曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
3) Install front spacer (2) and rear spacer (3) on spar (6) and secure them with bolts (1), washers (4) and new nuts (5). Torque according to "Specific cases" tightening procedure - refer to 20-00-01.
4) Wipe off excess sealant with a clean lintfree cloth moistened with cleaning agent (TB 11-003).
5) Make a bead of sealant around the spacers with sealant (TB 09-916) - refer to 20-00-09.
6) Mark nuts (5) with a red paint line.
7) Protect the spacers with sealant (TB 09-007) - refer to 20-00-09.
8) Install the wings - refer to 57-00-00.
5. REMOVAL OF WING REAR ATTACHMENT (Figures 403 and 404)
A. Tools and consumable materials
- 1 padded support for frame C7
- 2 wing padded supports, P / N TB10 99000911
- Cleaning agent (TB 11-003)
- Spatula
- Clean lintfree cloths
B. Procedure
S/N 1 - 1736,1742 - 1746 Pre-Kit OPT10 920400
1) Apply Kit OPT10 920400.
ACAA
Validity : S / N 1 - 9999 57 20-03Page 404
(DA) SEP 04
1 - Bolt
2 - Front spacer
3 - Rear spacer
4 - Washer
5 - Nut
6 - Spar
*
3
5
Spacer - Removal / Installation
Figure 402
ACM
Validity : S / N 1 - 9999 57-20 03Page 405
(DA) JUN 02
S/N 1737 - 1741, 1747 - 9999 and S/N 1 - 1736.1742 - 1746 Post-Kit OPT10 920400
1) Jack up the aircraft - refer to 07-10-00.
CAUTION : TO AVOID DAMAGING THE STRUCTURE, THE SUPPORTS MUST PERFECTLY FIT THE FUSELAGE PROFILE AND HAVE PADDED BEARING AREAS.
2) Install padded supports under the L.H. and R.H. wings at a rib, and under the rear fuselage at frame C7.
3) Remove the cowlings under hull 218A and 218F.
4) Remove and discard cotter pins (14) and (19), remove nuts (15) and (20), washers (16) and (21) and bolt (17).
5) Remove rod (18).
6) Remove and discard cotter pin (10), remove nut (11), washer (12) and bolt (13).
7) Disconnect rod (9).
8) Remove and discard cotter pin (8), remove nut (7) and washer (6).
9) Remove and discard blanking plug (1) and remove bolt (2).
10) Remove bellcrank (3) [4] and spacer (5).
11) Remove and discard nuts (33) and (37), remove and retain washers (34) and (38), bolts (35) and (39) and rod (36).
12) Check the type of attachment of the rear fitting (with rivets or bolts).
Attachment with AVDELOCK rivets
13) Remove and discard rivets (42) - refer to 51-40-02.
14) Remove rear fitting (30).
15) Apply a protection treatment to the sections bared during removal - refer to 20-00-04. NOTE : During installation, replace the rivets with bolts, washers and nuts - refer to the Illustrated Parts Catalog.
Attachment with bolts
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：TB20 MAINTENANCE MANUAL 57 机翼 TB20飞机维护手册(28)
|
