2 LAST 03/22/ ,833:37 30, NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF2 W/C: C OF2 PE T 03/31/2012 WO: 4678 ITEM: 50 MINIMUM CHECK: C INT> 36 M W/C: C OF1 W/C: C OF2 PE T 03/31/2012 WO: 4678 ITEM: 51 MINIMUM CHECK: C INT> 36 M

24 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 16 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF2 PE T 03/31/2012 MODEL 727 WO: 4678 ITEM: 52 MINIMUM CHECK: C INT> 36 M W/C: C OF1 W/C: C OF2 LAST 03/22/ ,833:37 30, NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF2 LAST 03/22/ ,833:37 30, NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C OF2 W/C: C OF2 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 53 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF4 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 39 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 40 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 03/23/ ,833:37 30, WO: 3542 ITEM: 44 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF4 LAST 03/23/ ,833:37 30, WO: 3542 ITEM: 45 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF1 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 41 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C OF1 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 42 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C OF3 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 43 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M

25 DATE: 01/13/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 15:40 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 17 AIRFRAME DATA AS OF: 01/12/2012 FLIGHT HOURS: 62,482:01 FLIGHT CYCLES: 34, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF3 LAST 01/26/ ,864:57 33, MODEL 727 WO: 5593 ITEM: 44 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C OF3 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 45 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C OF2 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 46 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M W/C: C OF2 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 55 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF1 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 56 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF1 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 57 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF1 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 58 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF1 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 59 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF1 LAST 12/13/ ,098:47 32, WO: 4678 ITEM: 60 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C OF3 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 47 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M W/C: C OF3 LAST 01/26/ ,864:57 33, WO: 5593 ITEM: 48 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M