EFTA00598367.pdf

Maintenance Due List Date Hours Landings Operator CELESTIAL AIRWAYS LIMITED LEVEL 7. LEGATUM PLAZA THE GATE PRECINCT. BUILDING 6. DI PO BOX 506717 DUBAI 71082 UNITED ARAB EMIRATES +971-56-68-1-5877 Make & Model Serial No BOEING B737-700IGW/800/900ER Component ENGINE 1 ENGINE 2 APU 30751 (YG062) Make & Model CFM56-7827133G14 CFM56-7B27B3G14 GTCP 131-9B 24-JUL-2014 5585:49 1578 Serial No Hours Cycles 874966 5585:49 1578 876101 5585:49 1578 P-5466 6986:59 3834 Items Due ATA/AD/SB Description Item No Part No / Serial No / Reference No Disposition Last C/W Intervals Tolerance Time At Inst Next Due Remaining" Group/Tracked Installed Adjustment 34 00-02 3849 5 0010 UPDATE NAVIGATION DATABASE A CHECK 71 00-00 PERFORM ENGINE RUMS ON BOTH ENGINES IAW AMA 71-00-00. 5008 29 230-00-01 919 OPERATIONAL CHECK STANDBY RUDDER SYSTEM TO INCLUDE OBSERVING LOW PRESSURE LIGHT ILLUMINATION AND TI-EN EXTINGUISHING. AIRFRAME A CK AIRFRAME AIRFRAME AIRFRAME MTC 29-230-00-01 SB 737-29-1114 HYDRAULIC POWER - MAIN - HYDRAULIC SYSTEMS A AND B OPEN RI PRESSURE MODULE CHECK VALVE INSPECTION AND 4756 REPLACEMENT AIRFRAME 04-NOV-2013 D: 28 H: 5536:31 L: 1567 24-JUL-2014 M: 1 H: 5585:49 L: 1578 24-JUL-2014 M:1 H: 5585:49 L: 1578 27-MAR-2014 D: 150 H: 5584:27 H: 1000:00 L: 1576 09-JAN-2014 M: -7 D: -19 24-AUG-2014 M:0 D: -4 24-AUG-2014 M: 0 D: -4 24-AUG-2014 M: 0 D: -4 H: 6584:27 H:99838 10-SEP-2014 M: 0 D: 13 Notes: ACCOMPLISHMENT OF THIS SERVICE BULLETIN INSPECTS AND REPLACES. IF NECESSARY. THE PARKER PM H6IC0552M1 CHECK VALVES INSTALLED IN HYDRAULIC SYSTEMS A AND B PRESSURE MOW FS. INSTALLATION OF IMPROVED PRESSURE MODULE CHECK VALVES WILL IMPROVE PERSONNEL SAFETY AND REDUCE PRESSURE MODULE CFECK VALVE RELATED UNSCHEDULED MAINTENANCE AND EXTENDED AIRPLANE DOWNTIME. 25 303-00-01 RESTORE NO. 1 LIFE RAFT (LA-I AFT CUPBOARD) RESTORE I3-SEP-2013 M: 12 M: 0 13-SEP-2014 M: 0 D: 16 3992 AIRFRAME RAPTI 210-10571 10880P FlIfihtdocs- powered by Ifightdocs Copyright © Flightdocs. Inc. All Rights Reserved. MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Page 1 of 11 EFTA00598367 Items Due (Continued) ATA/AD/SB Item No Description Part No / Serial No / Reference No Disposition Group/Tracked Last CAN Installed Intervals Tolerance Time At Inst Adjustment Next Due Remaining 25 383-00-01 RESTORE NO. 3 LIFE RAFT (MI FWD CLPBOARD) RESTORE 13-SEP-2013 M: 12 M: 0 13-SEP-2014 M: 0 D: 16 4029 AIRFRAME RAF1210-105T1 1069CP 25 383-00-01 RESTORE NO. 2 LIFE RAFT (LA-I FWD CLIPBOARD) RESTORE 13-SEP-2013 M: 12 IA: 0 13-SEP-2014 M: 0 D: 16 310 AIRFRAME RAF1210-105 2070JY 34 IM-01-01 SERVICE HEADS 12 DISPLAY OVERHEAD UNIT DESICCANT 24-JUN-2014 M:3 24-SEP-2014 M: 0 D: 27 CAPSULE H: 5585:00 1318 AIPFRAME L: 1577 MTC 34-M-01-01 5 0020 B1 CHECK 24-APR-2014 M:6 24-OCT-2014 M: 1 D: 26 B1 CK H: 5585:00 2 AIRFRAME L: 1577 5 0030 B2 CHECK 04-NOV-2013 M: 12 D: -11 24-OCT-2014 M: 1 D: 26 B2 CK H: 5536:31 3 AIRFRAME L: 1567 24 120-00 SWAP MAIN AND AUX BATTERY