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时间:2011-04-01 19:17来源:蓝天飞行翻译 作者:航空
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 27-31-54
 ALL  ú ú 02 Page 404 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 864-008
 (6)  Do this task: "Put the Elevator Hydraulic Systems A and B Back to the Condition Before the Pressure Removal" (Ref 27-31-00/201).
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 27-31-54
 ALL  ú ú 01 Page 405 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ELEVATOR FORWARD CONTROL QUADRANT - REMOVAL/INSTALLATION
________________________________________________________
 1.  General_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the elevator forward control quadrant (which is referred to as the forward quadrant). The procedure has these parts:
 (1)  
The removal of the forward quadrant

 (2)  
The installation of the forward quadrant

 (3)  
An adjustment of the forward quadrant.

 B.  
There is a forward quadrant on the right and left side. The procedure is the same for each forward quadrant.


 TASK 27-31-61-004-001
 2.  Elevator Forward Control Quadrant Removal_________________________________________
 A.  Special Tools and Equipment
 (1)  Rig Pins (E-1 and E-5) - 0.309/0.311 inch diameter, 6.7 |0.25 inches long (MS20392-4)
 NOTE: The rig pins are part of the kit F70207-69, -78 or -83.
____
 B.  References
 (1)  
27-31-00/201, Elevator and Tab Control System

 C.  
Access

 (1)  
Location Zone
 704 Tail Cone
 711 Elevator and Tab, LH
 712 Elevator and Tab, RH


 (2)  
Access Panels
 1103 Forward Access Door
 3701 Stabilizer Trim Access Door
 3801 Tail Cone Access Door, LH
 3802 Tail Cone Access Door, RH


 D.  
Procedure


 S 864-005
 (1)  Remove the elevator systems A and B hydraulic power
 (Ref 27-31-00/201).

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 27-31-61
 ALL  ú ú 01 Page 401 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 864-004
 (2)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P6 Circuit Breaker Panel
 1) AUTO FLT CONT SYS B MACH TRIM AC
 2) AUTO FLT CONT SYS B MACH TRIM DC
 3) AFDS MCP CRS-2
 4) AUTO FLT CONT SYS B SNSR EXC AC
 5) AUTO FLT CONT SYS B FCC DC

 

SEE  A 
RIG PIN E-5 
AFT CONTROL QUADRANT 
Rig Pin E-5 Location Figure 401  FWD  A 

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 27-31-61
 ALL  ú ú 01 Page 402 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

9.  INBOARD COUPLING BOLT
1.  CONTROL COLUMN
SEE A
2.  DUST CAP
8.  INBOARD
COUPLING
3.  RING
7.  ELEVATOR ASSEMBLY FORWARD QUADRANT
4.  DUST SEAL
CONTROLRIG PIN E-1FWD CABLE EA
5.  PITCH TRANSDUCER
CONTROL CABLE EB
SHOULDER OF CONNECTOR
10.
BEARING HOUSING

11.
LAMINATED SHIM


FACE
SPLINES

12. BEARING
13. CONNECTOR
A
Elevator Forward Control Quadrant Installation
Figure 402

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