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Hawker Siddeley HS 748
Hawker Siddeley HS 748
from Wikipedia

The Hawker Siddeley HS 748 (formerly Avro HS 748) is a medium-sized turboprop airliner originally designed and initially produced by the British aircraft manufacturer Avro. It was the last aircraft to be developed by Avro prior to its absorption into Hawker Siddeley.

Key Information

The HS 748 was developed during the late 1950s as a move to re-orient the company towards the civil and export markets. Powered by the popular Rolls-Royce Dart turboprop engine, it was specifically designed as a modern feederliner to act as a replacement for the aging Douglas DC-3s then in widespread service. Originally intended to seat a smaller number of passengers, market research indicated that a seating capacity of around 40 passengers would be optimal for the type. As a means to differentiate the new airliner from competitors, it was designed to possess a high level of performance, including its short takeoff and landing (STOL) capabilities and overall ruggedness. First flying on 24 June 1960, the series 1 HS 748 entered revenue service in 1961.

Once in service, the HS 748 found itself a niche within the short-haul market. Several different models of the regional airliner have been developed, typical improvements being the adoption of increasingly powerful Dart engines and a higher gross weight. Perhaps the most distinct variant was the HS 780 Andover, a dedicated military transport model developed for the Royal Air Force (RAF) that featured a large rear loading ramp and a squatting main landing gear to assist in loading bulky freight items.

By 1988, the year in which production of the type was terminated, 380 aircraft had been produced between Hawker Siddeley (the owning company of Avro) and Indian aviation company Hindustan Aeronautics Limited (HAL). During the 1990s, a larger, stretched development of the HS 748, the BAe ATP, was developed and had attempted to compete with market leaders such as the de Havilland Canada Dash 8 and ATR 42, but saw only limited sales prior to production being terminated.

Development

[edit]

Background

[edit]

Following the release of the 1957 Defence White Paper, in which then-Minister of Defence Duncan Sandys announced the termination of almost all manned military aircraft development, aircraft manufacturer Avro decided that it should place a greater emphasis upon the civilian market. Ten years prior, it had launched a civilian airliner, the Avro Tudor series, but this had encountered few sales; thus, during 1958, it was decided to commence work on a clean-sheet design, which would eventually become the HS 748. On 9 January 1959, the existence of the project, then referred to as the Avro 748, was announced to the public.[1]

By this point, the four-engined Vickers Viscount had already secured the larger end of the short-haul market; therefore, Avro decided that it would design a smaller regional airliner, powered by a pair of Rolls-Royce Dart turboprop engines. It was envisioned that this aircraft would be a suitable replacement for the many DC-3 Dakotas that were by then reaching the end of their economic lifespan. According to aviation periodical Flight International, a major goal for the design team was to produce an aircraft that would be capable of operating from any airfield from which the DC-3 could be operated.[2]

Initially, the airliner was planned to be a 20–30 seat aircraft, adopting a somewhat similar configuration to the future rival Fokker F27 Friendship; however, following discussions with several potential customers, the company opted for a low-wing 40-seat configuration. It was this latter arrangement that was chosen for the 748 project. Another important focus for the prospective airliner was compliance with both British and American standards of airworthiness; accordingly, it would be one of the first medium-sized aircraft to incorporate fail-safe design principles for its structure in place of the then-common safe-life principles being practiced.[2] The airframe effectively lacked any imposed lifespan; during development, it was successfully tested using a water tank for up to the equivalent of 100,000 flight hours.[2]

Avro was not the only company to see the potential for a DC-3 replacement and, by this point, work on the 748's direct competitor, the Dutch-built F27 Friendship, was well advanced. To differentiate itself from the competition, Avro decided to focus its efforts upon achieving a more rugged design that offered superior short takeoff and landing (STOL) performance, which enabled the prospective airliner to be operated from smaller and more austere airports, including those without modern runways.[3] This STOL capability was accomplished via several features, including the adoption of a long, high lift wing, which was fitted with a unique single slot flap with a hinged flap tab at the trailing edge. This wing was mounted low on the fuselage with dihedral from the root, allowing for good overall ground clearance and the easy mounting of strong landing gear. Operationally, pilots were provided with a choice of three takeoff flap settings to select the level of STOL performance required.[2]

