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SPECIFICATIONS:
Engine......1 Rotax Model 447 Twin Cylinder,
Two Cycle 436.5 cc, 40 hp @ 6500 rpm
Recommended TBO...............................250 hr
Propeller........................................66 in x 34 in
Length.................................................18 ft 1 in
Height.................................................8 ft 10 in
Wingspan............................................28 ft 0 in
Wing area...........................................156 sq ft
Wing loading..................................3.36 lb/sq ft
Power loading.................................13.12 lb.hp
Seats..............................................................1
Minimum flight crew........................................1
Empty weight...........................................250 lb
Useful load...............................................275 lb
Payload w/full fuel....................................245 lb
Max takeoff weight..................................525 lb
Fuel capacity.....................................5 U.S. gal
PERFORMANCE:
Takeoff distance, ground roll......................65 ft
Takeoff distance, 50 ft obst......................200 ft
Rate of climb......................................900 ft/min
Max level speed, sea level......................54 mph
Max operating altitude.........................14,000 ft
Landing distance
50 ft obstacle (with brake)...................200 ft
Landing distance
ground roll (with brake)..........................60 ft
CRUISE PERFORMANCE CHART:
(Speed/Range at sea level with
4.8 gal. usable fuel)
@ 55% power(5000 rpm)...............44 mph/84 mi
@ 65% power(5300 rpm)...............47 mph/84 mi
@ 75% power(5500 rpm)...............50 mph/80 mi
@ 100% power(6500 rpm).............54 mph/52 mi
FUEL FLOW:
@ 55% power ....................................2.5 gph
@ 65% power ....................................2.7 gph
@ 75% power ....................................3.0 gph
@ 100% power ..................................4.5 gph
LIMITING AND RECOMMENDED
SPEEDS:
Vx (Best angle of climb).......................33 mph
Vy (Best rate of climb).........................36 mph
Va (Design maneuvering)......................48 mph
Vne (Never exceed).............................65 mph
Vs (Stall, power off).............................24 mph
Landing approach speed.....................
(1.3 Vs)..........31 mph
Price
Total............................ $ COL 8.000.000 (US 4.000)
Engine......1 Rotax Model 447 Twin Cylinder,
Two Cycle 436.5 cc, 40 hp @ 6500 rpm
Recommended TBO...............................250 hr
Propeller........................................66 in x 34 in
Length.................................................18 ft 1 in
Height.................................................8 ft 10 in
Wingspan............................................28 ft 0 in
Wing area...........................................156 sq ft
Wing loading..................................3.36 lb/sq ft
Power loading.................................13.12 lb.hp
Seats..............................................................1
Minimum flight crew........................................1
Empty weight...........................................250 lb
Useful load...............................................275 lb
Payload w/full fuel....................................245 lb
Max takeoff weight..................................525 lb
Fuel capacity.....................................5 U.S. gal
PERFORMANCE:
Takeoff distance, ground roll......................65 ft
Takeoff distance, 50 ft obst......................200 ft
Rate of climb......................................900 ft/min
Max level speed, sea level......................54 mph
Max operating altitude.........................14,000 ft
Landing distance
50 ft obstacle (with brake)...................200 ft
Landing distance
ground roll (with brake)..........................60 ft
CRUISE PERFORMANCE CHART:
(Speed/Range at sea level with
4.8 gal. usable fuel)
@ 55% power(5000 rpm)...............44 mph/84 mi
@ 65% power(5300 rpm)...............47 mph/84 mi
@ 75% power(5500 rpm)...............50 mph/80 mi
@ 100% power(6500 rpm).............54 mph/52 mi
FUEL FLOW:
@ 55% power ....................................2.5 gph
@ 65% power ....................................2.7 gph
@ 75% power ....................................3.0 gph
@ 100% power ..................................4.5 gph
LIMITING AND RECOMMENDED
SPEEDS:
Vx (Best angle of climb).......................33 mph
Vy (Best rate of climb).........................36 mph
Va (Design maneuvering)......................48 mph
Vne (Never exceed).............................65 mph
Vs (Stall, power off).............................24 mph
Landing approach speed.....................
(1.3 Vs)..........31 mph
Price
Total............................ $ COL 8.000.000 (US 4.000)
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