EFTA01734611.pdf

Print Date 07/09/2016 14:10 P/N Last Compliance Print Page: 1 of 3 P/N: CR056-74327/63 PIN Description: GE AIRCRAFT ENGINE CFM: P/N S/N: 876170 P/N Hours: 12368:34 P/N Cycles: 4156 Days: 5950 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 05/08/2013 Schedule Remaining/ Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information 737-73A1011 ENGINE FUEL HOSE QUICK DISCONNECT. UPDATE 0 19/07/2001 00:00:00 AD99-03-08 B3-73A1011 Rev: Hours Cycles Category: ASB 55737-73A1011 E/C Reset At: Status: TERMINATED Reason Rev: 2 SB737-73A1011R2 ENGINE FUEL SUPPLY HOSE AND STRUT FUEL FITTING REPLACEMENT ENGINE FUEL SUPPLY HOSE AND STRUT FUEL FITTING REPLACEMENT 737-73A1016 INTRODUCE SOFTWARE VERSION 7.B.0 ( WO 3397 26/06/2003 00:00:00 i853M78P22) FOR EEC Rev:2 Hours Cycles Category: ASB E/C Reset At: Status: TERMINATED Reason Rev: 2 LATEST EEC SW VERSION 7BWF2 IS ALREADY C/OUT UAW CFM SB 73-0084 INSTALLED CFM56.75.72.140 INTRODUCE BONDED CAUTION PLATE ON HANDCRANKING COVER Category: ASB Status: N/A Reason Rev: 1 REFER THE ENGINE EDS CFM56-78.72.328 REDUCED INTERVAL AFT SUMP MAGNETIC CHIP DETECTOR INSPECTION Category: ASB Status: N/A Reason Rev: 0 WA. THE ENGINE SRI IS NOT IN THE AFFECTED LIST CFM56-713-72-329 REPLACEMENT OF NO.4 ROLLER BEARING IN DEFECTIVE BATCH Category: ASB Status: N/A Reason Rev: 0 ENGINE NOT IN THE AFFECTED LIST PER SB EFFECTIVITY EFTA_R1_00012998 EFTA01734611  Print Date 07/09/2016 14:10 P/N Last Compliance Print Page: 2 of 3 P/N: CFM56-7-827/B3 PIN Description: GE AIRCRAFT ENGINE CFM: P/N SIN: 876170 P/N Hours: 12368:34 P/N Cycles: 4156 Days: 5950 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 05/08/2013 Schedule Remaining/ Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information CFM56-78-72-336 INSTALLATION OF SAFETY WIRE LOCK OVER UPDATE 0 03/07/2001 00:00:00 THE OIL TEMP. PROBE 4 HOUSING Rev: Hours Cycles Category: ASB E/C Reset At: Status: TERMINATED Reason Rev: 0 TASK COMPLETED CFM56-78-73-0104 INSPECTION OF 3 FUEL SUPPLY TUBES FOR WO 12308 01/05/2008 12:00:00 WEAR AND INTODUCTION OF KAVLAR CUSHION CLAMP Rev:1 Hours Cycles Category: ASS E/C Reset At: Status: TERMINATED Rev: 1 CFM56-78-73-0204 ELECTRONIC CONTROL UNIT - NEW SOFTWARE 737-SL-73-013 VERSIONS TB.WF3 FOR SAC AND DAC ENGINES AND 7.B.WE2 FOR SAC ENGINES Category: ASB Status: TERMINATED Reason Rev: OA TASK COMPLETED CFM56-78-73-026 NTRODUCE SOFTWARE VERSION 7.84 FOR EEC Category: ASB Superseded By: CFMS6-7B-73-0204 Status: N/A Reason Rev: 0 SUPERSEDED BY SS 73-0204 CFM56-78-73-028 A INTRODUCE HYDRO MECHANICAL UNIT P/N UPDATE 0 03/12/1999 00:00:00 165.3M56P(M Rev: Hours Cycles Category: ASB SC Reset At: Status: TERMINATED Reason Rev: 1 INTRODUCED HYDRO MECHNICAL UNIT PM 1853$456P07 