曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(7)  Apply filler to the groove and the stop-drill holes.  Step 2. Use Acryfix 92 or Tensol cement No. 70. 
(8)  Let the filler cure.  Refer to the manufacturer’s data. 
(9)  If possible, turn the window so that the inner surface is up. Remove any plastic adhesive tape. 
(10)  Cut a groove along the crack in the inner surface of the window.  Refer to Figure 2, step 3. 
Note: This groove is less deep than the outer surface groove. It must cut into the outer layer of filler. This prevents holes in the filler. 
(11)  Countersink the filler in the stop-drill holes on the inner surface to 1 mm (0.04 in). 
(12)  Apply filler to the groove and the stop-drill holes.  Step 4. 
(13)  Let the filler cure.  Refer to the manufacturer’s data. 
(14)  Remove the masking materials. 
(15)  Grind the filler to the profile of the surface.  Grind both sides. Step 5. 
(16)  Polish the repair area with fine abrasive paper. 

Doc # 6.02.01 Page 205
Rev. 4 09 Jan 2003

56-10-00
AMM

Intentionally left blank
56-10-00
Wings
AMM

CHAPTER 57
WINGS

Doc # 6.02.01 Page 1
Rev. 4 09 Jan 2003

57-TITLE
AMM

Intentionally left blank
57-TITLE
Wings
AMM

TABLE OF CONTENTS
CHAPTER 57
WINGS

1. General ..............................................1

Section 57-10
Wing Structure
1.
General ..............................................1

2.
Description............................................3

 

Maintenance Practices
1.
General ............................................201

2.
Remove/Install the Wings ..............................201

3.
Remove/Install the A or B-Bolts..........................212

4.
Remove/Install Control Surface Hinge Brackets..............215

5.
Repair Data for the Wing Shells..........................217

 

Doc # 6.02.01 Page 1
Rev. 4 09 Jan 2003

57-CONTENTS
AMM

Section 57-50
Flaps

1.
General ..............................................1

2.
Description............................................3

 

Maintenance Practices
1.
General ............................................201

2.
Remove/Install a Flap .................................201

3.
Repair Data for the Flap Shells...........................203

 

Section 57-60
Aileron

1.
General ..............................................1

2.
Description............................................3

 

Maintenance Practices
1.
General ............................................201

2.
Remove/Install an Aileron ..............................201

3.
Repair Data for the Aileron Shells ........................203

 

Page 2 Doc # 6.02.01 09 Jan 2003 Rev. 4
57-CONTENTS
Wings
AMM

CHAPTER 57
WINGS

1. General
The DA 40 has cantilever wings. The wings are set low on the fuselage. Each wing has a flap attached to the inboard trailing edge. An aileron attaches to the outboard trailing edge.
The wings have a monocoque structure. Each wing has top and bottom shells. The shells have CFRP outer skins, a rigid foam core and GFRP inner skins. Each wing has two I-section spars. Uni-directional carbon fiber cloth makes the spar caps. Each wing also has GFRP ribs and webs.
The flaps and ailerons have a mixture of CFRP and GFRP cloth in the shells. The shells have rigid foam cores.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：鉆石40飛機維護手冊 DA 40 SERIES AMM 4(64)