|
Engine
Make/Model |
Lycoming
IO-540 -C4B5 |
|
Horsepower @ RPM @ Altitude
|
250 @
2575 @ Sea Level |
|
TBO
Hours |
2000 |
|
Gross
Take Off Weight (Lbs/Kg) |
3140/1424 |
|
Empty
Weight (Std) (Lbs/Kg) |
1975/896 |
|
Useful
Load |
1165/528 |
|
Fuel
Capacity (Std) (Lbs/Kg) |
76/90 -
288/341 |
|
Wheel
Track (Ft/M) |
11'2"/3.41 |
|
Seating
Capacity |
6 |
|
Cabin
Doors |
3 |
|
Baggage
Capacity (Lbs/Kg) |
200
Lbs/90.72 |
|
Service
Ceiling (Ft/M) |
14,700'/4481 |
|
Best
Rate of Climb @ Sea Level |
900/274 |
|
Cruise
Speed (Kts/Km) |
132/242
@ 6000'/1829 M @ 75% |
|
Max
Range (No Reserve) Nm/Km |
1050/1940 @ 55% |
|
Fuel
Consumption (Gph/Lph) |
2.8/48.45 (75%) |
|
Stall
Speed - (Flaps Up, Gear Up) |
55/104
Kt/Km |
|
Stall
Speed - (Flaps Down, Gear Down) - Kt/Km |
49/91 |
|
Takeoff
Roll - Land (Ft/M:Lbs/Kg) |
880/268
@ 3140/1424 600/183 @ 2600/1179 |
|
Takeoff
Roll - Water (Ft/M:Lbs/Kg) |
1250/381
@ 3140/1424 800/244 @ 2600/1179 |
|
Landing
Roll - Land (Ft/M) |
475/145 |
|
Landing
Roll - Water (Ft/M) |
600/183 |
| |