DURING PRODUCTION EFTA_R1_00012999 EFTA01734612  P/N Last Compliance Print Print Date 07/09/2016 14:10 Page: 3 of 3 P/N: CFM56-74327033 PIN Description: GE AIRCRAFT ENGINE CFM: P/N SIN: 876170 PIN Hours: 12368:34 P/N Cycles: 4156 Days: 5950 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 05/08/2013 Schedule Remaining/ Ament NO Document/SB E/C Description: HrslCys/DyslDte Next Due Last Compliance Information CFM56-7B-73-034 A INTRODUCTION OF A NEW FUEL PUMP WITH NEW FILTER COVER Category: ASB Status: TERMINATED Reason Rev: 01 LATEST FUEL PUMP PM IS INSTALLED. CFM56-7B-73-076 SERVO FUEL HEATERS. IDENTIFICATION OF POTENTIAL LEAKING UNITS Category: ASB Status: N/A Reason Rev: 0 WA - THE ENGINE ISNOT LISTED IN THE EFFECTTIAIT LIST CFM56-7B-73-A091 INSPECTION OF 3 FUEL SUPPLY TUBES FOR WEAR AT CLAMP LOCATIONS Category: ASB Status: N/A Superseded By: CFMSS-7B-73-0104 Reason Rev: 1 INSPECTION OF 3 FUEL SUPPLY TUBES FOR WEAR AT CLAMP LOCATIONS EFTA_R1_00013000 EFTA01734613  Print Date 07/09/2016 14:11 P/N Last Compliance Print Page: 1 of 3 P/N. CP056.7.827/83 PIN Description: GE AIRCRAFT ENGINE CFM: P/N S/N: 889151 PIN Hours: 6153:30 P/N Cycles: 2203 Days: 5717 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 12/0112001 Schedule Remaining/ Ament NO Document/SB E/C Description: HrslCys/Dys/Dte Next Due Last Compliance Information 737-73A1011 ENGINE FUEL HOSE QUICK DISCONNECT. AD99-03-08 B3-73A1011 Hours Cycles Category: ASB EIC Reset At: 6153:30 2203.00 Status: N/A Reason Rev: 2 SB737-73A1011R2 NOT AFFECTED TO LINE NO 737-73A1016 INTRODUCE SOFTWARE VERSION 7.B.0 ( 1853MT8P22) FOR EEC Hours Cycles Category: ASS FJC Reset At: 6153:30 2203.00 Status: TERMINATED Reason Rev: 2 LATEST EEC SW VERSION 76WF2 IS ALREADY INSTALLED CFM56-78-72-140 INTRODUCE BONDED CAUTION PLATE ON HANDCRANKING COVER Category: ASB Status: N/A Reason Rev: 1 REFER THE ENGINE EDS CFM56-78-72-328 REDUCED INTERVAL AFT SUMP MAGNETIC CHIP DETECTOR INSPECTION Category: ASB Status: N/A Reason Rev: 0 NIA- THE ENGINE SON IS NOT IN THE AFFECTED LIST CFM56-78-72-329 REPLACEMENT OF NO. 4 ROLLER BEARING IN DEFECTIVE BATCH Category: ASB Status: N/A Reason Rev: 0 WA BY ENGINE SW LISTED IN THE SD EFTA_R1_00013001 EFTA01734614  Print Date 07/09/2016 14:11 P/N Last Compliance Print Page: 2 of 3 P/N: CFM56-7-527/B3 PIN Description: GE AIRCRAFT ENGINE CFM: P/N S/N: 889151 P/N Hours: 6153:30 P/N Cycles: 2203 Days: 5717 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 12/01/2001 Schedule Remaining/ Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information CFM56-78-72-336 INSTALLATION OF SAFETY WIRE LOCK OVER WO 16115 16/09/2011 18:00:00 THE OIL TEMP. PROBE S. HOUSING Rev.0 Hours Cycles Category: ASB E/C Reset At: 2813:55 