曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 (a)  Refer to the applicable chapter for the instructions to remove or disconnect the equipment.
 S 024-003-B00
 (2)  Remove the fairing:
 (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.
 (b)  Remove the fairing.
 TASK 53-51-19-404-004-B00
 3.  Forward Wing-to-Body Fairing Installation_________________________________________
 A. General
 (1)  The wing-to-body fairing will be referred to as the fairing in this task.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 53-51-19
 ALL  ú ú B01 Page 401 ú Jul 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
A

Forward Wing-To-Body Fairing

Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 53-51-19
 ALL  ú ú B02 Page 402 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
G94691
 B.
C.
D.
E.
F.
A
737-300/400/500MAINTENANCE MANUAL
Standard Tools and Equipment
 (1)
Meter - BondingConsumable Materials

 (1)  
G00009 Compound - Corrosion inhibiting, BMS 3-23

 (2)  
G00508 Compound - Corrosion preventive, MIL-C-11796, Class 3

 (3)  
A00249 Compound - Sealing, BMS 5-26, Type II, Class A-2

 (4)
A00247 Sealant - Chromate, BMS 5-95, Type IReferences

 (1)  
AMM 12-31-21/201, Body Section 43 Access Doors and Panels

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

 (3)  
SWPM 20-20-00, Standard Wiring Practices Manual

 (4)  
AMM 20-30-11/201, Adhesives, Cements, and Sealers

 (5)  
AMM 51-21-95/701, Skin and Fastener Corrosion Removal and Control

 (6)  
AMM 51-31-00/000, Seals and Sealing

 (7)
AMM 51-51-00/801, Bonded Rub PadsAccess

 (1)  
Location Zones 300/400 Left wing/Right Wing

Procedure
 S 214-005-B00
 (1)  Examine the mating surfaces on the structure and the fairing panel.
 (a)  Make sure all mating surfaces are clean and free from any contamination or painting.
 S 214-006-B00
 (2)  Make sure the teflon rubstrip is in a good condition.
 (a)  If it is necessary, repair the teflon rubstrip (AMM
 51-51-00/801).

 S 214-007-B00
 (3)  Make sure the fasteners and the area around the fastener holes are clean.
 NOTE: Fastener locations with stainless steel fasteners are
____ usually at 4 locations per panel, (1) at each corner.
 S 024-008-B00
 (4)  
Remove any paint or primer covering the conductive surface at the panel in the area underneath dimpled washer.

 S 214-009-B00

 (5)  
If the conductive surface is flame sprayed aluminum, do the following:

 (a)  
Apply alodine over exposed aluminum

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

 (c)  
Measure the resistance.
 1) Maximum resistance shall not exceed 0.5 OHMs.

 

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 53-51-19
 ALL  ú ú B02 Page 403 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  Touch up finish
 S 214-010-B00
 (6)  If the conductive surface is anti-static coating, do the following:
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 機身 FUSELAGE(19)