Another supportive feature of the 748 was a design decision to adopt straightforward systems and use proven components where realistically possible.[2] For operator convenience, the engines were provided with an internal ignition system; various other systems and structures throughout the airliner were designed to be easy to inspect and to perform repairs upon, even when at unprepared airstrips with limited equipment available. Likely as a consequence of these favourable qualities, the 748 quickly attracted the attention of a variety of airlines, particularly those that typically operated in remote areas, which has been attributed to its ability to operate from short, rough fields without any ground service equipment while being capable of hauling payloads in excess of 10,000 lb.[citation needed]

Into flight

[edit]
BKS Air Transport Avro 748 Series 1 at Manchester in 1964
Aerolíneas Argentinas Avro 748 Series 1 at Aeroparque Jorge Newbery, Buenos Aires, in 1972

On 24 June 1960, the first Avro 748 made its maiden flight from the company's Woodford, Cheshire, aircraft factory.[3] Flight testing of the two prototypes quickly validated the type's short-field performance. Eighteen Avro 748 Series 1 aircraft were produced; during April 1962, the first production aircraft were delivered to launch customer Skyways Coach-Air Limited. However, the majority of the series 1 were export sales to operator Aerolíneas Argentinas.[citation needed] During the early 1960s, Avro's individual identity within the Hawker Siddeley Group was expunged, after which the airliner was marketed by the parent company as the HS 748.

After the initial batch of series 1 aircraft was completed, production transitioned to the improved series 2. The series 2 was largely similar to its predecessor, principally benefiting from the adoption of more powerful Dart RDa 7 Mk 531 engines and an increased gross weight. According to aviation periodical Flight International, during 1960, the basic price for a new Avro 748 Series 1 was £176,000, while that of the corresponding Avro 748 Series 2 was reportedly £196,000.[1]

During 1967, the series 2A was introduced, which was the same basic aircraft powered by Mk. 532 engines along with a further increase in gross weight. From 1971 onwards, several new options were made available to customers, including a large freight door in the rear cabin and a strengthened cabin floor. During 1979, the Series 2B was introduced, which saw a 4-foot increase in wingspan, the adoption of Mk 536-2 engines, along with a modernised passenger cabin, and various improvements to the fuel, water methanol injection system, and engine fire protection systems.[citation needed]

During 1976, Eric Johnson, sales engineering manager of Hawker Siddeley Manchester, stated that the company was studying options for equipping a model of the HS 748 with turbofan engines, and that a preferred powerplant at that point was the Rolls-Royce/SNECMA M45H, as used on the VFW-Fokker 614 jetliner.[2] Other changes would likely have been incorporated, including the addition of lift dumpers and adaptive brakes for better landing performance, while electrical, hydraulic and air conditioning systems would be redesigned; externally, a dihedral would have to be introduced to keep the tailplane clear of the jet exhaust. It was envisioned that the reengined aircraft could offer larger seating arrangements of up to 64 seats.[2]

In addition to the British production line, manufacture of the 748 was also performed overseas. Early on, India had placed orders for the type.[1] Both the 748 Series 1 and Series 2 were licence-produced by Indian manufacturer Hindustan Aeronautics (HAL), aircraft produced by the company were designated HAL-748. On 1 November 1961, the first Indian-assembled HAL-748 made its initial flight.[3] By the end of production, HAL had completed 89 Indian-built aircraft, 72 of which were for the Indian Air Force and 17 were delivered to national flag carrier Indian Airlines.[citation needed]