1178.00 Status: TERMINATED Reason Rev: 0 TASK COMPLETED CFM56-7B-73-0104 INSPECTION OF 3 FUEL SUPPLY TUBES FOR WO 20202 08/08/2014 08:45:00 WEAR AND INTODUCTION OF KAVLAR CUSHION CIAMP Rev:1 Hours Cycles Category: ASB E/C Reset At: 5107:40 1870.00 Status: TERMINATED Rev: 1 CFM56-78-73-0204 ELECTRONIC CONTROL UNIT - NEW SOFTWARE 737-SL-73-013 VERSIONS 7.B.WF3 FOR SAC AND DAC ENGINES AND 7.B.WF2 FOR SAC ENGINES Category: ASS Status: TERMINATED Reason Rev: OA TASK COMPLETED CFM56-78-73-026 NTRODUCE SOFTWARE VERSION 7.8.J FOR EEC Hours Cycles Category: ASB E/C Reset At: Superseded By: CFMS8-7B-73-0204 6153:30 2203.00 Status: N/A Reason Rev: 0 SUPERSEDED BY SS 73-0204 CFM56-78-73-028 A INTRODUCE HYDRO MECHANICAL UNIT P/N 165.3M5SPQ7 Hours Cycles Category: ASB E/C Reset At: 6153 :30 2203.00 Status: TERMINATED Reason Rev: 1 FACTORY COMPLIED. EFTA_R1_00013002 EFTA01734615  P/N Last Compliance Print Print Date 07/09/2016 14:11 Page: 3 of 3 P/N: CFM56-74327/B3 PIN Description: GE AIRCRAFT ENGINE CFM: P/N S/N: 889151 PIN Hours: 6153:30 P/N Cycles: 2203 Days: 5717 Installed NC: A6DFR Total NC Hours: 6153:30 Total NC Cycles: 2203 Installed Date: 12/01/2001 Schedule Remaining/ Ament NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information CFM56-78-73-034 A INTRODUCTION OF A NEW FUEL PUMP WITH NEW FILTER COVER Hours Cycles Category: ASB EIC Reset At: 6153 :30 2203.00 Status: TERMINATED Reason Rev: 01 LATEST FVEL PUMP PM IS INSTALLED CFM56-78-73-076 SERVO FUEL HEATERS. IDENTIFICATION OF POTENTIAL LEAKING UNITS Category: ASB Status: N/A Reason Rev: 0 NIA - THE ENGINE ISNOT LISTED IN THE EFFE0TTIAPe LIST CFM56-75-73-A091 INSPECTION OF 3 FUEL SUPPLY TUBES FOR WEAR AT CLAMP LOCATIONS Category: ASB Status: N/A Superseded By: CFM56.TB-73-0104 Rev: 1 EFTA_R1_00013003 EFTA01734616  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 1 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: ASB) Schedule Remaining/ Amant NO Document/SB E/C Description: Hrs/Cys/Dys/Dta Next Due Last Compliance Information E/C: 737-11A1109 SB 737-11A1109 INSTALLATION OF IN-FLIGHT SPEEDBRAKE Manual Compliance 16/09/2002 Rev: 1 USAGE LIMITATION MARKER NC Total Hours: 1103:35 NC Total Cycles: 595 COMLIED BY LHT DURING CABIN COMPLETION BY Category: ASB PRVE CUSTOMER. REFER LHT EO REPORT AT Status: TERMINATED DELIVERY TO AMIRI FLIGHT. Rev: 1 EARLIEST Freq: I E/C: 737-21A1139 5B737-21A1139 AIR CONDITIONING - INSTALLATION OF INSULATION ON OVERHEAD DUCTS Category: ASB Status: N/A Rev: 2 EARLIEST Reason Freq: 1 NOT APPLICABLE TO AIRCRAFT VARIABLE NO YG039 E/C: 737.22A1215 2014-16-14 Autothrottle System WO 20202 08/08/2014 Rev: 00 NC Total Hours: 5107:40 NC Total Cycles: 1870 Category: ASB Status: TERMINATED Rev: 1 EARLIEST Frog: 1 