N708AA Aircraft Specifications

N708AA Aircraft Specifications GENERAL INFORMATION Model No. B727-223 Manufacturer Line No. 1761 Registration No. N708AA Date of Manufacture 6-24-81 Manufacturer Boeing Selcal DGEK Serial No. 22465 Configuration AEI Cargo Mod. Variable No. QB805 Status Storage @ CVG 01-22-12 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: 04-30-12 Total Hours 62497 C Check Interval 3000 Hrs / 24 months Total Cycles 34554 Last C Check C-9 01-26-11 Next C Check Due @ 64865 Hrs / 01-13 Total Hours 61865 Remaining to Next C Ck 2368 Hrs / 9 months Total Cycles 33925 LANDING GEAR Part Number Serial Number Time since Overhaul Nose 65-72762-32 3BB112 2400 Hrs / 41 months Left 65-72761-35 6H96 632 Hrs/ 17 months Right 65-72761-36 8E56 632 Hrs/ 17 months Last Overhaul Interval Time Remaining Nose 11-28-08 20000 Hrs/120 months 17600 Hrs / 79 months Left 12-13-10 20000 Hrs/120 months 19368 Hrs / 103 months Right 12-13-10 20000 Hrs/120 months 19368 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 649184 JT8D-9A 88590 Hrs / 65166 Cyc 3495 Cyc C4 Due: 07/20/14 SB 6431 666377 JT8D-9A 50402 Hrs / 44363 Cyc 2148 Cyc T1 Due: 01/24/14 SB 6431 687796 JT8D-9A 66968 Hrs / 74804 Cyc 3812 Cyc T1 / T2 Due: 11/18/14 SB 6431

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.: 7200-0001-9184 CCI Part Number: JT8D-9A Mfg Serial Number: 649184 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 0 7200-0001-9184 FHR 61,956:10 525:51-88,575 - - - - - 526 - - JT8D-9A CYC 34,010.00 532.00-65,154 - - - - - 532 - NO LIMITS ENGINE, JT8D CAL 03/07/2011 0Y10M 5D - 3,458 - - - - - 318 - - 649184 POS: #1 GRN No.> 67826 1 7200-0002-7390 FHR INSTALLED 1,792:34-11,115 - - - - - - - 06/24/2021 848101 CYC WITH 1,827.00 20,000 9,645 10,355 - - - - - - 10,355 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 2Y 7M18D - 4,415 - - - - - - - FOR: L/L BBDUAP7390 POS: OLY GRN No.> N/A DUE >> 062421 1 7200-0003-1572 FHR INSTALLED 4,283:06 16,000 11,884 4,116 16,000 - - - - - 12/02/2014 745902 CYC WITH 3,816.00 19,000 8,316 10,684 19,000 - - - - - 4,116 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y 5M 6D - 3,432 - - - - - - - FOR: O/H BBDUAU1572 POS: OLY GRN No.> 16390 DUE >> 120214 DUE >> 120214 1 7200-0004-4116 FHR INSTALLED 4,283:06 30,000 23,533 6,467 - - - - - - 07/26/2016 799773 CYC WITH 3,816.00 20,000 14,682 5,318 - - - - - - 6,467 FHR COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y 5M 6D - 3,432 - - - - - - - FOR: L/L BBDUAJ4116 POS: OLY GRN No.> 16391 DUE >> 072616 1 7200-0005-1407 FHR INSTALLED 4,283:06 30,000 17,779 12,221 - - - - - - 03/26/2015 799504 CYC WITH 3,816.00 20,000 16,493 3,507 - - - - - - 3,507 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y 5M 6D - 1,985 - - - - - - - FOR: L/L R91407 POS: OLY GRN No.> 38885 DUE >> 032615 1 7200-0006-8438 FHR INSTALLED 4,283:06 30,000 12,811 17,189 - - - - - - 06/09/2020 745706 CYC WITH 3,816.00 20,000 10,787 9,213 - - - - - - 9,213 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y 5M 6D - 1,985 - - - - - - - FOR: L/L BBDUAJ8438 POS: OLY GRN No.> 38887 DUE >> 060920 1 7200-0007-9870 FHR INSTALLED 4,283:06 30,000 12,959 17,041 - - - - - - 05/25/2020 713105 CYC WITH 3,816.00 20,000 10,831 9,169 - - - - - - 9,169 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y 5M 6D - 1,985 - - - - - - - FOR: L/L P59870 POS: OLY GRN No.> 38886 DUE >> 052520 1 7200-0008-5654 FHR INSTALLED 4,283:06 30,000 14,303 15,697 - - - - - - 10/20/2021 815607 CYC WITH 3,816.00 20,000 9,291 10,709 - - - - - - 10,709 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y 5M 6D - 3,458 - - - - - - - FOR: L/L BENCAP5654 POS: OLY GRN No.> N/A DUE >> 102021 1 7200-0009-9553 FHR INSTALLED 4,283:06 30,000 4,283 25,717 - - - - - - 10/19/2026 822008 CYC WITH 3,816.00 20,000 3,816 16,184 - - - - - - 16,184 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y 5M 6D - 2,012 - - - - - - - FOR: L/L BENCAW9553 POS: OLY GRN No.> 38737 DUE >> 101926 1 7200-0010-4482 FHR INSTALLED 4,283:06 30,000 4,283 25,717 - - - - - - 10/19/2026 822109 CYC WITH 3,816.00 20,000 3,816 16,184 - - - - - - 16,184 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y 5M 6D - 1,985 - - - - - - - FOR: L/L BENCAW4482 POS: OLY GRN No.> 38888 DUE >> 101926 1 7200-0011-9524 FHR INSTALLED 4,283:06 30,000 4,283 25,717 - - - - - - 10/19/2026 821910 CYC WITH 3,816.00 20,000 3,816 16,184 - - - - - - 16,184 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y 5M 6D - 2,025 - - - - - - - FOR: L/L BENCAW9524 POS: OLY GRN No.> 38739 DUE >> 101926 1 7200-0012-1462 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 10/20/2021 815611 CYC WITH 4,978.00 20,000 9,291 10,709 - - - - - - 10,709 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BENCAP1462 POS: OLY GRN No.> 18112 DUE >> 102021 1 7200-0013-5493 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 10/20/2021 815612 CYC WITH 4,978.00 20,000 9,291 10,709 - - - - - - 10,709 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BENCAP5493 POS: OLY GRN No.> 18113 DUE >> 102021

