N713AA Aircraft Specifications

Transcription

1 GENERAL INFORMATION N713AA Aircraft Specifications Model No. B Manufacturer Line No Registration No. N713AA Date of Manufacture Manufacturer Boeing Selcal CKFH Serial No Configuration AEI Cargo Mod. Variable No. QB809 OPERATIOL WEIGHTS Max Taxi Weight 195,500 lb Max Zero Fuel Weight 155,000 lb Max Takeoff Weight 195,000 lb Operating Empty Weight 93,911 lb Max Landing Weight 164,000 lb Fuel Capacity 54,000 Ib TIME/CYCLE DATA - FUSELAGE All data as of: Total Hours Hrs C Check Interval 3000 Hrs / 24 months Total Cycles Cyc Last C Check C/W Next C Check Hrs / Total Hours Hrs Remaining to Next C Ck 1685 Hrs / 8 months Total Cycles Cyc LANDING GEAR Part Number Serial Number Time Since Overhaul Nose LG Hrs / 18 months Left C Hrs / 18 months Right ZT Hrs / 18 months Last Overhaul Interval Time Remaining Nose Hrs/120 months Hrs / 102 months Left Hrs/120 months Hrs / 102 months Right Hrs/120 months Hrs / 102 months AUXILIARY POWER UNIT Part No Serial No TIME / CYCLES DATA - ENGINE Serial No. Engine Type Total Time / Cycles Remaining to Limit Limiting Item JT8D Hrs / Cyc 2536 Cyc T1 / T3 Due: 12/25/13 SB JT8D-15A Hrs / Cyc 5905 FH C3-C6 Due: 07/24/14 SB JT8D Hrs / Cyc 7062 Cyc T1 Due: 06/30/15 SB 6431

2 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:18 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-15 Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 713 Sub Location: #3 Status: SERVICEABLE Time On A/C: FHRS = 63,205:42 CYCS = 35,316 Date = 03/20/2012 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 61,736:14 1,469:28-49, , JT8D-15 CYC 34, , , ,141 - NO LIMITS ENGINE, JT8D CAL 08/06/2010 1Y 7M14D , POS: #3 GRN No.> FHR 61,736:14 1,469: /16/ CYC 34, , ,000 10,604 9, ,396 CYC COMPRESSOR DISK, C1 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAW2335 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 8,995 21, /16/ CYC 34, , ,000 6,680 13, ,320 CYC COMPRESSOR DISK, C2 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAU8873 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 18,195 11, /08/ CYC 34, , ,000 10,993 9, ,007 CYC COMPRESSOR DISK, C3 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAJ4352 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 8,840 21, /25/ CYC 34, , ,000 5,741 14, ,259 CYC COMPRESSOR DISK, C4 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAX2846 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 8,839 21, /25/ CYC 34, , ,000 5,741 14, ,259 CYC COMPRESSOR DISK, C6 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAX4220 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 14,462 15, /15/ CYC 34, , ,000 10,060 9, ,940 CYC COMPRESSOR DISK, C5 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAN9703 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 1,469 28, /05/ CYC 34, , ,000 1,141 18, ,859 CYC COMPRESSOR DISK, C7 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAR9987 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 10,458 19, /05/ CYC 34, , ,000 10,636 9, ,364 CYC COMPRESSOR DISK, C8 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAR9987 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 1,469 28, /05/ CYC 34, , ,000 1,141 18, ,859 CYC COMPRESSOR DISK, C9 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAX4293 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 8,134 21, /20/ CYC 34, , ,000 5,932 14, ,068 CYC COMPRESSOR DISK, C10 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAL1623 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 13,202 16, /16/ CYC 34, , ,000 8,043 11, ,957 CYC COMPRESSOR DISK, C11 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAL2759 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 9,577 20, /21/ CYC 34, , ,000 5,659 14, ,341 CYC COMPRESSOR DISK, C12 CAL 08/06/2010 1Y 7M14D FOR: L/L BENCAR2759 POS: OLY GRN No.> DUE >>