LOCATIONS WHEN CAPACITY 22,JAN-2014 M: 12 24-OCT-2014 M: 1 D: 26 CHECKS ME CONDUCTED H: 5584:16 3833 AIRFRAME L: 1576 24 120-00-01 MAIN BATTERY 22,JAN-2014 M: 12 M:0 24-OCT-2014 M: 1 D: 26 H: 5584:16 233 AIRFRAME L: 1576 539CH-1 090520003F523 MTC 24-120-00-01 24 120-00-01 AUXILIARY BATTERY 22-JAN-2014 M: 12 M: 0 24-OCT-2014 M: 1 D: 26 H: 5584:16 234 AIRFRAME L: 1576 539CH-1 0905200046F7A MTC 24-120-00-01 74 010-01-01 DETAILED INSPECTION OF BOTH LEFT MAIN IGNITER 22-AUG-2001 C: 1600.00 C: 1637.00 C: 59.00 PLUGS. H: 87:00 2983 ENGINE 1 C: 37.00 80010-01-01 DETAIL INSPECTION OF THE ND. 1 ENGINE STARTER 22-AUG-2001 C: 1600.00 C: 1637.00 C: 59.00 MAGNETIC CHIP DETECTOR FOR METAL CHIPS. H: 87:00 2971 ENGINE 1 C: 37.00 FlIghtdocs- powered by flightdocs Copyright Rightdocs. Inc. All Rights Reserved. Page 2 of 11 MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 EFTA00598368 Items Due (Continued) ATA/AD/SB Description Disposition Last C/W Intervals Tolerance Time At Inst Next Due Remaining Item No Part No / Serial No / Reference No Group/Tracked Installed Adjustment 1C -O1 AED FRX DEFIBRILLATOR 04-JAN-2013 01-NOV-2014 M: 2 D: 4 H: 5272:23 3844 AIRFRAME L: 1513 G2005 037J-01396 25 2525 TRONAIR TIRE PRESSURE rar Cs CALIBRATION 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 H: 5536:31 4028 AIRFRAME L: 1567 H-2016-01 8840060223 23 100-00-02 OPERATIONALLY CHECK THE EMERGENCY LOCATOR 04-NOV-2012 M:24 04-NOV-2014 M: 2 D: 7 TRANSMITTER (AUTOMATIC / FIXED TYPE). H: 5536:31 2926 AIRFRAME L: 1567 28 054-00-01 CCERATIONALLY (BITE) CFECK THE FUEL FUMP GFI 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 RELAY. SPECIAL NOTE: AWL TASK (28-AWL-20) H: 5536:31 2945 INTERVAL FOR THIS TASK IS 1 YR. SEE MPD SECTION 9. AIRFRAME L: 1567 28 AWL-20 FUNCTIONALLY CI- ECK THE FUEL BOOST PUMP GROUND 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 FAULT INTERRUPTERS (APPLICABLE TO LINE NO. 2210 H: 5536:31 3060 AND ON OR WITH SB 737-28A1201 INCORPORATED AIRFRAME L: 1567 D626A001-OAR SB 737-24A1148R1 CORROSION PROTECTION CF THE ELECTRICAL CONNECTORS RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 IN THE MAIN WHEEL WELL. H: 5536:31 2613 AIRFRAME L: 1567 SB 737-27A1277 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 R2 RAI I REW AND BALL NUT LUBRICATION H: 5536:31 H: 1600:00 H: 7136:31 H: 1550:42 4796 AIRFRAME L: 1567 REF AD 2011-27-03 Notes: REF AD 2011-27-03 SB 737-27-1273 ACCOMPLISH LUBRICATICN OF THE AILERON BALANCE TAB RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 R2 PT 2 HINGE BEARINGS AND ROD END BEARINGS (PART 2) H: 5536:31 H: 4000:00 H: 9536:31 H: 3960:42 3840 AIRFRAME L: 1567 Notes: REF: AD 2006-21-01 AD 2005-18-23 DETAILED INSPECTION OF THE ELECTRICAL CONVECTORS RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 AMD 39-14264 CF THE LINE REPLACEABLE UNIT IN THE IALG WHEEL WELL H: 5536:31 2895 AIRFRAME L: 1567 Notes: THIS AD SUPERSEDES AD 2002-16-03. REF: SS 737-24A1148 R1 8 AMOC B-H340-05-4024 (130S-05-490) AD 2005-18-23- DATED 10/19/2035 TN, Filliphtdocs- powered by llightdocs Copyright © Flightdocs. Inc. All Rights Reserved. MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Page 3 of 11 EFTA00598369 Items Due (Continued) ATA/AD/SB Item No Description Disposition Part No / Serial No / Reference No Group/Tracked Last C/W Installed Intervals Tolerance Time At Inst Adjustment Next Due Remaining AD 2011-27-03 TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 MAD 39-16904 LOAD PATH FOR THE BALLSCREW IN THE DRIVE MECHANISM H: 5536:31 H: 1600:00 H: 7136:31 H: 1550:42 4153 OF THE HSTA AND SUBSEQUENT WEAR AND FAILURE OF THE AIRFRAME L: 1567 SECONDARY LOAD PATH - LUBAICATICN REF 93 737-27A1277 AD 2006-21-01 FREERAY-INDUCED VIBRATION OF THE AILERON BALANCE RECURRING 04-NOV-2013 M: 12 04-NOV-2014 M: 2 D: 7 PAM I TAB - LUBRICATE AILERON BALANCE TAB COMPONENTS H: 5536:31 H: 4000:00 H: 9536:31 H: 3950:42 ARID 39-147843090 USING BMS 3-33 GREASE. AIRFRAME L: 1567 Notes: COMPLIED WITH THROUGH THE ACCOMPLISHMENT OF SEVICE BULLETIN 737-27-1273R2. AD 2013-19-23 TO DETECT AND CCftRECT FATIGUE CRACKING OF VARIOUS OPEN 07-NOV-2014 M: 2 D: 10 MID 39-17605 PRINCIPAL STRUCTURAL ELEMENTS (PSES) REVISE 4960 MAINTENANCE PROGRAM AIRFRAME 23 TEST AND ru FAN CVR ULB BEACON 10,JAN-2013 M:24 10-JAN-2015 M: 4 D: 13 H: 5278:36 4032 AIRFRAME L: 1514 SEACCM DUKANE 03-TM-00037 31 TEST AND ru FAN FOR U.S BEACON 10-JAN-2013 M:24 10-JAN-2015 M: 4 D: 13 H: 5278:36 4033 AIRFRAME L: 1514 SEACOM DUKANE 03-TM-00037 33 020-00-02 OPERATIONAL CHECK FLIGHT DECK EMERGENCY LIGHTING 10,JAN-2013 M:24 10-JAN-2015 M: 4 D: 13 SWITCH "ON- AND "ARMED- POSITION AND ATTENDANT H: 5278:36 1270 PANEL EMERGENCY LIGHTING SWITCH -ON" POSITION. AIRFRAME L: 1514 MTC 33-020-00-02 35 00-05 HYDROSTATIC TEST NO. 2 PASSENGER OXYGEN CYLINDER HYDROSTATIC TEST 27,JAN-2012 M:36 M: 0 27-JAN-2015 M: 4 D: 30 H: 5005:24 1419 AIRFRAME L: 1459 806525-211 ALT282-9775 35 00-05 HYDROSTATIC TEST NO. 3 PASSENGER OXYGEN CYLINDER HYDROSTATIC TEST 27,JAN-2012 M: 36 M: 0 27-JAN-2015 M:4 D:30 H: 5005:24 1420 AIRFRAME L: 1459 806525-211 ALT282-9760 35 00-05 HYDROSTATIC TEST NO. 1 PASSENGER OXYGEN CYLINDER HYDROSTATIC TEST 27-JAN-2012 M: 36 M: 0 27-JAN-2015 M: 4 D: 30 H: 5005:24 1418 AIRFRAME L: 1459 8C6525-211 24966/596 TN_ . Flliphtdocs- powered by IlightdoCS Copyright Flightdocs. Inc. All Rights Reserved. MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Page 4 of 11 EFTA00598370 Items Due (Continued) ATA/AD/SB Description Item No Part No / Serial No / Reference No Disposition Last C/W Intervals Tolerance Time At Inst Next Duo Remaining Group/Tracked Installed Adjustment II0-01 2928 INSPECT (DETAILED) THE SMOKE HOODS FOR CONDITION. 