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时间:2011-10-25 12:49来源:蓝天飞行翻译 作者:航空
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7 — Washer
8 — Washer
9 — Crankpin
10 — Nut
11 — Cotter pin
12 — Connector
13 — Adjustment nut

14221200AAAEWZ4100 

Pitch servo—actuator — Removal / Installation
Figure 202
ACAC
Validity : CENTURY 31 22-11-00 (AM) Page 204
DEC 99
 
F. Removal of the pitch trim servo—actuator (Figure 203)
1) Open the "TRIM" circuit breaker.
2) Remove the access door of the baggage compartment bottom 242.
3) Disconnect the connector (11).
4) Place a cable clamp (2) P/N T700A2799000008 — see 20-00-07, rearward of the bracket (1) at frame
C6, as near as possible from pulleys.
5) Place a cable clamp (9) P/N T700A2799000008 — see 20-00-07, forward of the pitch trim actuator, as
near as possible from the spool (10).
6) Remove the 2 screws (14), retain the cable—guide (13).
7) Unscrew the 2 bolts (3), retain pulleys (5) and washers (4).
8) Hold the servo—actuator (12) and retain bolts (6), washers (7), discard nuts (8).
9) Remove the servo—actuator on the work bench.
G. Installation of the pitch trim servo—actuator (Figure 203)
NOTE : Before installation, check for the good condition of cables and pulleys — see 20-00-07
1) Position the servo—actuator (12).
2) Secure the servo—actuator (12) with bolts (6), washers (7) and new nuts (8).
3) Position pulleys (5) by routing the cable in pulley groove.
4) Secure pulleys (5) with bolts (3) and washers (4).
5) Secure the cable—guide (13) with 2 screws (14).
6) Remove both cable clamps at frame 6 and to the pitch trim actuator spool.
7) Connect the connector (11).
8) Install the access door of the baggage compartment bottom 242.
9) Close "TRIM" circuit breaker.
ACAC
Validity : CENTURY 31 22 11 00 (AM) Page 205
DEC 99
 
 
1 — Bracket
2 — Cable clamp
3 — Bolt
4 — Washer
5 — Pulley
6 — Bolt
7 — Washer
8 — Nut
9 — Cable clamp
10 — Spool
11 — Connector
12 — Servo—actuator
13 — Cable—guide
14 — Screw

 
Pitch trim servo—actuator — Removal / Installation
Figure 203
ACAC
Validity : CENTURY 31 22-11 Page 206
00 (AM) DEC 99
 
3. ADJUSTMENTS / TESTS — SERVO—ACTUATORS
A. Tools and consumable materials
— 2 seal retainers
— 2 protection shims
— a dynamometer
B. Tests on table
1) Procedure for roll control and pitch (Figure 204)
 
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本文链接地址:TB20 MAINTENANCE MANUAL 22 AUTO FLIGHT TB20飞机维护手册 22 自动飞行(13)