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Military Transport Aircraft ·Short Brothers

C-23 Sherpa

British short takeoff and landing military transport aircraft, developed in the late 20th century, extensively used for transporting cargo and personnel in regional military operations. Key figures: top speed 467 km/h, range 2,195 km, service ceiling 8,500 m, max takeoff weight 10,387 kg, built 60.

Short Brothers C-23 Sherpa military transport aircraft side profile drawing
Side profile · Short Brothers C-23 Sherpa · length 17.7 m
Short Brothers C-23 Sherpa military transport aircraft in flight
Max speed
467km/h
Range
2,195km
Produced
60units
Technical SpecificationsVersion: C-23A
Crew3 (2 pilots, cabin crew)
Length17.7 m (58.0 ft)
Wingspan22.8 m (74.7 ft)
Height5.0 m (16.2 ft)
Wing area42.1 m² (453.2 sqft)
Empty weight6,680 kg (14,727 lbs)
Max. takeoff weight10,387 kg (22,899 lbs)
Powerplant2 × Pratt & Whitney Canada PT6A-45-R 893 kW each
PerformanceVersion: C-23A
Maximum speed467 km/h (290 mph)
Operational range2,195 km (1,364 mi)
Service ceiling8,500 m (27,887 ft)
Climb rate6.0 m/s (19.7 ft/s)
Operators — 2026
No country is operating the C-23 Sherpa in 2026.
All Operators
🇩🇯 Djibouti· 🇵🇭 Philippines· 🇺🇸 United States

Description

The Short C-23 Sherpa is a twin-engine short takeoff and landing (STOL) military transport aircraft designed by Belfast-based Short Brothers, which was acquired by Bombardier in 1989. Developed from the Short SC.7 Skyvan, Short 330, and Short 360 family, the aircraft was produced from 1984 to 1997. The Sherpa won an early 1980s competition for a European Distribution System Aircraft (EDSA) to transport aviation parts in Western Europe. The first freighter variant flew on December 23, 1982. A total of 60 aircraft were procured for the U.S. armed forces.

Design

Featuring a square fuselage cross-section, the C-23 utilizes a twin tail and a full-width rear cargo door and ramp. The cabin measures 6.5 feet wide, 6.5 feet high, and 29 feet long, providing a cargo volume of 1,230 cubic feet and an 8,000 lb cargo capacity. Power is provided by two Pratt & Whitney Canada PT6A-45-R turboprop engines rated at 1,198 shp each, driving five-bladed Hartzell constant-speed propellers. The aircraft has a maximum takeoff weight of 22,900 lb, a maximum speed of 252 knots, a cruise speed of 228 knots, and a range of 1,185 nautical miles with a 7,000 lb payload.

Operational History

The C-23A entered U.S. Air Force service in 1985 with the Military Airlift Command at Zweibrücken Air Base, serving the EDSA role until retirement in November 1990. Retired aircraft were distributed to the USAF Test Pilot School, the U.S. Army, and the U.S. Forest Service. The U.S. Army and Army National Guard operated C-23B and C-23B+ variants, using them for intra-theater transport during the Iraq War (2003–2011). In 2001, a Florida Army National Guard C-23B crashed in Georgia due to a center-of-gravity shift, resulting in 21 fatalities. The U.S. Army retired the type in January 2014, transferring surplus airframes to the U.S. Forest Service, NASA, and international operators. Active international operators include the Philippine Army and the Djibouti Air Force. Estonia declined a proposed transfer in 2015 due to maintenance costs, while a planned purchase of eight upgraded aircraft by Brazil was canceled in 2020.

Variants

  • C-23A Sherpa: Twin-engine transport built for the U.S. Air Force based on the Short 330-UTT, featuring a strengthened cabin floor, a portside cargo door, and a hydraulic rear cargo door and ramp.
  • C-23B Sherpa: Twin-engine transport built for the Army National Guard, adding cabin windows, stronger landing gear, inward-opening rear paratroop doors, and an air-operable cargo ramp.
  • C-23B+ Super Sherpa: Modified civil Short 360 aircraft fitted with the twin tail and rear cargo ramp of the Sherpa to replace the original single vertical stabilizer.
  • C-23C: Upgraded C-23B and C-23B+ aircraft featuring modernized flightdeck avionics under the Avionics System Cockpit Upgrade program.
  • C-23D: Upgraded C-23C aircraft featuring modernized avionics under the Safety Avionics Modification program, of which only four were completed.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 23 July 2026. Suggest a change

Frequently Asked Questions

What type of aircraft is the C-23 Sherpa?
The Short Brothers C-23 Sherpa is a military transport aircraft aircraft developed by Short Brothers and entered service in 1984.
What is the maximum speed of the C-23 Sherpa?
The Short Brothers C-23 Sherpa has a maximum speed of 467 km/h (290 mph).
What is the range of the C-23 Sherpa?
The Short Brothers C-23 Sherpa has an operational range of 2,195 km (1,363 miles). This range can vary based on payload, altitude, and mission profile.
When did the C-23 Sherpa first fly?
The Short Brothers C-23 Sherpa made its first flight on August 06, 1984. It entered operational service in 1984.
How many C-23 Sherpa have been built?
Approximately 60 units of the Short Brothers C-23 Sherpa have been produced since it entered service in 1984.
What is the service ceiling of the C-23 Sherpa?
The Short Brothers C-23 Sherpa has a service ceiling of 8,500 meters (27,887 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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Latest Data Updates
  1. JUL 232026 Updated Sources and cross-references refreshed
  2. JUL 12026 Created Page created: C-23 Sherpa