25 420-00-01 FIRST AID KIT 319 AFAK 050206039 MTC 25-420-00-01 Notes: EXPIRATION 01/31/2015 25 6V SMOKE DETECTOR UNIT (SOU) BATTERY (OT 2) 4110 160-1173-02 NSN 2600-09 REPLACE CABIN SMOKE DETECTOR BATTERIES 21-N0V-2011 M: 36 H: 4953:12 L: 1447 AIRFRAME RESTORE AIRFRAME AlFtFRAME 28,JAN-2013 M: 24 H: 5292:55 L: 1516 22,JAN-2014 M: 12 H: 5584:16 L: 1576 054)N-2011 M:72 445 AlFtFRAME JET CENTER DOC. 099054010 AD 2010-02-04 TO PREVENT THE FAILLRE OF THE VALVE IN THE CLOSED OPEN MD 39-16175 POSITION. OPEN POSITION. OR PARTIALLY OPEN 4003 POSITION AIRFRAME Notes: CUSTOMER SET NEXT DUE. 49 120-00-01 AFU - CLEAN COMBUSTER DRAIN VALVE 3124 API) 17-FEB-2035 H:4000:00 H: 3354:06 C: 1798.00 28-JAN-2015 M: 5 D: 0 M: 0 31-JAN-2015 M:5 D:3 M: 0 17-FEB-2015 M: 5 D: 20 17-FEB-2015 M: 5 D: 20 18-FEB-2015 M: 5 D: 21 H: 7354:06 H: 367:07 AD 2013-07-09 TO PREVENT AN INGITION SOURCE. WHICH COULD RESULT OPEN 20-MAY-2015 M: 8 D: 22 AMD 39-17413 IN AN OXYGEN-FED FIRE OR AN IN VALVE JAM IN A 4915 CREW OXYGEN MASK STOWAGE BOX UNIT AIRFRAME Notes: REFERENCE SB 737-35A1121. REVISION 1. DATED NOVEMBER 7. 2011 AND INTERTECI-NIOUE SE.S8MXP1/4-35-175. REVISION 2. DATED MAY 10. 2011. A REVIEW OF AIRPLANE MAINTENANCE RECORDS IS ACCEPTABLE IN LIEU OF THIS INSPECTION IF THE SERIAL NUMBER OF THE CREW OXYGEN MASK STOWAGE BOX UNIT CAN BE OONCLUSIVELY DETERMINED FROM THAT REVIEW 25 410-00-01 RESTORE COCKPIT #3 SMOKE HOOD REPLACE 014UN-2005 M: 120 M: 0 01-JUN-2015 M: 9 D: 4 363 AIRFRAME 802300-14 0605001083 MTC 25-410-00-01 25 410-00-01 RESTORE COCKPIT p1 SMOKE HOOD REPLACE 01-JUN-2005 M: 120 M: 0 01-JUN-2015 M: 9 D: 4 361 802300-14 Fllghtdocs powered by flightdocs Copyright Rightdocs. Inc. All Rights Reserved. Page 5 of 11 AIRFRAME 0605001084 MTC ZS-410-00-01 MAINTENANCE DUE UST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 EFTA00598371 Items Due (Continued) ATA/AD/SB Item No Description Disposition Part No / Serial No / Reference No Group/Tracked last C/W Installed Intervals Tolerance Time At Inst Adjustment Next Due Remaining AD 2013-08-01 TO DETECT AND CORRECT DAMAGE TO THE FIRE SEALS. OPEN 10-JUN-2015 M: 9 D: 13 AMD 39-17418 1.M-IICH COULD ALLOW AIRFLOW INTO THE ENGINE FIRE 4924 ZONE AIRFRAME Notes: REFERENCE SB 737-78-1086 - THIS APPLIES TO LINE NUMBERS 1 THROUGH 3028 INCLUSIVE AND REOUIERS A GVI OF THE L/I-I AND R/H THRUST REVERSER HALVES OF EACH ENGINE FOR DAMAGE TO THE UPPER FIRE SEALS. 35 0006 NO. 1 PASSENGER OXYGEN CYLINDER LIFE LIMIT 27,JAN-2012 M: 180 M:0 254UL-2015 M: 100: 27 H: 5006:24 1422 AIRFRAME L: 1459 8C6525-211 24966/596 Notes: NEXT DUE ACCORDING TO HT AS DATE OF MANUFACTURE IS MISSING 350006 NO. 3 PASSENGER OXYGEN CYLINDER LIFE LIMIT 01-SEP-2000 M: 180 M: 0 01-SEP-2015 M: 120:4 1424 AIRFRAME 8C6525-211 A17282-9760 Notes: NEXT DUE AS THE HT DUE TO UNKNOWN AC DATE 3500-06 NO. 2 PASSENGER OXYGEN CYLINDER LIFE LIMIT 01-SEP-2000 M: 180 M: 0 01-SEP-2015 M: 120:4 1423 AIRFRAME 8C6525-211 A17282-9775 35 031-00 HYDROSTATIC TEST CREW OXYGEN CYLINDER HYDROSTATIC TEST 02-SEP-2012 M: 36 M: 0 02-SEP-2015 M: 120: 5 H: 5218:00 1417 AIRFRAME L: 1503 801307-00 618742 AVOX SIL-35-103 25290-00-01 RESTORE CREW LIFE JACKETS RESTORE 30-SEP-2010 M: 60 M:0 30-SEP-2015 M: 130:2 299 AIRFRAME P0724-105 MTC 25-293-00-01 Notes: MFR - EAM SB 737-34-2454 NAVIGATION - AIR DATA SYSTEM - ALTIMETRY SYSTEM OPEN 31-OCT-2015 M: 14 0: 3 TEST 4967 AIRFRAME Notes: PERFORM THIS 58 AT THE SAME TIME AS THE 24 MONTH MPD ATA 34 ALTIMETER TESTS. 