A320飞机维护手册 AMM 动力装置 POWER PLANT 1(88)

曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 - HPTACC valve  180 ml/hr (3 cc/min) (60 drops/min) (up to 90 drops/min allowed for 25 cycles)  Replace the HPTACC valve(Ref. TASK 75-21-10-000-002) and (Ref. TASK 75-21-10-400-002).
 - LPTACC valve  180 ml/hr (3 cc/min) (60 drops/min) (up to 90 drops/min allowed for 25 cycles)  Replace the LPTACC valve(Ref. TASK 75-22-10-000-002) and (Ref. TASK 75-22-10-400-002).
 - RACC valve  180 ml/hr (3 cc/min) (60 drops/min) (up to 90 drops/min allowed for 25 cycles)  Replace the RACC valve(Ref. TASK 75-23-10-000-002) and (Ref. TASK 75-23-10-400-002).
 - Fuel manifold  180 ml/hr (3 cc/min) (60 drops/min) (up to 90 drops/min allowed for 25 cycles) Replace the Fuel manifoldseals (Ref. TASK 73-11-31-000-041).

 F 『R EEFF : 106-149, 212-299, 301-399, 401-499, E Page B50171-00-00
 E E Aug 01/05 E E ECES E

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

 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
- HMU  180 ml/hr (3 cc/min) (60 Replace the HMU (Ref. TASK drops/min) (up to 90 73-21-10-000-002) and drops/min allowed for 25 (Ref. TASK 73-21-10-400-cycles) 002).
 3. The hydraulic source
 - The hydraulic pump  (Ref. TASK 29-00-00-790-pad 001)

 F 『R EEFF : 106-149, 212-299, 301-399, 401-499, E Page B50271-00-00
 E E Aug 01/05 E E ECES E **ON A/C ALL

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

 TASK 71-00-00-790-005
 Drain Mast Leakage Identification Procedure
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific plastic bottles No specific tubes No specific access platform 1.5 m (4 ft. 11 in.)
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-00-00-710-003 Engine Automatic Start 71-00-00-710-028 Engine Shutdown 71-00-00-790-002 Fuel or Hydraulic or Oil Leakage Limits 71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 78-30-00-081-041 Make the Thrust Reverser Serviceable after
 Maintenance 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
 Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 78-36-00-410-040 Closing of the Thrust Reverser Doors
 F 『R EEFF : ALL E Page B50371-00-00
 E E Aug 01/05 E E ECES E 3. Job Set-up

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

__________ Subtask 71-00-00-010-105
 A. Get Access
 (1) Open the fan cowl doors (Ref. TASK 71-13-00-010-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 (2) Put the access platform in position. Subtask 71-00-00-040-072

 B. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 71-00-00-010-106

 C. Open the thrust reverser doors (Ref. TASK 78-36-00-010-040):
 FOR 1000EM1
 451AL, 452AR
 FOR 1000EM2
 461AL, 462AR

 Subtask 71-00-00-869-199
 D. Prepare for Test.
 (1) For source identification of a fuel leak at the drain mast:
 (a) Install the plastic bottles and tubes on all possible fuel leakage sources (Refer to 71-70-00).
 NOTE : For identification of a static fuel leak , the VBV gear
____ motor must be disconnected first (this is the more likely accessory to be suspect).
 (2) For source identification of an oil leak at the drain mast:
 (a) Install the plastic bottles and tubes on all possible oil leakage sources (Refer to 71-70-00).
 F 『R EEFF : ALL E Page B50471-00-00
 E E Aug 01/05 E E ECES E Subtask 71-00-00-410-102

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

 E. Close Access
 (1) Close the thrust reverser doors (Ref. TASK 78-36-00-410-040): FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR
　
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 动力装置 POWER PLANT 1(88)