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.: 7200-0001-9184 CCI Part Number: JT8D-9A Mfg Serial Number: 649184 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 1 7200-0014-5069 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 10/20/2021 5003613-01 CYC WITH 4,978.00 20,000 9,291 10,709 - - - - - - 10,709 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BBDUAU5069 POS: OLY GRN No.> 18114 DUE >> 102021 1 7200-0015-1398 FHR INSTALLED 6,037:23 30,000 14,304 15,696 - - - - - - 10/20/2021 587501 CYC WITH 4,978.00 20,000 9,291 10,709 - - - - - - 10,709 CYC TURBINE DISK,T1 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BKLBCU1398 POS: OLY GRN No.> 18115 DUE >> 102021 1 7200-0016-2921 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 02/25/2018 802522 CYC WITH 4,978.00 16,000 9,291 6,709 - - - - - - 6,709 CYC TURBINE DISK,T2 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BLDLCB2921 POS: OLY GRN No.> 18119 DUE >> 022518 1 7200-0017-0473 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 02/25/2018 618703 CYC WITH 4,978.00 16,000 9,291 6,709 - - - - - - 6,709 CYC TURBINE DISK,T3 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BKDLCC0473 POS: OLY GRN No.> 18120 DUE >> 022518 1 7200-0018-7958 FHR INSTALLED 6,037:23 30,000 14,303 15,697 - - - - - - 10/20/2021 769104 CYC WITH 4,978.00 20,000 9,291 10,709 - - - - - - 10,709 CYC TURBINE DISK,T4 CAL ASSEMBLY 9Y 5M18D - 3,458 - - - - - - - FOR: L/L BLDLCM7958 POS: OLY GRN No.> 18121 DUE >> 102021 *** END OF REPORT ***

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.: 7200-0001-6377 CCI Part Number: JT8D-9A Mfg Serial Number: 666377 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 0 7200-0001-6377 FHR 61,057:48 1,424:13-50,388 - - - - - 3,661 - - JT8D-9A CYC 33,079.00 1,463.00-44,351 - - - - - 3,208 - NO LIMITS ENGINE, JT8D CAL 01/11/2010 2Y 0M 1D - 2,169 - - - - - 2,148 - - 666377 POS: #2 GRN No.> 35299 1 7200-0002-8861 FHR INSTALLED 1,424:13-10,485 - - - - - - - 08/27/2024 848001 CYC WITH 1,463.00 20,000 6,167 13,833 - - - - - - 13,833 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 2Y 0M 2D - 3,453 - - - - - - - FOR: L/L BBDUAT8861 POS: OLY GRN No.> 21051 DUE >> 082724 1 7200-0003-9246 FHR INSTALLED 3,661:00 16,000 13,371 2,629 16,000 - - - - - 11/16/2013 745902 CYC WITH 3,208.00 19,000 12,535 6,465 19,000 - - - - - 2,629 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAU9246 POS: OLY GRN No.> 35322 DUE >> 111613 1 7200-0004-3601 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 799773 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAY3601 POS: OLY GRN No.> 35324 DUE >> 110418 1 7200-0005-0389 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 799504 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAY0389 POS: OLY GRN No.> 35325 DUE >> 110418 1 7200-0006-1364 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 745706 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAY1364 POS: OLY GRN No.> 35327 DUE >> 110418 1 7200-0007-7296 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 745705 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAY7296 POS: OLY GRN No.> 35326 DUE >> 110418 1 7200-0008-2476 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 815607 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BENCAP2476 POS: OLY GRN No.> 35328 DUE >> 110418 1 7200-0009-5724 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 815708 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BENCAR5724 POS: OLY GRN No.> 35330 DUE >> 110418 1 7200-0010-3348 FHR INSTALLED 3,661:00 30,000 3,661 26,339 - - - - - - 05/10/2027 822109 CYC WITH 3,208.00 20,000 3,208 16,792 - - - - - - 16,792 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y10M18D - 2,148 - - - - - - - FOR: L/L BENCAW3348 POS: OLY GRN No.> 39076 DUE >> 051027 1 7200-0011-6694 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 815610 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BENCAR6694 POS: OLY GRN No.> 35332 DUE >> 110418 1 7200-0012-8857 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 815611 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BENCAR8857 POS: OLY GRN No.> 35333 DUE >> 110418 1 7200-0013-7550 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 815612 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BENCAR7550 POS: OLY GRN No.> 35334 DUE >> 110418

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.: 7200-0001-6377 CCI Part Number: JT8D-9A Mfg Serial Number: 666377 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 1 7200-0014-1726 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 11/04/2018 5003613-01 CYC WITH 3,208.00 20,000 12,535 7,465 - - - - - - 7,465 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BBDUAY1726 POS: OLY GRN No.> 35335 DUE >> 110418 1 7200-0015-2637 FHR INSTALLED 3,661:00 30,000 17,215 12,785 - - - - - - 01/01/2014 587501 CYC WITH 3,208.00 20,000 17,840 2,160 - - - - - - 2,160 CYC TURBINE DISK,T1 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L S42637 POS: OLY GRN No.> 35336 DUE >> 010114 1 7200-0016-7208 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 03/12/2015 802522 CYC WITH 3,208.00 16,000 12,535 3,465 - - - - - - 3,465 CYC TURBINE DISK,T2 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BLDLCG7208 POS: OLY GRN No.> 35337 DUE >> 031215 1 7200-0017-0662 FHR INSTALLED 3,661:00 30,000 13,371 16,629 - - - - - - 03/12/2015 618703 CYC WITH 3,208.00 16,000 12,535 3,465 - - - - - - 3,465 CYC TURBINE DISK,T3 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L BLDLCC0662 POS: OLY GRN No.> 35338 DUE >> 031215 1 7200-0018-7399 FHR INSTALLED 3,661:00 30,000 20,215 9,785 - - - - - - 04/19/2018 769104 CYC WITH 3,208.00 20,000 13,132 6,868 - - - - - - 6,868 CYC TURBINE DISK,T4 CAL ASSEMBLY 5Y11M 9D - 2,169 - - - - - - - FOR: L/L P87399 POS: OLY GRN No.> 35339 DUE >> 041918 *** END OF REPORT ***

