Remos GXiS, Pilot Operating Handbook

Page: 9 / 237

iS
G3-8 MA FM 9401 - R01
1 General Information
General Information 1 - 3
1.4 Quick Reference
Type:
Full composite carbon fiber aircraft with two seats.
Design: High wing design with struts, front mounted engine
and
propeller, traditional stabilizer concept,
differential ailerons. Electrically operated flaps (0°,
15° and 35°), electric elevator trim, three-wheel
landing gear with steerable nose wheel. Main gear
with hydraulic disc brakes. The cabin is equipped with
two seats side by side and can be entered and exited
by doors on the left and right side of the fuselage.
Layout: Main components are built in half shells from
composite fiber material, which are bonded together
(carbon fiber, Kevlar and glass fiber).
1.5 Technical Specifications
wingspan
9.32 m ( 30 ft 7 in)
length
6.64 m ( 21 ft 10 in)
height
2.28 m ( 7 ft 4 in)
wing area
10.97 m
2
( 118 sq ft)
MTOW
600 kg (1,320 lb)
wing loading 54.7 kg/m
2
( 11.2 lb/sq ft
)