3 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:18 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-15 Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 713 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 61,736:14 1,469:28 30,000 10,177 19, /14/ CYC 34, , ,000 8,784 11, ,216 CYC COMPRESSOR DISK, C13 CAL 08/06/2010 1Y 7M14D FOR: L/L BBDUAU4957 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 18,374 11, /25/ CYC 34, , ,000 12,858 7, ,142 CYC TURBINE DISK,T1 CAL 08/06/2010 1Y 7M14D FOR: L/L BKLBB33762 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 8,619 21, /01/ CYC 34, , ,000 6,447 13, ,553 CYC TURBINE DISK,T2 CAL 08/06/2010 1Y 7M14D FOR: L/L BLDLCR7522 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 12,671 17, /09/ CYC 34, , ,000 12,448 7, ,552 CYC TURBINE DISK,T3 CAL 08/06/2010 1Y 7M14D FOR: L/L BLDLAJ4399 POS: OLY GRN No.> DUE >> FHR 61,736:14 1,469:28 30,000 14,217 15, /03/ CYC 34, , ,000 10,641 9, ,359 CYC TURBINE DISK,T4 CAL 08/06/2010 1Y 7M14D FOR: L/L BLDLCB2061 POS: OLY GRN No.> DUE >> *** END OF REPORT ***

4 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-17 Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 713 Sub Location: #1 Status: SERVICEABLE Time On A/C: FHRS = 63,205:42 CYCS = 35,316 Date = 03/20/2012 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 56,468:46 6,736:56-49, , , JT8D-17 CYC 30, , , , ,559 - NO LIMITS ENGINE, JT8D CAL 02/11/2006 6Y 1M 9D - 4, , , POS: #1 GRN No.> FHR INSTALLED 13,084:07-17, /30/ CYC WITH 8, ,000 12,207 7, ,793 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L BBDUAJ5523 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 10,318:14 30,000 25,902 4, /03/ CYC WITH 6, ,000 15,869 4, ,098 FHR COMPRESSOR DISK, C2 CAL ASSEMBLY 9Y 6M 0D - 3, FOR: L/L BBDUAJ9916 POS: OLY GRN No.> DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC COMPRESSOR DISK, C3 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T56048 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC COMPRESSOR DISK, C4 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T03055 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC COMPRESSOR DISK, C6 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T20630 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC COMPRESSOR DISK, C5 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T60501 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 6,736:56 30,000 17,609 12, /24/ CYC WITH 4, ,000 11,952 8, ,048 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAP1791 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,736:56 30,000 12,791 17, /01/ CYC WITH 4, ,000 11,652 8, ,348 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAR5721 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,736:56 30,000 6,737 23, /23/ CYC WITH 4, ,000 4,559 15, ,441 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAW5155 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,736:56 30,000 6,737 23, /23/ CYC WITH 4, ,000 4,559 15, ,441 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAW4845 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,736:56 30,000 6,737 23, /23/ CYC WITH 4, ,000 4,559 15, ,441 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAW7982 POS: OLY GRN No.> DUE >> FHR INSTALLED 6,736:56 30,000 17,609 12, /24/ CYC WITH 4, ,000 11,952 8, ,048 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 6Y 1M13D - 2, FOR: L/L BENCAP3602 POS: OLY GRN No.> DUE >>

5 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-17 Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 713 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 13,084:07 30,000 13,084 16, /21/ CYC WITH 8, ,000 8,946 11, ,054 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L BBDUAU4969 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 27,359 2, /25/ CYC WITH 8, ,000 17,688 2, ,641 FHR TURBINE DISK,T1 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L R40389 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC TURBINE DISK,T2 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T23838 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 27,359 2, /25/ CYC WITH 8, ,000 17,688 2, ,641 FHR TURBINE DISK,T3 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L R42413 POS: OLY GRN No.> N/A DUE >> FHR INSTALLED 13,084:07 30,000 22,504 7, /25/ CYC WITH 8, ,000 14,684 5, ,316 CYC TURBINE DISK,T4 CAL ASSEMBLY 12Y 9M11D - 4, FOR: L/L T25087 POS: OLY GRN No.> N/A DUE >> *** END OF REPORT ***

