-kink ................... ........................ 11.20%
-tip .................... ........................ 10.84%
Root-wing setting ........ ........................ 3.66 degrees
Dihedral of wing reference plane................... 5.11 degrees
Wing - Geometry
Figure 003
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R Wing - Geometry
R Figure 003A
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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).
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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
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CENTER WING - DESCRIPTION AND OPERATION_______________________________________ 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM WINGS 机翼1(39)
