| 1963 Piper Comanche 250 |
| The Piper PA-24 Comanche is a four-seat, low-wing, all-metal, light aircraft with retractable landing gear that was first flown in 1957. Together with the twin-engine version of the same airframe, the Twin Comanche, it made up the core of the Piper aircraft line-up until 1972 when the production lines for both aircraft were wiped out in a flood. |
| Specifications: Engine make/model: Lyc. O-540-A1A Horsepower: 250 TBO: 2000 Propeller: Const. spd.3-Blade Hartzell Propeller Landing gear type: Tri/Retr. Gross weight (lbs.): 3000 Empty weight (lbs.): 1778 Useful load (lbs.): 1223 fuel (gals.): 60 Wingspan: 36 ft. Overall length: 24 ft. 9 in. Height: 7 ft. 3 in. Wing area (sq. ft.): 178 Seating capacity: 4 Cabin width (in.): 45 Cabin height (in.): 47 Baggage capacity (lbs.): 200 Perfomance : Cruise speed (knots): 75% power: 157 65% power: 160 Max range 75% power: 643 65% power: 960 Fuel consumption (gph): 75% power: 13.1 65% power: 12.3 Estimated endurance (65% power ): 6 hrs. Stall speed (gear, flaps down) (knots): 58 Best rate of climb (fpm): 1350 Service ceiling (ft.) 22,000 Takeoff ground roll (ft.): 1095 Landing ground roll (ft.): 885 |
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