34 00-01 TEST STANDBY ALTIMETER INDICATOR (FAR 91.411) 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 H: 5536:31 3157 AIRFRAME L: 1567 WL102AM53 AF197 FAR 91.411 51 00-01 VISUAL INSPECTION OXYGEN TAWS AND WATER TANK 04-NOV-2013 M: 24 04-N0.1-2315 M: M D: I STRUCTURE IN THE AFT CARGO COMPARTMENT H: 5536:31 1514 AIRFRAME L: 1567 JET CENTER DOC. 099054010 Flight .siocs- tr. yhtdocS MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Copyright ©Flightdocs. Inc. All Rights Reserved. Page 6 of 11 EFTA00598372 Items Due (Continued) ATA/AD/SB Item No Description Part No / Serial No / Reference No Disposition Group/Tracked Last C/W Installed Intervals Tolerance Time At Inst Next Due Adjustment Remaining 23 050-00-01 FUNCTIONAL CFECK VOICE RECORDER FOR AUDIO FIDELITY 04-NOV-2013 M:24 :D: . H: 5536:31 176 AIRFRAME L: 1567 MTC 23-050-00-01 23060-00-01 OPERATIONAL CHECK OF THE CVR UNDERWATER LOCATOR 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 BEACON H: 5536:31 177 AIRFRAME L: 1567 MTC 23-060-00-01 25390-00-01 REPLACE EMERGENCY FLASHLIGHT BATTERIES 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 H: 5536:31 317 AIRFRAME L: 1567 MTC 25-M0-00-01 27 110-00-01 DETAILED VISUAL INSPECTION CF THE STABILIZER TRIM 04-NOV-2013 M:24 04-NOV-2015 M: 14 0: 7 JACKSCREW. BALLNUT. BALLNUT RETURN TUBES AND THE H: 5536:31 525 UPPER AND LOWER GIMBALL PINS AIRFRAME L: 1567 MTC 27-110-00-01 33 060-00-02 RESTORE (TWO OR MORE COMPLETE DEEP CYCLES) RESTORE 04-NOV-2013 M:24 04-NOV-2015 M: 14 0: 7 BATTERY CAPACITY TO REQUIRED STANDARD H: 5536:31 1272 AIRFRAME L: 1567 MTC 33-060-00-02 34 010-00-01 FUNCTIONAL LEAK CHECK OF THE CAPTAINS PITOT SYSTEM 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 H: 5536:31 1304 AIRFRAME L: 1567 MTC 34-010-00-01 34 020-00-01 FUNCTIONAL LEAK CHECK OF THE FIRST OFFICERS PITOT 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 SYSTEM . H: 5536:31 1305 AIRFRAME L: 1567 MTC 34-020-00-01 34 030-00-01 FUNCTIONAL LEAK CHECK OF THE STANDBY PITOT SYSTEM 04-NOV-2013 M: 24 04-NOV-2015 M: 14 0: 7 H: 5536:31 1306 AIRFRAME L: 1567 MTC 34-030-00-01 34 040-00-01 FUNCTIONAL LEAK CFECK OF THE CAPTAINS STATIC 04-NOV-2013 M:24 04-NOV-2015 M: 14 D. 1 SYSTEM. H: 5536:31 3121 AIRFRAME L: 1567 Flightdocs- powered by !Iightdocs Copyright © Flightdocs. Inc. All Rights Reserved. Page 7 of 11 MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU I-CURS: 8131:59 EFTA00598373 Items Due (Continued) ATA/AD/SB Item No Description Disposition Last C/W Intervals Tolerance Time At Inst Next Due Part No / Serial No / Reference No Group/Tracked Installed Adjustment Remaining CL:04:0-0 FUNCTIONAL LEAK CHECK OF THE FIRST OFFICERS STATIC 04-NOV-2013 M:24 04-N0V-2015 M: 14 0: 7 SYSTEM . H: 