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- the flaps,
- the ailerons.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Wing 2 500 / 600 / 57-20-00
Wing tip 2 500 / 600 / 57-30-00
Flap 2 500 / 600 / 57-50-00
Aileron 2 500 / 600 / 57-60-00
3. DESCRIPTION
A. Wings - refer to 57-20-00 The wings allow aircraft lift.
Wings characteristics :
Profile RA16-3C3
Aspect ratio 8
Dihedral 6°3
Aerodynamic chord 4.002 ft - 1.220 m
True chord 4.085 ft - 1.245 m
Wing area 128.091 sq.ft - 11.90 m2
Wing setting + 3°
B. Wing tips - refer to 57-30-00 The wing tips include the navigation lights, the anti-collision lights and the recognition lights.
C. Wing flaps - refer to 57-50-00 The flaps allow to increase the lift at low speed by modifying the wing profile.
ABAA
Validity : S / N 1 - 9999 57 00 00 (CA)UN 01
jPage 1
Recoil and slotted type flaps characteristics :
Unit area 10 sq.ft - 0.93 m2
Mean span 8.366 ft - 2.550 m
D. Ailerons - refer to 57-60-00
The ailerons allow aircraft maneuver around the roll axis.
Ailerons characteristics :
Unit area 4.897 sq.ft - 0.46 m2
Mean span 4.081 ft - 1.244 m
ABAA
Validity : S / N 1 - 9999 57 00-00Page 2
(CA) JUN 01
A - Flap
B - Aileron
C - Wing tip
D - Wing
Wings - Identification and location of components
Figure 1
PAGE INTENTIONALLY LEFT BLANK
WINGS
SERVICING
1. REPLACEMENT OF THE ANTI-SKID COATING ON THE WINGS
A. Tools and consumable materials
- Anti-skid coating (TB 05-919)
- Sealant (TB 09-910)
- Hot air generator
- Clean lintfree cloths
- Nylon spatula
- Cleaning agent (TB 11-003).
B. Procedure
1) Remove and discard the blanking plug on the wing upper surface.
2) Moderately heat anti-skid coating (TB 05-919) with a hot air generator to soften the adhesive.
3) De-bond defective anti-skid coating (TB 05-919) with a nylon spatula.
4) Clean the bared surface with clean lintfree cloths moistened with cleaning agent (TB 11-003).
5) Position the new coating to cut out the footstep area.
6) Bond the new anti-skid coating (TB 05-919).
7) Apply sealant (TB 09-910) on the periphery of anti-skid coating (TB 05-919), make an even bead overlapping anti-skid coating (TB 05-919) and wing upper surface.
8) Mark the location of the blanking plug orifice, cut the anti-skid coating (TB 05-919) and clear the orifice.
9) Install a new blanking plug.
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