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
• A static discharger is secured to the external trailing edge of each aileron.
With the control wheel fully turned, aileron deflection is as follows :
- Upward 15° ± 1.5,
- Downward 15° ± 1.5.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Aileron 2 520
620 / 57-60-00
Ailerons - Identification and location of components
Figure 1
AAAA
Validity : S / N 1 - 9999 57-60-00Page 2
(BA) JUN 01
AILERONS
REMOVAL / INSTALLATION
NOTE : This procedure is applicable to L.H. and R.H. installations. Information specific to R.H. installation are given in square brackets.
1. REMOVAL OF THE AILERON (Figure 401)
A. Tools and consumable materials - Padded supports
B. Procedure
1) Remove the tip - refer to 57-30-00.
2) Close main switch-breaker. CAUTION : MAKE SURE THE FLAP AREA IS CLEAR.
3) Extend the flaps.
4) Open main switch-breaker.
5) Remove stop screw (3) and washer (2).
6) Remove bolt (5), spacer (9) and disengage input rod (7).
7) Hold the aileron and remove bolts (4) and (10), lockplates (6), washers (8) and spacers (1). Discard lockplates (6).
NOTE : Disengage the bonding strap, if installed.
8) Disengage the aileron and place it on two padded supports.
2. INSTALLATION OF THE AILERON (Figure 401)
A. Tools and consumable materials
None
B. Procedure
NOTE : In case of repair, painting or addition of an option to the aileron, check aileron balancing -refer to 51-60-00.
1) Lubricate hinges and rod end - refer to 12-21-04.
2) Position the aileron and secure it with bolts (4) and (10), new lockplates (6), washers (8) and spacers (1).
NOTE : Secure the bonding strap, if installed. Perform the bonding procedure - refer to 20-00-12.
3) Secure input rod (7) to the aileron with bolt (5) and spacer (9).
4) Lock bolts (4), (5) and (10) with lockplates (6).
5) Install stop screw (3) and washer (2).
6) Make sure all the tools and materials are removed and the work area is clean and free from debris.
AAAA
Validity : S / N 1 - 9999 57-60 00Page 401
(BA) SEP 04
7) Close main switch-breaker. CAUTION : MAKE SURE THE FLAP AREA IS CLEAR.
8) Retract the flaps.
9) Open main switch-breaker.
10) Install the tip - refer to 57-30-00.
11) Check the roll control - refer to 27-10-00.
12) Perform a test flight - refer to 05-30-00.
AAAA
Validity : S / N 1 - 9999 57 60-00Page 402
(BA) SEP 04
Ailerons - Removal / Installation
Figure 401
AAAA
Validity : S / N 1 - 9999 57-60-00Page 403
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(37)
|