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.: 7200-0001-7796 CCI Part Number: JT8D-9A Mfg Serial Number: 687796 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 0 7200-0001-7796 FHR 58,535:36 3,946:25-66,954 - - - - - 3,946 - - JT8D-9A CYC 30,896.00 3,646.00-74,792 - - - - - 3,646 - NO LIMITS ENGINE, JT8D CAL 01/21/2007 4Y11M22D - 1,840 - - - - - 1,861 - - 687796 POS: #3 GRN No.> 41782 1 7200-0002-7387 FHR 61,359:02 1,122:59 - - - - 5,740 - - 5,740-10/18/2023 848101 CYC 33,434.00 1,108.00 20,000 7,108 12,892-4,072 - - 4,072-12,892 CYC COMPRESSOR DISK, C1 CAL 05/17/2010 1Y 7M26D - 4,043 - - 2,842 - - 2,842 - FOR: L/L BBDUAP7387 POS: OLY GRN No.> 55972 DUE >> 101823 1 7200-0003-7863 FHR INSTALLED 3,946:25 30,000 23,342 6,658 - - - - - - 09/13/2016 790832 CYC WITH 3,646.00 20,000 14,549 5,451 - - - - - - 6,658 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L N87863 POS: OLY GRN No.> 41784 DUE >> 091316 1 7200-0004-3827 FHR INSTALLED 3,946:25 30,000 22,395 7,605 - - - - - - 05/14/2017 799773 CYC WITH 3,646.00 20,000 13,614 6,386 - - - - - - 7,605 FHR COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BBDUAJ3827 POS: OLY GRN No.> 41785 DUE >> 051417 1 7200-0005-8523 FHR INSTALLED 3,946:25 30,000 16,590 13,410 - - - - - - 12/29/2016 799504 CYC WITH 3,646.00 20,000 14,560 5,440 - - - - - - 5,440 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L S58523 POS: OLY GRN No.> 41786 DUE >> 122916 1 7200-0006-0172 FHR INSTALLED 3,946:25 30,000 16,742 13,258 - - - - - - 10/29/2017 745706 CYC WITH 3,646.00 20,000 13,648 6,352 - - - - - - 6,352 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BBDUAT0172 POS: OLY GRN No.> 41788 DUE >> 102917 1 7200-0007-9784 FHR INSTALLED 3,946:25 30,000 16,742 13,258 - - - - - - 10/29/2017 745705 CYC WITH 3,646.00 20,000 13,648 6,352 - - - - - - 6,352 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BBDUAR9784 POS: OLY GRN No.> 41787 DUE >> 102917 1 7200-0008-8516 FHR INSTALLED 3,946:25 30,000 5,070 24,930 - - - - - - 12/15/2016 774407 CYC WITH 3,646.00 18,904 13,507 5,397 - - - - - - 5,397 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAJ8516 POS: OLY GRN No.> 41789 DUE >> 121516 1 7200-0009-0164 FHR INSTALLED 3,946:25 30,000 13,717 16,283 - - - - - - 02/12/2021 787208-001 CYC WITH 3,646.00 20,000 10,041 9,959 - - - - - - 9,959 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAN0164 POS: OLY GRN No.> 41790 DUE >> 021221 1 7200-0010-2530 FHR INSTALLED 3,946:25 30,000 3,946 26,054 - - - - - - 12/15/2026 822109 CYC WITH 3,646.00 20,000 3,646 16,354 - - - - - - 16,354 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAX2530 POS: OLY GRN No.> 41791 DUE >> 121526 1 7200-0011-2944 FHR INSTALLED 3,946:25 30,000 11,892 18,108 - - - - - - 04/20/2021 772510-001 CYC WITH 3,646.00 20,000 9,841 10,159 - - - - - - 10,159 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAM2944 POS: OLY GRN No.> 41792 DUE >> 042021 1 7200-0012-8039 FHR INSTALLED 3,946:25 30,000 10,400 19,600 - - - - - - 06/18/2021 815611 CYC WITH 3,646.00 20,000 9,665 10,335 - - - - - - 10,335 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAM8039 POS: OLY GRN No.> 41793 DUE >> 061821 1 7200-0013-5867 FHR INSTALLED 3,946:25 30,000 22,332 7,668 - - - - - - 01/18/2016 798512-001 CYC WITH 3,646.00 20,000 15,599 4,401 - - - - - - 4,401 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BENCAK5867 POS: OLY GRN No.> 41794 DUE >> 011816

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.: 7200-0001-7796 CCI Part Number: JT8D-9A Mfg Serial Number: 687796 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 1 7200-0014-9856 FHR INSTALLED 3,946:25 30,000 19,630 10,370 - - - - - - 08/26/2015 5003613-01 CYC WITH 3,646.00 20,000 16,034 3,966 - - - - - - 3,966 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L R49856 POS: OLY GRN No.> 41795 DUE >> 082615 1 7200-0015-7349 FHR INSTALLED 3,946:25 30,000 16,180 13,820 - - - - - - 07/09/2015 587501 CYC WITH 3,646.00 20,000 16,176 3,824 - - - - - - 3,824 CYC TURBINE DISK,T1 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BKLBB17349 POS: OLY GRN No.> 41796 DUE >> 070915 1 7200-0016-9343 FHR INSTALLED 3,946:25 30,000 16,180 13,820 - - - - - - 07/09/2015 802722 CYC WITH 3,646.00 20,000 16,176 3,824 - - - - - - 3,824 CYC TURBINE DISK,T2 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BLDLBC9343 POS: OLY GRN No.> 41799 DUE >> 070915 1 7200-0017-9299 FHR INSTALLED 3,946:25 30,000 11,443 18,557 - - - - - - 11/14/2017 618703 CYC WITH 3,646.00 16,000 9,601 6,399 - - - - - - 6,399 CYC TURBINE DISK,T3 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L P79299 POS: OLY GRN No.> 41797 DUE >> 111417 1 7200-0018-1603 FHR INSTALLED 3,946:25 30,000 13,609 16,391 - - - - - - 05/16/2020 769104 CYC WITH 3,646.00 20,000 10,858 9,142 - - - - - - 9,142 CYC TURBINE DISK,T4 CAL ASSEMBLY 5Y 0M14D - 1,840 - - - - - - - FOR: L/L BLDLB21603 POS: OLY GRN No.> 41798 DUE >> 051620 *** END OF REPORT ***

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 EDM31-1 5 Mode "S" antenna doubler removal and re-installation Cotney EDM31-2 6 BM-5310-05-00 * Ventura 9G barrier STC ST00848LA Lower cargo smoke detector 7 BM-2611-01-02 by Holingsead STC ST00399LA-D 8 BM-2540-01-07 * Modification of fwd lav by Aero Design Services Drawing BB99-1381 9 BM-2520-09-00 * Library cabinet Aero Analytics Drawing 981204 10 Altair ZFW weight increase STC ST00076SE 11 Altair MTGW weight increase STC ST00077SE 12 BM-5108-02-01* Altair floor loading without reinforcement? STC 00731SE SIE STC ST00779LA (part of 13 BM-5108-03-01 * 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 5586-2120-22465 16 IS&S DADC system for RVSM (STC ST009957SC) 17 EGPWS by EMTEQ STC ST2995AT 18 BM5230-0002R0 Cargo door safety system AEI SB 04-02, MA 5230-002 19 BM-5610-0001R0 Remove eyebrow windows & install plates CCIA BM-5610-001 & STC ST01704SE 20 BM-2810-02-01 * Aux Fuel Tank Removal 708, 713 709 712 ORDER 99CCAL-011M-1D Reactivate TCAS OHM 34-43-00, MM34-44-00, 21 BM-3445-0005R0* 708,713,715,427 WD 34-21-01 AEI Door Hinge Fail-Safe AD 2002-16-20 22 BM-5230-01-00 Hinge AA

