Overview
The Pilatus PC-21 is an advanced turboprop trainer developed to prepare military pilots for front-line jet aircraft. Designed to reduce training costs while maintaining high performance, it integrates modern avionics and mission simulation systems. The aircraft has been adopted by several air forces worldwide.
Specifications
Units
- Engine
- 1 × Pratt & Whitney PT6A-68B
- Engine type
- Turboprop
- Power
- 1,600 shp · 1,193 kW
- Avionics
- BARCO and Meggitt Avionics , Becker Avionics BXT6500 ADS-B transponder
- Wing tips
- No winglets
- Seats
- 2
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 36 ft 10 in · 11.22 m
- Tail height
- 12 ft 4 in · 3.75 m
- Fuselage diameter
- 3 ft 3 in · 1.00 m
- Wing span
- 29 ft 11 in · 9.11 m
- Baggage volume
- —
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 9,350 lb · 4,250 kg
- Max landing weight
- 8,900 lb · 4,050 kg
- Max payload
- 2,550 lb · 1,150 kg
- Fuel capacity
- 150 gal · 500 L · 400 kg (Jet A)
- Max cruise speed
- 370 kt · 426 mph · 685 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- 81 kt · 93 mph · 150 km/h
- Range
- 720 nm · 830 mi · 1,330 km
- Fuel burn
- 1.13 nm/gal · 0.55 km/L
- Ceiling
- 25,000 ft · 7,600 m
- Rate of climb
- 4,250 ft/min · 22 m/s
- Takeoff distance
- 2,400 ft · 730 m
- Landing distance
- 2,950 ft · 900 m
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