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History Brief, by Johan Visschedijk

September 16, 2003

Short 330


The Short 330 started under the designation SD3-30 as a development of the SC.7 Skyvan. It used the same rectangular fuselage section, lengthened by 12 ft 5 in, and wing and other parts of the Skyvan. The 330 is a 30-seat (hence the 30 in the original SD3-30 designation) transport for short- and medium range distances, and one of the first to make use of the Civil Aeronautics Board deregulation for regional and commuter air services (up to 30 passengers and a maximum load of 7,500 lb).

The first prototype flew on August 22, 1974, the first production aircraft flew December 15, 1975, starting revenue services on August 24, 1976 with Time Air of Canada. The freighter version is known as the 330C, while the 330 Combi can seat 18 passengers and carry an additional load of 2,200 lb, or be converted to all-freight configuration. The 330-UTT (Utility Tactical Transport) is a freighter version with strengthened floor and an increased maximum take off weight.

The USAF ordered 18 of the 330-UTT and used it as the European Distribution System Aircraft (EDSA) under the designation of C-23A Sherpa. When the EDSA program ended on October 1991, the C-23As were distributed over the USAF flight Test Center, US Army and US Forestry Services. Later Sherpa additions to the US military services received the designations C-23B and C-23C. At least one US Army Sherpa was converted for electronic warfare (JC-23A) and used in the Gulf war.

A total of 179 Short 330 were built. The 330 was developed into the 360, differing primarily in having a 3 ft cabin insertion ahead of the wing and a complete redesigned tail section, replacing the twin tail with a conventional one. The seating capacity of this short-haul airliner was increased to 36. Its prototype (G-ROOM) was first flown on June 1, 1981, scheduled services began December 1, 1982 with Suburban Airlines in the USA. Total delivered: 164

330 Ed Coates Memorial Collection

Specifications (C-23A Sherpa)

Type:

High wing light military utility transport

Engine:

Two 1,198 shp Pratt & Whitney (Canada) PT6A-45R turboprops

Wingspan:

74 ft 9 in (22.78 m)

Length:

58 ft 0 in (17.69 m)

Height:

16 ft 3 in (4.95 m)

Wing area:

543 sq ft (42.10 m²)

Empty Wt:

14,200 lb (6,440 kg)

Max T/O Wt:

22,900 lb (10,387 kg)

Max speed:

218 mph (352 km/h) at 10,000 ft (3,050 m)

Max climb:

1,180 ft/min (6.0 m/sec)

Ceiling:

11,500 ft (3.500 m)

Range:

770 mls (1,239 km) with 5,000 lb (2,268 kg) payload and reserves

Models

330-100:

initial production

330-200:

increased fuel for greater range

330-UTT:

utility tactical transport, strengthened floor, structural reinforcement

C-23A Sherpa:

USAF-version of 330-UTT, 2 cabin windows on each side

C-23B:

US Army National Guard-version of 330-UTT 11 cabin windows on each side

C-23C:

rebuilt version of V2 and V4

JC-23A Sherpa:

US Army Sherpa converted for electronic warfare

360-100:

initial production P&W PT-6A-65 engines

360-200:

PT-6A-65AR engines

360-300:

PT-6A-67AR engines and autopilot

360-300:

Freighter version