GlaStar
Glasair Aviation, LLC
фотография с сайта www.glasairaviation.com
SPECIFICATIONS Fuselage Length Continental IO-240 (rigged for flight) 22 ft., 4 in. Continental IO-240 (wings folded) 24 ft., 6 in. Lycoming engine (rigged for flight) 22 ft., 4 in. Lycoming engine (wings folded) 25 ft. Wing Span Rigged for flight 35 ft. Wings folded & tail removed 8.0 ft. Other Wing Data Area 128 sq. ft. Aspect ratio 09.июн Wing loading (at max. gross) 15.3 lbs. per sq. ft. Structural limit loads (at max. gross) +3.8 / -1.5 Gs Maximum Height Tricycle (on gear) 9 ft., 1 in. Tricycle (wings folded) 6 ft., 4 in. Taildragger 6 ft., 11 in. Cabin Dimensions Width (at hips) 44 in. Width (at shoulders) 46 in. Door width 37 in. Door height 31.5 in. Baggage space 32 cu. ft. Weights Maximum gross weight (on wheels) 1,960 lbs. Maximum gross weight (on floats) 2,100 lbs. Empty weight (typical)* 1,200 lbs. Useful load (typical)* 760 lbs. Full-fuel payload (standard tanks) 594 lbs. Full-fuel payload (with auxiliary tanks) 489 lbs. Maximum baggage capacity 250 lbs. Fuel Capacity (usable)** Standard tanks 27.6 gals. With auxiliary tanks 45.1 gals.
PERFORMANCE* 125 h.p. Top Speed (TAS at sea level) 156 m.p.h. / 136 kts. Cruise Speed (TAS) 75% power at 8,000 ft. 151 m.p.h. / 131 kts. 65% power at 8,000 ft 140 m.p.h. / 122 kts. Stall Speed (at max. gross)** No flaps (Vs) Full flaps (Vso) Rate of Climb Solo 1,300 f.p.m. Max. gross 1,000 f.p.m. Range (at 65% power)*** Range Standard Fuel VFR Reserve mi. 597 Range Standard Fuel VFR Reserve n.m. 520 Range Extended Fuel VFR Reserve mi. 1021 Range Extended Fuel VFR Reserve n.m. 888 Fuel Consumption (at 65% power) 5.8 g.p.h. Service Ceiling (estimated) 17,000 ft.
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