E/C: 737-23A1170 AD2000-14-02 VHF COMMUNICATION SYSTEM-VHF1 AND VHF2 ANTENNAS INTERCHANGE. B3-23A1170 Category: ASB SB737-23A1170 Status: N/A SB737-23A1170R2 Rev: 3 EARLIEST Reason Freq: 1 SB 737-23A1170 EFFECTIVITY DOES NOT INCLUDE THE V/N NO. OF THIS AIRCRAFT. SB IS NA BY THE VARIABLE NO. EFTA_R1_00013004 EFTA01734617  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 2 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: MB) Schedule Remaining/ Anent NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 737-24A1141 2006-10.17 P5 PANEL - BRKT. REPLACEMENT & WIRE 737.24A1141R1 INSTALLATION REVISION Category: ASB 737-24A1141R2 Status: N/A 737-24A1141R3 Rev: 4 737-SL-24-136 EARLIEST Reason Freq: 1 SB 737.24A1141 EFFECTIVITY LIST DOES NOT INCLUDE THIS AIRCRAFT VARIABLE NO. SB IS NA TO THIS AIRCRAFT E/C: 737-24A1148 2002-16-03 CORROSION PROTECTION OF ELECTRICAL WO 50505 05/02/2016 Rev: 5 2005-18-23 CONNECTORS IN THE MAIN WHEEL WELL NC Total Hours: 5887:00 NC Total Cycles: 2120 Category: ASB 737-24A1148R1 730 Dys 515 Status: OPEN 04/02/2018 Rev: 5 Recur EARLIEST Freq: 1 E/C: 737-24A1150 B3-24A1150 INSP POWER SUPPLY VOLTAGE : CPT'S Manual Compliance 16/04/2002 Rev: 3 PITOT HEATERS NC Total Hours: 1103:35 NC Total Cycles: 595 ACCOMPLISHED ON NC BY THE PREV CUSTOMER. Category: ASB REFER LHT E0 REPORT AT DELIVERY TO AMIRI Status: TERMINATED FLIGHT. . Rev: 3 EARLIEST Freq: 1 E/C: 737-25A1372 SB 737-25A1372 FWD INSTRUMENT PANEL / RUDDER PEDAL INSTALLATION Category: ASB Status: N/A Rev: 3 EARLIEST Reason Freq: 1 NOT APPLICABLE TO AIRCRAFT VARIABLE NO YG039 EFTA_R1_00013005 EFTA01734618  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 3 of 21 NC: A6DFR Type/Series: 5737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: ASB) Schedule Remaining/ Amant NO Document/SB FJC Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information E/C: 737-25A1383 SB737.25A1383 RUDDER PEDAL COVER FASTNER Category: ASS Status: N/A Rev: 2 EARLIEST Reason Free: i NOT APPLICABLE TO AIRCRAFT VARIABLE NO YG039 EC: 737-26A1109 2003-23-05 ENGINE APU CARGO FIRE BOTTLE HOSE Manual Compliance 03/11/2003 Rev: 3 737-26A1109R1 INSP NC Total Hours: 1103:35 NC Total Cycles: 595 CM AT PRODUCTION ON 03/11/2003. REFER Category: ASB 737-26A1109R2 A6-DFR DELIVERY DOCUMENTS. Status: TERMINATED 737-26A1109R3 Rev: 3 EARLIEST Froq: 1 E/C: 737-26A1137 FIRE PROTECTION - CARGO BAY SMOKE 9000 Hrs 8690:35 WO 50658 30/12/2015 Rev: 01 DETECTION - EQUIPMENT COOLING NC Total Hours: 5844:05 NC Total Cycles: 2109 SYSTEM SMOKE CLEA NCE MODE Category: ASB OPERATIONAL TEST OAR CARGO SMOKE Status: OPEN PROTECTION 31107/2028 Rev: 02 Recur EARLIEST Reason Frog: 1 THIS TASK REPEATES AT 9000 FLIGHT HOUR INTERVAL EIC: 737-27A1219 SB 737-27A1219 