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: 34,542.00 2000-02-19 TO PREVENT FATIGUE CRACKS OF INS DOC: AD-2000-02-19 THE FRONT SPAR WEB OF THE W/C: 2000-02-19 (a) CENTER SECTION OF THE WINGS B727-57-0177 INS DOC: AD-2000-02-19 W/C: 2000-02-19 (a)(1) LAST 11/10/2008 60,098:47 32,189.00 WO: 4678 ITEM: 12 NEXT 35,189.00 MINIMUM CHECK: C INT> 3,000 INS DOC: AD-2000-02-19 W/C: 2000-02-19 (a)(2) INS DOC: AD-2000-02-19 W/C: 2000-02-19(D)2(I) MOD DOC: SB-57-0177 MA : 5700-0177 PE T 60,000.00 2000-05-19 TO PREVENT FATIGUE CRACKING OF INS N/A THE FUSELAGE SKIN AND BONDED DOUBLER AREA ABOVE THE ENTRY DOORWAY. MOD DOC: SB-53-0186 MA : 5300-0186 PE T 60,000.00 2000-07-12 TO PREVENT DEGRADATION OF INS DOC: AD-2000-07-12 REV#: 1 STRUCTURAL CAPABILITIES W/C: SB57-127 MOD DOC: AD-94-07-08 MA : 5700-0127 2000-14-07 TO DETECT AND CORRECT CRACKING INS DOC: AD-2000-14-07 OF THE REAR SPAR WEB, WHICH W/C: 2000-14-07 (a)(2) LAST 11/16/2008 60,098:47 32,189.00 COULD PERMIT FUEL LEAKAGE INTO WO: 4678 ITEM: 13 THE AIRFLOW MULTIPLIER NEXT 35,189.00 MINIMUM CHECK: C INT> 3,000 MOD DOC: SB-57A0182 MA : 5700-0182 PE T 60,000.00 2001-20-09 TO PREVENT FAILURE OF THE INS DOC: AD-2001-20-09 BEARING SUPPORT FITTING OF THE W/C: 2001-20-09 (A) FORWARD TRUNNION INS DOC: AD-2001-20-09 W/C: 2001-20-09(e)/(f) LAST 01/08/2011 61,864:57 33,925.00 WO: 5593 ITEM: 12 NEXT 01/08/2021 45,925.00 MINIMUM CHECK: C INT> 10 Y 12,000 MOD DOC: AD-2001-20-09 MA : 5743-0001 PC 01/18/2001 52,355:00 26,688.00 2001-22-12 FIND AND FIX CORROSION OR INS DOC: AD-2001-22-12 REV#: 1 CRACKING IN HINGE PINS OF HORIZ W/C: 2001-22-12(e)PRT3 STAB S/B727-55A0090 WO: 3542 ITEM: 4 INS DOC: AD-2001-22-12 W/C: 2001-22-12(e)PRT4 LAST 11/13/2008 60,096:06 32,187.00 NEXT 11/13/2016 72,096:06 MINIMUM CHECK: C INT> 96 M 12,000

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: 34,542.00 *** CONTINUED *** 2001-24-02 TO PREVENT DETACHMENT OF THE INS DOC: AD-2001-24-02 SHOULDER RESTRAINT HARNESS OF W/C: 2001-24-02 SU 02/12/2007 THE ATTENDANT OR OBSERVER SEAT FROM ITS MOUNTING BRACKET MOD DOC: AD-2001-24-02 MA : 2510-0005 2002-04-06 FIND AND FIX CRACKING OF UPPER INS DOC: AD-2002-04-06 REV#: 1 CHORD OR REAR SPAR OF THE WINGS W/C: 2002-04-06 (A) LAST 03/21/2006 57,833:37 30,422.00 SB727-57-0184 WO: 3542 ITEM: 5 NEXT 34,922.00 MINIMUM CHECK: C INT> 4,500 2002-07-09 TO REPAIR CRACKING IN THE LOWER INS DOC: AD-2002-07-09 SKIN PANEL AT LOWER ROW OF W/C: 2002-07-09 KLH PE T 55,000.00 FASTENERS OF LAP JOINTS MINIMUM CHECK: C INT> 55,000 INS DOC: AD-2002-07-09 W/C: 2002-07-09H LOW INS DOC: AD-2002-07-09 W/C: 2002-07-09INT HJ PE T 35,000.00 MINIMUM CHECK: C INT> 35,000 INS DOC: AD-2002-07-09 W/C: 2002-07-09LOW JKH INS DOC: AD-2002-07-09 W/C: 2002-07-09MED H INS DOC: AD-2002-07-09 W/C: 2002-07-09MED HJK INS DOC: AD-2002-07-09 W/C: 2002-07-09MED L INS DOC: AD-2002-07-09 W/C: 2002-07-09MOD H PE T 48,000.00 MINIMUM CHECK: C INT> 48,000 2002-12-13 TO PREVENT CRACKING OF ELEVATOR INS N/A REV#: 1 HINGE SUPPORT RIBS S/B727-55A091 MOD DOC: AD-2002-12-13 MA : 5511-0002 TM 01/11/2003 2002-16-20 TO PREVENT STRUCTURAL FAILURE INS DOC: AD-2002-16-20 OF MAIN DECK CARGO DOOR HINGE W/C: 2002-16-20 (A) PC 05/22/2003 54,843:11 28,251.00 OR FAILURE OF CARGO DOOR SYSTEM WO: 2552 ITEM: 85 INS DOC: AD-2002-16-20 W/C: 2002-16-20 (E) TM 04/15/2006 57,833:37 30,422.00 WO: 3542 ITEM: 98 FAA GRANTED 8 MO. EXTENSION TO AD INS DOC: AD-2002-16-20 W/C: 2002-16-20 A

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: 34,542.00 *** CONTINUED *** 2002-16-20 TO PREVENT STRUCTURAL FAILURE INS DOC: AD-2002-16-20 OF MAIN DECK CARGO DOOR HINGE W/C: 2002-16-20(B)&(F) PC 05/22/2003 54,843:11 28,251.00 OR FAILURE OF CARGO DOOR SYSTEM WO: 2552 ITEM: 88 2002-16-22 TO PREVENT STRUCTURAL FAILURE INS DOC: AD-2002-16-22 OF MAIN DECK CARGO DOOR HINGE W/C: 2002-16-22 OR FAILURE OF CARGO DOOR SYSTEM INS DOC: AD-2002-16-22 W/C: 2002-16-22 (A) INS DOC: AD-2002-16-22 W/C: 2002-16-22 B,E&F 2002-17-05 INSPECTION OF WIRE BUNDLE FOR INS DOC: AD-2002-17-05 CHAFFING AT STANDBY HYD W/C: 2002-17-05 TM 01/02/2003 54,349:48 27,936.00 RESERVOIR AREA 2002-22-12 INSPECTION AND IF NECESSARY INS DOC: AD-2002-22-12 REPLACEMENT OF TITEFLEX HOSES W/C: 2002-22-12 TM 05/23/2003 54,843:11 28,251.00 TO PREVENT FAILURE OF A HOSE WO: 2552 ITEM: 90 WHEN EXPOSED TO FIRE. MOD DOC: AD-2002-22-12 MA : 7310-0001 CW 05/30/2003 54,842:01 28,250.00 2003-03-15 TO PREVENT INCAPACITATION OF INS DOC: AD-2003-03-15 FLIGHTCREW DUE TO LACK OF W/C: 2003-03-15 CW 05/29/2003 54,842:01 28,250.00 OXYGEN - TABLE 2 - FIGURE 1 2003-11-03 TO PREVENT HIGH-VELOCITY INS DOC: AD-2003-11-03 SEPARATION OF A BARREL, PISTON, W/C: 2003-11-03 OR END CAP FROM A HYDRAULIC ACCUMULATOR. 2003-11-19 To prevent undesirable and INS N/A potentially dangerous pitch TM 06/02/2003 oscillations during coupled instrument landing system 2004-09-36 To prevent undetected cracking INS N/A of the H-11 bolts TM 03/07/2007 2004-10-06 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