6 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 1 ROTABLE CONTROL NO.: CCI Part Number: JT8D-15A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: A/C Location Identity: 713 Sub Location: #2 Status: SERVICEABLE Time On A/C: FHRS = 63,205:42 CYCS = 35,316 Date = 03/20/2012 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 61,388:06 1,817:36-37, , JT8D-15A CYC 33, , , ,023 - NO LIMITS ENGINE, JT8D CAL 04/16/2010 1Y11M 4D - 1, , POS: #2 GRN No.> FHR INSTALLED 4,593:20-14, /27/ CYC WITH 3, ,000 8,197 11, ,803 CYC COMPRESSOR DISK, C1 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BBDUAP4317 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 10,212 19, /27/ CYC WITH 3, ,000 7,833 12, ,167 CYC COMPRESSOR DISK, C2 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L S56286 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 23,989 6, /08/ CYC WITH 3, ,000 13,926 6, ,011 FHR COMPRESSOR DISK, C3 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L T56171 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 23,989 6, /08/ CYC WITH 3, ,000 13,926 6, ,011 FHR COMPRESSOR DISK, C4 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L B114AA0257 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 23,989 6, /08/ CYC WITH 3, ,000 13,926 6, ,011 FHR COMPRESSOR DISK, C6 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L T41308 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 23,989 6, /08/ CYC WITH 3, ,000 13,926 6, ,011 FHR COMPRESSOR DISK, C5 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L T70378 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 10,209 19, /14/ CYC WITH 3, ,000 6,774 13, ,226 CYC COMPRESSOR DISK, C7 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAR3263 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 14,044 15, /21/ CYC WITH 3, ,500 8,003 8, ,497 CYC COMPRESSOR DISK, C8 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAP3308 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 4,593 25, /17/ CYC WITH 3, ,000 3,023 16, ,977 CYC COMPRESSOR DISK, C9 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAX2115 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 6,978 23, /09/ CYC WITH 3, ,000 4,052 15, ,948 CYC COMPRESSOR DISK, C10 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAS8492 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 11,494 18, /27/ CYC WITH 3, ,000 7,010 12, ,990 CYC COMPRESSOR DISK, C11 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAL9904 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 11,494 18, /27/ CYC WITH 3, ,000 7,010 12, ,990 CYC COMPRESSOR DISK, C12 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BENCAR0412 POS: OLY GRN No.> DUE >>

7 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 3.24E TIME: 10:16 ASSEMBLY CONFIGURATION / STATUS REPORT PAGE NO.: 2 ROTABLE CONTROL NO.: CCI Part Number: JT8D-15A Mfg Serial Number: Description Of Rotable: ENGINE, JT8D Assy Location >> Location Type: Location Identity: 713 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 4,593:20 30,000 13,402 16, /14/ CYC WITH 3, ,000 10,155 9, ,845 CYC COMPRESSOR DISK, C13 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BBDUAN6484 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20-15, /06/ CYC WITH 3, ,000 9,998 10, ,002 CYC TURBINE DISK,T1 CAL ASSEMBLY 5Y 5M 7D - 1, FOR: L/L BKLBCL7032 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 10,921 19, /13/ CYC WITH 3, ,000 7,693 12, ,307 CYC TURBINE DISK,T2 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BLDLCU2690 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 11,494 18, /27/ CYC WITH 3, ,000 7,010 12, ,990 CYC TURBINE DISK,T3 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BLDLCK9947 POS: OLY GRN No.> DUE >> FHR INSTALLED 4,593:20 30,000 11,494 18, /27/ CYC WITH 3, ,000 7,010 12, ,990 CYC TURBINE DISK,T4 CAL ASSEMBLY 5Y 5M 4D - 1, FOR: L/L BLDLB44036 POS: OLY GRN No.> DUE >> *** END OF REPORT ***

