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
C. Rudder balancing re-adjustment procedure 604
D. Aileron balancing re-adjustment procedure 604
ADAA
Validity : S / N 1 - 9999 Page 2
51 -TC (EA) SEP 04
STANDARD PRACTICES / STRUCTURES
DESCRIPTION AND OPERATION
1. GENERAL
This chapter describes special approved repairs, typical approved repairs, materials, damage classification, fasteners and the procedures applicable to the aircraft structures hereafter.
Aircraft structure features all metal! construction and conventional design, incorporating aluminum alloys, steel and other materials as appropriate.
- Fuselage : the cabin portion is constructed with metal panels assembled to form a rigid structure. Metal floor
panels extend the length of the cabin area and baggage compartment. The aft fuselage is constructed of sheet aluminum alloy panels which form a semi-monocoque structure - refer to 53-00-00.
- Doors and landing gear doors are provided in fuselage. For cabin door and front baggage compartment
see 52-00-00.
- The fuselage is provided with windows. The windows consists of windshield, cabin door window and cabin windows.
- The empennage structure consists of horizontal and vertical stabilizers. Fixed stabilizers consist of spars, ribs and skins - see 55-00-00.
- The wing structure consists of spars, ribs and skins. Wing structure provides attach fittings for the main
landing gear, aileron and flap. Wing incorporates a sealed structure for fuel storage - see 57-00-00.
WA
Validity : S / N 1 - 9999 51-00-00Page 1
(BA) OCT 97
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I AAAA
Validity S / N 1 - 9999 51-00-00Page 2
(BA) OCT 97
MATERIALS
DESCRIPTION AND OPERATION
1. GENERAL
This chapter concerns the materials used in the aircraft structure. Most of them are aluminum alloys. Others such as steel alloys and composites are also used. Sealants ensure cabin and tank sealing.
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Main skins / / / 51-30-01
Composite materials / / / 51-30-02
WA
Validity : All 51-30-00Page 1
(BA) SEP 91
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WA
Validity : All 51-30-00Page 2
(BA) SEP 91
MAIN SKINS
MAINTENANCE PRACTICES
1 QUALITIES AND THICKNESS OF MAIN SKINS
Fuselage skins
Figure 201
Axe symetrie avion Aircraft centerline
14513001AAAAV714000 (AV - FWD
Wing skins
Figure 202
ABAA
Validity : S / N 1 - 9999 51-30-01Page 202
(CA) SEP 04
14513001AAAAVZ14200
Skins of empennages
Figure 203
2. SKIN MATERIAL CHARACTERISTICS
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本文链接地址：TB20 MAINTENANCE MANUAL 51 标准施工/结构 TB20飞机维护手册(3)
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