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: 34,542.00 *** CONTINUED *** 2005-05-19 TO PREVENT STRUCTURAL FAILURE INS DOC: AD-2005-05-19 OF THE WING AND FUEL LEAKS IN W/C: 2005-05-19 (G) CW 05/15/2005 56,898:06 29,722.00 THE AIRPLANE DUE TO STRESS CORROSION CRACKING OF THE WING INS DOC: AD-2005-05-19 W/C: 2005-05-19 (H)(1) CW 05/06/2006 57,863:05 30,450.00 COMPLETED ON >> WO: 3542 ITEM: 6 INS DOC: AD-2005-05-19 W/C: 2005-05-19 (h)(2) LAST 11/10/2010 61,801:48 33,867.00 WO: 4678 ITEM: 125 NEXT 11/10/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD-2005-05-19 W/C: 2005-05-19 (h)(3) LAST 11/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 126 NEXT 11/13/2012 MINIMUM CHECK: A INT> 48 M INS DOC: AD-2005-05-19 W/C: 2005-05-19 (h)(4) LAST 11/10/2010 61,801:48 33,867.00 WO: 4678 ITEM: 127 NEXT 11/10/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD-2005-05-19 W/C: 2005-05-19 (h)(5) LAST 11/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 128 NEXT 11/13/2012 MINIMUM CHECK: A INT> 48 M 2005-14-07 FATIGUE CRACKING OF THE ATTACH INS DOC: AD-2005-14-07 FITTINGS OF FOREFLAP CARRIAGE W/C: 2005-14-07(f)1&2 LAST 12/14/2010 61,864:57 33,925.00 OF THE WINGS WO: 5593 ITEM: 83 NEXT 34,925.00 MINIMUM CHECK: A INT> 1,000 INS DOC: AD-2005-14-07 W/C: 2005-14-07(h)&(m) CW 12/02/2008 60,096:06 32,187.00 COMPLETED ON >> WO: 4678 ITEM: 130 2005-19-24 TO PREVENT FATIGUE CRACKING OF INS DOC: AD-2005-19-24 THE FORWARD SUPPORT FITTING OF W/C: 2005-19-24 LAST 12/22/2010 61,864:57 33,925.00 THE #1 & #3 ENGINES WO: 5593 ITEM: 13 NEXT 12/22/2012 64,864:57 MINIMUM CHECK: C INT> 24 M 3,000 INS DOC: AD-2005-19-24 W/C: 2005-19-24 (j) CW 01/23/2006 57,679:22 30,297.00 INS DOC: AD-2005-19-24 W/C: 2005-19-24 (m) LAST 01/12/2011 61,864:57 33,925.00 WO: 5593 ITEM: 14 NEXT 01/12/2013 36,925.00 MINIMUM CHECK: A INT> 24 M 3,000 INS DOC: AD-2005-19-24 W/C: 2005-19-24 708AMC PE T 01/12/2013 36,425.00 MINIMUM CHECK: A INT> 2 Y 2,500

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: 34,542.00 *** CONTINUED *** 2005-19-24 TO PREVENT FATIGUE CRACKING OF INS DOC: AD-2005-19-24 THE FORWARD SUPPORT FITTING OF W/C: 2005-19-24 815AMC THE #1 & #3 ENGINES INS DOC: AD-2005-19-24 W/C: 2005-19-24 AMOC INS DOC: AD-2005-19-24 W/C: 2005-19-24(g)AMOC TM 12/02/2008 60,022:19 32,128.00 2005-20-13 TO DETECT CRACKS IN THE FRAMES, INS DOC: AD-2005-20-13 WHICH COULD RESULT IN CRACKS IN W/C: 2005-20-13 (G) PE T 40,000.00 THE SKIN PANELS AND RAPID MINIMUM CHECK: A INT> 3,500 DECOMPRESSION OF THE AIRCRAFT 2005-23-07 To prohibit the resetting of a INS N/A tripped circuit breaker for a TM 11/10/2005 fuel pump 2006-07-10 TO PREVENT LOSS OF STRUCTURAL INS DOC: AD-2006-07-10 INTERITY OF FWD ENTRY DOORWAY W/C: 2006-07-10 (f) DUE TO CRACKING AT BS 303.9. INS DOC: AD-2006-07-10 W/C: 2006-07-10 (h) INS DOC: AD-2006-07-10 W/C: 2006-07-10 (h)r INS DOC: AD-2006-07-10 W/C: 2006-07-10 (j) PE T 34,951.00 MINIMUM CHECK: C INT> 4,500 INS DOC: AD-2006-07-10 W/C: 2006-07-10 (j)r MOD DOC: SB-53-0153 MA : 5300-0153 PE T 60,000.00 2006-13-16 TO PREVENT EXCESSIVE VIBRATION INS DOC: AD-2006-13-16 OF THE OUTBOARD AILERON BALANCE W/C: 2006-13-16 (g)(1) LAST 11/05/2010 61,792:44 33,859.00 TAB AND RUDDER TAB. WO: 4678 ITEM: 14 NEXT 11/05/2012 69,792:44 MINIMUM CHECK: C INT> 24 M 8,000 INS DOC: AD-2006-13-16 W/C: 2006-13-16 (g)(2) LAST 10/01/2011 62,385:12 34,440.00 WO: 5593 ITEM: 15 NEXT 07/01/2012 65,585:12 MINIMUM CHECK: C INT> 9 M 3,200 INS DOC: AD-2006-13-16 W/C: 2006-13-16(G)(1)I CW 01/11/2008 59,425:54 31,624.00 INS DOC: AD-2006-13-16 W/C: 2006-13-16(G)(2)I CW 04/20/2007 58,780:02 31,065.00