8 CCIA Major Alterations (B727 acft) N713AA 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 AA 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 7 BM Lower cargo smoke detector 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 BM * Altair floor loading with 12 reinforcement? STC 00731SE BM * SIE STC ST00779LA (part of 13 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 BM * Installation of Library Cabinet RPT , DWG Only 21 BM * Aux Fuel Tank Removal 708, ORDER 99CCAL-011M-1D 22 BM R0* Reactivate TCAS 708,713,715,427 OHM , MM , WD BM AEI Door Hinge Fail-Safe AD Hinge BM * Floor Beam Modification 755 STC ST00731SE, RPT and 713 ONLY

9 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 1 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, TO PREVENT FATIGUE CRACKS OF INS DOC: AD THE FRONT SPAR WEB OF THE W/C: (a) PE T 40, CENTER SECTION OF THE WINGS MINIMUM CHECK: C INT> 40,000 B INS DOC: AD W/C: (a)(1) 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 11/29/ ,995:55 34, COULD PERMIT FUEL LEAKAGE INTO WO: 5592 ITEM: 12 THE AIRFLOW MULTIPLIER NEXT 37, 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 11/23/ ,995:55 34, WO: 5592 ITEM: 13 NEXT 11/23/ , MINIMUM CHECK: C INT> 10 Y 12,000 MOD DOC: AD MA : PC 03/15/ ,864:00 27, FIND AND FIX CORROSION OR INS DOC: AD REV#: 1 CRACKING IN HINGE PINS OF HORIZ W/C: (e)PRT3 STAB S/B727-55A0090 INS DOC: AD W/C: (e)PRT4 LAST 08/22/ ,496:22 32, WO: 4524 ITEM: 17 NEXT 08/22/ ,496:22 MINIMUM CHECK: C INT> 96 M 12,000

10 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 2 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** 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 11/01/ ,995:55 34, SB WO: 5592 ITEM: 14 NEXT 38, 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 CW 08/11/ ,494:42 32, COMPLETED ON >> WO: 4524 ITEM: 95 INS DOC: AD W/C: LOW JKH INS DOC: AD W/C: MED H INS DOC: AD W/C: MED HJK LAST 08/11/ ,494:42 32, NEXT 39, MINIMUM CHECK: C INT> 7,000 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 01/24/ TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF MAIN DECK CARGO DOOR HINGE W/C: (A) PC 06/24/ ,359:52 28, OR FAILURE OF CARGO DOOR SYSTEM INS DOC: AD W/C: (E) TM 02/11/ ,468:46 30, WO: 3508 ITEM: 5 INS DOC: AD W/C: A INS DOC: AD W/C: (B)&(F) PC 06/24/ ,359:52 28,806.00

11 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 3 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE OF MAIN DECK CARGO DOOR HINGE OR FAILURE OF CARGO DOOR SYSTEM 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 01/03/ ,698:29 28, RESERVOIR AREA INSPECTION AND IF NECESSARY INS DOC: AD REPLACEMENT OF TITEFLEX HOSES W/C: TM 06/24/ ,359:52 28, TO PREVENT FAILURE OF A HOSE WHEN EXPOSED TO FIRE. MOD DOC: AD MA : CW 06/24/ ,360:44 28, COMPLETED ON >> WO: 2578 ITEM: TO PREVENT INCAPACITATION OF INS DOC: AD FLIGHTCREW DUE TO LACK OF W/C: CW 05/29/ ,258:41 28, OXYGEN - TABLE 2 - FIGURE 1 COMPLETED ON >> WO: 2531 ITEM: 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 06/29/2003 FITTINGS OF THE HYDRAULIC HEAT EXCHANGER AND THE REAR SPARS OF

