F 『
 E C F M E
 E E
 E 56-5B E
 E E

 C. Expendable Parts
 -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
10 gasket 73-11-48 01A-030 15 gasket 73-11-11 01A-070
 D. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-13-79-610-002  Check oil level and replenish Check Pop Out Indicator of EMCD (Electrical Master Chip Detector)
 20-28-00-720-005  Check of the Electrical Bonding of the Different Components (But not the Fluid Systems and the Components Installed on Composite materials)
 22-97-00-710-001 Operational Test of the LAND CAT III Capability 24-21-00-210-046 Check of the Oil Level and Oil-Filter Differential-Pressure Indicator (DPI) 24-21-00-720-041 Operational Test of the IDG Disconnect and Reconnect (Reset) Function - Engine in Operation 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 30-21-00-710-002 Operational Test of the Engine Air Intake Ice Protection (with the Engines in operation) 31-32-00-860-012 Procedure to Get Access to the SYSTEM REPORT/TEST/ENG Page 31-36-00-740-005 Update of the Engine Hours and Cycles in the DMU
 after Engine or DMU Replacement 31-60-00-860-001 EIS Start Procedure 34-10-00-860-004 IR Alignment Procedure 71-00-00-710-003 Engine Automatic Start 71-00-00-710-006 Minimum Idle Check 71-00-00-710-008 Power Assurance Check 71-00-00-710-009 Vibration Check 71-00-00-710-025 Accel Check 71-00-00-710-028 Engine Shutdown 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 71-13-00-800-041 Adjustment of the Fan Cowl Doors 73-11-50-360-002 Leak Check of the Fuel Return Valve 73-21-60-720-040 Functional Test of the Electronic Control Unit (ECU)
 F 『 EEFF : ALL E Page 43371-00-00
 E E May 01/05 ERE ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
73-21-60-740-006 Read the LRU Identification Report and the Thrust
 Reverser Shut-off Valve Status 73-21-60-740-008 Entry of the Engine Serial Number Through MCDU 73-29-00-710-040 Operational Test of the FADEC on the ground (with
 Engine Motoring)
 78-30-00-081-041 Make the Thrust Reverser Serviceable after
 Maintenance
 78-30-00-481-041 Make the Thrust Reverser Unserviceable for

 Maintenance 78-31-00-710-042 Operational Test of the Thrust Reverser System 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors 78-36-41-820-042 Adjustment of the Thrust Reverser Half Door Latches 78-36-42-820-002 Adjustment of the LH or R/H Thrust Reverser "J" Ring
 on Wing
 ESPM 20-48-23
 SIL 73-019
 SPM 703213
 SPM 703223
 71-00-00-991-910 Fig. 401
 71-00-00-991-911 Fig. 402
 71-00-00-991-912 Fig. 403

R **ON A/C 001-049, 051-099, 101-149, 151-152, 154-199, 201-299, 301-399, R 401-499,
 71-00-00-991-913 Fig. 404
 **ON A/C 153-153,
 71-00-00-991-913-A Fig. 404A
 **ON A/C ALL
 71-00-00-991-914 Fig. 405
 **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
 71-00-00-991-915 Fig. 406
 F 『 EEFF : ALL E Page 43471-00-00
 E E Aug 01/05 E E ECES E -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

R **ON A/C 151-199, 401-499,
 71-00-00-991-915-A Fig. 406A
 **ON A/C ALL
 71-00-00-991-929 Fig. 407 71-00-00-991-916 Fig. 408 71-00-00-991-917 Fig. 409 71-00-00-991-918 Fig. 410 FOR FIN 1000EM1 29-11-00-710-001 Operational Test of the Green Hydraulic System 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector FOR FIN 1000EM2 29-13-00-710-002 Operational Test of the Yellow Hydraulic System 29-14-00-614-002 Pressurization of the Hydraulic Reservoirs through
 the Ground Connector
 3. Job Set-up
__________
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 動力裝置 POWER PLANT 1(22)