Overview
The Pilatus PC-9 M is a turboprop military trainer designed for basic and intermediate pilot training. Developed from the earlier PC-7, it introduced improved aerodynamics and avionics. The aircraft has been widely exported to air forces worldwide.
Live Fleet Activity (PC9)
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Specifications
Units
- Engine
- 1 × Pratt & Whitney PT6A-62 turboprop
- Engine type
- Turboprop
- Power
- 1,150 shp · 858 kW
- Avionics
- Head Up Display (HUD) and Electronic Flight Instrumentation System (EFIS)
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 33 ft 5 in · 10.18 m
- Tail height
- 10 ft 8 in · 3.26 m
- Fuselage diameter
- 3 ft 7 in · 1.10 m
- Wing span
- 33 ft 5 in · 10.19 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 7,050 lb · 3,200 kg
- Max landing weight
- —
- Max payload
- 2,300 lb · 1,050 kg
- Fuel capacity
- 240 gal · 900 L · 700 kg (Jet A)
- Max cruise speed
- 320 kt · 368 mph · 593 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 77 kt · 89 mph · 143 km/h
- Range
- 860 nm · 990 mi · 1,590 km
- Fuel burn
- 8.14 nm/gal · 3.98 km/L
- Ceiling
- 37,990 ft · 11,600 m
- Rate of climb
- 3,880 ft/min · 20 m/s
- Takeoff distance
- 1,300 ft · 400 m
- Landing distance
- 2,250 ft · 690 m
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