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时间:2011-03-28 13:42来源:蓝天飞行翻译 作者:航空
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

 AMM 27-54-54-000-001 Removal of the Hydraulic Motor of the Flap Power R Control-Unit (6201CM) with the Pressure-Off Brake and R the Valve Block Assembly
 AMM 27-54-54-400-001 Installation of the Hydraulic Motor of the Flap Power R Control-Unit (6201CM) with the Pressure-Off Brake and R the Valve Block Assembly
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 224
 May 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

 

AMM 27-54-61-000-001 Removal of the Inboard Flap
 AMM 29-10-00-863-001 Pressurize the Green Hydraulic System
 AMM 29-10-00-864-002 Depressurize the Yellow Hydraulic System

 3. Fault Confirmation
__________________
 A. Test
 (1) Do the operational test of the flap system (Ref. AMM TASK 27-54-00-710-001):
 - if the flaps do not move, but the left and right flap transmission shafts move freely, do the fault isolation procedure in Para 4.A.(1)

 - if the flaps do not move and one of the flap transmission shafts does not move freely, do the fault isolation procedure in Para 4.A.(4).


 4. Fault Isolation
_______________
 A. Procedure.
 (1) Do a check of the Position Pick-off Units (PPUs) on the Centralized Fault Display System (CFDS) and make a record of the APPU and FPPU synchro angles (Ref. AMM TASK 27-54-49-000-001) and (Ref. AMM TASK 27-54-49-400-001).
 NOTE : This data will let you compare APPU and FPPU angles, before
____ removal and after installation of a part of the flap transmission system. The difference in angles must be in the specified limits.
 (2) Move the Flap control lever to a different applicable position and see if there is movement of the PCU (6201CM) output shafts:

 - if there is movement of the PCU output shafts, go to step (4)

 - if there is no movement of the PCU output shafts, do the next step.

 

 (3) Replace the POWER CONTROL UNIT (6201CM), (Ref. AMM TASK 27-54-51-000-001) and (Ref. AMM TASK 27-54-51-400-001).

 (4) Do the detailed visual inspection of the Transmission Assembly (Ref. AMM TASK 27-54-00-200-001).


 (a) If it is not possible to move the flaps for the visual inspection, move the flaps manually (Ref. AMM TASK 27-54-61-000-001).
 NOTE : The failure will be outboard of a torque limiter that has
____
 operated.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 225
 May 01/05R CES

 

 (b) Do the reset of the torque limiters (Ref. AMM TASK 27-50-00-866-010).

 (c) If a fault is found, correct or repair as necessary (Ref. AMM chap 27).


 (5) Do the test in Para. 3.A:

 - if the fault continues, do the next step.

 (6) Remove each transmission shaft, one at a time to do a check for
 friction in each component of the flap system, (Ref. AMM chap. 27)
 removal installation procedures.


 (a) If a fault is found, correct or repair as necessary (Ref. AMM chap. 27).

 (b) Make sure you install all components removed.

 

 (7) Do the test in Para 3.A:

 - if the fault continues, do the next step.

 (8) Disconnect the transmission shafts on each side of the WTB 33CV
 (34CV) (Ref. AMM TASK 27-51-51-000-001):


 (a) Make sure the WTB is easily turned by hand:

 - if the WTB is easily turned by hand, connect the transmission shafts (Ref. AMM TASK 27-51-51-400-001) and do step (9)

 - if the WTB is not easily turned by hand, or there is an incorrect noise, do the next step.

 

 (b) Replace the WTB BRAKE-L WING TIP (33CV) or BRAKE-R WING TIP (34CV) (Ref. AMM TASK 27-51-51-000-001) and (Ref. AMM TASK 27-51-51-400-001).

 

 (9) Do the test in Para. 3.A:


 - if the fault continues, do the next step.
 (10) If no fault has been found during this procedure, as a precaution:
 (a) Replace those Rotary Actuators that have a torque limiter tripped (Ref. AMM 27-54-49).
 NOTE : A torque limiter tripped during a WTB reset can be
____
 ignored.

 (11) Set the CFDS MENU MODE and access the SYSTEM STATUS FLAP and make sure that NO FAULTS is shown.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 226
 
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