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TB20 MAINTENANCE MANUAL 53 机身 TB20飞机维护手册(15)

时间:2011-11-11 09:54来源:蓝天飞行翻译 作者:航空
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S / N 796 - 9999 and S / N 1 - 795 Post-Kit OPT10 914500 - refer to Detail A
4) Remove bolts (1) and washers (2)
S / N 1 - 9999
5) Remove bracket assembly (6) [3].
6) Remove the sealant with a spatula and clean the surfaces with a lintfree clean cloth moistened with cleaning agent (TB 11-003).
2. INSTALLATION OF BRACKET ASSEMBLY (Figure 401)
A. Tools and consumable materials
- Red paint
- Torque wrench 0 - 177 lbf.in (0 - 20 N.m)
Sealant (TB 09-916)
- Petrolatum (TB 04-012)
- Cleaning agent (TB 11-003)
- Lintfree clean cloth
WA
Validity : S / N 1 —9999 53-20-05Page 401
(BA) SEP 04
 
B. Procedure
1) Apply a very thin layer of petrolatum (TB 04-012) to the bearing face of bracket assembly (6) [3]. S / N 1 - 795 Pre-Kit OPT10 914500 - refer to Detail B
2) Apply some sealant (TB 09-916) to the bearing face of bracket assembly (6) [3] and bolts (1) and (7) -refer to 20-00-09.
3) Position bracket assembly (6) [3] on frame C9 and secure with bolts (1) and (7), washers (2) and (4) and new nuts (5).
4) Torque according to "Specific cases" tightening procedure - refer to 20-00-01. S / N 796 - 9999 and S / N 1 - 795 Post-Kit OPT10 914500 - refer to Detail A
2) Apply some sealant (TB 09-916) to the bearing face of bracket assembly (6) [3] and bolts (1) - refer to 20-00-09.
3) Position the bracket assembly (6) [3] on frame C9 and secure with bolts (1), washers (2) and (4) and new nuts (5).
4) Torque according to "Specific cases" tightening procedure - refer to 20-00-01.
S / N 1 - 9999
5) Wipe off excess sealant with a lintfree clean cloth moistened with cleaning agent (TB 11-003).
6) Mark nuts (5) with a red paint line.
7) Make sure all the tools and materials are removed and the work area is clean and free from debris.
8) Install the elevator - refer to 55-20-01.
9) Install the tail cone - refer to 53-20-04.
WA
Validity : S / N 1 - 9999 53-20-05 (BA) Page 402 SEP 04
 
Fittings - Removal / Installation
Figure 401
 
PAGE INTENTIONALLY LEFT BLANK
AAAA
Validity : S / N 1 - 9999
Page 404
53-20-05
(BA) SEP 04
 
UPPER FUSELAGE PANEL STRUCTURE
DESCRIPTION AND OPERATION
1. GENERAL
I Aerodynamic fairing is ensured by an upper fuselage panel.
The upper fuselage panel structure consists of :
- the front part,
- the central part,
- the rear part.
2. LOCATION (Figure 1)

COMPONENT QTY AREA ACCESS DOOR REFERENCE
Front part / 240 / 53-40-00
Central part / 240 / 53-40-02
Rear part / 240 / 53-40-00
 
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