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时间:2011-04-03 11:42来源:蓝天飞行翻译 作者:航空
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 (a)  
Apply anti-static paint over exposed area

 (b)  
Install fasteners (stainless steel bolt and dimpled washer)

 (c)  
Measure the resistance.
 1) Maximum resistance shall not exceed 300,000 OHMs.


 (d)  
Touch up finish.


 NOTE: Do not apply anti-static paint to flame sprayed
____
 aluminum.

 S 374-012-B00
 (7)  
Apply the corrosion preventive compound, MIL-C-11796, to the flanges on the fairing which touches the structure.

 S 374-013-B00

 (8)  
Apply the sealing compound, BMS 5-26 or BMS 5-95, to the flanges on the fairing which touches the body skin.

 S 374-014-B00

 (9)  
Apply the corrosion inhibitive compound, BMS 3-23, to the area on the structure and the body skin which touches the fairing.

 S 424-015-B00

 (10)
 Install the fasteners which attach the fairing to the structure.


 NOTE: Make sure you install the stainless steel bolts and
____ dimpled washers at the same locations on the fairing panel as they were prior to removal of the panels. Installing different hardware in these locations may result in unacceptable electrical bonding.
 (a)  Torque fasteners to 25-35 lb. inches (2.8-4.0 Nm).
 S 764-017-B00
 (11) Measure the electrical bonding resistance between conductive fasteners and the fairing panel conductive surface.
 NOTE: Maximum resistance shall not exceed 300,000 OHMs for
____
 conductive paint.

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 53-51-19
 ALL  ú ú B02 Page 404 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 764-018-B00
 (12) Maximum resistance shall not exceed 0.5 OHMs for flame spray.
 NOTE: Make resistance measurement prior to painting the
____ panel and the mounting hardware. If the fairing panels and bolts have been covered with paint, use sharp probes and make sure the probes contact the conductive finish on the panel and the metal on the mounting hardware. Then you can measure the resistance.
 S 434-019-B00
 (13) Connect or install the equipment to the fairing and do an operational test if the equipment was disconnected or removed.
 (a)  Refer to the applicable chapter for the instructions to connect, install or do an operational test of the equipment.
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 53-51-19
 ALL  ú ú B01 Page 405 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 MID WING-TO-BODY FAIRING - REMOVAL/INSTALLATION
_______________________________________________
 1.  General_______
 A. This procedure has these tasks:
 (1)  
Mid Wing-to-Body Fairing Removal.

 (2)  
Mid Wing-to-Body Fairing Installation.


 TASK 53-51-20-004-001-B00
 2.  Mid Wing-to-Body Fairing Removal________________________________
 A. General
 (1)  The upper and lower wing-to-body fairing will be referred to as the fairing in this task.
 B. References
 (1)  
AMM 12-31-21/201, Body Section 43 Access Doors and Panels

 (2)  
AMM 12-31-31/201, Body Scetion 46 Access Doors and Panels


 C. Access
 (1)  Location Zone
 300/400 Left Wing/Right Wing

 D. Procedure
 S 034-002-B00
 (1)  If it is necessary, remove or disconnect the equipment that is attached to the fairing.
 (a)  Refer to the applicable chapter for the instructions to remove or disconnect the equipment.
 S 024-003-B00
 (2)  Remove the fairing (Fig. 401):
 (a)  Remove the fasteners which attach the fairing to the structure.
 NOTE: Different types of fasteners are used to hold the
____ fairing panels. Stainless steel bolts and dimpled washers are used to hold the fairing panel and also to provide electrical bonding. Make sure you install these fasteners in the same locations when repair and maintenance is completed.
 
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