Pilatus PC-21

Summary

Category	Training aircraft
Origin country	🇨🇭 Switzerland
First flight	1 July 2002
Year of introduction	2008
Number produced	211 units

Description

The Pilatus PC-21 is a military training aircraft manufactured by Pilatus Aircraft Ltd. It was developed as a successor to the PC-7, with upgraded features and enhanced capabilities. Designed primarily for training purposes, the PC-21 is equipped with advanced avionics, a fully digital glass cockpit, and a state-of-the-art mission system. With a high-performance turboprop engine, it offers exceptional maneuverability and endurance. The aircraft has been widely used by various air forces around the world for military pilot training, as well as for advanced operational training and light attack missions. Its versatility and adaptability make it a reliable platform for pilots to acquire essential skills and experience.

Technical specifications

Version: PC-21
Maximum speed	624 km/h (388 mph)
Wing area	15.2 m² (163.8 sqft)
Wingspan	9.1 m (29.9 ft)
Height	3.8 m (12.3 ft)
Length	11.2 m (36.8 ft)
Service ceiling	11580 m (37992 ft)
Empty weight	2270 kg (5004 lbs)
Max. takeoff weight	4250 kg (9370 lbs)
Climb rate	20.32 m/s (66.7 ft/s)
Powerplant	1 × turboprop Pratt & Whitney Canada PT6A-68B delivering 1193 kW