Doc # 6.02.01 Page 215
Rev. 4 09 Jan 2003
57-10-00
AMM
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
57-10-00
Wings
AMM
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
Rev. 4 09 Jan 2003
57-10-00
AMM
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
57-10-00
Wings
AMM
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
57-10-00
AMM
32
Item No. Layers Reference No. Type Remarks
2, 3 1 CCC 459 Al carbon/aluminum 0°/90o - lightning protection.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:钻石40飞机维护手册 DA 40 SERIES AMM 4(70)