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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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 (e)  
Remove the rig pin E-4.

 (f)  
Remove the caps and plugs from the pneumatic ports and lines.

 (g)  
Install the two pitot-static lines to the feel computer.


 NOTE: Be sure to follow guidelines for tube installation.
____ See AMM 20-10-51/401 for tube installation guidelines.
 CAUTION: MAKE SURE YOU CONNECT THE PRESSURE AND RETURN LINES TO THE
_______ CORRECT PORTS. IF YOU INSTALL THE HYDRAULIC LINE TO INCORRECT PORT, YOU CAN CAUSE DAMAGE TO THE FEEL COMPUTER.
 (h)  
Install the hydraulic lines to the feel computer: 1) Remove the plugs. 2) Install the two pressure lines, two return lines, and two

 computer pressure lines to the feel computer housing.

 (i)  
Install the pitot-static lines at the fittings on the feel computer: 1) Remove the plugs. 2) Connect the pitot-static lines at the fittings on the feel

 computer.
 3) Tighten the clamps.


 (j)  
Install the electrical connector D756.


 S 864-007
 (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).

 S 874-006

 (7)  
Bleed the elevator control system:

 (a)  
Move the control column in a longitudinal direction through the full range of travel until the movement is smooth.


 NOTE: When you bleed the remaining air out of the system, the
____
 artificial feel force increases.

 S 714-003
 (8)  
Examine the hydraulic connections at the feel computer for leaks.

 S 864-004

 (9)  
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Circuit Breaker Panel
 1) AUTO FLT CONT SYS B
 2) INDICATOR MASTER DIM BUS
 3) STABILIZER TRIM ACTUATOR

 

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 27-31-37
 ALL  ú ú 02 Page 406 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 4) STABILIZER TRIM CONT
 S 714-005
 (10) Do this task:  "System Test - Feel Force System and Autopilot Authority" (Ref 27-31-00/501).
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 27-31-37
 ALL  ú ú 01 Page 407 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ELEVATOR FEEL COMPUTER - INSPECTION/CHECK
_________________________________________
 1.  General_______
 A.  This subject has one task. The task is an inspection of the elevator feel computer. The procedure has these parts:
 (1)
The removal of the elevator feel computer

 (2)
An inspection of the elevator feel computer

 (3)
The installation of the elevator feel computer.


 TASK 27-31-37-206-004
 2.  Elevator Feel Computer Wear Limits Inspection (Fig. 601)_____________________________________________
 A.  Standard Tools and Equipment
 (1)
Micrometer - 0-1 inch

 (2)
Vernier Caliper

 B.  
References

 (1)
27-31-37/401, Elevator Feel Computer

 C.  
Access

 (1)  
Location Zone
 702 Tail Compartment Access Door

 



SEE  A 

B
B
A
Elevator Feel Computer Wear Limits Figure 601 (Sheet 1)
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 27-31-37
 ALL  ú ú 01 Page 601 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

1. ARM/BOLT
6. ARM/BOLT
INBD  FWD
 
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