通航信息_通航_通用航空_General Aviation

ADAA
Validity : S / N 1 - 9999 53 TC (EA) Page 4 SEP 04
 
FUSELAGE
DESCRIPTION AND OPERATION
1. GENERAL
The fuselage is a metallic, aluminium alloy structure of semi-monocoque design.
It is composed of frames and fittings, cross beams and stringers, formed and riveted light alloy fairings and
skins.
The fuselage consists of :
- the forward fuselage structure,
- the rear fuselage structure,
- the upper fuselage panel structure,
- the footstep,
- the access door mechanism.
2. LOCATION (Figure 1)

COMPONENT QTY AREA ACCESS DOOR REFERENCE
Forward fuselage structure 1 210 / 53-10-00
Rear fuselage structure 1 220 / 53-20-00
Upper fuselage panel structure 1 240 / 53-40-00
Footstep 2 210 / 53-70-00
Access door mechanism 2 230 233L / 233R 53-80-00

3. DESCRIPTION
• A. Forward fuselage structure
The forward fuselage structure provides attachment for the engine mount, the nose landing gear mount and the wings. It includes the cockpit and the baggage compartment, the latter being accessible through a door located on the L.H. side of the fuselage.
　
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本文链接地址：TB20 MAINTENANCE MANUAL 53 机身 TB20飞机维护手册(4)