Overview
The Pilatus PC-6 Turbo Porter is a single-engine utility aircraft renowned for exceptional short takeoff and landing capability. Designed for operations in remote and mountainous regions, it has served military and civilian operators worldwide. The aircraft is noted for its durability and adaptability.
Specifications
Units
- Engine
- 1 × Pratt & Whitney PT6A-27
- Engine type
- Turboprop
- Power
- 550 shp · 410 kW
- Avionics
- Honeywell Avionics Suite
- Wing tips
- No winglets
- Seats
- 10
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- —
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- —
- Baggage volume
- 1 ft³ · 0.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 13,500 lb · 6,100 kg
- Max landing weight
- —
- Max payload
- 1,550 lb · 700 kg
- Fuel capacity
- Max cruise speed
- 83 kt · 96 mph · 154 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- —
- Fuel burn
- 2.92 nm/gal · 1.43 km/L
- Ceiling
- —
- Rate of climb
- —
- Takeoff distance
- 190 ft · 60 m
- Landing distance
- 130 ft · 40 m
Gallery
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Private Single Engine
ICAO: PC12
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