Weight
xxxxxxxx
Empty
1,325 lbs
Gross (standard
wing) . 2,000 lbs
Gross
(extended
wint) . 2,100 lbs
Dimensions
xxxxxxxxxx
Fuselage
length
20.2 ft
Wing Span
(standard) .23.3 ft
Wing Span
(extended) . 27.3 ft
Maximum
Heighth
6.8 ft
Cabin
Width
42 in
Roll Rate
xxxxxxxx
Standard
wing .140
degree/sec
ExtendedWing
. 100 degree/sec
Fuel Capacity
xxxxxxxxxxx
Main
Tank
Wing
40 gal
Header Tank
(oversize)
10 gal
Wing Tip
Extensions
11
gal
The Glasair IIS-RG is a high
performance experimental aircraft sold "as is" and without
warranty
G-limits
xxxxxxxxx
Limit
Loads
+6/-4 G's
Ultimate
Loads
.+9/-6 G's
OEM Published Specifications
Wing Data
xxxxxxx
Wing Area
(standard) . 81.3 sq ft
Wing Tip Extension
Area .10.2 sq ft
Aspect Ratio
(stadard)
6.20
Aspect Ratio
(extended) . 7.64
Fuel Consumpton
xxxxxxxxx
. 2,200 rpm @ 55% 7.9 gal/hr @ 199 mph
2,400
rpm @ 65% 9.2 gal/hr @ 218 mph
2,700 rpm @75% 10.7 gal/hr @ 235 mph
Propeller & Governor
xxxxxxxxxxx
Type Non-Aerobatic
Pitch
Constant Speed
Woodward
Governor
Matched
Lycoming Engine
xxxxxxxxx
Model
IO-360-B1E
Cylinders
4
Displacement
361 cu.in. / 5.9 liters
Fuel
System
Injected
Fuel
Type
91/96 octane
100/130 octane
100 /100LL