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时间:2011-04-01 08:47来源:蓝天飞行翻译 作者:航空
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 22-31-11
 ALL  ú ú 01 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 E. Procedure
 S 024-007
 (1)  Remove the autothrottle power lever angle synchro:
 (a)  Install a 0.25-inch rig pin in the part power rig hole R of the MEC fuel control box (Fig. 401).
 NOTE: You can move the power lever back and forward if it is
____
 necessary.

 (b)  
Remove the two bolts and two plates above the synchro flange.

 (c)  
Collect all the removed parts and keep them in a safe location.

 (d)  
Remove the PLA synchro.


 NOTE: Do not remove the rig pin.
____
 TASK 22-31-11-404-019
 3. Power Lever Angle Synchro Installation
_______________________________________
 A. Standard Tools and Equipment
 (1)  Rig Pin Kit - F70207
 NOTE: Rig pin F70207-23 or MS20392-3C pin (optional), or
____ equivalent 0.248 (+0.000/-0.002)-inch diameter 3-inch long rod or bolt.
 B. References
 (1)  
71-11-02/201, Fan Cowl Panels - MP

 (2)  
22-31-11/501, Autothrottle Power Lever Angle Synchro -Adjustment/Test.

 (3)  
12-31-01/201, Left and Right Nacelle Panel


 C. Access
 (1)  
Location Zone
 502 Engine No. 1 - 7:00 o'clock position
 602 Engine No. 2 - 7:00 o'clock position


 (2)  
Access
 5746L Engine No. 1 - Left Fan Cowl Panel
 5846R Engine No. 2 - Left Fan Cowl Panel

 

 D. Prepare for the installation
 S 864-016
 (1) Do these tasks to prepare for the autothrottle PLA installation:
 (a)  Open these circuit breakers on the P18-1 load control center: 1) AUTO THROTTLE AC
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-31-11
 ALL  ú ú 01 Page 403 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 2) AUTO THROTTLE DC
 (b)  
Set the thrust lever approximately 20 degrees angle to install the rig pin in part power rig hole R.

 (c)  
Install the DO-NOT-OPERATE identifier.

 (d)  
Open the left (right) fan cowl panel on the applicable engine (Ref 71-11-02/201).

 (e)  
Disconnect the electrical connector from the synchro.


 E. Procedure
 S 424-008
 (1)  Install the autothrottle power lever angle synchro
 (a)  Align the index mark (engraved bar) on the synchro gear with the flange index mark on the PLA synchro.
 CAUTION: MAKE SURE YOU ENGAGE THE PLA SYNCHRO GEAR WITH THE GEAR IN
_______
 THE CONTROL BOX CORRECTLY.

 (b)  Attach the PLA synchro to the control box.
 NOTE: Make sure you align the flange index mark with the rigging
____
 mark on the control box.

 CAUTION: MAKE SURE YOU THEN TIGHTEN THE PLATE BOLTS TO PREVENT
_______
 DAMAGE TO THE PLA SYNCHRO GEAR SHAFT.

 (c)  
Attach the plates with the two bolts.

 (d)  
Align and connect the electrical connector.

 (e)  
Install the wire bundle clamp on the wire bundle.


 S 734-015
 (2)  Adjust the PLA synchro (Ref 22-31-11/501).
 F. Put the Airplane Back to Its Initial condition
 S 414-009
 (1)  
Install the left and right fan cowl panel (Ref 71-11-02/201).

 S 864-010

 (2)
Close these circuit breakers on the P18-1 load control center:

 (a)  
AUTO THROTTLE AC

 (b)  
AUTO THROTTLE DC

 


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 22-31-11
 ALL  ú ú 01 Page 404 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AUTOTHROTTLE POWER LEVER ANGLE SYNCHRO - ADJUSTMENT/TEST
 
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