12 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 4 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE INS DOC: AD OF THE WING AND FUEL LEAKS IN W/C: (G) CW 06/18/ ,834:29 30, THE AIRPLANE DUE TO STRESS COMPLETED ON >> WO: 3508 ITEM: 101 CORROSION CRACKING OF THE WING INS DOC: AD W/C: (H)(1) CW 01/19/ ,468:46 30, COMPLETED ON >> WO: 3508 ITEM: 6 INS DOC: AD W/C: (h)(2) LAST 11/05/ ,995:55 34, WO: 5592 ITEM: 149 NEXT 11/05/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD W/C: (h)(3) LAST 11/05/ ,995:55 34, WO: 5592 ITEM: 150 NEXT 11/05/2014 MINIMUM CHECK: A INT> 48 M INS DOC: AD W/C: (h)(4) LAST 11/05/ ,995:55 34, WO: 5592 ITEM: 151 NEXT 11/05/2012 MINIMUM CHECK: A INT> 730 D INS DOC: AD W/C: (h)(5) LAST 11/05/ ,995:55 34, WO: 5592 ITEM: 152 NEXT 11/05/2014 MINIMUM CHECK: A INT> 48 M FATIGUE CRACKING OF THE ATTACH INS DOC: AD FITTINGS OF FOREFLAP CARRIAGE W/C: (f)1&2 LAST 11/19/ ,995:55 34, OF THE WINGS WO: 5592 ITEM: 15 NEXT 35, MINIMUM CHECK: A INT> 1,000 INS DOC: AD W/C: (h)&(m) CW 09/08/ ,494:42 32, COMPLETED ON >> WO: 4524 ITEM: TO PREVENT FATIGUE CRACKING OF INS DOC: AD THE FORWARD SUPPORT FITTING OF W/C: LAST 11/12/ ,995:55 34, THE #1 & #3 ENGINES WO: 5592 ITEM: 16 NEXT 11/12/ ,995:55 MINIMUM CHECK: C INT> 24 M 3,000 INS DOC: AD W/C: (j) CW 01/24/ ,468:46 30, INS DOC: AD W/C: (m) LAST 11/12/ ,995:55 34, WO: 4524 ITEM: 101 NEXT 11/12/ , MINIMUM CHECK: A INT> 24 M 3,000 INS DOC: AD W/C: AMC

13 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 5 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** 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 12/05/ ,494:42 32, WO: 3508 ITEM: 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) CW 12/01/ ,995:55 34, COMPLETED ON >> WO: 5592 ITEM: 17 INS DOC: AD W/C: (j)r PE T 38, MINIMUM CHECK: C INT> 3,700 MOD DOC: SB MA : PE T 60, TO PREVENT EXCESSIVE VIBRATION INS DOC: AD OF THE OUTBOARD AILERON BALANCE W/C: (g)(1) LAST 11/23/ ,995:55 34, TAB AND RUDDER TAB. WO: 5592 ITEM: 18 NEXT 11/23/ ,995:55 MINIMUM CHECK: C INT> 24 M 8,000 INS DOC: AD W/C: (g)(2) LAST 08/17/ ,722:15 34, WO: 5592 ITEM: 19 NEXT 05/17/ ,922:15 MINIMUM CHECK: C INT> 9 M 3,200 INS DOC: AD W/C: (G)(1)I CW 01/14/ ,930:02 32, INS DOC: AD W/C: (G)(2)I CW 04/12/ ,100:47 31,679.00

