Culver Aircraft Logo Culver NC41705
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Culver Cadet LFA Specifications

Powerplant Franklin  4AC-199-E3 90 hp
Propeller Sensenich  2 blade wood

Dimensions
Length   17' 8"
Height   5' 6"
Wingspan    27'
Wing area   120 sq ft
Wing loading   10.9 lb/sqft
Power loading   14.5 lbs/hp
Seats      2
Cabin length    26.5"
Cabin width at rear of seat  35.5"
Cabin width at front of seat  36"
Cabin height, seat to top  36"
Distance from rear of seat to rudder pedals  41"
Distance from rear of seat to front of seat  17"

Weights
Basic empty weight    850 lbs
Max gross weight   1305 lbs
Useful load     455 lbs
Max payload     335 lbs
Fuel capacity     20 gals (120 lbs)
Oil capacity     5 qts (8qts opt long range tank)
Baggage Capacity   50 lbs

Performance
Takeoff distance, ground roll  600 ft
Rate of Climb SL  800 fpm
Max level speed, SL  145 mph
Cruise speed @75%  120 mph
Service ceiling  17,500 ft
Landing distance, ground roll  400 ft

Limiting and Recommended speeds
VX (best angle of climb)  65 mph
VY (best rate of climb)  75 mph
VLE (max gear extended)  175 mph
VLO (max gear operating)  175 mph
VNO (max structural cruising)  145 mph
VNE (Never exceed)  175
VS1 (stall, clean)  45 mph
VSO (stall, landing config)  45 mph

Manufactures stated data, no other data currently available


Web Site Link for General Specifications
Specifications

Link for a Microsoft Flight Sim 2004 Model of the Culver Cadet

MSFlight Sim 2004 model