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时间:2011-04-10 09:54来源:蓝天飞行翻译 作者:航空
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 2.  Rudder Hinge No. 1, 4, 5, 9, 10, or 11 Removal (Fig. 401)______________________________________________
 A.  Special Tools and Equipment
 (1)
ST2580-267 Spanner Wrench Adapter Set

 B.  
References

 (1)
AMM 06-09-07/201, Fin and Rudder Access Doors and Panels

 (2)
AMM 24-22-00/201, Manual Control

 (3)
AIPC 27-21-01, Fig. 2

 (4)
AIPC 55-40-52, Fig. 1

 C.  
Access

 (1)  
Location Zone 324 Vertical Fin, Rear Spar to Trailing Edge 325 Rudder, Lower 326 Rudder, Upper

 (2)  
Access Panel
 324BL Inspection Access Panel
 324CL Inspection Access Panel
 324EL Inspection Access Panel
 324FL Inspection Access Panel
 324GL Inspection Access Panel
 324KL Inspection Access Panel
 324LL Inspection Access Panel
 324ML Inspection Access Panel
 324UL Inspection Access Panel

 

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 27-21-03
 ALL  ú ú 01 Page 401 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL 
FIN VERTICAL 
NO. 11 HINGE SEE B 
RUDDERS SEE A  UPPER RUDDER PACKAGE FOR THE POWER CONTROL  HINGE NO. 9 SEE NO. 10 SEE HINGE B B 
HINGE NO. 5 SEE B 
POWER CONTROL PACKAGE FOR THE LOWER RUDDER  HINGE NO. 4 SEE B 
SPAR FRONT RUDDER 1. BOLT  11. WASHER 10. BOLT  12. RUDDER HINGE SEGMENT  RUDDERS A  HINGE NO. 1 SEE B 
9. BOLT  A 
13. COVER FOR THE VERTICAL FIN SEGMENT  A NUT  JUMPER BONDING 
HINGES NO. 1, 4, 5, 9, 10, AND 11 

Figure 401 (Sheet 1) Hinges 1, 4, 5, 9, 10 and 11 

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 27-21-03
 ALL  ú ú 01 Page 402 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


HINGES NO. 1 AND 4
A-A

1. BOLT

3. NUT (INSTALL IF NECESSARY)
HINGES NO. 5, 9, 10 AND 11 A-A
INSTALL AS MANY LARGE WASHERS (2) AS NECESSARY TO GET A CLEARANCE OF 0.01 - 0.06 INCH.

Hinges 1, 4, 5, 9, 10 and 11
Figure 401 (Sheet 2)

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 27-21-03
 ALL  ú ú 01 Page 403 ú Jun 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E99172
A
747-400 MAINTENANCE MANUAL
 D. Prepare to Remove Hinge No. 1, 4, 5, 9, 10, or 11
 S 864-093
 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 864-094

 (2)  
Find the switches for the FLT COLTROL HYD POWER on the Pilot's Overhead Maintenance Panel, P461.

 (a)  
Put the TAIL switches in the SHUT OFF position.


 S 864-095
 (3)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  
P7, Overhead Circuit Breaker Panel
 1) 7D16, RUD TRIM CONT


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

 

 S 014-096
 (4)  
Remove the applicable access panels (AMM 06-09-07/201).

 (a)  
324BL, 324CL, for access to hinge No. 1

 (b)  
324EL, 324FL, for access to hinge No. 4

 (c)  
324FL, 324GL, for access to hinge No. 5

 (d)  
324UL, 324KL, for access to hinge No. 9

 (e)  
324KL, 324LL, for access to hinge No. 10

 (f)  
324LL, 324ML, for access to hinge No. 11

 E.
Remove the Hinge


 S 024-097
 
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本文链接地址:747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(79)