14 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 6 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT EXCESSIVE VIBRATION OF THE OUTBOARD AILERON BALANCE TAB AND RUDDER TAB Shoulder restraint harness of INS N/A the attendant or observer seat detaching from the mounting bracket. MOD DOC: AD MA : TM 12/29/ ,165:28 29, 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 INS DOC: AD W/C: (L)INT CW 06/02/ ,288:31 31, INS DOC: AD W/C: (M) CW 06/08/ ,308:45 31, Q TO DECTECT AND CORRECT CRACKS INS DOC: AD IN THE SKIN, DOUBLER AND BEAR W/C: (g) STRAP AT THE HINGE CUTOUTS OF WO: 4524 ITEM: 102 THE FWD ENTRY DOOR INS DOC: AD W/C: (i)dvi LAST 11/01/ ,995:55 34, WO: 5592 ITEM: 20 NEXT 37, MINIMUM CHECK: C INT> 3,000 INS DOC: AD W/C: (i)HFEC LAST 11/01/ ,995:55 34, NEXT 54, 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> 3,500

15 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 7 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT THE POTENTIAL FOR INS DOC: AD IGNITION SOURCES INSIDE FUEL W/C: (G) TM 12/12/ ,771:15 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 TO PREVENT A FRACTURED SIDE INS DOC: AD STRUT, WHICH COULD RESULT IN W/C: (F) LAST 08/28/ ,496:22 32, COLLAPSE OF THE MLG WO: 4524 ITEM: 20 NEXT 08/28/2018 MINIMUM CHECK: C INT> 120 M INS DOC: AD W/C: (G) LAST 08/28/ ,496:22 32, WO: 4524 ITEM: 21 NEXT 08/28/2018 MINIMUM CHECK: C INT> 120 M TO DETECT AND CORRECT CRACKING INS DOC: AD IN THE VINYL INTERLAYER OR W/C: (f) #2 LAST 11/22/ ,995:55 34, DAMAGE TO THE STRUCTURAL INNER WO: 5592 ITEM: 21 GLASS PANES OF THE FLIGHT DECK NEXT 11/22/ ,495:55 MINIMUM CHECK: C INT> 36 M 7,500 INS DOC: AD W/C: (f)#2 I CW 08/07/ ,494:42 32, INS DOC: AD W/C: (f)4/5 INS DOC: AD W/C: (f)4/5I WO: 4524 ITEM: 88 MOD DOC: AD MA : TM 08/29/ ,494:42 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 11/26/ ,995:55 34, WO: 5592 ITEM: To detect and correct damage to INS DOC: AD the aft attachement lugs of the W/C: (f) PE T 05/26/ ,995:55 37, elevator quadrant support MINIMUM CHECK: C INT> 30 M 4,000 3,000 assembly that could lead to the

16 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 8 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** To detect and correct damage to INS DOC: AD the aft attachement lugs of the W/C: (f)i CW 11/26/ ,995:55 34, elevator quadrant support COMPLETED ON >> WO: 5592 ITEM: 23 assembly that could lead to the INS DOC: AD W/C: Pt To ensure that insulation INS DOC: AD blankets constructed of AN-26 W/C: (f) PE T 12/15/2016 are removed from the fuselage MINIMUM CHECK: C INT> 96 M 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) PE T 71,995:55 41, shear ties of the kickload MINIMUM CHECK: C INT> 10,000 7,500 beam. INS DOC: AD W/C: (f)int CW 11/01/ ,995:55 34, COMPLETED ON >> WO: 5592 ITEM: 24 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 11/01/ ,995:55 of the fuel system MINIMUM CHECK: C INT> 36 M 7,000 INS DOC: AD W/C: (f)int CW 11/01/ ,995:55 34, COMPLETED ON >> WO: 5592 ITEM: 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

17 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 9 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** To detect and correct cracking INS DOC: AD in the aft pressure bulkhead W/C: (g)(2) web, which could adversely affect the structural integrity INS DOC: AD W/C: (g)(2)I 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 08/06/1981 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 12/09/ ,995:55 34, WO: 5592 ITEM: 1 NEXT 64,995:55 CHECK: C INS DOC: AD W/C: C LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 1 NEXT 64,995:55 CHECK: C