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: 34,542.00 *** CONTINUED *** 2006-26-13 Shoulder restraint harness of INS N/A the attendant or observer seat detaching from the mounting bracket. MOD DOC: AD-2006-26-13 MA : 2510-0005 TM 01/03/2005 2007-11-08 TO DETECT AND CORRECT CHAFING INS DOC: AD-2007-11-08 OF THE FUEL BOOST PUMP W/C: 2007-11-08 (L) PE T 46,027.00 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-2007-11-08 W/C: 2007-11-08 (L)INT CW 03/31/2007 58,731:08 31,027.00 INS DOC: AD-2007-11-08 W/C: 2007-11-08 (M) CW 06/08/2007 58,891:36 31,172.00 2007-12-14 TO DECTECT AND CORRECT CRACKS INS DOC: AD-2007-12-14 IN THE SKIN, DOUBLER AND BEAR W/C: 2007-12-14 (g) STRAP AT THE HINGE CUTOUTS OF WO: 4678 ITEM: 16 THE FWD ENTRY DOOR INS DOC: AD-2007-12-14 W/C: 2007-12-14 (i)dvi LAST 11/20/2008 60,096:06 32,187.00 NEXT 35,187.00 MINIMUM CHECK: C INT> 3,000 INS DOC: AD-2007-12-14 W/C: 2007-12-14(i)HFEC LAST 11/20/2008 60,096:06 32,187.00 NEXT 52,187.00 MINIMUM CHECK: C INT> 20,000 MOD DOC: AD-2007-12-14 MA : 5300-0198 PE T 60,000.00 2007-21-04 TO DETECT AND CORRECT A CRACKED INS DOC: AD-2007-21-04 PRESSURE BULKHEAD WEB, WHICH W/C: 2007-21-04 (F) PE T 40,000.00 COULD RESULT IN RAPID MINIMUM CHECK: C INT> 3,500 DECOMPRESSION OF THE AIRPLANE INS DOC: AD-2007-21-04 W/C: 2007-21-04 (F)(1) 2008-02-13 TO DETECT AND CORRECT FATIGUE INS DOC: AD-2008-02-13 CRACKS OF THE CROWN SKIN W/C: 2008-02-13 (F) PE T 66,000.00 MINIMUM CHECK: C INT> 3,500 2008-04-10 TO PREVENT THE POTENTIAL FOR INS DOC: AD-2008-04-10 IGNITION SOURCES INSIDE FUEL W/C: 2008-04-10 (G) TM 12/12/2008 60,098:47 32,189.00 TANKS CAUSED BY LATENT FAILURES, ALTERATIONS, REPAIRS INS DOC: AD-2008-04-10 W/C: 2008-04-10 (H) PE T 03/28/2014 MINIMUM CHECK: A INT> 72 M

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: 34,542.00 *** CONTINUED *** 2008-04-10 TO PREVENT THE POTENTIAL FOR IGNITION SOURCES INSIDE FUEL TANKS CAUSED BY LATENT FAILURES, ALTERATIONS, REPAIRS 2008-08-02 TO PREVENT A FRACTURED SIDE INS DOC: AD-2008-08-02 STRUT, WHICH COULD RESULT IN W/C: 2008-08-02 (F) LAST 12/09/2008 60,098:47 32,189.00 COLLAPSE OF THE MLG WO: 4678 ITEM: 17 NEXT 12/09/2018 MINIMUM CHECK: C INT> 120 M INS DOC: AD-2008-08-02 W/C: 2008-08-02 (G) LAST 12/09/2008 60,098:47 32,189.00 WO: 4678 ITEM: 18 NEXT 12/09/2018 MINIMUM CHECK: C INT> 120 M 2008-11-09 TO DETECT AND CORRECT CRACKING INS DOC: AD-2008-11-09 IN THE VINYL INTERLAYER OR W/C: 2008-11-09(f) #2 LAST 10/23/2011 62,410:42 34,466.00 DAMAGE TO THE STRUCTURAL INNER NEXT 10/23/2014 69,910:42 GLASS PANES OF THE FLIGHT DECK MINIMUM CHECK: C INT> 36 M 7,500 INS DOC: AD-2008-11-09 W/C: 2008-11-09(f)#2 I CW 11/10/2008 60,096:06 32,187.00 COMPLETED ON >> WO: 4678 ITEM: 19 INS DOC: AD-2008-11-09 W/C: 2008-11-09(f)4/5 INS DOC: AD-2008-11-09 W/C: 2008-11-09(f)4/5I WO: 4678 ITEM: 20 MOD DOC: AD-2008-11-09 MA : 5610-0001 TM 12/09/2008 60,098:47 32,189.00 2008-17-14 To prevent cracking of the INS DOC: AD-2008-17-14 elevator rear spar at the tab W/C: 2008-17-14 (f) hinge locations INS DOC: AD-2008-17-14 W/C: 2008-17-14 (i) INS DOC: AD-2008-17-14 W/C: 2008-17-14 (n) INS DOC: AD-2008-17-14 W/C: 2008-17-14 (q) TM 10/16/2010 61,745:31 33,812.00 2008-22-12 To detect and correct damage to INS DOC: AD-2008-22-12 the aft attachement lugs of the W/C: 2008-22-12 (f) PE T 12/24/2013 66,235:29 37,290.00 elevator quadrant support MINIMUM CHECK: C INT> 30 M 4,000 3,000 assembly that could lead to the INS DOC: AD-2008-22-12 W/C: 2008-22-12 (f)i CW 06/24/2011 62,235:29 34,290.00 INS DOC: AD-2008-22-12 W/C: 2008-22-12 Pt 3

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: 34,542.00 *** CONTINUED *** 2008-22-12 To detect and correct damage to the aft attachement lugs of the elevator quadrant support assembly that could lead to the 2008-23-09 To ensure that insulation INS DOC: AD-2008-23-09 blankets constructed of AN-26 W/C: 2008-23-09 (f) are removed from the fuselage 2009-05-03 To prevent an electrical fault INS DOC: AD-2009-05-03 in the fuel pump system W/C: 2009-05-03 (f) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M INS DOC: AD-2009-05-03 W/C: 2009-05-03 (g) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M INS DOC: AD-2009-05-03 W/C: 2009-05-03 (h) PE T 04/03/2014 MINIMUM CHECK: C INT> 60 M 2009-20-03 TO detect and correct cracking INS DOC: AD-2009-20-03 of the LH/RH side web posts & W/C: 2009-20-03 (f) shear ties of the kickload beam. INS DOC: AD-2009-20-03 W/C: 2009-20-03 (f)int PE T 64,872:39 35,915.00 MINIMUM CHECK: C INT> 4,000 3,000 INS DOC: AD-2009-20-03 W/C: 2009-20-03(f)INT2 2009-20-08 To detect and correct failure INS DOC: AD-2009-20-08 of the engine fuel suction feed W/C: 2009-20-08 (f) PE T 04/16/2014 69,059:19 of the fuel system MINIMUM CHECK: C INT> 36 M 7,000 INS DOC: AD-2009-20-08 W/C: 2009-20-08 (f)int CW 04/16/2011 62,057:52 34,109.00 2011-01-05 To detect and correct cracking INS DOC: AD-2011-01-05 in the aft pressure bulkhead W/C: 2011-01-05(g)(1) web, which could adversely affect the structural integrity INS DOC: AD-2011-01-05 W/C: 2011-01-05(g)(1)I PE T 37,462.00 MINIMUM CHECK: A INT> 3,500 INS DOC: AD-2011-01-05 W/C: 2011-01-05(g)(2) INS DOC: AD-2011-01-05 W/C: 2011-01-05(g)(2)I