5536:31 1307 AIRFRAME L: 1567 MTC 34-050-00-01 34 060-00-01 FUNCTIONAL LEAK DECK OF THE STANDBY STATIC SYSTEM 04-NOV-2013 M:24 04-NOV-2015 M: 14 D: 7 H: 5536:31 1308 AIRFRAME L: 1567 MTC 34-060-00-01 34 110-00-01 TEST NO. 1 ATC TRANSPONDER MANDATORY 04-NOV-2013 M:24 04-N0V-2015 M: 14 D: 7 H: 5536:31 1316 AIRFRAME L: 1567 34 110-00-02 TEST NO. 2 ATC TRANSPONDER MANDATORY 04-NOV-2013 M:24 04-NOV-2015 M: 14 0: 7 H: 5536:31 1317 AIRFRAME L: 1567 SB 737-27A1277 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - RECURRING 04-NOV-2013 M:24 04-NOV-2015 M: 14 0: 7 R2 RAIIOPREW AND BALL NJT INSPECTION H: 5536:31 H: 6400:00 H: 11936:31 H: 6350:42 4794 AIRFRAME L: 1567 REF AD 2011-27-03 Notes: REF AD 2011-27-03 SB 737-27-1273 ACCOMPLISH FREERAY CHECK OF TI-E AILERON BALANCE RECURRING 04-NOV-2013 M:24 04-N0V-2015 M: 14 0: 7 R2 PT 1 TAB FREEPLAY (PART 1) H: 5536:31 H: 8000:00 H: 13536:31 H: 7950:42 3839 AIRFRAME L: 1567 Notes: REF: AD 2006-21-01 AD 2011-27-03 TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY RECURRING 04-NOV-2013 M:24 04-NOV-2015 M: 14 CI: 7 MID 39-16904 LOAD PATH FOR THE BALLSCREW IN THE DRIVE MECHANISM H: 5536:31 H: 6403:00 H: 11936:31 H: 6350:42 4152 OF THE HSTA AND SUBSEOUENT WEAR AND FAILURE OF THE AIRFRAME L: 1567 SECONDARY LOAD PATH - DETAILED INSPECTION PEF 58 737-27A1277 Notes: PEF SB 373-27A1277 R2 AD 2013-19-03 TO DETECT AND CORRECT POSSIBLE DAMAGE CAUSED BY OPEN 04-NOV-2015 M: 14 0: 7 MID 39-17585 INSUFFICIENT SEPARATION BETWEEN THE WIRE BUNDLES 4956 AND HYDRAULIC TUBING IN THE MAIN LANDING GEAR AIRFRAME (MLG) WHEEL WELL Notes: THIS AD APPLIES TO THE BOEING COMPANY MODEL 737-600. -703. -700C. -800. -900. AND -900ER SERIES AIRPLANES. CERTIFICATED IN ANY CATEGORY. LINE NUMBERS (L/NS) 1060 THROUGH 3289 INCLUSIVE. AND 3294. BUT EXCLUDING &NS 3138. 3158. 3169. 3175. 3216. 3224. 3253. AND 3274. FlIghtdocs- powered by flightdocs Copyright © Rightdocs. Inc. All Rights Reserved. MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Page 8 of 11 EFTA00598374 Items Due (Continued) ATA/AD/SB Description Item No Part No / Serial No / Reference No Disposition Last C/W Intervals Tolerance Time At Inst Next Duo Remaining Group/Tracked Installed Adjustment AD 2006-21-01 PAM G AMO 39-147843pes FREERAY-INDUCED VIBRATION OF THE AILERON BALANCE TAB - MEASURE AILERON BALANCE FREE PLAY RECURRING AIRFRAME 04-NOV-2013 M:24 H: 5536:31 H: 8000:00 L: 1567 Notes: COMPLIED WITH THROUGH THE ACCOMPLISI-MENT OF SEVICE BULLETIN 737-27-1273R2. 26 461-01 INSPECT LEFT FWD CLOSET PORTABLE HALON BOTTLE 4008 AD 2008-11-08 AMO 39-15530 3949 25 100-02 3889 25 103-03 5013 SB 737-30A1063 R2 4987 AD 2012-24-08 AMO 39-17278 4780 1600 W-762035 HR3 INC. DETAILED INSPECTION OF FLIGHT DECK NO. 2 WINDOW FOR CRACKING AND DAMAGE (TABLE 1) 01-JAN-2010 M: 72 AlFtFRAME COMPLIED WITH 10-JAN-2013 H: 5278:36 AIRFRAME L: 1514 M:36 H: 7500:00 04-NOV-2015 M: 14 0: 7 H: 13536:31 H: 7950:42 01-JAN-2016 M: 160: 4 10-JAN-2016 M: 16 0: 13 H: 12778:36 