18 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 10 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** MAIN LANDING GEAR LOCK INS DOC: AD REV#: 3 INSPECTION W/C: C-123 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 1 NEXT 64,995:55 CHECK: C INS DOC: AD W/C: C LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 1 NEXT 64,995:55 CHECK: C TO ASSURE THE FLIGHT CREW HAS INS N/A POSITIVE WARNING WHEN THE L/E PC 11/19/1982 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 07/18/ TO ASSURE ADEQUATE LAVATORY INS N/A FIRE PROTECTION PC 08/22/ RAM AIR DUCT CORROSION INSP PER INS DOC: AD REV#: 1 PARA "B" VISUALLY INSPECT UPPER W/C: A1 LAST 11/01/ ,995:55 34, WALL OF AIR CONDITIONING RAM WO: 5592 ITEM: 42 AIR PLENUM CHAMBER IAW PART II NEXT 11/01/ ,995:55 MINIMUM CHECK: C INT> 48 M 8, TO REPLACE SEALED NEEDLE INS DOC: AD BEARINGS IN THE DOWNLOCK OUTER W/C: LH PE T 11/04/2020 LINK OF THE STRUT UPPER SEGMENT MINIMUM CHECK: A INT> 10 Y

19 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 11 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO REPLACE SEALED NEEDLE INS DOC: AD BEARINGS IN THE DOWNLOCK OUTER W/C: RH PE T 11/04/2020 LINK OF THE STRUT UPPER SEGMENT MINIMUM CHECK: A INT> 10 Y 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 11/14/1988 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 01/25/ ,468:46 30, WO: 3508 ITEM: 9 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 11/14/ TAKE-OFF WARNING SYS INS DOC: AD W/C: E INS DOC: AD W/C: N LAST 01/06/ ,047:31 35, WO: 5592 ITEM: 43 NEXT 63,247:31 MINIMUM CHECK: A INT> TO PREVENT FAILURE OF MLG INS N/A SUPPORT LINK SHAFT PC 11/11/1989

20 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 12 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT FAILURE OF MLG SUPPORT LINK SHAFT FAILURE OF THE MLG TO EXTEND AS INS N/A A RESULT OF LOOSENING OF THE SELF-LOCKING NUT AT THE ATTACHMENT OF THE DOWNLOCK FWD TO PREVENT BINDING OF THE INS N/A AILERON CONTROL WHEEL CAUSED BY PC 08/24/1990 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 08/24/1990 DISCONNECT OF LG CONTROL SELECTOR VALVE ACTUATOR ARM Takeoff configuration nuisance INS N/A warnings when taxi operations PC 08/24/ TO PREVENT STRUCTURAL FAILURE - INS N/A AGING AIRCRAFT MOD DOC: AD MA : MOD DOC: AD MA : PC 08/24/1990 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 :

21 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 13 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** TO PREVENT STRUCTURAL FAILURE - MOD DOC: AD AGING AIRCRAFT MA : MOD DOC: AD MA : MOD DOC: AD MA : PE T 60, MOD DOC: AD MA : PE T 60, 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, 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 : PE T 60, 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 : PC 08/24/1990

22 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 14 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** INBOARD TRAINING EDGE FLAPS INS DOC: AD INBOARD TRACK S/B & W/C: A1b(1) LAST 07/16/ ,643:39 34, WO: 4524 ITEM: 36 NEXT 01/16/ , MINIMUM CHECK: C INT> 18 M 3,000 INS DOC: AD W/C: A1b(2) INS DOC: AD W/C: A1c LAST 07/16/ ,643:39 34, NEXT 01/16/ , 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 11/01/ ,995:55 34, WO: 5592 ITEM: 44 NEXT 37, 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 11/04/ ,995:55 34, MODEL 727 WO: 5592 ITEM: 55 NEXT 11/04/2020 MINIMUM CHECK: C INT> 120 M W/C: C OF1 LAST 11/04/ ,995:55 34, WO: 5592 ITEM: 56 NEXT 11/04/2020 MINIMUM CHECK: C INT> 120 M W/C: C OF6 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 7 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF6 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 8 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF6 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 9 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF6 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 10 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M