While the HS 748 was originally intended to be marketed principally towards the civilian market, numerous examples were sold to military customers around the world. Hawker Siddeley used the design as the basis for the HS 780 Andover, a military transport aircraft developed and produced for the Royal Air Force. In terms of its design, the HS 780 was broadly similar to the 748, differing primarily by its redesigned rear fuselage and empennage, which incorporated a large rear loading ramp and a squatting main landing gear to better facilitate the loading of bulky freight items. The 780 also used the more powerful RDa.10/1 3,245 hp (2,419.80 kW) estimated power at 15,000 rpm, with Water/Methanol injection [3]

During 1988, production of the HS 748 was terminated, while the last British-assembled aircraft made its first flight on 1 December of that year.[3] BAE then started producing a product improved, stretched version the BAE ATP 61 which uses the PWC 126/127 engines. Total production of this variant was only 67 aircraft. According to BAE Systems, a successor company to Hawker Siddeley, during the type's production life, a total of 381 aircraft had been produced, which included both the Andover and HAL-built examples.[3]

Operational history

[edit]

Within its first decade of its availability, sales of the HS 748 had reportedly been relatively brisk; by 1976, the sale of 312 aircraft had been recorded, of which 259 had been to export customers.[2] Within ten years of its launch, India had emerged as the largest single market for the airliner, Indian Airlines being the largest HS 748 operator with a fleet of 26 aircraft.[4] It had been popular with numerous commercial operators; across the Caribbean and Latin America alone, 63 HS 748s were in operation with 11 separate operators.[4]

The HS 748 had been able to achieve some triumphs over competing rivals, including the F27 Friendship. Philippine Airlines had been the F27's largest operator prior to its decision to replace both it and its remaining DC-3s with the HS 748, which represented a significant sales coup for Hawker-Siddeley.[2] Other major civil operators included Aerolíneas Argentinas, VARIG, Thai Airways, LAN-Chile, and Bouraq Airlines.[3] Several of these operators would utilise its STOL capabilities in their services; according to Flight International, over one-third of all scheduled operations reportedly involved operations from rough airstrips with minimalist facilities.[4]

Another key market for the HS 748 was the executive role; the type was repeatedly procured to serve as the designated aircraft for various heads of state, including those of Argentina, Brazil, Chile, India, Venezuela, Zambia, Thailand and the United Kingdom.[4] The HS 748 was one of the last planes to be flown by noted aviator and business magnate Howard Hughes. During 1972, Hughes performed several flights of the type, each time accompanied by Hawker Siddeley test pilot Tony Blackman, flying from the company's airport in Hatfield, Hertfordshire.[5][6]

The Australian military purchased several aircraft; specifically, the Royal Australian Air Force (RAAF) procured a fleet of ten HS 748s, the first of which arrived in 1968 for navigation training and transporting VIPs.[7] The Royal Australian Navy (RAN) operated a pair of HS 748s starting in 1973 as a navigational trainer. Following Cyclone Tracy, relief aid was delivered across Darwin, Northern Territory, using the type; after being fitted with various electronic countermeasures (ECM) during the late 1970s, HS 748s were also used for electronic warfare training.[7]

In a typical passenger configuration, the HS 748 can accommodate around 40–48 economy class seats in a four abreast layout; however, the majority of later-serving passenger HS 748s were typically operated as quick change combis. These aircraft are fitted with a movable bulkhead that divides the main cabin, housing between 4 and 40 seats in the rear section while cargo is placed in the forward section.[4] The 748 has also been widely used as a pure freighter, having a typical maximum payload of about 12,000 lbs. Several carriers have used the 748 as a bulk fuel hauler, in which capacity it is normally with either seven or eight fixed tanks in the cabin, possessing a total capacity of about 7,500 L (1,600 imp gal; 2,000 US gal).[8]

The ICAO designator as used in flight plans is A748.[citation needed]

The CAA are withdrawing the Type Certificate on the 1st July 2025 at request of the Type Certificate holder (BAE Systems (Operations) Ltd[9]

