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时间:2011-03-27 17:13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

 447AL, 448AR


 (2) Remove the warning notice(s).


 F 『 EEFF : ALL E Page 50577-31-30
 E E Feb 01/98 E E ECES E TURBINE REAR FRAME BEARING VIBRATION SENSOR - INSPECTION/CHECK

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______________________________________________________________
 TASK 77-31-30-210-002
 Visual Inspection of the TRF Vibration Sensor
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific soft-nose connector pliers No specific warning notice
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 71-13-00-410-040 Closing of the Fan Cowl Doors 77-31-30-000-002 Removal of the Turbine Rear Frame Vibration Sensor 77-31-30-400-002 Installation of the Turbine Rear Frame Vibration
 Sensor 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 77-31-30-991-300 Fig. 601
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 E E Feb 01/98 E E ECES E E 56-5B E

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 3. Job Set-up
__________ Subtask 77-31-30-941-053
 A. Safety Precautions
 (1) On the center pedestal, on the ENG panel 115VU:

 (a) Put a warning notice to tell persons not to start the engine.

 (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.

 (3) On the overhead maintenance panel 50VU:

 (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.

 (b) Put a warning notice to tell persons not to energize the FADEC 1(2).

 


 Subtask 77-31-30-010-057
 B. Open the left fan cowl doors: (Ref. TASK 71-13-00-010-040)
 FOR 1000EM1
 437AL
 FOR 1000EM2
 447AL

 Subtask 77-31-30-040-055
 C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 77-31-30-010-063
 D. Open the left thrust reverser doors: (Ref. TASK 78-36-00-010-040) FOR 1000EM1 451AL FOR 1000EM2 461AL
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 E E Feb 01/98 E E ECES E 4. Procedure

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_________
 (Ref. Fig. 601/TASK 77-31-30-991-300)
 Subtask 77-31-30-210-051
 A. Visual Inspection of the TRF Vibration Sensor:
 (1) Disconnect the aircraft harness from the TRF sensor connector. Use soft-nose connector pliers only if necessary.
 -------------------------------------------------------------------------------INSPECT/CHECK MAXIMUM REMARKS SERVICEABLE LIMITS -------------------------------------------------------------------------------
1. Examine the sensor accelerometer for:
 A. Cracks in mounting Not permitted  Replace TRF vibration
 flange  sensor (Ref. TASK 77-31-30-000-002) and (Ref. TASK 77-31-30-400-002).
 2. Examine all the attachment points of the sensor to the engine for:
 A. Loose bolts  Not permitted TORQUE bolts as told in (accelerometer and installation topic lead) (Ref. TASK 77-31-30-400-
002)
 B. Loose screws,  Not permitted TORQUE screws, install missing half plate half plate and lockwire as , broken or told in installation topic missing lockwire (Ref. TASK 77-31-30-400-(connector end) 002)
 3. Examine the braid of the lead for:
 A. Chafing (wear) or Not permitted  Replace TRF vibration
 fraying  sensor (Ref. TASK 77-31-30-000-002) and (Ref. TASK 77-31-30-400-002)
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 E E Feb 01/98 E E ECES E F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E

 

 Visual Inspection of the TRF Vibration Sensor
 Figure 601/TASK 77-31-30-991-300- 12 (SHEET 1)
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