23 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 15 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF6 LAST 12/09/ ,995:55 34, MODEL 727 WO: 5918 ITEM: 11 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF6 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 12 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF1 W/C: C OF1 W/C: C OF4 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 63 NEXT 12/09/2015 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 64 NEXT 12/09/2015 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 01/27/ ,468:46 30, WO: 3508 ITEM: 31 NEXT 01/27/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF4 LAST 01/27/ ,468:46 30, WO: 3508 ITEM: 32 NEXT 01/27/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF1 LAST 12/09/ ,995:55 34, WO: 5918 ITEM: 13 NEXT 06/09/2012 MINIMUM CHECK: C INT> 18 M W/C: C OF3 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 66 NEXT 12/09/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF3 LAST 12/13/ ,995:55 34, WO: 5592 ITEM: 67 NEXT 12/13/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF3 LAST 12/13/ ,995:55 34, WO: 5592 ITEM: 68 NEXT 12/13/2016 MINIMUM CHECK: C INT> 72 M

24 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 16 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF2 LAST 12/09/ ,995:55 34, MODEL 727 WO: 5592 ITEM: 69 NEXT 12/09/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 70 NEXT 12/09/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF2 W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 71 NEXT 12/09/2013 MINIMUM CHECK: C INT> 36 M W/C: C OF1 W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 72 NEXT 12/09/2013 MINIMUM CHECK: C INT> 36 M W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 73 NEXT 12/09/2013 MINIMUM CHECK: C INT> 36 M W/C: C OF1 W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 74 NEXT 12/09/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 75 NEXT 12/09/2016 MINIMUM CHECK: C INT> 72 M W/C: C OF2 W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 76 NEXT 12/09/2014 MINIMUM CHECK: C INT> 48 M W/C: C OF4 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 77 NEXT 12/09/2015 MINIMUM CHECK: C INT> 60 M

25 DATE: 03/21/2012 Capital Cargo International - AMIS-2012 RPT CODE: 4.12A TIME: 11:09 FLEET COMPLIANCE STATUS - TYPE: AD PAGE NO.: 17 AIRFRAME DATA AS OF: 03/21/2012 FLIGHT HOURS: 63,207:09 FLIGHT CYCLES: 35, *** CONTINUED *** AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM, W/C: C OF4 LAST 12/09/ ,995:55 34, MODEL 727 WO: 5592 ITEM: 78 NEXT 12/09/2015 MINIMUM CHECK: C INT> 60 M W/C: C OF4 LAST 01/28/ ,468:46 30, WO: 3508 ITEM: 47 NEXT 01/28/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF4 LAST 01/30/ ,468:46 30, WO: 3508 ITEM: 48 NEXT 01/30/2016 MINIMUM CHECK: C INT> 120 M W/C: C OF1 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 79 NEXT 12/09/2015 MINIMUM CHECK: C INT> 60 M W/C: C OF1 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 80 NEXT 12/09/2018 MINIMUM CHECK: C INT> 96 M W/C: C OF3 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 81 NEXT 12/09/2018 MINIMUM CHECK: C INT> 96 M W/C: C OF3 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 82 NEXT 12/09/2018 MINIMUM CHECK: C INT> 96 M W/C: C OF3 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 83 NEXT 12/09/2018 MINIMUM CHECK: C INT> 96 M W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 84 NEXT 12/09/2012 MINIMUM CHECK: C INT> 24 M Reason For Change(s) Made By Empl#: 9920 On 09/21/2010 correct ext date W/C: C OF2 LAST 12/09/ ,995:55 34, WO: 5592 ITEM: 85 NEXT 12/09/2014 MINIMUM CHECK: C INT> 48 M