Variants

[edit]
  • 748 Series 1 – The original Avro 748 twin-engined short / medium-range airliner, powered by two Rolls-Royce Dart RDa 7 Mk 514 turboprop engines. 24 built.[3]
  • 748 Series 2 – The Series 2 entered production in 1961 with a higher take-off weight and Mk 531 engines. 111 built.
  • 748 Series 2A – Introduced in 1967, with a further increase in take-off weight and Mk 532 or 534 engines. 157 built, making the 748 one of the more successful British airliners and the 2A the most popular variant.
  • 748 Series 2B – The main production model after Hawker-Siddeley was absorbed by British Aerospace, the 2B featured a 4-foot increase in wingspan, increased gross weight, Mk 536 engines, a modernized cabin, and systems improvements. 28 built.
  • 748 Series 5 – Version with overwing-mounted Rolls-Royce M-45H turbofans and a 78 in (2.0 m) fuselage extension for 64 passengers. Not built.
  • Super 748 – Basically the same as the 2B but fitted with engine hush kits. 8 built.
  • Hawker Siddeley HS780 Andover – Modified version of the 748 design for the Royal Air Force. Fitted with kneeling undercarriage, raised tail unit and rear loading ramp.
  • Coastguarder – A maritime patrol version.[3][10]
  • 748 Andover – Military passenger transport versions of the 748.[3]
  • 748AEW – Airborne early warning variant to AST.400. Not built.
  • 748AEW (FASS) – Version of 748AEW powered by four Avco Lycoming T53-21A turboprops. Not built.
  • 748B – 36-seat variant. Not built.
  • 748COD – Version planned for the U.S. Navy for a deck-landing fleet support aircraft. Not built.
  • 748CF – Civil version of Type 780. Not built.
  • 748E – Variant of Series 2 with fuselage extended to 76 feet to carry 52-60 passengers and wing from Type 780. Not built.
  • 748 Super E – Version of 748E with lower AGW and greater wingspan. Not built.
  • 748EW – AEW aircraft for Sweden with twin rudders and fins. Not built.
  • 748 Executive – Executive/VIP version of Series 2. Not built.
  • 748F – Freighter version of Series 2 with large freight door and strengthened floor. Not built, marketed as 748 Series 2 LFD.
  • 748J – Turbojet version with rear-mounted engines and a T-tail. Not built.
  • 748L – Large diameter (10'6") fuselage version of Series 2. Not built.
  • 748ML – Maritime reconnaissance version. Not built.
  • 748SFV – Version of Series 2A for US STOL requirement to carry 40 passengers. Not built.
  • 748STOL – STOL variant for U.S. airlines with four Avro Lycoming T53-21A engines. Not built.
  • 748X – Executive variant of Series 2 with increased fuel capacity. Not built.
  • 748-502 – Turbojet version with 2 Avco Lycoming ALF502 engines. Not built, developed into Series 5.
  • 757 – Version of Series 1 with strengthened floor and revised avionics for the Indian Air Force. Not built. Also known as 748M.
  • 758 – High-wing version of 748. Not built. Also known as 748R.
  • HAL 748 – Licence production by Hindustan Aeronautics Limited at Bangalore, India. Indian aircraft were later modified for a variety of roles including a trials aircraft for an Airborne Early Warning version fitted with a large radome, known as the Airborne Surveillance Platform (ASP).[3] 89 built.
  • HAL 748 Series 2M – Production for the Indian Air Force (the last 20 built) were Series 2M aircraft with a large freight door.
  • C-91Brazilian Air Force designation for the HS 748 Series 2A.[11]
  • B.L.5 – (Thai: บ.ล.๕) Royal Thai Armed Forces designation for the HS 748-208.[12]

Operators

[edit]

Current civil operators

[edit]

