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时间:2011-04-04 10:01来源:蓝天飞行翻译 作者:航空
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 (a)  The following can help remove the bolts from the leading edge panels: 1) A leverage adapter, B20004-21, 2) A removal anti cam-out ribbed (ACR) bit,
 NOTE: The bit should have a hardness of 56-58 RC.
____
 NOTE: A combination removal/installation ACR bit is not
____ recommended.
 CAUTION: ONLY APPLY FASTENER REMOVAL COMPOUND TO THE BIT IF
_______ NEEDED. CLEAN THE BIT AFTER EACH USE. DO NOT APPLY FASTENER REMOVAL COMPOUND TO THE FASTENER RECESSES, HOLES, OR THREADS. THIS CAN CAUSE DAMAGE TO THE FASTENERS.
 3)  Apply a fastener removal compound on the driver bit if a fastener is difficult to remove.
 (b)  Remove the leading edge.
 S 214-010-B00
 (5)  Examine the leading edge for aerodynamic smoothness (SRM 51-70-00).
 TASK 55-33-11-404-006-B00
 3.  Vertical Stabilizer (Fin) Leading Edge Installation
___________________________________________________
 A.  Equipment
 (1)  Access Panel Leverage Adapter, B20004-21
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 ALL  ú ú B03 Page 402 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

Vertical Stabilizer (Fin) Leading Edge Installation
Figure 401 (Sheet 1)

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 ALL  ú ú B03 Page 403 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
ANTENNA FEEDLINE OF THE ATTACH BOLT

A-A

Vertical Stabilizer (Fin) Leading Edge Installation
Figure 401 (Sheet 2)

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 ALL  ú ú B03 Page 404 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 B.
C.
D.
E.
A
737-300/400/500MAINTENANCE MANUAL
 (2)
Ohmeter - Electrical Bonding (Model T477W)Consumable Materials

 (1)
B00624 Compound - Anti-seize, BMS 3-28References

 (1)  
AMM 20-50-11/201, Standard Torques

 (2)
AMM 23-11-00/501, HF Communication System TestAccess

 (1)  
Location Zone 706 Vertical Stabilizer

 (2)  
Access Doors 9572, 9573 Leading Edge Access Doors


Procedure (Fig. 401)
 S 864-022-B00
 (1)  Make sure these circuit breakers are open and DO-NOT-CLOSE tags are attached:
 (a)  
P6-1 Panel
 1) HF AC
 2) HF DC


 (b)  
P18-2 Panel
 1) HF AC
 2) HF DC

 

 S 424-023-B00
 WARNING: MAKE SURE PERSONNEL STAY A MINIMUM OF 6 FEET AWAY FROM THE
_______ VERTICAL STABILIZER WHEN THE HF SYSTEM TRANSMITS. RF ENERGY FROM THE HF COMMUNICATION ANTENNA CAN CAUSE INJURIES TO PERSONNEL.
 (2)  Install the fin leading edge.
 (a)  
Put the leading edge in its position on the stabilizer.

 (b)  
Connect the electrical feedline tube and the antenna conductor.

 (c)  
Install the fasteners which attach the leading edge.


 NOTE: The fasteners must be aligned within the tolerance
____ of 0.010 inch below the surface to 0.002 inch above the surface.
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 ALL  ú ú B07 Page 405 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 CAUTION:_______ WHEN INSTALLING FASTENERS, MAKE SURE THAT THE DRIVER BIT
 IS IN LINE WITH A FASTENER.  THIS WILL PREVENT DRIVER BIT
 
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