PA-34-200T SENECA

The PA-34-200T Seneca II is a twin-engine aircraft with two Continental TSIO-360-RB engines, each producing 220 hp. Key specifications include a maximum takeoff weight of 4,750 lbs, a service ceiling of 25,000 ft, and a maximum speed of 204 knots (235 mph). It can carry 1 crew member and 5 or 6 passengers.

General characteristics

• Crew: 1
• Passengers: 5-6
• Length: 28 ft 8 in
• Wingspan: 38 ft 11 in
• Height: 9 ft 11 in
• Wing area: 208.7 sq ft
• Empty weight: 3,212 lbs
• Max takeoff weight: 4,750 lbs

Performance

• Engines: 2 x Continental TSIO-360-RB, 220 hp each
• Maximum speed: 204 kn (235 mph) at 23,000 ft
• Cruise speed: 188 kn (216 mph) in economy cruise
• Stall speed: 61 kn (70 mph) with wheels and flaps down
• Range: 870 nmi (1,000 mi) with maximum fuel
• Service ceiling: 25,000 ft
• Rate of climb: 1,550 ft/min
• Wing loading: 21.2 lb/sq ft
• Power/mass: 0.1 hp/lb