REVISION TO AIR / GRD SIGNAL SOURSE Category: ASS Status: N/A Rev: 2 EARLIEST Reason Freq: 1 SB 737-27A1219 EFECTIVITY LIST DOES NOT INCLUDE THIS AIRCRAFT EFTA_R1_00013006 EFTA01734619  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 4 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: ASB) Schedule Remaining/ Arrant NO Document/SB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 737-27A1222 SB 737-27A1222 MAIN RUDDER PCU DISPLACEMENT TEST. Category: ASB Status: N/A Rev: 1 EARLIEST Reason Freq: i SB 737-27A1222 EFFECTIVITY LIST DO NOT INCLUDE THIS AIRCRAFT SC: 737-27A1228 1999-10-13 5245 TRAILING E0G FLAP LIMIT SWITCH SB 737-27A1228 Category: ASB Status: N/A Rev: 2 EARLIEST Reason Froq: 1 N/A - BY VARIABLE NUMBER. YO039 (A6-DFR) NOT LISTED. SC: 737-27A1234 AD2002-06-03 ELEVATOR PCU RETENTION BRKT & BOLT 5B737.27A1234 INSP Category: ASB Status: N/A Rev: 2 EARLIEST Reason Freq: i NOT APPLICABLE TO AIRCRAFT VARIABLE NO YG039 E/C: 737-27A1239 SB 737-27A1239 RVDDER TRIM-RELOCATION OF WIRE BUNDLES AWAY FROM FEEL & CENTERING UINT Category: ASB Status: N/A Rev: 1 EARLIEST Reason Froq: 1 NOT APPLICABLE TO AIRCRAFT VARIABLE NO YG039 EFTA_R1_00013007 EFTA01734620  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 5 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: MB) Schedule Remaining/ Arrant NO DocumanVSB FJC Description: Hrs/CyslDyslDte Next Due Last Compliance Information SC: 737-27A1245 SB737.27A1245 ELEVATOR & TAB - INSP OF JAM NUTS ON Manual Compliance 14/03/2002 Rev: 2 THE TAB CONTROL RODS NC Total Hours: 1103:35 NC Total Cycles: 595 CNV AT LHT ON 14/03/2002, REFER A6-DFR Category: ASB DELIVERY DOCUMENTS. Status: TERMINATED Rev: 2 EARLIEST Freq: I ESC: 737-27A1260 2002-19-51 FLIGHT CONTROLS HYDRAULIC MODULAR PACKAGE - REPLACEMENT OF DISCREPANT COMPENSATORS Category: ASB Status: N/A Rev: 3 EARLIEST Reason Freq: 1 NOT AFFECTED BY SERIAL NUMBERS OF FLIGHT CONTROL MODULE. REFER LHT AD STATUS AT DELIVERY TO AMIRI FLIGHT. SC: 737-27A1271 2005-26-03 ELEVATOR INPUT TORQUE TUBE Manual Compliance 03/08/2005 Rev: 7 737-27A1271 R1 MODIFICATION NC Total Hours: 1103:35 NC Total Cycles: 595 MODIFIED IAW EO 146233 BY LHT ON 03/08/2005 AT Category: ASB SWCB73-27-018 672 FH & 329 FC. REFER LHT EO REPORT AT Status: TERMINATED DELIVERY TO AMIRI FLIGHT. Rev: 8 LATEST Freq: 1 E/C: 737-27A1277 WP1 2011.27-O3 WP1 HORIZONTAL STABILIZER TRIM CONTROL 1600 Hrs 1600:00 WO 50719 21/0812016 Rev: 3 27-102-00-01 SYSTEM • BALLSCREW AND NUT NC Total Hours: 6153:30 NC Total Cycles: 2203 INSPECTION AND LUBRICATION Category: ASB 27-110.00-01 365 Dys 348 Status: OPEN 737-27A1277 WP2 21/08/2017 Rev: 3 737-27A1277 WP3 Recur EARLIEST 737-27A1277R1 737-27A1277R2 Freq: 1 EFTA_R1_00013008 EFTA01734621  