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时间:2011-03-27 16:58来源:蓝天飞行翻译 作者:航空
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_________ Subtask 72-32-00-420-052
 A. Install the IGV and stage 3 lever arms. CAUTION : CORRECTLY ALIGN THE WITNESS MARK ON THE VANE STEM WITH THE
_______ LEVER ARM. BLADE DAMAGE CAN OCCUR IF THE VANE STEM IS NOT CORRECTLY ALIGNED.
 (1) Install the replacement bushing in the stator case.

 (2) Install the replacement lever arms on the vane while you engage the lever arm pin into the actuation ring.

 (3) Make sure the lever arm fully engages the vane stem flats.

 (4) Install the washer and nut on the vane stem. Hold the lever arm with LEVER, COUNTERTORQUE - CPRSR STATOR VANE ACTUATION ARM (856A1012G01), while you tighten the nut.

 (5) TORQUE the nut to between 55 and 70 lbf.in (0.62 and 0.79 m.daN). Do not let the vane turn.


 Subtask 72-32-00-210-053
 B. Do a visual check.
 (1) The lever arm must fully engage the vane stem flats.
 (Ref. Fig. 801/TASK 72-32-00-991-301)


 (2) A minimum of 2 vane stem threads must be above the nut.
 (Ref. Fig. 802/TASK 72-32-00-991-302)

 

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________ Subtask 72-32-00-410-058
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close the thrust reverser doors: (Ref. TASK 78-36-00-410-040) FOR 1000EM1 451AL, 452AR FOR 1000EM2 461AL, 462AR


 Subtask 72-32-00-440-054
 B. Make the thrust reverser serviceable (Ref. TASK 78-30-00-081-041). Subtask 72-32-00-410-059
 C. Close Access
 (1) Close the fan cowl doors: (Ref. TASK 71-13-00-410-040)
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR.


 (2) Remove the access platform(s).

 (3) Remove the warning notice(s).


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 TASK 72-32-00-000-004 Removal of the Actuation Ring Connecting Links
 1. Reason for the Job

__________________
 Self Explanatory


 2. Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice
 No specific access platform 1 m (3 ft. 3 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-13-00-010-040 Opening of the Fan Cowl Doors 78-30-00-481-041 Make the Thrust Reverser Unserviceable for
 Maintenance 78-36-00-010-040 Opening of the Thrust Reverser Doors 72-32-00-991-303 Fig. 803
 3. Job Set-up
__________ Subtask 72-32-00-941-055
 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.


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 (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 72-32-00-010-062
 B. Get Access
 (1) Open the fan cowls doors: (Ref. TASK 71-13-00-010-040) FOR 1000EM1 437AL, 438AR FOR 1000EM2 447AL, 448AR.
 (2) Put the access platform in position. Subtask 72-32-00-040-057

 C. Make the thrust reverser unserviceable (Ref. TASK 78-30-00-481-041). Subtask 72-32-00-010-063


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

 4. Procedure
_________ (Ref. Fig. 803/TASK 72-32-00-991-303) Subtask 72-32-00-020-053
 A. Remove the connecting link.
 (1) Disconnect the tie rod from the clevis of the defective connecting link as follows:
 
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