The Short 330 was developed by Short Brothers of Belfast from their earlier Short SC.7 Skyvan STOL utility transport. The 330 has a longer wingspan and fuselage than the Skyvan, while retaining the Skyvan's square shaped fuselage cross section, allowing it to carry up to 30 passengers while retaining good short field characteristics. The 330 entered commercial service in 1976.3
In addition to the passenger aircraft, Shorts also planned two freight versions. The Short 330-UTT (for Utility Tactical Transport) was a military transport version fitted with a strengthened cabin floor and paratroop doors,4 which was sold in small numbers, primarily to Thailand, which purchased four. The Short Sherpa was a freighter fitted with a full-width rear cargo door/ramp. This version first flew on 23 December 1982,5 with the first order for 18 aircraft being placed by the United States Air Force in March 1983. These aircraft were assigned to Military Airlift Command (MAC) for the European Distribution System Aircraft (EDSA) role, flying cargo and personnel between United States Air Forces in Europe (USAFE) air bases.6 Eventually, 60 would be procured by for the U.S. armed forces and serve well into the 21st century. The C-23 Sherpa was the winner of a competition to enhance cargo delivery in that theater.7 One of its competitors as that time was the CASA C.212 Aviocar.8
The Sherpa's cabin is 6.5 ft (1.98 m) wide, 6.5 ft (1.98 m) high and 29 ft (8.84 m) long.9 It offers a cargo volume of 1,230 cu ft (34.83 m3), with a cargo capacity of 8,000 lb (3,629 kg).10 The Sherpa is also capable of operating from unpaved runways and making short takeoff and landings (STOL).11
In U.S. military service, the Short 330 was designated C-23A Sherpa. The C-23B Sherpa is similar to the C-23A, but with cabin windows.12 The C-23B+ Short 360 derivative was created by replacing the rear fuselage of Short 360s obtained on the second-hand market with the twin tail and rear loading ramp of the Short Sherpa.
The C-23 was produced at the Short Brothers' facility in Belfast, Northern Ireland.13
In 2024, De Havilland Canada’s did a study to evaluate returning the C-23 Sherpa to production, noting that the aviation market had seen other succesfull revivals such as the Twin Otter and CL-415 (DHC-515 Firefighter).14
The C-23 served with USAF starting in the 1980s, and later the U.S. Army. It was retired from the USAF in 1990 and the Army until 2014.
The C-23A Sherpa entered service with the United States Air Force in Europe in 198515 based at Zweibrücken Air Base. It continued in use in the EDSA role until November 1990 with the post-cold war force reductions.16 All the Sherpas returned to the United States; three aircraft were transferred to the USAF Test Pilot School at Edwards AFB, eight aircraft went to the U.S. Army and the remaining seven to the U.S. Forest Service. The Test Pilot School's aircraft were retired in 1997.17
The eight former USAF aircraft were used for test duties at different units; two were re-designated as JC-23A.18
The Army purchased four civil Short 330 aircraft to replace the de Havilland Canada C-7 Caribou being used to support the Kwajalein Missile Range. These were not given a C-23 designation, and were retired in 1992.19 In 1988, the Army ordered ten new-build Short 330s designated C-23B to replace the DHC C-7 Caribou used by the U.S. Army National Guard Aviation and Repair Activity Depots. In 1990, a further six were ordered.20
When the Army wanted 20 more C-23s in 1990 the production line had closed; second-hand Short 360 aircraft were purchased instead. Designated C-23B+, these were modified from the original single tail to the twin-tail and cargo ramp of the other C-23Bs.21 In 1994, another eight aircraft were converted to replace the de Havilland Canada UV-18 Twin Otters used in Alaska.22 (which was also out of production since 1988)23
During Iraq War (2003–2011), the C-23 served the Army's intra-theater needs of cargo and personnel transport. It provided an economic alternative for transporting some 20 people or three pallets of cargo when speed was not critical.24
