c
AILERQNS
AKD
INTERCEPT0RS.t
The ailerons are the Frieze type, of
2024
alclad
diagonal rib truss structure, fabric covered,
They
are
hinged at both ends and operated by a push-pull tube at the
ce&ex,
The interceptors consist of heavy aluminum alloy curved plates (inboard)
and forward of each
aileron).
They emerge from the wings
incon-
junction with the ailerons.
FLAPS.
The flaps are of a single spar all-metal
constructfon,
They
are supported to the wing structure by three flap tracks and are
actuated by push-pull tubes at the center and outboard tracks,
TAIL
GROUF.
The tail group is composed of a vertical fin and rudder,
and an all-movable horizontal surface equipped with an anti-balance
and
t&n
tab.
All tail surfaces are of aluminum alloy construction.
FIN:
Two-spar construction,
RUDDER:
Single-spar construction
STABILATUR:
Sfngle-spar
construction
FUSELAGE. The forward fuselage structure is a welded steel tube
truss.
It is covered with
alclad
sheet in the cabin section; the
remaining portion is semi-monocoque.
LANDING GEAR.
-
The main landing gear is the Spring Steel type mounted
in a box
section
of the fuselage structure.
The Nose Wheel is the
air-oil shock strut type and is attached to the engine mount.
§PECXFZCATECMS
Gross Weight
Empty Weight
Wing Span
Wing Chord
Wing Area
(Slats retracted)
Overall Length
Aileron Area
(Each Surface)
3400
lbs,
Fuel Capacity (Useable)
2023 lbs.
Octane Rating
39 ft.
Oil Capacity
72 in.
Power
Plant
231
sq.
ft,
Take-off Horsepower
30 ft. 4 in.
Normal Rated Horsepower
10135
sq. ft.
Flap Area (Each Surface)
Slat Span (Each Wing) 203.93 in.
Stabilator Area
Rudder and Fin Area
24.40 sq. ft. Wheel Tread
58,s
gals.
100 (Min.)
12 qts. (Max.)
10 qts. (Desired)
GO-480-GlA6
Lycoming
295
280
19.05
sq*
ft.
37.50
sq,
ft.
102.00
in.
2
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