Overview
Piper PA-28 Arrow — retractable-gear single-engine aircraftThe Arrow first flew in 1967 and entered service shortly thereafter. It retained the low-wing configuration of the Cherokee family. Retractable landing gear provided higher cruise efficiency.A Lycoming piston engine producing approximately 200 horsepower powered the Arrow. Cruise speed approached 140 knots (259 km/h). Maximum takeoff weight exceeded 2,700 pounds (1,225 kg).The Arrow became widely used for commercial pilot training. Its systems introduced pilots to more complex aircraft operations. Many examples remain active today.
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Specifications
- Engine
- 1 × Lycoming IO 360 C1C6
- Engine type
- Piston
- Power
- 200 hp · 149 kW
- Avionics
- Garmin G500 TXi
- Wing tips
- No winglets
- Seats
- 4
- Crew
- —
- Cabin width
- 3 ft 6 in · 1.06 m
- Cabin height
- 3 ft 11 in · 1.20 m
- Cabin length
- 7 ft 3 in · 2.20 m
- Exterior length
- 24 ft 7 in · 7.50 m
- Tail height
- 7 ft 10 in · 2.40 m
- Fuselage diameter
- 3 ft 11 in · 1.20 m
- Wing span
- 35 ft 5 in · 10.80 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 2,750 lb · 1,250 kg
- Max landing weight
- —
- Max payload
- 950 lb · 450 kg
- Fuel capacity
- 70 gal · 300 L · 200 kg (AvGas)
- Max cruise speed
- 148 kt · 170 mph · 274 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 47 kt · 54 mph · 87 km/h
- Range
- 880 nm · 1,010 mi · 1,630 km
- Fuel burn
- 28.74 nm/gal · 14.06 km/L
- Ceiling
- 15,000 ft · 4,600 m
- Rate of climb
- 1,000 ft/min · 5 m/s
- Takeoff distance
- 1,600 ft · 490 m
- Landing distance
- 1,520 ft · 460 m
Gallery