ADAA
Validity : S / N 1 - 9999 22 TC (EA) Page 5 NOV 01
SUBJECT CHAPTER
B38 PITCH TRIM SERVO ACTUATOR 22-12-06 (BA)
REMOVAL / INSTALLATION PAGE
401
401
1. REMOVAL OF B38 PITCH TRIM SERVO ACTUATOR 401
A. Tools and consumable material 401
B. Procedure 401
2. INSTALLATION OF B38 PITCH TRIM SERVO ACTUATOR 401
A. Tools and consumable material 401
B. Procedure 401
3. REMOVAL OF THE MOUNTING PLATE 402
A. Tools and consumable materials 402
B. Procedure 402
4. INSTALLATION OF THE MOUNTING PLATE 402
A. Tool and consumable materials 402
B. Procedure 402
B38 PITCH TRIM SERVO ACTUATOR 22-12-06 (BA) 501
ADJUSTMENT/TEST 501
1. CABLE TENSION ADJUSTMENT 501
A. Tool and consumable materials 501
B. Procedure 501
ADAA
Validity : S / N 1 - 9999 22 TC (EA) Page 6 NOV 01
1. GENERAL
This chapter describes components and equipment for aircraft automatic flight control.
It includes equipment and components which control either the roll axis only or both the roll and pitch axes.
2. DESCRIPTION The aircraft is equipped with an autopilot — refer to 22-10-00.
ACAA
Validity : OPTION 22 00-00Page 1
(BE) DEC 99
PAGE INTENTIONALLY LEFT BLANK
ACAA
Validity : OPTION 22-00-00Page 2
(BE) DEC 99
1. GENERAL The autopilot combines all auto flight functions in a single computer.
2. DESCRIPTION The section describes the autopilot systems CENTURY 21 and 31 — refer to 22-11-00.
ABAA
Validity : EDO AIRE MITCHELL 22-10-00 (.) Page 1
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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(6)
