IAI Westwind

Jet Commander/Westwind
The Westwind, a business aircraft with a mid-wing and two aft-mounted engines
General information
TypeBusiness jet
ManufacturerAero Commander
Israel Aircraft Industries
StatusLimited service
Primary userPel-Air
Number built442
History
Manufactured1965–1987
Introduction date
1965
First flight27 January 1963
Developed from
Aero Commander 500
Developed into
IAI Astra
Gulfstream G100

The IAI Westwind is a business jet that was initially designed and produced by Aero Commander as the 1121 Jet Commander.

Developed as a jet-powered derivative of the successful preceding Aero Commander 500, the prototype made its maiden flight on 27 January 1963. Powered by a pair of GE CJ610 turbojets, the initial production model of the aircraft received type certification on 4 November 1964 and the first deliveries took place two months later. As a consequence of North American Rockwell's purchase of Aero Commander, the programme was promptly sold onto Israel Aircraft Industries (IAI) in 1968. In addition to continuing to produce the Westwind, IAI committed to the further development of the type. It was stretched slightly to create the 1123 Westwind, and subsequently re-engined with Garrett TFE731 turbofans to produce the 1124 Westwind. 442 aircraft were completed before production was terminated in 1987 in favour of the IAI Astra, a derivative of the Westwind.

The largest model of the aircraft, which had a 16,800–23,500 lb (7.6–10.7 t) MTOW, can carry up to ten passengers. The ovoid shape of its fuselage permitted the cabin to be larger while its low-mounted door was particularly useful to aeromedical operators. While possessing a fairly orthodox arrangement for a business jet, one unusual feature was its mid-mounted wings, which lessened the impact of turbulence. The wing is usually equipped with tip tanks; when combined with auxiliary fuel tanks, the Westwind is capable of crossing the Atlantic Ocean or the continental United States without any fuel stops and is the only light jet capable of such range. The Seascan, a dedicated maritime patrol aircraft variant of the aircraft, was operated by the Israeli Air Force (IAF) for several decades.

Development

External image
image icon Business Machine of the Air – promotional film covering the early history of the aircraft
Early 1121 Jet Commanders are powered by thin CJ610 turbojets, and they have five starboard and three or four port windows.
Later 1123 Westwinds are stretched by 22 in (56 cm), they have tip tanks, and six starboard and five port windows.
The 1124 Westwind is powered by two larger Garrett TFE731 turbofans, the Sea Scan maritime patrol aircraft of the Israeli Air Force has a nose radome and additional aerials.
The 1124A Westwind 2 has winglets on the tip tanks.

Origins

The Westwind was originally designed in the United States by Aero Commander as a jet-powered derivative of its twin-propeller namesake aircraft. The prototype performed its maiden flight on 27 January 1963, being initially known as the Aero Commander 1121 Jet Commander. Following initial testing of this prototype, it was modified to production standard, which included the addition of 2.5 ft to the fuselage length and increased payload and maximum weights. The second prototype first flew on 14 April 1964 and was followed by the first production aircraft in November 1964. Type certification of the aircraft was received by the Federal Aviation Administration (FAA) in November of that year, enabling the first customer delivery to take place on 11 January 1965.

Shortly after deliveries of the aircraft commenced, Aero Commander was acquired by North American Rockwell. However, the Jet Commander posed an issue for this acquisition, since Rockwell were already selling an executive jet of its own design, the Sabreliner; due to antitrust laws, the company could not continue to keep both aircraft in production. Therefore, the company decided to sell off the rights to the Jet Commander; consequently, in 1968, Israel Aircraft Industries (IAI) purchased the programme, after which it was rebranded as the Westwind.

Under Israel Aircraft Industries

Jet Commander production amounted to 150 aircraft in the United States and Israel before IAI undertook a series of modifications to create the 1123 Westwind. These included stretching the fuselage and increasing maximum takeoff, maximum landing, and maximum zero-fuel weights, with the wing modified to incorporate double-slotted flaps and drooped leading edges and tip tanks. The trimmable horizontal stabiliser was also modified to have increased span and more travel. Not long after the aircraft went into production, the original General Electric CJ610 turbojet engines were replaced by more fuel-efficient Garrett TFE731 turbofans. Numerous airframe modifications also were made, such as drooped leading edges on the wings, a dorsal fin, revised engine pylons and nacelles, and further increases in maximum takeoff, maximum landing, and maximum zero-fuel weights. With improvements to a number of onboard systems incorporated, as well, these changes resulted in the 1124 Westwind, deliveries of which commenced in 1976.

In 1980, deliveries of the improved Model 1124A commenced; modifications included a new wing centre-section and the addition of winglets to the tips. This revamped aircraft, called the Westwind II, promptly replaced the original model in production. IAI constructed the final Westwind in 1987, after a total of 442 Jet Commanders and Westwinds had been built, after which production was switched to a newer derivative aircraft, the IAI Astra.

