Piper Seneca

Piper Seneca

As the only approved Multi Engine Aircraft for miles around our Seneca is used for Commercial, Multi and Instrument courses.

Below are some generic figures not to be used for any planning of any sort.

Crew: 1 Pilot

Capacity: Five or six passengers
Length: 28 ft 7.44 in (8.72 m)
Wingspan: 38 ft 10.87 in (11.86 m)
Height: 9 ft 10.8 in (3.02 m)
Wing area: 208.7 ft² (19.39 m²)
Airfoil: laminar flow NACA 652-415
Empty weight: 3212 lb (1457 kg)
Loaded weight: 4773 lb (2165 kg)
Max. take-off weight: 4750 lb (2155 kg)
Powerplant: 2 × Continental TSIO-360RB and LTSIO-360RB 6-cylinder

Air-cooled horizontally-opposed piston engine: 220 hp (164 kW) each

Piper Seneca Performance.

Never exceed speed: 204 knots (378 km/h 235 mph)

Maximum speed: 204 knots (378 km/h 235 mph)
at 23000 ft (7000 m)
Cruise speed: 188 knots (348 km/h 216 mph) econ cruise at 25000 ft (7600 m)
Stall speed: 61 knots (113 km/h 70 mph)
wheels and flaps down
Range: 870 nmi (1611 km 1000 mi) max fuel econ cruise at 18000 ft (5500 m) no reserves
Service ceiling: 25000 ft (7620 m)
Rate of climb: 1550 ft/min (7.87 m/s)
Wing loading: 21.2 lb/ft² (104 kg/m²)

Power/mass: 0.1 hp/lb (164 W/kg)

Take a look at our other Aircraft