Ailerons And Interceptors; Flaps; Tail Group; Fuselage - Helio HT-295 Owner's Manual

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
junction with the ailerons.
The flaps are of a single spar all-metal constructfon, They

FLAPS.

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.
FIN:
RUDDER:

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.
in a box section of the fuselage structure.
air-oil shock strut type and is attached to the engine mount.
Gross Weight
Empty Weight
Wing Span
Wing Chord
Wing Area
(Slats retracted)
Overall Length
Aileron Area
(Each Surface)
Slat Span (Each Wing) 203.93 in.
Rudder and Fin Area
The ailerons are the Frieze type, of
They emerge from the wings incon-
aileron).
All tail surfaces are of aluminum alloy construction.
Two-spar construction,
Single-spar construction
The main landing gear is the Spring Steel type mounted
3400 lbs, Fuel Capacity (Useable)
2023 lbs. Octane Rating
Oil Capacity
39 ft.
72 in. Power Plant
Take-off Horsepower
231 sq. ft,
Normal Rated Horsepower
30 ft. 4 in.
Flap Area (Each Surface)
Stabilator Area
24.40 sq. ft. Wheel Tread
2
The Nose Wheel is the
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.