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Edition - Rev 0
57 -10
WINGS – DESCRIPTION AND OPERATIONS
The aileron is made of an aluminum spar to which a formed sheet metal skin and metal
ribs are attached. Flaps are made of a centre spar to which front and rear ribs are
joined.
Aluminum skin panels wrap-around the flap structure.
Wing tips are moulded epoxy resin, fibreglass reinforced. At the inboard end of the
wing's leading edge is an integrated aluminum fuel tank with individual filler cap.
Wing station 0 (STA 0) is the intersection between the chord’s plane and the a/c
plane of symmetry.
The transversal dihedral angle between the chord plane and the a/c horizontal
reference is 5°.
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