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: 34,542.00 *** CONTINUED *** 2011-02-05 To detect and correct scribe INS DOC: AD-2011-02-05 lines which can develop into W/C: 2011-02-05 (g) PE T 03/01/2013 fatigue cracks in the skin MINIMUM CHECK: A INT> 24 M INS DOC: AD-2011-02-05 W/C: 2011-02-05 801 INS DOC: AD-2011-02-05 W/C: 2011-02-05 801a INS DOC: AD-2011-02-05 W/C: 2011-02-05 801b INS DOC: AD-2011-02-05 W/C: 2011-02-05 801c 69-16-01 To provide the flight crew with INS N/A more complete procedures if all TM 09/12/1969 generators are lost. 76-15-06 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 5 77-03-02 TO PREVENT RUPTURE OF ENGINE INS N/A FUEL FEED HOSE ASSEMBILES 78-26-07 REWORK THRUST REVERSER INS N/A 79-04-01 MAIN LANDING GEAR LOCK INS DOC: AD-79-04-01 REV#: 3 INSPECTION W/C: C-115 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C INS DOC: AD-79-04-01 W/C: C-115.1 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C INS DOC: AD-79-04-01 W/C: C-123 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C

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: 34,542.00 *** CONTINUED *** 79-04-01 MAIN LANDING GEAR LOCK INS DOC: AD-79-04-01 REV#: 3 INSPECTION W/C: C-123.1 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 1 NEXT 64,864:57 CHECK: C 80-22-12 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 81-20-04 TO PREVENT IN FLIGHT FIRES INS N/A PC 10/21/1981 82-22-01 LEADING EDGE SLAT ACTUATOR ASSY INS DOC: AD-82-22-01 SB727-27-209 W/C: 82-22-01 INS DOC: AD-82-22-01 W/C: 82-22-01 (A) 83-01-05 TO PREVENT UNDETECTED PROLONGED INS N/A ENGINE STARTER PC 06/12/1985 85-16-05 TO ASSURE ADEQUATE LAVATORY INS N/A FIRE PROTECTION PC 06/15/1986 85-24-02 RAM AIR DUCT CORROSION INSP PER INS DOC: AD-85-24-02 REV#: 1 PARA "B" VISUALLY INSPECT UPPER W/C: 85-24-02 A1 LAST 11/10/2008 60,098:47 32,189.00 WALL OF AIR CONDITIONING RAM WO: 4678 ITEM: 34 AIR PLENUM CHAMBER IAW PART II NEXT 11/10/2012 68,098:47 MINIMUM CHECK: C INT> 48 M 8,000 87-06-10 TO REPLACE SEALED NEEDLE INS DOC: AD-87-06-10 BEARINGS IN THE DOWNLOCK OUTER W/C: 87-06-10 LH PE T 12/13/2020 LINK OF THE STRUT UPPER SEGMENT MINIMUM CHECK: A INT> 10 Y INS DOC: AD-87-06-10 W/C: 87-06-10 RH PE T 12/13/2020 MINIMUM CHECK: A INT> 10 Y

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: 34,542.00 *** CONTINUED *** 87-08-09 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 87-22-06 TO PREVENT MLG DOOR RELEASE INS N/A LEVER FROM MOVING TO THE DOOR PC 04/07/1988 OPEN POSITION DURING FLIGHT 88-01-02 TO PREVENT MAIN LANDING GEAR INS N/A FAILURE TO EXTEND PROPERLY AS A RESULT OF STRUCTURAL FAILURE IN THE LOCK SYSTEM 88-17-06 ENSURE STRUCTURE INTEGRITY OF INS DOC: AD-88-17-06 WING UPPER SURFACE STRINGER S/B W/C: 88-17-06 (A)(3) 727-57A159 INS DOC: AD-88-17-06 W/C: 88-17-06 (B)(1) INS DOC: AD-88-17-06 W/C: 88-17-06 (B)(2) LAST 03/29/2006 57,833:37 30,422.00 NEXT 41,422.00 MINIMUM CHECK: C INT> 11,000 MOD DOC: SB-57A159 MA : 5700-0159 PE T 60,000.00 88-20-07 MAIN LANDING GEAR ACTUATOR INS DOC: AD-88-20-07 JAMMING S/B 727-32-0358 W/C: 88-20-07 PC 10/29/1988 88-22-09 TAKE-OFF WARNING SYS INS DOC: AD-88-22-09 W/C: 88-22-09E INS DOC: AD-88-22-09 W/C: 88-22-09N LAST 11/04/2011 62,432:59 34,490.00 WO: 5593 ITEM: 91 NEXT 62,632:59 MINIMUM CHECK: A INT> 200 88-24-01 TO PREVENT FAILURE OF MLG INS N/A SUPPORT LINK SHAFT PC 02/07/1990 88-24-12 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

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: 34,542.00 *** CONTINUED *** 89-07-05 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 89-21-02 TO PREVENT ENGINE SEPARATION INS N/A TM 03/07/2007 90-02-08 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 90-03-18 Takeoff configuration nuisance INS N/A warnings when taxi operations PC 01/01/1991 90-06-09 TO PREVENT STRUCTURAL FAILURE - INS N/A AGING AIRCRAFT MOD DOC: AD-90-06-09 MA : 5200-0094 MOD DOC: AD-90-06-09 MA : 5300-0055 PC 01/01/1991 MOD DOC: AD-90-06-09 MA : 5300-0065 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0086 MOD DOC: AD-90-06-09 MA : 5300-0116 MOD DOC: AD-90-06-09 MA : 5300-0124 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0134 MOD DOC: AD-90-06-09 MA : 5300-0136 MOD DOC: AD-90-06-09 MA : 5300-0144 MOD DOC: AD-90-06-09 MA : 5300-0145 MOD DOC: AD-90-06-09 MA : 5300-0147 MOD DOC: AD-90-06-09 MA : 5300-0149 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0153 PE T 60,000.00

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: 34,542.00 *** CONTINUED *** 90-06-09 TO PREVENT STRUCTURAL FAILURE - MOD DOC: AD-90-06-09 AGING AIRCRAFT MA : 5300-0159 MOD DOC: AD-90-06-09 MA : 5300-0166 MOD DOC: AD-90-06-09 MA : 5300-0169 MOD DOC: AD-90-06-09 MA : 5300-0171 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0175 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0178 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0181 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0182 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0188 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5300-0198 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5500-0071 MOD DOC: AD-90-06-09 MA : 5700-0112 TM 12/18/2000 MOD DOC: AD-90-06-09 MA : 5700-0127 MOD DOC: AD-90-06-09 MA : 5700-0130 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5700-0134 TM 04/07/2006 57,833:37 30,422.00 MOD DOC: AD-90-06-09 MA : 5700-0159 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5700-0171 TM 05/19/2003 MOD DOC: AD-90-06-09 MA : 5700-0172 PE T 60,000.00 MOD DOC: AD-90-06-09 MA : 5700-0178 PC 01/01/1991 90-07-05 INBOARD TRAINING EDGE FLAPS INS DOC: AD-90-07-05 INBOARD TRACK S/B 727-57-117 & W/C: 90-07-05 A1b(1) LAST 10/23/2011 62,410:42 34,466.00 57-178 WO: 4678 ITEM: 122 NEXT 04/23/2013 37,466.00 MINIMUM CHECK: C INT> 18 M 3,000 INS DOC: AD-90-07-05 W/C: 90-07-05 A1b(2)