As of July 2020, a total of 13 HS 748 aircraft (all variants) remained in airline service.[13] As of May 2023, Transport Canada (TC) listed 7 HS 748 in Canada with a current Certificate of Registration.[14]

Current operators are:

Former civil operators

[edit]
Belgian air force Hawker Siddeley HS-748
 Afghanistan
 Botswana
 Antigua & Barbuda
 Argentina
 Austria
 Bahamas
 Bophuthatswana
 Brazil
  • Varig (11) [one Avro 748 Series 2 prototype and 10 production aircraft]
 British Virgin Islands
 Canada
 Cape Verde
 Chile
 Colombia
 Fiji
 Germany
 Guyana
 India
 Indonesia
 Ireland
  • Ryan Air (2) 1986–1989 Inaugurating the Dublin-London (Luton) Service
 Kenya
 Madagascar
 Malawi
 Marshall Islands
 Mexico
   Nepal
 New Zealand
 Panama
 Philippines
 Portugal
 Samoa
 South Africa
 Sri Lanka
 Thailand
 Trinidad and Tobago
  • Trinidad and Tobago Air Service (TTAS)

 Oman

 United Kingdom
 United States
 Venezuela
 Zambia

Current military operators

[edit]
 India

Former military operators

[edit]
Royal Australian Air Force HS.748 at RAAF Laverton in 1971
An HS 748 of 723 Squadron Royal Australian Navy
 Australia
 Belgium
 Benin
 Brazil
 Brunei
 Burkina Faso ( Upper Volta)
 Cameroon
 Colombia
 Ecuador
 India
 Madagascar
   Nepal
 South Korea
 Sri Lanka
 Tanzania
HS 748 Royal Thai Air Force, Children day 2016, Bangkok, Thailand, 2016
 Thailand
 United Kingdom
 Venezuela
 Zambia

