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Pilatus PC-21

Pilatus PC-21

Training Turboprop Aircrafts
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Basic Information
Name
Pilatus PC-21
Designation
Pilatus PC-21
Alternate Designation
JEPAS PC-21 (Swiss Air Force PC-21 training program)
Equipment Type
Training Turboprop Aircrafts
Manufacturer
Pilatus Aircraft
Date of Introduction
2007
Description

The Pilatus PC-21 is a new tandem tow-seat, low-wing swept monoplane developed by Pilatus Aircraft to meet the requirements of modern air forces over the next 30 years. The project was launched in January 1999 and the first PC-21 trainer was rolled out in 2002. The Swiss Federal Office for Civil Aviation (FOCA) awarded type certification on January 24, 2005. The PC-21 focuses in three areas: superior aerodynamic performance compared with any other turboprop on the market; a complex integrated training system; and a life-cycle costs not to exceed existing turboprop training systems such as PC-7 or PC-9. The resulting trainer is suitable for basic flying training; advanced flying training; and mission system management training in the fighter lead-in role. The Pilatus PC-21 is powered by a single Pratt & Whitney PT6A-68B turboprop rated at 1,600-shp. The engine drives a scimitar five blade graphite propeller. The PC-21 digital engine management system schedules power as a function of airspeed to give jet-like acceleration throughout the speed range and to provide a progressive and controllable power delivery at take-off and in the circuit. Standard equipment includes 0-0 (0 altitude and 0 airspeed) ejection seats, OBOGS, hydraulic ailerons and spoilers, six underwing stations, open architecture digital mission computer, automatic yaw compensation, pressurized refueling, anti-g system, and pressurized, stepped cockpit with birdstrike resistant canopy. The aircraft's structure is made primarily of aluminum and composite material. The cockpit is fitted with large fighter-like LCDs and is compatible with night vision goggles. To date, the Pilatus PC-21 trainer has been selected by the Air Forces of Singapore and Switzerland. The Royal Singapore Air Force (RSAF) ordered 19 PC-21 advanced turboprop trainers on November 3, 2006, as part of a training program which was awarded to Lockheed Martin to be carried out at the Royal Australian Air Force Base Pearce, north of Perth in Western Australia. The Swiss Air Force ordered six PC-21s (JEPAS PC-21) in January 2007 to provide training in support of the F/A-18C/D aircraft. First delivery was due by the end of 2007 with the training course expected to commence in March 2008.

Air & Air Defense Specifications
Crew 2
Max Speed 889.1 km/h
Range 1333.4 km
Wingspan 9.10 m
Overview (Deagel)
Group Training Turboprop Aircrafts
Status Active
Also Known As JEPAS PC-21 (Swiss Air Force PC-21 training program)
Origin Switzerland
Contractor Pilatus Aircraft
Initial Operational Capability (IOC) 2007
First Flight 2002
Total Production 269
Unitary Cost CHF 20.0 million
Specifications (Deagel)
Crew 2
External Stations 6
Number of Engines 1
Propeller Blades 5
Area — Wing Area 14.9 square meter
Dimensions — Height 3.9 meter
Dimensions — Length 11.2 meter
Dimensions — Wingspan 9.1 meter
G-load — Max Maneuvering Load Factor 8 g
G-load — Min Maneuvering Load Factor -4.00 g
G-load — Sustained Load Factor 3.7 g
Mass — Empty Weight 2,270 kilogram
Mass — Max Takeoff Weight 3,100 kilogram
Mass — Payload 1,150 kilogram
Performance — Landing Run Distance 900 meter
Performance — Max Range 720 nautical mile
Performance — Take Off Run Distance 725 meter
Power — Max Power at TakeOff 1,600 shp
Speed — Climb Rate 4,250 fpm
Speed — Stall Speed 81 knot
Speed — Top Speed at High Altitude 0.72 mach
Speed — Top Speed at Sea Level 323 knot
Gear (Deagel)
Item 1 Turboprop Engines: PT6A-68B (1)
Details
Country of Origin Switzerland
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
11.2 m
Width
9.1 m
Height
3.9 m
Weight
3100 kg
Operators (11)
France
United Kingdom
Spain
Australia
Canada
Jordan
Qatar
Saudi Arabia
Singapore
Switzerland
United Arab Emirates
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