Handley Page Jetstream

Source: Wikipedia, the free encyclopedia.

Jetstream
Role Regional airliner
Manufacturer Handley Page
Scottish Aviation
First flight 18 August 1967
Introduction 1969
Retired 2011
Status Retired
Produced 1967–1975
Number built 66
Developed into
BAe Jetstream 41

The Handley Page HP.137 Jetstream is a small twin-

BAe Jetstream 32
, featuring different turboprop engines.

Development

Handley Page was in an awkward position in the 1960s, wishing to remain independent of the "big two" British companies (Hawker Siddeley and the British Aircraft Corporation), but without the money needed to develop a large new airliner that would keep it in the market. After studying the market it decided that its next product would be a highly competitive small airliner instead, filling a niche it identified for a 12–18 seat high-speed design. Compared to its three closest rivals, the Beechcraft King Air, Aero Commander Turbo Commander and Swearingen Merlin it offered "more capacity, better range-payload, higher speed and greater comfort".[1] American salesman and modification engineer Jack Riley claimed to have written the design specifications.[2] The design garnered intense interest in the US when it was first introduced, and an order for 20 had been placed even before the drawings were complete. Charles Joy was responsible for the design.

The original design dates from 1965 as a 12-seat (six rows with a centre aisle) aircraft. The aircraft was a low-wing,

main spar
formed a step in the aisle, which was a tripping hazard.

Final assembly took place in a new factory at the Radlett aerodrome, but large portions of the structure were subcontracted, including complete wings being built by Scottish Aviation at Prestwick, Scotland and the tail section by Northwest Industries of Edmonton, Alberta, Canada. The original design used Turbomeca Astazou XVI engines of approximately 840 hp (626 kW), and flew on 18 August 1967 as the Jetstream 1.[4] Throughout the test program the engines proved to be a weak point, being generally underpowered for the design, and surprisingly temperamental for what was then a mature and widely used turboshaft design. Testing was eventually moved to the Turboméca factory airfield in the south of France, both to allow faster turnaround with engine work, and in order to improve the schedule by taking advantage of the better weather.

In order to improve sales prospects in the US, the fifth prototype was fitted with the US-built

Garrett TPE-331 in place of the French Astazou. Changing to the US-built engine was enough to allow the United States Air Force to consider it for cargo use. It eventually placed an order for 11, fitted with a cargo door and accommodation for 12 passengers or six stretcher cases, to be known as the C-10A, or Jetstream 3M. The US Air Force cancelled its order in October 1969 citing late delivery.[5]

The first production model Jetstream 1 flew on 6 December 1968,[6] and over the next year 36 would be delivered. However, by this point Handley Page had given up on the original engine, and the Jetstream 2 was launched with the larger 965 hp (720 kW) Astazou XVI, starting deliveries in late 1969. The late delivery and engine problems had driven development costs to over £13 million, far more than the original £3 million projections. Only three Jetstream 2s would be completed before Handley Page went bankrupt, and the production line was eventually shut down in 1970.

There was enough interest in the design that it was first picked up by a collaboration of investors and Scottish Aviation which formed a company called "Jetstream Aircraft" to produce the aircraft. Initially production moved to Sywell Aerodrome in Northamptonshire, the CEO being Bill Bright. A further ten Jetstream 1s were produced by this team. Scottish Aviation continued production of the Jetstream 2 as well, although referring to it as the Jetstream 200. In February 1972, 26 Jetstream 201s were ordered by the

trainers as the Jetstream T.1. Fourteen of these were modified as observer trainers for the Royal Navy, receiving the designation
Jetstream T2.

Variants

Jetstream Mk 1

Jetstream 200

Jetstream 3M

Improved variant with TPE331 engines for the United States Air Force.

C-10A

United States Air Force military designation for the Jetstream 3M. Production started but the order was cancelled and none was delivered.