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: 34,542.00 *** CONTINUED *** 90-07-05 INBOARD TRAINING EDGE FLAPS INS DOC: AD-90-07-05 INBOARD TRACK S/B 727-57-117 & W/C: 90-07-05 A1c LAST 10/23/2011 62,410:42 34,466.00 57-178 NEXT 04/23/2013 37,466.00 MINIMUM CHECK: A INT> 18 M 3,000 MOD DOC: SB-57-0178 MA : 5700-0178 PE T 60,000.00 90-24-11 BODY STATION 1183, PRESSURE INS DOC: AD-90-24-11 BULKHEAD WEB S/B 727-53A0171 W/C: 90-24-11 C INS DOC: AD-90-24-11 W/C: 90-24-11 G LAST 11/10/2008 60,098:47 32,189.00 WO: 4678 ITEM: 35 NEXT 35,689.00 MINIMUM CHECK: C INT> 3,500 MOD DOC: SB-53A0171 MA : 5300-0171 PE T 60,000.00 90-25-03 AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C32-131-01 1OF1 LAST 11/30/2008 60,096:06 32,187.00 MODEL 727 NEXT 11/30/2018 MINIMUM CHECK: C INT> 120 M W/C: C32-135-01 1OF1 LAST 12/13/2010 61,864:57 33,925.00 WO: 5593 ITEM: 36 NEXT 12/13/2020 MINIMUM CHECK: C INT> 120 M W/C: C53-100-01 1OF6 PE T 01/27/2012 WO: 4678 ITEM: 43 MINIMUM CHECK: C INT> 18 M W/C: C53-100-01 2OF6 PE T 01/27/2012 WO: 4678 ITEM: 44 MINIMUM CHECK: C INT> 18 M W/C: C53-100-01 3OF6 PE T 01/27/2012 WO: 4678 ITEM: 45 MINIMUM CHECK: C INT> 18 M W/C: C53-100-01 4OF6 PE T 01/27/2012 WO: 4678 ITEM: 46 MINIMUM CHECK: C INT> 18 M W/C: C53-100-01 5OF6 PE T 01/27/2012 WO: 4678 ITEM: 47 MINIMUM CHECK: C INT> 18 M W/C: C53-100-01 6OF6 PE T 01/27/2012 WO: 4678 ITEM: 48 MINIMUM CHECK: C INT> 18 M W/C: C53-100-02 1OF1 W/C: C53-100-03 1OF1

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: 34,542.00 *** CONTINUED *** 90-25-03 AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C53-100-05 1OF4 LAST 01/26/2011 61,864:57 33,925.00 MODEL 727 WO: 5593 ITEM: 37 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C53-100-05 2OF4 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 38 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C53-100-05 3OF4 LAST 03/23/2006 57,833:37 30,422.00 WO: 3542 ITEM: 28 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C53-100-05 4OF4 LAST 03/23/2006 57,833:37 30,422.00 WO: 3542 ITEM: 29 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C53-100-06 1OF1 PE T 01/27/2012 WO: 4678 ITEM: 49 MINIMUM CHECK: C INT> 18 M W/C: C53-111-01 1OF3 LAST 04/14/2006 57,833:37 30,422.00 NEXT 04/14/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-111-01 2OF3 LAST 03/23/2006 57,833:37 30,422.00 NEXT 03/23/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-111-01 3OF3 LAST 04/14/2006 57,833:37 30,422.00 NEXT 04/14/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-111-02 1OF2 LAST 03/22/2006 57,833:37 30,422.00 NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-111-02 2OF2 LAST 03/22/2006 57,833:37 30,422.00 NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-111-03 1OF2 W/C: C53-111-03 2OF2 PE T 03/31/2012 WO: 4678 ITEM: 50 MINIMUM CHECK: C INT> 36 M W/C: C53-111-04 1OF1 W/C: C53-113-01 1OF2 PE T 03/31/2012 WO: 4678 ITEM: 51 MINIMUM CHECK: C INT> 36 M

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: 34,542.00 *** CONTINUED *** 90-25-03 AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C53-113-01 2OF2 PE T 03/31/2012 MODEL 727 WO: 4678 ITEM: 52 MINIMUM CHECK: C INT> 36 M W/C: C53-113-02 1OF1 W/C: C53-132-01 1OF2 LAST 03/22/2006 57,833:37 30,422.00 NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-132-01 2OF2 LAST 03/22/2006 57,833:37 30,422.00 NEXT 03/22/2012 MINIMUM CHECK: C INT> 72 M W/C: C53-132-02 1OF2 W/C: C53-132-02 2OF2 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 53 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-132-03 1OF4 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 39 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C53-132-03 2OF4 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 40 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C53-132-03 3OF4 LAST 03/23/2006 57,833:37 30,422.00 WO: 3542 ITEM: 44 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C53-132-03 4OF4 LAST 03/23/2006 57,833:37 30,422.00 WO: 3542 ITEM: 45 NEXT 03/23/2016 MINIMUM CHECK: C INT> 120 M W/C: C53-137-01 1OF1 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 41 NEXT 01/26/2016 MINIMUM CHECK: C INT> 60 M W/C: C53-221-01 1OF1 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 42 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C53-224-01 1OF3 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 43 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M

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: 34,542.00 *** CONTINUED *** 90-25-03 AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C53-224-01 2OF3 LAST 01/26/2011 61,864:57 33,925.00 MODEL 727 WO: 5593 ITEM: 44 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C53-224-01 3OF3 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 45 NEXT 01/26/2019 MINIMUM CHECK: C INT> 96 M W/C: C53-224-03 1OF2 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 46 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M W/C: C53-224-03 2OF2 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 55 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-224-04 1OF1 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 56 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-224-05 1OF1 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 57 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-224-06 1OF1 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 58 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-224-07 1OF1 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 59 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C53-224-08 1OF1 LAST 12/13/2008 60,098:47 32,189.00 WO: 4678 ITEM: 60 NEXT 12/13/2012 MINIMUM CHECK: C INT> 48 M W/C: C54-451-01 1OF3 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 47 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M W/C: C54-451-01 2OF3 LAST 01/26/2011 61,864:57 33,925.00 WO: 5593 ITEM: 48 NEXT 01/26/2013 MINIMUM CHECK: C INT> 24 M