-kink ................... ........................ 11.20%

 -tip .................... ........................ 10.84%
 Root-wing setting ........ ........................ 3.66 degrees
 Dihedral of wing reference plane................... 5.11 degrees

 Wing - Geometry
 Figure 003

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 57-00-00Page 9 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

R  Wing - Geometry 
R  Figure 003A 
R 1EFF :  301-399,  1  57-00-00 Page 10 
1  1  May 01/04
 1  1
 1CES  1

 Dihedral of trailing edge inboard of kink.......... 8.65 degrees
 Dihedral of trailing edge outboard of kink ........ 5.35 degrees

 **ON A/C ALL
 (1) Movable Control Surfaces for each Outer Wing
 Leading edge:
 -Slats 1 thru 5
 Trailing edge:

 -Aileron
 -Spoilers 1 thru 5
 -Inboard and outboard flaps
 (2) Control Surface Areas
 Aileron ................ ................ ............. 1.37 m2

 (14.75 ft2)
 Spoiler 1 .............. ................ ............. 1.18 m2

 (12.70 ft2)
 Spoiler 2 .............. ................ ............. 1.17 m2

 (12.60 ft2)
 Spoiler 3 .............. ................ ............. 1.11 m2

 (11.95 ft2)
 Spoiler 4 .............. ................ ............. 1.02 m2

 (11.98
 ft2)
 Spoiler 5 .............. ................ ............. 1.02 m2

 (11.98
 ft2)

 NOTE : For surface movements of the Flight Controls (Ref. 27-00-00).
____

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 (3) High Lift Surface Areas
 Slat 1 ................. ................ ............. 1.58 m2

 (17.00 ft2)
 Slat 2 ................. ................ ............. 1.41 m2

 (15.18 ft2)
 Slat 3 ................. ................ ............. 1.19 m2

 (12.81 ft2)
 Slat 4 ................. ................ ............. 1.12 m2

 (12.06 ft2)
 Slat 5 ................. ................ ............. 1.02 m2

 (11.98 ft2)

 Inboard Flap ........... ................ ............. 4.65 m2

 (50.05 ft2)
 Outboard Flap .......... ................ ............. 5.90 m2

 (63.51 ft2)

 NOTE : For surface movements of the Flight Controls (Ref. 27-00-00).
____
 **ON A/C 301-399,
 (3) High Lift Surface Areas
 Slat 1 ................. ................ ............. 1.58 m2

 (17.00 ft2)
 Slat 2 ................. ................ ............. 1.41 m2

 (15.18 ft2)
 Slat 3 ................. ................ ............. 1.19 m2

 (12.81 ft2)
 Slat 4 ................. ................ ............. 1.12 m2

 (12.06 ft2)
 Slat 5 ................. ................ ............. 1.02 m2

 (11.98 ft2)
 Inboard Flap ........... ................ ............. 4.36 m2

 (46.91 ft2)
 Outboard Flap .......... ................ ............. 4.85 m2

 (52.19 ft2) Inboard Tab ............ ................ .............

 1.45 m2 (15.60 ft2)
 Outboard Tab ........... ................ ............. 2.27 m2

 (24.43 ft2)

 NOTE : For surface movements of the Flight Controls (Ref. 27-00-00).
____
 **ON A/C ALL
 D. Materials
 The outer-wing main-box structure and the slats are made of high-grade
 aluminium alloys.
 The ailerons, flaps, spoilers and fairings are made of Carbon Fiber
 Reinforced Plastic (CFRP).
 Titanium alloys and steel alloys are used where necessary.

 E. Protective Treatment
 This is given in Protective Treatment (Ref. 51-21-00).
 1EFF : ALL 1 57-00-00Page 12 1 1 May 01/05R 1 1 1CES 1

 F. Paint Coatings This is given in Paint Coatings (Ref. 51-23-11).
 G. Outer Wing Tank Sealing (Ref. Fig. 004)
 The illustration that follows shows the way that the fuel tanks are sealed, while the outer wing is being assembled.

 Outer Wing - Tank Sealing
 Figure 004
 1EFF :  ALL  1  57-00-00 Page 14 
1  1  May 01/04
 1  1
 1CES  1

 CENTER WING - DESCRIPTION AND OPERATION_______________________________________
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼1(39)