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Library > Fact Sheets > U-28A
U-28A
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Printable Fact Sheet
Mission
The U-28A utility aircraft provides intra-theater support for special operations forces.
Features
The U-28A is the Air Force variant of the Pilatus PC-12 and was selected for its versatile performance characteristics and ability to operate from short and unimproved runway surfaces. The U-28A is also certified to land on dirt and grass strips.
Due to it's efficient design and the use of a single engine, the U-28A's direct operating cost is about a third less than a comparable multi-engine aircraft and nearly half that of the nearest comparable jet.
The aircraft is equipped with weather radar and a suite of advanced communications and navigation gear.
General Characteristics
Primary Function: Intra-theater support for special operations forces
Builder: Pilatus
Power Plant: One Pratt & Whitney PT6A-67B turboprop
Thrust: 1605 shaft horsepower flat-rated to 1200 shp.
Length: 47 feet, 3 inches
Height: 14 feet
Wingspan: 53 feet, 3 inches
Max Cruise Speed: 270 knots true airspeed
Max Payload: 2,973 lbs.
Ceiling: 30,000 feet
Maximum Takeoff Weight: 9,920 lbs.
Ground Roll: 1,475 ft. at max takeoff weight
Range: 1,513 nautical miles
Crew: Two pilots. However, the aircraft can be flown by one.
Date Deployed: August 2005
Unit Cost: 3.5 million plus cost of upgrades
Inventory: 6
Point of Contact
Air Force Special Operations Command, Public Affairs Office, 229 Cody Ave., Suite 103; Hurlburt Field, FL 32544-5312; DSN 579-5515 or (850) 884-5515; email: afsoc.pa@hurlburt.af.mil
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