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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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 NOTE: Install tags on the lines and port fittings to show
____ the correct connection location. See AMM 20-10-51/401 for instructions.
 1) Seal all the lines with plugs.
 WARNING: RELEASE THE CONNECTION SLOWLY AND LET THE PRESSURE
_______ DECREASE BEFORE YOU COMPLETELY REMOVE THE HYDRAULIC LINE. IF YOU DISCONNECT THE HYDRAULIC LINE WHEN IT HAS PRESSURE, A SPRAY OF HYDRAULIC FLUID CAN CAUSE INJURY TO PERSONS.
 (e)  
Remove the two pressure lines, two return lines, and two computer pressure lines from the feel computer.

 (f)  
Remove the pitot static lines from the fittings on the feel computer.

 (g)  
Seal the hydraulic and pneumatic lines with caps.

 (h)  
Seal all the open ports with plugs.

 (i)  
Remove the four mounting bolts.

 (j)  
Remove the feel computer from the airplane.


 TASK 27-31-37-404-002
 3. Elevator Feel Computer Installation
___________________________________
 A. Special Tools and Equipment
 (1)  Rig Pin (E-4) - 0.309/0.311 inch diameter, 4.5 |0.25 inches long, (MS20392-4)
 NOTE: The rig pin is part of the rig pin kit F70207-69, -78 or -83.
____
 (2)  
F80055-1 - Trammel Bar

 (3)  
F80153-1 - Elevator Feel Computer Safety Pin

 B.
Standard Tools and Equipment

 (1)  
Spring Scale - 0 to 50 pounds capacity

 C.
Consumable Materials

 (1)  
D00054 Lube, Skydrol Assembly - MCS 352

 D.
References

 (1)  
27-31-00/201, Elevator and Tab Control System


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 27-31-37
 ALL  ú ú 03 Page 404 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
27-31-00/501, Elevator and Tab Control System

 (3)  
27-31-37/601, Elevator Feel Computer

 E.  
Access

 (1)  
Location Zone
 702 Tail Compartment Access Door


 (2)  
Access Panels
 3701 Stabilizer Trim Access Door


 F.  
Procedure


 S 224-013
 (1)  Do this task: "Elevator Feel Computer Wear Limits Inspection" (Ref 27-31-37/601).
 S 864-014
 CAUTION: DO NOT LIFT THE FEEL COMPUTER BY THE INPUT ARM, OR APPLY A
_______ TORQUE OF MORE THAN 300 POUND-INCHES TO THE INPUT ARM. THE FEEL COMPUTER IS VERY SENSITIVE AND CAN BE EASILY DAMAGED.
 (2)  
If you replace the feel computer, prepare the replacement computer:

 (a)  
Lightly lubricate the O-rings with Skydrol Assembly Lube.

 (b)  
Install the pneumatic and hydraulic fittings in the feel computer.

 (c)  
Set the B dimension at 41.57 |0.01 inches (Fig. 401).


 S 094-009
 (3)  
Remove the safety pin.

 S 494-010

 (4)  
Install the rig pin E-4 in the input arm (3) and the feel computer.

 S 424-011

 (5)  
Install the feel computer (Fig. 402):

 (a)  
Set the feel computer in the airplane.

 (b)  
Install the four mounting bolts, nuts, and washers.

 1)  With the rig pin E-4 installed, make sure you can install the bolt easily by hand through the stabilizer pushrod (1) and the input arm (3).

 (c)  
If you cannot install the bolt, adjust the length of the pushrod (1): 1) Loosen the checknut (2). 2) Turn the rod end fitting until you can install the bolt


 easily by hand.
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 27-31-37
 ALL  ú ú 02 Page 405 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 3) Make sure the rod end extends more than half of the distance across the inspection hole in the rod. 4) Tighten the checknut (2).
 (d)  
Connect the spring (4) to the feel computer.
 
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