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Performance:
SPEED
Maximum at Sea Level...............................................................
Cruise, 80% Power at 6000 Ft...................................................
CRUISE
Using recommended lean mixture with fuel allowance for engine start, taxi,
takeoff, climb and 45 minutes reserve.
75% Power at 6000 Ft.................................................. Range
88 Gallons (333 L) Usable Fuel .....................................Time
RATE OF CLIMB AT SEA LEVEL............................................................
SERVICE CEILING.................................................................................
TAKEOFF PERFORMANCE:
Ground Roll...............................................................................
Total Distance Over 50 Ft. Obstacle...........................................
LANDING PERFORMANCE:
Ground Roll...............................................................................
Total Distance Over 50 Ft. Obstacle............................................
STALL SPEED:
Flaps Up, Power Off..................................................................
Flaps Down, Power Off..............................................................
MAXIMUM WEIGHT:
Ramp........................................................................................
Takeoff.....................................................................................
Landing.....................................................................................
STANDARD EMPTY WEIGHT................................................................
MAXIMUM USEFUL LOAD....................................................................
BAGGAGE ALLOWANCE......................................................................
WING LOADING: Lbs/Sq Ft...................................................................
POWER LOADING: Lbs/HP...................................................................
Engine:
FUEL CAPACITY...................................................................................
OIL CAPACITY....................................................................................... ENGINE: Textron Lycoming...................................................................
230 BHP at 2400 RPM
PROPELLER: Diameter 3-blade..........................................................
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