H: 7192:47 Notes: — NOTE— INCORPORATION OF SIC STO1Plees TERMINATES NE REPETITIVE INSPECTIONS OF THE LH AND RH WINDOW NO. 4 AND NO. 5. REFER TO PATS AIRCRAFT LLC WORK ORDER 6562-010R-0556. RENEW REGISTRATION FOR EMERGENCY LOCATOR TRANSMITTER (4066/HZ) BEACON ID 20075 30000 FFBFF. RESEW REGISTRATION FOR EMERGENCY LOCATOR TRANSMITTER (406M-IZ) BEACON ID ADCCO 8720F 00801. ICE AND RAIN PROTECTION - PITOT AND STATIC - AIR DATA PROBE ANTI-ICING SYSTEM - AIR DATA PROBE HEAT AUTOMATION INSTALLATION (REV. 2) AIRFRAME AIRFRAME OPEN AIRFRAME 14-JAN-2014 M:24 14-JAN-2016 M: 16 0: 17 14-JAN-2014 M:24 14-JAN-2016 M: 16 0: 17 Notes: REF AD 2012-24-08. GLOBAL AMCC LETTER 1306-14-66 EXTENDS COMPLIANCE THE TO 36 MONTHS FROM AD EFFECTIVE DATE. TO PREVENT ICE FROM FORMING ON AIR DATA SYSTEM SENSORS AND CONSEQUENT LOSS OF OR MISLEADING AIRSPEED INDICATION ON ALL AIRSPEED INDICATING SYSTEMS Notes: REFERENCE SB 737-30A1063. GLOBAL AMOC LETTER 130S-14-66 EXTENDS COMPLIANCE TO 36 MONTHS FROM EFFECTIVE DATE. OPEN AIRFRAME 25 290-00-01 RESTORE PASSENGER LIFE JACKETS RESTORE 28-JAN-2011 M: 60 H: 4656:36 307 AIRFRAME L: 1373 SB 737-78-1090 25 100-04 5010 P0724-105C MTC 25-290-00-01 Notes: MFR - EAM EXHAUST - THRUST REVERSER SYSTEM - INSPECTION FOR AND REMOVAL OF NE THRUST REVERSER INNER WALL COOLING HOLE BLOCKAGE RENEW REGISTRATION FOR EMERGENCY LOCATOR TRANSMITTER (406M-IZ) BEACON ID ADCCO 87213 5014 00801. FlIpphtdocs- powered by flightdocs Copyright Flightdocs. Inc. All Rights Reserved. Page 9 of 11 OPEN AIRFRAME AIRFRAME M: 0 14-JAN-2016 M: 16 0: 17 14-JAN-2016 M: 16 0: 17 28-JAN-2016 M: 17 0: 0 31-JAN-2016 M: 17 CI: 3 11-FEB-2014 M:24 11-FEB-2016 M: 17 0: 14 MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 EFTA00598375 Items Due (Continued) ATA/AD/SB Item No Description Disposition Part No / Serial No / Reference No Group/Tracked Last C/W Installed Intervals Tolerance Time At Inst Adjustment Next Due Remaining SB 737-31A1332 INDICATING / RECORDING SYSTEMS - AURAL WARNING OPEN 06-MAR-20I6 M: 180: 7 R4 SYSTEM - INSTALLATION OF THE CABIN ALTITUDE 4966 WARNING SYSTEM AND TAKEOFF CONFIGURATION WARNING AIRFRAME SYSTEM LIGHTS (REV. 4) Notes: REF AD 2013-02-05. AD 2013-02-05 TO PREVENT FAILURE OF THE FLIGHTCREW TO RECOGNIZE OPEN 06-WtR-2016 M: 18D: 7 MD 39-17326 AND REACT TO A VALID CABIN ALTITUDE WARNING HORN 4789 AIRFRAME Notes: REF SB 737-31A1332. REVISION 3. REVISION 4 IS APPROVED AMOC. 26 00-08 NO. 3 CARGO FIRE EXTINGUISHER 60711E FORWARD SOUIB LIFE LIMIT 22-JUN-2009 M: 120 M: 39 22-MAR-2016 M: 180: 23 H: 4429:54 427 AIRFRAME L: 1325 M446290 00098 HOLLINGSEAD DOC. 20689 35 111-00 HYDROSTATIC TEST PORTABLE OXYGEN BOTTLE SALON HYDROSTATIC TEST 24-MAY-2011 M: 60 M: 0 24-MAY-2016 M: 20 0: 26 H: 4767:54 1438 AIRFRAME L: 1408 5600-1C1A-F23A 175943 AVOX SIL-35-103 49 190-00-01 APU - VISUAL INSPECTION LUBE MODULE FOR LEAKAGE. 