Riley Jetstream

A few early Jetstream 1 aircraft were converted by Riley Aircraft of Carlsbad, California, to this version. The aircraft were fitted with two PT6A turboprop engines.[7]

Jetstream T.1

United Kingdom military designation of Mk 1s for the Royal Air Force as multi-engine trainers.

Jetstream T.2

Conversion of T1s for the Royal Navy as rear-crew trainers.

Century III

Conversions with TPE331 engines.

Operators

The aircraft was used mainly by corporate operators and scheduled passenger commuter/regional airlines.

Civil operators

 Argentina
 Libya
 Colombia
 Denmark
 Germany
 United States
  • Air Illinois
  • Air US
  • Apollo Airways (subsequent name change to Pacific Coast Airlines)
  • Big Sky Airlines
  • Dorado Wings (operated in the Caribbean from Puerto Rico)
  • Cal-State Air Lines
  • JetAire Airlines
  • Interstate Airlines
  • Sierra Pacific Airlines
  • South Central Air Transport (SCAT) (aircraft subsequently acquired by Air Illinois)
  • Sun Airlines (announced by the airline but may have not been actually delivered or operated)
  • Texas Star Airways
  • Western Air Stages
  • Zia Airlines

Military operators

Jetstream T1 of the Royal Air Force
Jetstream T2 of the Royal Navy
 United Kingdom
Apollo Airways Fleet, Santa Barbara California
 Uruguay

Jetstream in the film "Moonraker"

A Jetstream operated by Apollo Airways, a commuter airline based at the

007) is thrown out of the aircraft while it is in flight.[8]

Accidents and incidents

Aircraft on display

Germany
Netherlands
United Kingdom

Specifications (Series 200)

Data from Jane's All The World's Aircraft 1976–77.[16]

General characteristics

  • Crew: two
  • Capacity: 16 passengers
  • Length: 47 ft 2 in (14.37 m)
  • Wingspan: 52 ft 0 in (15.85 m)
  • Height: 17 ft 5 in (5.32 m)
  • Wing area: 270.0 sq ft (25.08 m2)
  • Empty weight: 7,683 lb (3,485 kg)
  • Max takeoff weight: 12,566 lb (5,700 kg)
  • Fuel capacity: 384 Imp Gallons (1,745 L)
  • Powerplant: 2 × Turbomeca Astazou XVIC turboprop, 921 hp (687 kW) each

Performance

  • Maximum speed: 282 mph (454 km/h, 245 kn)
  • Cruise speed: 269 mph (433 km/h, 234 kn) (econ cruise)
  • Stall speed: 88 mph (142 km/h, 76 kn) (flaps down)
  • Never exceed speed: 345 mph (555 km/h, 300 kn)
  • Range: 1,380 mi (2,220 km, 1,200 nmi)
  • Service ceiling: 25,000 ft (7,600 m)
  • Rate of climb: 2,500 ft/min (13 m/s)

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes
  1. ^ article "Handley Page Jetstream",Flight International, 11 May 1967, p.737
  2. ^ "The Man that invented the STC". Air PRogress: 67. September 1989.
  3. ^ article "Handley Page Jetstream",Flight International, 11 May 1967, p.738
  4. ^ Jackson 1973, p. 263.
  5. ^ Jackson 1973, p. 264.
  6. ^ Barnes 1976, p. 591.
  7. ^ Dallas debuts Flight, 11 October 1973, p. 598
  8. ^ "James Bond Locations: Back from the African job - Apollo Airways". 16 October 2012.
  9. ^ "National Transportation Safety Board : Aircraft Accident Report : Mid-Air Collision" (PDF). Libraryonline.erau.edu. 17 April 1981. Retrieved 1 November 2021.
  10. ^ "Jetstream". 11 August 2016.
  11. ^ "Jetstream". 7 May 2022.
  12. ^ Ellis 2016, p. 186
  13. ^ Ellis 2016, p. 132
  14. ^ Ellis 2016, p. 193
  15. ^ Ellis 2016, p. 262
  16. ^ Taylor 1976, pp. 193–194.
Bibliography