Pilatus Switserland

Pilatus PC-21 Trainer

Pilatus PC-12 Trainer

Switserland Aircraft

Pilatus PC-21 Trainer

Pilatus

The Pilatus PC-21 is a turboprop-powered advanced trainer with a stepped tandem cockpit. It is manufactured by Pilatus Aircraft of Switzerland.

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In November 1997, Pilatus flew a modified PC-7 Mk.II in order to test improvements for a prospective next generation turboprop trainer. As a result of these tests, Pilatus elected to fund the development of a new training system in November 1998; development of the new trainer, designated as the PC-21, formally started in January 1999.[2] The PC-21 would be developed and certified as a completely new training system, aimed at meeting future military customers’ specifications in terms of capability and life-cycle costs for the next three decades.

Design

The Pilatus PC-21 is an advanced single-engine trainer aircraft; it is often referred to by Pilatus as being the “Twenty-first Century Trainer”.[3][4] The type can be applied for various training capacities, including basic flying training, advanced flight training, full mission management training, and embedded simulation/emulation. In order to perform these functions, the aircraft possesses a powerful, flexible, and cost-effective integrated training system; providing sufficient ease of use for inexperienced pilots while posing greater challenge to advanced pilots.[8] According to Pilatus, upon product launch, the PC-21 possessed “superior aerodynamic performance when compared with any other turboprop trainer on the market”

RoleAdvanced trainer aircraft
ManufacturerPilatus Aircraft
DesignerPilatus Aircraft
First flight1 July 2002
IntroductionApril 2008
StatusActive service
Primary usersSwiss Air Force
Republic of Singapore Air Force
Royal Australian Air Force
Royal Saudi Air Force
Produced2002–present
Number built211

 

Operators

 Australia
 France
 Jordan
 Qatar
 Saudi Arabia
 Singapore
  • Republic of Singapore Air Force: launch customer; operates nineteen in Australia on Basic Wings Course (BWC) as part of a contract for availability, together with Lockheed Martin and Hawker Pacific.
 Spain
  Switzerland
 United Arab Emirates
 United Kingdom

General characteristics

  • Crew: 2
  • Length: 11.233 m (36 ft 10 in)
  • Wingspan: 9.108 m (29 ft 11 in)
  • Height: 3.74 m (12 ft 3 in)
  • Wing area: 15.221 m2 (163.84 sq ft)
  • Empty weight: 2,270 kg (5,004 lb)
  • Max takeoff weight: 3,100 kg (6,834 lb) aerobatic
4,250 kg (9,370 lb) normal

Performance

Performance

  • Maximum speed: 685 km/h (426 mph, 370 kn)
  • Stall speed: 170 km/h (110 mph, 92 kn) gear and flaps up (20 km/h (12 mph; 11 kn) less with flaps and gear down)
  • Range: 1,333 km (828 mi, 720 nmi)
  • Service ceiling: 11,580 m (37,990 ft)
  • g limits: +8.0 4.0 aerobatic / +5.0 to 2.5 utility
  • Rate of climb: 20.317 m/s (3,999.4 ft/min)
  • Wing loading: 208 kg/m2 (43 lb/sq ft)
  • Power/mass: 0.39 kW/kg (0.24 hp/lb)

Related

Aircrafttoaal encyclopedia

The company has mostly produced aircraft for niche markets, in particular short takeoff and landing (STOL) aircraft as well as military training aircraft. During the 1950s and 1960s, Pilatus developed on a short takeoff and landing (STOL) light civil transport aircraft, the PC-6 Porter. During 1973, it was decided to restart work on the PC-7 programme; it entered production as the PC-7 Turbo Trainer. In 1979, Pilatus acquired Britten-Norman, constructor of the Britten-Norman Islander and Britten-Norman Defender aircraft. During the 1980s, it developed the PC-9, an improved derivative of the PC-7.