13-DEC-2013 H: 1000:00 H: 7974:48 H: 987:49 GENERAL CONDITION. AND SECURITY OF INSTALLATION H: 6974:48 3129 APU C: 3821.00 49 200-00-01 APU - DETAILED INSPECTION OIL FILTER DELTA P 13-DC-C-2013 H: 1000:00 H: 7974:48 H: 987:49 INDICATOR H: 6974:48 3130 APU C: 3821.00 72 320-01-01 DETAILED INSPECTION OF THE LEFT ENGINE FWD SUMP. 02-JUL-2012 H: 500:00 H: 5652:33 H: 66:44 AFT SUMP. AGB/TGB MAGNETIC CHIP DETECTORS OR H: 5152:33 3001 DEBRIS MONITORING SYSTEM DETECTORS AND SCAVENGE AIRFRAME L: 1488 SCREENS FOR PARTICLES. 72 320-02-01 DETAILED INSPECTION OF THE RIGHT ENGINE FWD SUMP. 02-JUL-2012 H: 500:00 H: 5652:33 H: 66:44 AFT SUMP. AGB/TGB MAGNETIC CHIP DETECTORS OR H: 5152:33 3002 DEBRIS MONITORING SYSTEM DETECTORS AND SCAVENGE AIRFRAME L: 1488 SCREENS FOR PARTICLES. C: 1488.00 35 111-00 HYDROSTATIC TEST LEFT FWD CLOSET PORTABLE OXYGEN HYDROSTATIC TEST 08-JUL-2011 M: 60 M: 0 08-JUL-2016 M: 220: 10 BOTTLE H: 4789:06 1437 AIRFRAME L: 1412 5600-1CIA-F23A 175944 AVOX SIL-35-103 25 243-00-01 COCKPIT LIFE JACKET 18-JUL-2011 M: 60 M: 0 18-JUL-2016 M: 22 D: 20 H: 4789:06 4120 AIRFRAME L: 1412 P0723E105P 10081110038 FlIghtdocs- powered by flightdocs Copyright Flightdocs. Inc. All Rights Reserved. MAINTENANCE DUE LIST N737L 28-AUG-2014 PROJECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 Page 10 of 11 EFTA00598376 Items Due (Continued) ATA/AD/SB Item No Description Disposition Part No / Serial No / Reference No Group/Tracked Last C/W Installed Intervals Tolerance Time At Inst Adjustment Next Due Remaining 25 290-00-01 COCKPIT LIFE JACKET 18-JUL-20I I M:60 01: I 8-JUL-2016 M: 220: 20 H: 4789:06 4119 AlFtFRAME L: 1412 P0723E105P 10081110010 26 00-08 NO. 3 CARGO FIRE EXTINGUISHER BOTTLE AFT SQUIB LIFE LIMIT 22-JUN-2009 M: 120 t.,1: 35 22-JUL-2016 M: 22 0: 24 H: 4429:54 428 AlFtFRAME L: 1325 M446290 00038 HOU_INGSEAD DOC. 20689 53 070-00-01 INSPECT (INTERNAL-GENERAL VISUAL) FORWARD OF 22-AUG-2001 M: 180 22-AUG-2016 M: 23 0: 25 NOSE WHEEL WELL H: 87:00 1625 AlFtFRAME L: 37 MTC 53-070-00-01 53 120-00-01 INSPECT (INTERNAL-GENERAL VISUAL) 22-AUG-2001 M: 180 22-AUG-2016 M: 23 0: 25 ELECTRICAUELECTRONIC COWARTMENT. STATION 294.5 H: 87:00 1720 TO 396 AlFtFRAME L: 37 MTC 53-120-00-01 53 130-00-01 INSPECT (INTERNAL-GENERAL VISUAL) FORWARD CARGO 22-AUG-2001 M: 180 22-AUG-2016 M: 23 0: 25 COMPARTMENT SKIN PANELS H: 87:00 1784 AlFtFRAME L: 37 MTC 53-133-00-01 25240-00-02 FORWARD SERVICE ESCAPE SLIDE 04-NOV-2013 M: 36 M: 0 31-AUG-2016 M: 24 0: 3 H: 5536:31 291 AIRFRAME L: 1567 5A3307-5 ENG2502 MTC 25-240-00-02 Notes: NEXT DUE OF SLIDE IS BASED ON NEXT HYDROSTATIC TEST CF CYLINDER 25240-00-01 FORWARD ENTRY ESCAPE SLIDE 04-NOV-2013 M: 36 M: 0 30-SEP-2016 M: 25 0: 2 H: 5536:31 290 AIRFRAME L: 1567 5A3307-5 ENG5262 MTC 25-240-00-01 Notes: NEXT DUE OF SLIDE IS BASED ON NEXT HYDROSTATIC TEST CF CYLINDER FIliphtdocs- powered by flioNdocs Copyright Rightdocs. Inc. All Rights Reserved. Page 11 of 11 MAINTENANCE DUE LIST N737L 28-AUG-2014 PROTECTED TO DATE: FRI SEP 30 2016 HOURS: 5662:07 LANDINGS: 1654 CYCLES: 2341 APU HOURS: 8131:59 EFTA00598377