As part of the U.S. Army's Constant Hawk intelligence gathering program, five Short 360s were modified for use in Iraq and flew in theater between 2006 and 2011. A further two modified aircraft collided in mid-air before delivery to Iraq. The Constant Hawk aircraft were not given a military designation.25
On 13 June 2007, the Alenia C-27J was selected to replace the C-23 in U.S. Army service.2627 A total of 43 C-23s were in service with the U.S. Army as of November 2008 (all US C-27 aircraft at that time were transferred to the US Coast Guard in 2012 due to budget shortfalls).28 The C-23 Sherpa was retired from the Army National Guard in January 2014.29 As part of the National Defense Authorization Act for Fiscal Year 2014, 8 C-23s may be transferred to the State of Alaska to operate from short rural runways for search-and-rescue and medium-lift missions.30
While the US Army does not operate many fixed wing aircraft besides the Sherpa (due to Key West Agreement), they lost a C-23B in 2001 in Georgia, USA, and 21 died.3132 This was the worst peacetime aviation disaster of the U.S. National Guard.33
On 3 March 2001, a C-23B Sherpa belonging to the 171st Aviation Regiment of the Florida Army National Guard was carrying 18 construction workers of the Virginia Air National Guard from Hurlburt Field, Florida to Naval Air Station Oceana, Virginia. The pilot left the flight deck to use the aft bathroom. His weight in the tailcone shifted the center of gravity sufficiently that the airplane became unstable when a patch of severe turbulence was encountered. The violent g-force shifts then encountered rendered the crew unconscious and caused the breakup of the aircraft in flight near Unadilla, Georgia, killing the 21 persons on board.34 Later calculations determined that the aircraft had been loaded outside its operating envelope at the start of the flight.
The C-23 was retired from Army National Guard service in 2014, having served with distinction in such missions as disaster relief and transport, earning the distinction of being a "workhorse" aircraft.35
Several surplus aircraft were sold to United States operators,36 who used them to transport equipment and crews to remote work sites.
In 2014 the Army transferred more than dozen C-23 to the U.S. Forestry Service.37
NASA operates one C-23 for atmospheric research from Wallops Flight Facility.3839
In December 2014, it was announced that US would supply eight aircraft to Estonia, Djibouti, and Philippines.4041 Estonia ended up not taking the Sherpa, a decision they reached in 2015 because they could not afford the maintenance, despite the low initial cost procuring of the aircraft. Also, the landing and take off ability of the C-23 was not short enough for their requirement.42 The Estonians were operating two Antonov An-2, a single engine biplane transport known for its low stall speed.43 In 2019, the Estonian Air Force received PZL C-145 instead which was a better match for their requirement, they were donated from the USAF which was retiring its fleet.44
Brazil briefly considered procuring up to eight upgraded C-23 Sherpa in the late 2010s, for service in the 2020s; the aircraft would be upgraded with new radars, TCAS, and night vision and approved the purchase.4546
The Brazilian Army Aviation had interest in acquiring eight Sherpa planes to supply its Special Border Platoons in the Amazon. A presidential decree allowed the army to possess fixed-wing aircraft in 2020, but it was revoked just two days after its publication. The acquisition was harshly opposed by air force officers and even some army officers. They considered the heavy expenditure on these aircraft inopportune at a time of scarce resources, preferring that investment be made in the FAB's existing planes.474849
Former USAF and US Army aircraft have been sold to civil operators including:
Data from Jane's All the World's Aircraft 1988–198964
General characteristics
Performance
Related development
Aircraft of comparable role, configuration, and era
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157 kn (181 mph; 291 km/h) at 21,000 lb (9,525 kg) AUW at 10,000 ft (3,048 m) ↩
90 kn (104 mph; 167 km/h) flaps and gear up ↩
669 nmi (770 mi; 1,239 km) with 5,000 lb (2,268 kg) payload, max fuel, reserves for 45 minute hold and 43 nmi (49 mi; 80 km) diversion ↩