WMU College of Aviation

PA-34 Seneca

The Piper Arrow serves the College of Aviation's needs as a reliable and efficient aircraft for use as a complex single-engine trainer. With its Garmin GNS 430/530 cockpit the Arrow provides a good mix of traditional and advanced instruments.

Number in Fleet

2

Primary Use

Complex Trainer, Commercial License and CFI

Engine

Textron Lycoming IO-360-C1C6 (200BHP)

Fuel Capacity

72 gal

Weight

1789 lbs (Standard Empty)

2750 lbs (Max Takeoff)

969 lbs (Max Useful Load)

Dimensions

27'9" Long

7'10" High

35'5" Wing Span

170 ft² Wing Area

Speed

145 kts (Max @ Sea Level)

137 kts (Cruise, 80% Power @ 10,000 ft)

Stall Speed

55 kts (Flaps Down, Power Off)

Cruising Range

880 nm (55% Power @ 9,000 ft)

Max Operating Altitude

16,200 ft

Takeoff Distance

1,600 ft (Total Distance over 50 ft Obstacle)

Landing Distance

1,520 ft (Total Distance Over 50 ft Obstacle)