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Specifications:
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Powerplant
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Lycoming O-360-C2A
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Horse Power @ RPM
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180 @ 2700 rpm
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Propeller – Fixed Pitch
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McCauley 1A200HFA
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Propeller Diameter
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72 in.
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Length
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23.0 ft.
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Height
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9.7 ft.
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Wingspan
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36.2 ft.
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Wing Area
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180 sq. ft.
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Wing Loading
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11.9 lb. / sq. ft.
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Power Loading
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11.9 lb. / HP
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Seats
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2, Tandem
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Cabin Length
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8 ft. 10 in.
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Cabin Width
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2 ft. 6 in.
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Cabin Height
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3 ft. 11 in.
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Empty Weight
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1392 lbs.
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Maximum Gross Weight
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2150 lbs.
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Useful Load
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757 lbs.
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Payload with Full Fuel
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541 lbs.
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Fuel Capacity, Standard
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36 gal. (35 gal. Usable)
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Oil Capacity
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8 quarts
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Baggage Capacity
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100 lbs. (10.4 cubic feet)
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Performance:
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Takeoff Distance, Ground Roll
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490 ft.
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Takeoff Distance Over 50-ft Obstacle
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1025
ft
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Maximum Demonstrated Crosswind
Component |
17 kts. |
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Rate of Climb, Sea Level
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1075 fpm
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Maximum Level Speed, Sea Level
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140 mph
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Cruise Speed / Endurance with 45
Minute Reserve @ 75% Power
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130 mph / 2.7 hours
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Fuel Consumption @
Altitude
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10.3 gph @ 5000 ft.
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Speed / Endurance with 45 Minute Reserve @ 55% Power |
112 mph / 3.8 hours |
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Fuel Consumption @
Altitude
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7.7 gph @ 5000 ft.
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Service Ceiling
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17000 ft.
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Landing Distance over 50-ft. Obstacle
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1235 ft.
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Landing Distance, Ground Roll
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420 ft.
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Airspeeds:
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VX (Best Angle)
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61 mph
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VY (Best Rate)
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80 mph
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VA (Design Maneuvering)
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115 mph
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VF (Maximum Flap Speed)
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100 mph
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VNO (Maximum Structural
Cruising)
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130 mph
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VNE (Never Exceed)
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162 mph
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VR (Rotation, 14° flaps)
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53 mph
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VS1 (Stall, Clean)
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57 mph
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VS0 (Stall, Full Flaps)
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52 mph
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