Aircraft Specifications
ROTAX 912 A (or 912 UL)
Airframe
All-metal construction
Wingspan
28'6"
Fuselage length
18'0"
Wing area 92.5 sq.ft
Gross weight 1168 lbs
Empty weight 727 lbs
Wing loading 12.6 lbs/sq.ft
Power loading 14.6 lbs/hp
Engine 80 hp
Fuel tank capacity
13.1
US gallons,
DATA
PERFORMANCE
VNE 134 kts IAS
Maximum level speed ISA Sea Level 104 kts TAS
Cruising speed, 75% 95 kts TAS
Stall speed clean max. weight 45 kts CAS
Roll rate 60 kts with 40
º
Flaps 30
º
/sec
Rate of climb, max. weight 650ft/min
TO Dist to 50ft ISA sea level, max. weight <1614 ft
Ground roll <892 ft
Load factor flaps up +3.8g -1.5g
Useful load 441 lbs
Estimated fuel consumption 4.5 US gallons/h