Design

The Jet Commander/Westwind is of a broadly conventional arrangement for a business jet, typically being powered by a pair of turbofan engines mounted in nacelles carried on the rear fuselage aft of the rear bulkhead to lower cabin noise. Somewhat atypical for an aircraft of this class is the mounting of its wings at the mid-point of the fuselage (instead of the more common low-wing arrangement); this configuration reduces the impact of turbulence and makes the aircraft smoother in-flight. The wing is usually equipped with tip tanks, which can function as sponsons in the event of a water landing. The Westwind also possesses a strong short-field landing capability. At FL310 and Mach 0.74 (434 kn; 804 km/h), the 1124 burns 1,600 lb (730 kg) per hour, and 1,200 lb (540 kg) at Mach 0.7 (411 kn; 761 km/h). When outfitted with auxiliary fuel tanks, the range of the aircraft can be increased to 2,900 nautical miles, which made the Westwind the only light jet capable of crossing the Atlantic Ocean or the continental United States without needing to refuel.

The Westwind has a relatively spacious cabin, which was partially attributable to the design of its fuselage; specifically, it had ovoid shape, rather than a pure oval. The cabins of most models can be configured to comfortably carry up to eight passengers; options such as a three-place divan are also available. Cabin refurbishment packages are available for the type. The aircraft is furnished with a relatively low-mounted door, which has proven to be particularly attractive to aeromedical operators as it eases the loading and unloading of patients. The aircraft also has a sizable baggage compartment and a lavatory aft of the cabin. Pilots have reported instances of corrosion between the deicing boots and the leading edge of the wing, as well as along the aircraft's underside. Furthermore, rough or heavy landings of the aircraft risk damage to the fuel cells, which causes fuel leaks.

At the time of its first flight, the Westwind was provisioned with a relatively advanced cockpit for the era, being equipped with both analogue and early digital flight instrumentation. Later models have been furnished with newer avionics suites, either to increase operational efficiency or for regulatory compliance; avionics upgrade packages have also been produced for existing aircraft.

Operational history

In 1976, in the wake of the terrorist takeover of the Savoy hotel in Tel Aviv, the Israeli Air Force (IAF) decided to use the Westwind as the basis for a maritime patrol aircraft, which became known as the IAI Sea Scan. It had originally been developed to meet a requirement for the United States Coast Guard (USCG) to replace the Grumman HU-16 Albatross, however, the USCG ultimately selected the Dassault Falcon instead.[citation needed] The Seascan, nicknamed "Seagull" (Hebrew: שחף, romanized: Shahhaf), was adopted by the service. Following the reassingment of the maritime patrol mission to the IAI Heron unmanned aerial vehicle, the IAF withdrew its last Seascan in 2017.

By 2018, a 1980s-era Westwind 1124s was typically priced from $300,000 to $700,000. The sustained low price for used examples of the type makes it relatively affordable to acquire, but allegedly puts off owners from investing into avionics upgrades or other improvements.

Variants

Type certificate data sheet
ModelApprovedEnginesThrustMmoCeilingMTOWpaxfuelSerials
Aero
Commander
1121 4 November 1964 CJ610-1/-5 2,850–2,950 lbf
12.68–13.12 kN
0.765 40,000 ft
12,192 m
16,800–17,500 lb
7,620–7,938 kg
8 926 US gal
3,505 L
3-120
1121A 19 September 1967 CJ610-1 2,850 lbf
12.68 kN
41,000 ft
12,497 m
17,500 lb
7,938 kg
1,090 US gal
4,126 L
121-131
1121B 23 April 1968 CJ610-5 2,950 lbf
13.12 kN
132-150
IAI 1123 8 December 1971 CJ610-9 3,100 lbf
13.79 kN
20,700 lb
9,389 kg
10 1,300 US gal
4,921 L
  36 built
1124 17 March 1976 TFE-731-3-1G 3,700 lbf
16.46 kN
45,000 ft
13,716 m
23,500 lb
10,659 kg
1,400 US gal
5,300 L
1124A 17 April 1980 0.785
  1. ↑ overwing refuelling points with integral fuel tanks, new wheels, tires and brakes, improved cockpit lighting[citation needed]
  2. ↑ with passengers, 45,000 ft (13,716 m) with crew only
  3. ↑ Increased fuselage length, tip tanks, double-slotted flaps and drooped leading edge, Increased horizontal tail span...
  4. ↑ plus Microturbo SAPHIR III APU
  5. ↑ Improved drooped leading edge, added dorsal fin, new pod and pylon shapes, new wheel well fairing...
  6. ↑ winglets on the wing tip tanks, New leading edge profile

The 1122 Type Certificate was cancelled, the two airplanes manufactured have been converted to model 1123. The 1124N Sea Scan is a maritime surveillance aircraft, and the 1124 was renamed Westwind I after the introduction of the 1124A Westwind II. The 1121C is an unofficial designation for 1121 aircraft modified under a Supplemental Type Certificate with an increased all-up weight available from 1971.[citation needed] The 1123 Westwind was stretched by 22 in (56 cm).

