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时间:2011-05-24 14:58来源:蓝天飞行翻译 作者:航空
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A. Remove Control Surface Hinge Brackets
Detail Steps/Work Items  Key Items/References 
(1)  Remove the control surface.  Refer to Sections 57-50 and 57-60. 
(2)  For brackets at the control horn hinge: S Remove the control bell-crank access panel under the wing. S Remove the attaching nuts and large washers. S Remove the bolts and small washers. S Remove the bracket.  The flap brackets have 3 bolts. The aileron brackets have 2 bolts. From inside of the wing. 
(3)  For brackets not at the control horn hinge: S Remove the bolts and small washers. S Remove the bracket.  All brackets have 2 bolts. 

Doc # 6.02.01 Page 215
Rev. 4 09 Jan 2003

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B. Install Control Surface Hinge Brackets
Detail Steps/Work Items  Key Items/References 
(1)  For brackets at the control horn hinge: S Put the bracket in position on the rear web. S Install the bolts with small washers. S Install the large washers and self-locking nuts. S Install the control bellcrank access panel under the wing.  The flap brackets have 3 bolts. The aileron brackets have 2 bolts. From inside of the wing. Torque: 3.6 Nm (2.7 ft.lb). 
(2)  For brackets not at the control horn hinge: S Put the bracket in position on the rear web. S Install the bolts and small washers.  All brackets have 2 bolts. Torque: 3.6 Nm (2.7 ft.lb.). 
(3)  Install the control surface.  Refer to Sections 57-50 and 57-60. 

Page 216 Doc # 6.02.01 09 Jan 2003 Rev. 4
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5. Repair Data for the Wing Shells
Figures 6 through 9 show the layers of glass fiber cloth in the wing shells. Use this data when you need to repair the wing.
The Figures show the main layers of cloth. The cross-hatching on the figure shows the orientation of the fibers. The orientation is also given in the related table. When you repair the wing, you must use the same type of cloth with the same fiber orientation.
The numbers in circles beside each drawing give the order in which the layers are applied (‘Stages’). The first stage is a layer of filler and is not shown. Stage 1 is the outer face of the shell.
Always do a burn test on a piece of composite from the damaged area before you do a repair. Refer to Section 51-20 for the burn test.
Doc # 6.02.01 Page 217
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6


7


10 1112 13


Item No.  Layers  Reference No.  Type  Remarks 
2, 3  1  CCC 459 Al  carbon/aluminum  0°/90o - lightning protection. 
6  2  8.3520.80  carbon cloth  0°/90o, 100 mm wide. 
7  1  8.3520.80  carbon cloth  ±45o 
10 - 13  3 each  8.3520.80  carbon cloth  ±45o, 200 mm x 200 mm 
14, 15  3 each  8.3520.80  carbon cloth  ±45o, 200 mm x 250 mm 
16  3 each  8.3520.80  carbon cloth  ±45o, 160 mm x 160 mm 

Figure 6: Layers of Cloth in the Wing Bottom Shell - Stages 2 - 6
Page 218 Doc # 6.02.01 09 Jan 2003 Rev. 4
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20 18


22


23


Item No.  Layers  Reference No.  Type  Remarks 
18, 20  1 each  H 60  6 mm rigid foam 
22  2  8.4551.60 glass  twill 2/2  ±45o, 90 mm wide. 
23  1  8.4551.60 glass  twill 2/2  ±45o 

Figure 7: Layers of Cloth in the Wing Bottom Shell - Stages 7 - 9
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32

 

 

Item No.  Layers  Reference No.  Type  Remarks 
2, 3  1  CCC 459 Al  carbon/aluminum  0°/90o - lightning protection. 
 
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