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
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Horizontal stabilizer 1 330 / 55-20-00
Vertical stabilizer 1 330 / 55-30-00
Rudder 1 330 / 55-40-00
3. DESCRIPTION
I A. Horizontal stabilizer
The horizontal stabilizer enables the aircraft to be controlled around the pitch axis.
B. Vertical stabilizer
The vertical stabilizer supports the rudder.
The vertical stabilizer is secured to the rear fuselage.
C. Rudder
The rudder enables the aircraft to be controlled around the yaw axis.
ABAA
Validity : S / N 1 - 9999 55 00-00Page 1
(CA) SEP 04
Stabilizers - Identification and location of components
Figure 1
ABAA
Validity : S / N 1 - 9999 55 00-00Page 2
(CA) JUN 01
HORIZONTAL STABILIZER
DESCRIPTION AND OPERATION
1. GENERAL
The horizontal stabilizer is a single-piece, all-metal structure with an automatic tab. It allows the pilot to maneuver the aircraft around the pitch axis.
The horizontal stabilizer is composed of two elements :
- the elevator,
- the elevator tab.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Elevator 1 330 / 55-20-01
Elevator tab 2 330 / 55-20-02
3. DESCRIPTION (Figure 2) A. Elevator
The elevator is located at the rear of the fuselage. It is articulated on two fittings which are mounted aft of frame C9. It is controlled by the pilot via the control wheel and a pitch control linkage composed of rods and bellcranks.
Two static dischargers are secured to the elevator external trailing edge. The elevator travel is as follows :
- nose-up - 16° ± 1°
- nose-down + 3° ± 1°
It is fitted with a balancing weight of different values :
Balancing weight Tolerance Validity
kg lbs kg lbs
7.330 16.159 +0 ; + 0.150 +0 ; + 0.33 S / N 1 - 479
7.508 16.552 + 0 ; + 0.150 + 0 ; + 0.33 S / N 480 - 9999 Pre-MOD. 183 and without airframe de-icing
7.581 16.713 + 0 ; + 0.150 + 0 ; + 0.33 S / N 480 - 9999 Pre-MOD. 183 and without airframe de-icing
7.581 16.713 + 0 ; + 0.230 + 0 ; + 0.5 S / N 480 - 9999 Post-MOD. 183 and without airframe de-icing
6.581 14.508 + 0 ; + 0.230 + 0 ; + 0.5 With airframe de-icing
B. Elevator tab
The elevator tab is located aft of the elevator. It is articulated on two hinges fixed to the upper surface of the elevator trailing edge.
The tab fulfills two functions :
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：TB20 MAINTENANCE MANUAL 55 安定面 TB20飞机维护手册(3)
| 