Operators

Civil operators

 Australia
  • Pel-Air: six, of which four are in aero medical configuration.
  • Medex Aero: three, two of which are in aero medical configuration and one in corporate configuration
 Canada
 Brazil
  • Brasil Vida Táxi Aéreo: four aircraft, two in aero medical configuration
 Fiji
  • Helipro Fiji: one aircraft is in aero medical configuration.
 Philippines
 United States

Military operators

 Chile
 Ecuador
 Honduras
 Israel
 Mexico
 Panama
 Uganda
 United States

Accidents and incidents

Specifications (1124A Westwind II)

IAI Westwind II

Data from Jane's All The World's Aircraft 1982-83

General characteristics

Performance

See also

References

Citations

  1. ↑ "Sport and business". Flight International. 14 February 1963.
  2. 1 2 3 4 5 6 7 8 9 10 11 Huber, Mark (June 2010). "Aircraft: Westwind II". Business Jet Traveler.
  3. ↑ Thompson 1990, p. 108.
  4. ↑ Schlaeger 1963, p. 30.
  5. 1 2 3 4 5 6 7 Frawley 1997, p. 123.
  6. 1 2 3 4 "FAA Type Certificate Number A2SW" (PDF). Federal Aviation Administration. April 17, 1980.
  7. ↑ Field, Hugh (25 November 1978). "Westwind 1124 in the air". Flight International.
  8. ↑ "Aircraft Operating Cost and Performance Guide: IAI Westwind II". conklindedecker.jetsupport.com/. Retrieved 12 October 2026.
  9. ↑ "IAI Westwind 1123". jetadvisors.com. Retrieved 12 October 2026.
  10. ↑ מתכננים "ווסטווינד‭-"‬מדגם חדש לסיוע טקטי לחילות ים, Davar, 20 September 1976
  11. ↑ Foster, Peter R. (16 March 2017). "Israel Retires Last Seascan". Key Aero. Retrieved 12 October 2026.
  12. ↑ Huber, Mark (December 2018). "For many models, market hitting the apex" (PDF). Aviation International News. pp. 20–21, 24. Archived from the original (PDF) on 27 December 2018. Retrieved 27 December 2018.
  13. ↑ "At the NBAA convention". Flight International. 9 October 1969.
  14. 1 2 3 4 Hartoch 1979, pp. 42-44.
  15. ↑ "Rockwell 1121 Statistics". Aviation Safety Network. 30 March 2020.
  16. ↑ "IAI 1124 Statistics". Aviation Safety Network. 30 March 2020.
  17. ↑ "Accident description for N100RC". Aviation Safety Network. Retrieved October 29, 2020.
  18. ↑ "ASN Aircraft accident Rockwell 1121B Jet Commander N200RC Tampa International Airport, FL (TPA)". aviation-safety.net. Retrieved 2023-02-04.
  19. ↑ "Incident Report – Israel Aircraft Industries LAX94FA073 – December 15, 1993". National Transportation Safety Board. 1993. Archived from the original on March 15, 2013. Retrieved December 24, 2011.
  20. ↑ "Accident description". Aviation Safety Network database.
  21. ↑ "NTSB Aviation Accident Final Report FTW03FA036". National Transportation Safety Board. Retrieved 5 December 2019.
  22. ↑ "Accident description for N280AT". Aviation Safety Network. Retrieved 12 October 2023.
  23. ↑ Grass, Jonathan (June 18, 2014). "Plane crash at Huntsville International Airport claims 3 lives". The Huntsville Times. AL.com. Retrieved June 19, 2014.
  24. ↑ Robinson, Carol; Davidson, Tiffany (June 19, 2014). "3 men killed in Wednesday plane crash identified". The Huntsville Times. AL.com. Retrieved June 19, 2014.
  25. ↑ Jason Gutierrez (29 March 2020). "8 Killed After Philippine Plane Bursts Into Flames". The New York Times.
  26. ↑ "Eight killed after medical evacuation plane crashes in Manila's Ninoy Aquino International Airport". Channel News Asia. 29 March 2020. Archived from the original on 30 March 2020. Retrieved 30 March 2020.
  27. ↑ Taylor 1982, pp. 124–126.
  28. ↑ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.

Bibliography