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Pilatus U-28


Intelligence-Surveillance-Reconnaissance (ISR) Aircraft


Aviation / Aerospace

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Image from the United States DoD DVIDS imagery database; Public Release.

The U-28A is an ISR-centric U.S. special forces reworking of the civilian-minded Pilatus PC-12 turboprop-powered utility aircraft.



Authored By: Staff Writer | Last Edited: 5/14/2020 | Content ©www.MilitaryFactory.com
In the mid-2000s, during the height of American involvement in the Afghanistan and Iraq theaters of war, United States Special Operations COMmand - US SOCOM - required a budget-friendly (commercially-available) light utility aircraft capable of fulfilling very-mission-specific parameters for its special forces missions. The result was the reimagining of the Swiss-originated Pilatus PC-12 passenger/cargo aircraft to become the "U-28". Since their inception, the fleet has been used for a myriad of special-minded tasks including mission support through (manned) tactical Intelligence-Surveillance-Reconnaissance (ISR), Search and Rescue (SAR), and humanitarian operations support.

The PC-12 series has seen formal operations since introduction in 1994 and over 1,700 have been built to date - marking it a successful aircraft design for Swiss-based Pilatus Aircraft.

All of the form and function of the original civilian market PC-12 is retained in the U-28 including its single engine layout, crew/passenger cabin, low-mounted wing mainplanes, and single-rudder "T-style" tail unit. A retractable tricycle wheeled undercarriage allows for ground-running. Beyond inherent reliability and excellent performance from its nose-mounted turboprop, the U-28 also showcases short-field / rough-field capabilities.

Where differences end between the U-28 and its civilian market counterpart is in the installed equipment: the platform bristles with tactical communications sets, Electro-Optical (EO) sensors, protected data-links (DoD and NATO types support), real-time full-motion video processing, and survivability systems. These systems result in special protrusions emanating from the fuselage and wing members and not seen in the commercial model.

The U-28's crew consists of four personnel made up of two pilots, a Combat Systems Officer (CSO), and Tactical Systems Officer (TSO). The crew is seated side-by-side in a 2x2 arrangement in the cabin. The instrument panel includes an all-modern glass cockpit.

Power is served from a single Pratt & Whitney PT6A-67B turboprop engine installed at the nose and used to drive a four-bladed propeller unit in conventional "tractor" fashion. This provides the aircraft with a maximum speed of around 220 knots, a range out to 1,500 nautical miles, and a service ceiling up to 30,000 feet. Maximum Take-Off Weight (MTOW) reaches 11,000 lb.

The United States Air Force has operated as many as twenty-eight U-28A models with 14 currently (2020) noted as in-service with the branch. The 34th, 318th, and 319th Special Operations Squadrons are listed as key operators of the type while the 5th and 19th Special Operations Squadrons are charged with the types training.



May 2020 - U.S. SOCOM is intending to replace its in-service fleet of U-28 aircraft with the winner of the USAF's "Armed Overwatch" program.

Specifications



Year:
2006
Status
Active, In-Service
Crew
4
[ 28 Units ] :
Pilatus Aircraft - Switzerland
National flag of United States United States
- Airborne Early Warning (AEW)
- Reconnaissance (RECCE)
- Special Forces
Length:
47.24 ft (14.4 m)
Width:
53.31 ft (16.25 m)
Height:
13.94 ft (4.25 m)
(Showcased structural dimension values pertain to the Pilatus U-28 production model)
Empty Weight:
11,023 lb (5,000 kg)
MTOW:
11,023 lb (5,000 kg)
(Diff: +0lb)
(Showcased weight values pertain to the Pilatus U-28 production model)
1 x Pratt & Whitney PT6A-67B turboprop engine developing 1,200 horsepower driving a four-bladed propeller unit at the nose.
(Showcased powerplant information pertains to the Pilatus U-28 production model)
Max Speed:
253 mph (407 kph; 220 kts)
Service Ceiling:
30,003 feet (9,145 m; 5.68 miles)
Max Range:
1,740 miles (2,800 km; 1,512 nm)
Rate-of-Climb:
2,000 ft/min (610 m/min)
(Showcased performance values pertain to the Pilatus U-28 production model; Compare this aircraft entry against any other in our database)
None. Mission equipment consists solely of sensors and systems related to the airborne ISR role.
(Showcased armament details pertain to the Pilatus U-28 production model)
U-28 - Base Series Designation.
U-28A - Primary operational service model.
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