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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 29-11-00/201, Main Hydraulic Supply System

 (4)  
AIPC 27-41-08, Fig. 1

 (5)  
AIPC 27-41-09, Fig. 1

 C.  
Access

 (1)  
Location Zone
 313 Stabilizer Torsion Box Compartment, LH
 314 Stabilizer Torsion Box Compartment, RH

 

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 27-41-14
 ALL  ú ú 04 Page 206 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (2)  
Access Panel
 312A Horizontal Stabilizer Jackscrew Access Door
 315A Access Door


 D.
Prepare for Removal


 S 012-023
 (1)  
Open the access door 312A (AMM 06-09-05/201).

 S 862-024

 (2)  
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).

 S 862-025

 (3)  
Do this task: "Supply Hydraulic Power" (AMM 29-11-00/201).

 S 862-028

 (4)  
Set the STAB TRIM 2 and 3 switches to ON.

 S 862-108

 (5)  
Use the STAB TRIM ALTN switches to set the stabilizer to the neutral rig position (3 units of trim).

 S 862-031

 (6)  
Set the STAB TRIM 2 and 3 switches to CUTOUT.

 S 862-029

 (7)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P7, Overhead Circuit Breaker Panel
 1) 7E7, STAB TRIM L S/O VLV
 2) 7E20, STAB TRIM R S/O VLV

 

 S 862-072
 (8)  
If the hydraulic power is not necessary, do this task: "Remove Hydraulic Power" (AMM 29-11-00/201).

 S 862-030

 (9)  
If the electrical power is not necessary, do this task: "Remove Electrical Power" (AMM 24-22-00/201).

 S 492-031

 (10)
 Install the air blower and the hose to supply air to the stabilizer center section.

 E.
Remove the Door Mechanism


 S 022-032
 (1)  
Remove the door mechanism:

 (a)  
Remove the stabilizer blade seals.

 (b)  
Remove the bolts to disconnect the two control links at the two ends.

 (c)  
Remove the crossbolts to remove the crank.

 (d)  
Remove the nut to remove the yoke from the crank.


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 27-41-14
 ALL  ú ú 06 Page 207 ú Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (e)  Keep the body seal door in the retracted position to prevent damage to the door.
 TASK 27-41-14-402-033
 5.  Horizontal Stabilizer Body Seal Door Mechanism Installation___________________________________________________________
 A.  References
 (1)  
AMM 27-41-14/601, Horizontal Stabilizer Body Seal Doors

 (2)  
AIPC 27-41-08, Fig. 1

 (3)  
AIPC 27-41-09, Fig. 1

 B.  
Access

 (1)  
Location Zone
 313 Stabilizer Torsion Box Compartment, LH
 314 Stabilizer Torsion Box Compartment, RH


 (2)  
Access Panel 312A Horizontal Stabilizer Jackscrew Access Door 315A Access Door

 C.  
Procedure


 S 222-034
 (1)  
Do this task to make sure the door mechanism and the attachment fittings are in the tolerances: "Horizontal Stabilizer Body Seal Door Inspection" (AMM 27-41-14/601).

 S 422-035

 (2)  
Install the door mechanism.

 (a)  
Apply a thin layer of grease to all the bolts.

 (b)  
Install the yoke on the crank with the washers, the nut and the cotter pin.

 (c)  
Tighten the nut by hand.

 1)  If it is necessary to install the cotter pin, loosen the nut to the next slot.
 
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