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时间:2011-04-10 09:58来源:蓝天飞行翻译 作者:航空
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 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-08
 ALL  ú ú 01 Page 220 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (c)  
Install the filter element into the manifold hole.

 (d)  
Install the new packing (5) and backup ring (4) on the filter cap (6).

 (e)  
Install the filter cap into the manifold assembly and tighten it to 400-450 pound-inches.

 (f)  
Apply a thin layer of sealant around the filter cap.


 S 412-100
 (2)  
Install the access panels (Ref 06-09-06/201).

 S 862-098

 (3)  
Remove the DO-NOT-CLOSE tag and close these circuit breakers:

 (a)  
P180, Power Distribution Panel
 1) 180H8, ELEV/RUD VLV SYS 1
 2) 180E7, ELEV/RUD VLV SYS 2
 3) 180H23, ELEV/RUD VLV SYS 3
 4) 180E22, ELEV/RUD VLV SYS 4

 

 S 862-097
 (4)  
Set all FLT CONTROL HYD POWER TAIL switches on the P461, Pilots' Overhead Panel in NORM.

 F.
Do a Test of the Outboard Elevator PCP Filter


 S 862-074
 (1)  Do this task: "Supply Electrical Power" (AMM 24-22-00/201).
 S 862-077
 WARNING: MOVE ALL PERSONS AND EQUIPMENT AWAY FROM THE RUDDERS AND
_______ THE ELEVATORS BEFORE YOU TURN THE HYDRAULIC POWER ON. THE RUDDERS OR THE ELEVATORS WILL MOVE QUICKLY AND CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  
Pressurize the hydraulic system No. 1 (left outboard elevator), or No. 4 (right outboard elevator)(AMM 29-11-00/201).

 S 712-078

 (3)  
Move the elevator up and down until the movement is smooth and continuous.

 (4)  
Examine the outboard elevator PCP for hydraulic leakage.

 (5)
Release the pressure in the hydraulic system (AMM 29-11-00/201).


 S 792-079
 S 862-080
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-08
 ALL  ú ú 01 Page 221 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
 (6)  S 862-102Remove the DO-NOT-CLOSE tags and close these circuit breakers: (a) P7, Overhead Circuit Breaker Panel 1) 7E7, L STAB TRIM S/O VLV 2) 7E20, R STAB TRIM S/O VLV
 (7)  S 862-103Set the STAB TRIM 2 and 3 switches on the control stand to ON.
 (8)  S 612-083Fill the hydraulic reservoirs if it is necessary (AMM 12-12-01/301).
 (9)  S 862-085If the electrical power is not necessary, do this task: Electrical Power" (AMM 24-22-00/201). "Remove

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-08
 ALL  ú ú 01 Page 222 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 OUTBOARD ELEVATOR POWER CONTROL PACKAGE - INSPECTION/CHECK
__________________________________________________________
 1.  General_______
 A.  This procedure has one task. The task is an inspection of the power control package (PCP) for the outboard elevator.
 B.  In this procedure you measure the inner or outer diameter of the parts which attach the PCP actuator to the attachment fitting. The parts include bearing, bolts and bushings.
 C.  You must disassemble the PCP actuator to the attachment fitting to do this procedure.
 NOTE: Missing Power Control Package, rod end and trunnion bearing
____ dust seals are not reasons for removing the control package. Seals should be replaced at convenience on overhaul. The bearings will generate a small amount of dark colored powder which may be observed at the edge of the bearing lines. This powder is the normal product of the self lubricating liner.
 TASK 27-31-08-206-001
 2.  Outboard Elevator Power Control Package (PCP) Inspection________________________________________________________
 
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