CESSNA 150 AEROBAT

Manual del avión

• Crew: 1
• Capacity: 1 passenger
• Length: 7.54 m
• Wingspan: 10.16 m
• Height: 2.6 m
• Wing area: 15 m²
• Empty weight: 504 kg (1,111 lb)
• Maximum takeoff weight: 1,600 lb 730 kg
• Powerplant: 1 × liter four cylinder opposed air-cooled Continental O-200A.
• Power: 75 kW (100 hp, 101 hp)
• Propellers: 1 × two-bladed fixed pitch motor.


• Never exceeded speed (Vne): 259 km / h (161 mph, 140 kt)/li>
• Maximum operating speed (VNO): 261 kilometer per hour (141 kt).
• Cruising speed (Vc): 152 km / h (94 mph; 82 kt)
• Stall speed (Vs): 78 km / h (48 mph; 42 kt)
• Scope: 589 km
• Flight ceiling: 4,300 m (14,108 ft)
• Rate of climb: 3.40 m / s (670 ft / min)

GA 7 COUGAR

Manual del avión

• Crew: 1
• Capacity: 3 passengers
• Length: 28 ft 8 in (8.74 m)
• Wingspan: 36 ft 10 in (11.23 m)
• Height: 10 ft 4 in (3.15 m)
• Wing area: 184 sq ft (17.1 m2)
• Empty weight: 2,569 lb (1,165 kg)
• Gross weight: 3,800 lb (1,724 kg)
• Powerplant: 2 × Lycoming O-320-D1D four cylinder, horizontally-opposed aircraft engines, 160 hp (120 kW) each


• Maximum speed: 168 kn (193 mph; 311 km/h)
• Cruise speed: 160 kn (184 mph; 296 km/h) true airspeed
• Stall speed: 63 kn (72 mph; 117 km/h) calibrated airspeed, flaps down
• Never exceed speed: 188 kn (216 mph; 348 km/h) indicated airspeed
• Minimum control speed: 61 kn (70 mph; 113 km/h) indicated airspeed
• Range: 1,170 nmi (1,346 mi; 2,167 km) maximum economy with no reserves
• Service ceiling: 17,400 ft (5,300 m)
• Rate of climb: 1,150 ft/min (5.8 m/s)
• Wing loading: 20.65 lb/sq ft (100.8 kg/m2)
• Power/mass: 11.9 lb/hp (0.14 kg/kW)