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时间:2011-04-06 23:21来源:蓝天飞行翻译 作者:航空
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 744-077
 (7)  
Do this task: Ground Test - Yaw Damper (Ref 22-21-00/501).

 S 744-078

 (8)  
Do this task: Ground Test - Yaw Damper Actuator (Ref 22-21-00/501).


 E. Airplane to Its Initial Condition
 S 864-072
 (1)  
Push and release the engage switch of the applicable yaw damper (P5) to disengage the yaw damper system.

 S 864-073

 (2)  
Set all the mode selector switches on the IRS control panel (P5) to the OFF position if it is not necessary (Ref 34-21-00/201).

 S 414-074

 (3)  
Install the 117AL electronics compartment access door
 (Ref 06-09-01/201).


 S 864-075

 (4)  
Remove hydraulic power if it is not necessary
 (Ref 29-11-00/201).


 S 864-076

 (5)  
Remove electrical power if it is not necessary
 (Ref 24-22-00/201).

 

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 22-21-02
 ALL  ú ú 01 Page 405 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 MODAL SUPPRESSION ACCELEROMETER - REMOVAL/INSTALLATION
______________________________________________________
 1.  General________
 A.  This procedure contains two tasks. The first task is for the removal of a modal suppression accelerometer. The second task is for the installation of a modal suppression accelerometer.
 B.  There are four modal suppression accelerometers. The procedure is the same for each modal suppression accelerometer.
 C.  You can find the left and the right forward accelerometers (M7953, M7954) at station 320 (LBL/RBL 85, WL 194.68) below the main deck floor. You can find the left and the right aft accelerometers (M7955, M7956) at station 2260 (LBL/RBL 65, WL 194.68) below the main deck floor.
 TASK 22-21-03-004-022
 2.  Modal Suppression Accelerometer Removal (Fig. 401)_______________________________________
 A.  References
 (1)  
53-21-02/401, Main and Upper Deck Floor

 (2)  
IPC 22-21-03, Fig. 1


 B.  Access
 (1)  Location Zone 115 Area between Nose Gear Well and Fuselage, LH 116 Area between Nose Gear Well and Fuselage, RH 145 Bulk Cargo Compartment, LH 146 Bulk Cargo Compartment, RH
 C.  Procedure
 S 864-023
 (1) Open these circuit breakers and attach the DO-NOT-CLOSE tags:
 (a)  P7 Overhead Circuit Breaker Panel
 1) 7C10 FLT CONT ELEC 2L AC
 2) 7C12 FLT CONT ELEC 1L AC
 3) 7C14 FLT CONT ELEC 1R AC
 4) 7C16 FLT CONT ELEC 2R AC

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 22-21-03
 ALL  ú ú 03 Page 401 ú Jun 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
STA

Modal Suppression Accelerometer Installation
Figure 401

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 22-21-03
 ALL  ú ú 01 Page 402 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 014-024
 (2)  Remove the applicable panel in the main deck floor (Ref 53-21-02/401).
 NOTE: You can get to the forward accelerometers and do not have
____ to open the main deck floor. Get into the electrical and electronics compartment and then go forward. The forward accelerometers are on the forward side of the station 320 bulkhead.
 S 024-025
 (3)  Do these steps to remove the accelerometer:
 (a)  
Disconnect the electrical connector from the accelerometer.

 (b)  
 
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