AIRCRAFT PROFILE:
SPECIFICATIONS |
||
Engine |
1Rotax Model 582 |
Cruise Performance Chart |
|
Twin Cylinder, Two cycle |
(Speed/Range at sea level) |
|
580.7cc, 64 hp |
At 55 % power (5000rpm /43hp) |
Recommended TBO |
250hrs |
At 65 % power (5300rpm/52hp) |
(Time Between Overhaul) |
|
At 75 % power (5600rpm/54hp) |
Propeller |
Wooden, 68”X36” |
At 100% power (6500rpm/61hp) |
|
|
|
Length |
17.5ft |
Fuel Flow |
Height |
9.3ft |
At 55% power 4.1gph/63ml |
Wingspan |
32.75ft |
At 65% power 4.8g ph/65ml |
Wing area |
180sq.ft |
At 75% power 5.6gph/63ml |
Wing Loading |
4.0lb/sq.ft |
At 100% power 7.4gph/54ml |
Power loading |
11.25lb/hp |
|
Seats |
2 |
|
Min. flight crew |
1 |
|
Empty Weight |
330lbs |
Recommended Air Speeds |
Useful
load |
390lbs |
Vx
(Best angle of climb) 37mph |
Payload
with full fuel |
354lbs |
Vy
(Best rate of climb) 39mph
|
Max.takeoff
weight |
720lbs
|
Va
(Design maneuvering) 64mph |
Fuel
capacity |
6
gallons |
Vne
(Never exceed speed) 75mph |
|
|
Vs1
(Stall, power off) 32mph |
Performance |
|
Landing
approach speed 45mph |
Takeoff
distance (ground roll) |
121ft |
|
Takeoff
distance (50ft.obstacle) |
260
ft. |
|
Rate
of climb |
1145feet
per minute |
|
Max.level
speed, sea level |
67mph |
|
Landing
distance (50 ft.obstacle) |
300
ft |
|
Landing
distance, ground roll |
75
ft. |
|
Glide
Ratio |
5:1 |
|
Minimum
sink rate |
630
feet per minute |
|