Pilatus PC-7 Mk II

The turboprop trainer built for reliable basic flight instruction.

Overview

Pilatus Switzerland 1978–Present $3.9 million

The Pilatus PC-7 Mk II is an updated version of the original PC-7 military trainer. Designed for basic flight training, it combines simplicity with modern avionics. The aircraft has been widely exported for military training programs.

Specifications

Units
Engine
—
Engine type
-
Power
700 hp · 522 kW
Avionics
Honeywell Avionics
Wing tips
No winglets
Seats
2
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
13,100 lb  ·  5,950 kg
Max landing weight
—
Max payload
1,050 lb  ·  450 kg
Fuel capacity
Max cruise speed
157 kt  ·  181 mph  ·  291 km/h
Maximum speed
—
Cruise speed
—
Approach speed
—
Range
—
Fuel burn
9.60 nm/gal  ·  4.70 km/L
Ceiling
—
Rate of climb
—
Takeoff distance
3,850 ft  ·  1,180 m
Landing distance
2,600 ft  ·  800 m
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Operational Context

Pilatus PC-7 Mk II — basic turboprop trainer

The PC-7 first flew in the 1970s as a turboprop-powered military trainer derived from the PC-3. The Mk II variant introduced in the 1990s incorporated structural refinements and a more powerful engine while retaining the proven airframe. It entered service with multiple international air forces.

Powered by a Pratt & Whitney Canada PT6A-25C turboprop engine producing approximately 700 shaft horsepower, the PC-7 Mk II cruises at about 270 knots (500 km/h). Maximum takeoff weight is roughly 6,000 pounds (2,700 kg). The aircraft features a tandem cockpit and limited aerobatic capability for training purposes.

The PC-7 Mk II is used for ab initio and basic military pilot training. Its straightforward systems and reliable performance make it well suited to early training stages. The type remains a widely recognized turboprop trainer in global service.