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 6 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC S/N: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EIC (Category: ASB) Schedule Remaining/ Arrant NO Document/SS E/C Description: Hrs/CysloysIDte Next Due Last Compliance Information E/C: 737-27A1277 WP2 2011.27-03 WP2 HORIZONTAL STABILIZER TRIM CONTROL 25000 His 18846:30 27-108-00-01 SYSTEM - STABILIZER TRIM ACTUATOR MODIFICATION • WORK PACKAGE 2 Category: ASB 737-27A1277 WP1 Status: OPEN 737-27A1277 WP3 26/06/2042 Rev: 3 737-27A1277R2 Once 737-37A1277R1 EARLIEST BC: 737-27A1277 WP3 2011-27-03 WP3 HORIZONTAL STABILIZER TRIM CONTROL 25000 His 18846:30 27-108.00-01 SYSTEM • STABILIZER TRIM ACTUATOR OVERHAUL - WORK PACKAGE 3 Category: ASB 737-27A1277 WP1 Status: OPEN 737-27A1277 WP2 26/06/2042 Rev: 3 737-27A1277R1 Recur EARLIEST 737-27A1277Ft2 BC: 737-27A1280 737-27-1253 RUDDER & RUDDER TRIM CONTROL 737-27A1280 FORCE FIGHT SYSTEM - OPERATIONAL TEST OF THE STANDBY HYDRAULIC ACTUATION SYSTEM Category: ASB 737-27A1280 STANDBY AND RUDDER MAIN POWER CONTROL UNIT Status: CANCEL FORCE FIGHT MONITOR TEST -TEST Rev: 0 FREQUENCY CHANGE EARLIEST Superseded By: 737-27A1280 STANDBY E/C: 737-27A1280 FORCE Fit 1.148725713 RUDDER & RUDDER TRIM CONTROL Manual Compliance 15/07/2007 Rev: 1 2007-03-07 SYSTEM • RUDDER MAIN POWER NC Total Hours: 1103:35 NC Total Cycles: 595 CONTROL UNIT FORCE FIGHT MONITOR INSPECTED IAW EO 152488 BY LHT ON 15107/2007 Category: ASB 737-27-1253 TEST - TEST FREQUENCY CHANGE AT 1044 FH & 573 FC. REFER LHT EO REPORT AT Status: TERMINATED 737-27A1280 STANDBY DELIVERY TO AMIRI FLIGHT. Rev: 1 737-27A1280R1 EARLIEST SWCB73-27-020 Reason Free: 1 INSPECTED IAW EO 152488 BY LHT ON 15/07/2007 AT 1044 FH & 573 FC. REFER LHT EO REPORT AT DELIVERY TO AMIRI FLIGHT. EFTA_R1_00013009 EFTA01734622  Print Date 07/09/2016 13:53 NC Actual Compliance Last Page: 7 of 21 NC: A6DFR Type/Series: B737.700IBBJ1 NC SIN: 30884 NC Hours: 6153:30 NC Cycles: 2203 As Of: 03/08/2016 EC (Category: ASB) Schedule Remaining/ Arrant NO DocumenVSB E/C Description: Hrs/Cys/Dys/Dte Next Due Last Compliance Information SC: 737-27A1280 STANDBY 1.148725713 RUDDER & RUDDER TRIM CONTROL Manual Compliance 15/07/2007 Rev: 1 2007.03-O7 SYSTEM - OPERATIONAL TEST OF THE NC Total Hours: 1103:35 NC Total Cycles: 595 STANDBY HYDRAULIC ACTUATION SYSTEM INSPECTED IAW EO 152488 BY LHT ON 15/07/2007 Category: ASB 737-27-1253 - TEST FREQUENCY CHANGE AT 1044 FH & 573 FC. REFER LHT EO REPORT AT Status: TERMINATED 737-27A1280 FORCE FIGHT DELIVERY TO AMIRI FLIGHT. Rev: 1 737-27A1280R1 EARLIEST SWCB73-27-020 Freq: I E/C: 737-27A1296 737-27A1299 ELEVATOR TAB CONTROL MECHANISM WO 14633 15/04/2010 Rev: 0 DETAILED INSPECTION NC Total Hours: 2