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Piper Seneca III - AeroClub




Class 1


Piper Seneca III
Climb Chart
Climb Chart
Descent Chart
Descent Chart
Continental engines
870 nm range
5 pax, 500 lbs cargo capacity

One of the most successful six place light twin aircraft since its introduction, the PA-34 Seneca is a twin engine development of the Cherokee Six.

In 1981, the PA-34-220T Seneca III was introduced, with an engine upgrade to Continental TSIO-360-KB engines producing 220HP. The horsepower increase, with the new engines' limit of 2800 rpm combined for much improved climb and cruise performance. The aircraft's gross weight was increased to 4,570 lb (2,073 kg) for takeoff and 4,513 lb (2,047 kg) for landing.

General Information
Length8.69 m
Wingspan11.85 m
Height3.02 m
EngineTSIO-360-KB
Cruise Speed188 kts
Service Ceiling25,000 ft
Gross Weight2 t
Capacity5 pax | 500 lbs
Crew1 pilot
Price1M EUR
ManufacturerPIPER
PicturesAirliners.net
Operating Information
OEW3,212 lbs
MTOW4,750 lbs
Fuel Capacity122 gal
Fuel Weight820 lbs
Long Range Altitude18,000ft
Long Range Speed197 kts
Max Speed204 kts
Range (MLoad...MFuel) 870... 870
Engine Thrust2x220 HP
Takeoff RWY Length (Min)920 ft
Takeoff RWY Length (Max)1,210 ft
Landing RWY Length1,400 ft
V Rotate / Flaps85kts / 25 deg
V Approach / Flaps85kts / 40 deg
Max climb rate1700 ft/min
Max descent rate-1500 ft/min
 


Liveries and Downloads

MSFS 2004


Piper Seneca IIIMSFS 2004