PC-21

INTRODUCTION

• Single-turboprop
• Low wing swept monoplane
• Advanced trainer
• Stepped tandem cockpit
• Manufactured by Pilatus in Switzerland

General characteristics

Crew: Two. (student & instructor)

Length: 11.233 m
Wingspan: 9.108 m
Height: 3.749 m
Wing area: 15.221 m²
Empty weight:2,270 kg
4 Air-To-Ground mounts

Performance

Maximum speed: 685 km/h
Stall speed: 170 km/h
Range: 1,333 km
Rate of climb: 1,219 m/min
Wing loading: 208 kg/m²

PC-21 DESIGN ( OUTSIDE )

• Turbo-powered engine with five propellers
• Tandem cockpit
• Low wings
• Conventional landing gears
• Standard tail

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PC-21 ( INSIDE )

• Three large ( LCD ) screens
• Head-up-displays ( HUD )
• Hands on throttle and stick (HOTAS)
• Zero zero ejection seats

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FIRST RELEASED

• Swiss Air Force ( 2008 )
• Republic of Singapore Air Force ( 2008 )
• UAE Air Force ( 2010 )

Questions?