Accidents and incidents

[edit]
  • On 10 July 1965, an Avro 748-101 Series 1 G-ARMV of Skyways Coach-Air was written off in a landing accident at Lympne Airport. The 51 people on board survived. This was the first accident that resulted in a write-off of an Avro 748 / HS748.
  • On 15 August 1967, two accidents involving HS-748-222 Series 2 aircraft of Channel Airways Limited, occurred roughly 90 minutes apart at Portsmouth Airport. In the first incident, G-ATEK operating a scheduled service from Southend to Paris via Portsmouth, landed in rainy conditions and was unable to stop in the available distance on the grass runway. The aircraft slid sideways, left the runway and stopped on an embankment. Some 90 minutes later , aircraft G-ATEH, operating a scheduled service from Jersey, via Guernsey to Portsmouth, landed and slid on the runway, crashed through a perimeter fence and came to rest on the main Eastern Road. There were no injuries in either accident, but both aircraft sustained substantial damage. An AIB investigation[32] reported that "both accidents were caused by inadequate braking which had resulted from the extremely low coefficient of friction provided by the very wet grass surface over the hard, dry and almost impermeable sub-soil".
  • On 4 February 1970, Aerolíneas Argentinas Flight 707, an Avro 748–105, crashed into the ground after the pilots lost control of the aircraft. The aircraft crashed at Loma Alta, Argentina, and killed all 37 on board.
  • On 21 April 1970, Philippines Airlines Flight 215, an Avro 748-209, crashed after a bomb explosion. All 36 on board perished
  • On 9 December 1971, an HS 748 of Indian Airlines was descending into Madurai near Chinnamanur when it flew into high terrain about 50 mi (80 km) from the airport, killing the four crew members and 17 passengers. There were ten survivors among the passengers. The accident occurred in reduced visibility during daylight hours.[33][34][35]
  • 20 January 1976 – a TAME HS 748-246 Series 2A registration HC-AUE crashed while flying over mountainous terrain at 10,000 feet. The aircraft struck trees with its right wing, lost control and crashed into the side of the mountain. The plane was en route from Loja, Ecuador, to Simón Bolívar International Airport in Guayaquil, Ecuador. Six crewmembers and 28 passengers were killed; 8 passengers survived.
  • 3 March 1978 – Línea Aeropostal Venezolana Hawker Siddeley HS 748 crashed on departure from Simón Bolívar International Airport, Venezuela, all 47 on board are killed.
  • 7 September 1978 – Air Ceylon HS 748 4R-ACJ was destroyed by fire while parked at Colombo-Ratmalana, resulting from detonation of a bomb placed on board by terrorists. There were no fatalities.
  • 31 July 1979 - At Sumburgh Airport in the Shetland Islands, Scotland, Dan-Air Flight 0034, an HS 748 series 1 (registration G-BEKF) operating an oil industry support flight crashed. The aircraft failed to become airborne and crashed into the sea. The accident was due to the elevator gust-lock having become re-engaged, preventing the aircraft from rotating into a flying attitude. The aircraft was destroyed and 17 persons died from drowning.
  • 4 August 1979 - The Indian Airlines HAL-748 (VT-DXJ) was operating a scheduled flight from Pune to Bombay, India. The aircraft crashed in the Kiroli Hills near Panvel about 11 km east of Bombay. The aircraft was destroyed. All 45 persons on board were killed.[36]
  • 22 August 1979 – An aircraft mechanic (a former non-commissioned officer of the Colombian Air Force), stole a military HS 748 (FAC-1101) from a military hangar at the Eldorado International Airport in Bogotá, Colombia. According to the news, this person stole the aircraft with the intention of crashing it against his parents' house. After some minutes in the air, it ran out of fuel and crashed, killing the impromptu pilot and three people on the ground.[37]
  • 27 April 1980 - Thai Airways Flight 231 stalled and crashed after entering a thunderstorm on approach to Bangkok .The accident kill 44 out of 53 people on board.
  • 26 June 1981 – Dan-Air Flight 240, an HS 748 2A mail flight from Gatwick Airport to East Midlands Airport, crashed at Nailstone, Leicestershire, killing the 3 crew members. While descending, the right-hand rear door detached, struck the horizontal tail plane and became lodged on its leading edge. Control was lost, and the aircraft entered a steep dive. During the dive, the wings and tail plane failed due to being overstressed.
  • 19 August 1981 – Indian Airlines Flight 557, an HAL 748 (VT-DXF) overshot the runway at Mangalore-Bajpe Airport in wet weather. The aircraft came to a halt just beyond the runway edge. There were no fatalities but the damaged aircraft was written off. One of the passengers on board was Veerappa Moily ex-Cabinet Minister for Law, Justice and Company Affairs in the Government of India.[38][39]
  • 11 October 1983 – Air Illinois Flight 710 crashed at night in a thunderstorm between Pinckneyville and Tamaroa, IL. The flight originated at Chicago's Meigs Field and had stopped at Springfield, Illinois. The left generator had failed after takeoff and the first officer had mistakenly isolated the right generator. Attempts to restore the right generator were unsuccessful. The captain chose to continue to the destination rather than return to the nearby airport. The cloud base was at 2000 feet MSL, but ATC could not provide an IFR below 3,000 feet. Before the crash, the crew indicated a total loss of electrical power. The left generator drive shaft had sheared.[40] All ten passengers and crew were killed.[41]
  • 27 June 1987 – Philippine Airlines Flight 206 crashed into a mountain after poor visibility hampered the pilot's attempt to land at Loakan Airport in Baguio, Philippines. All 50 passengers and crew were killed.
  • 15 September 1988 - A Bradley Air Services HS-748 (C-GFFA) cargo plane crashed on approach to Ottawa International Airport, (YOW), Ontario, Canada, killing both pilots. It had unloaded all cargo at Montreal-Dorval International Airport (YUL), Quebec, before departing at 09:58 for Ottawa on an instrument flight rules (IFR) flight plan. At about 10:19, while in level cruise flight at 3000 feet at approximately 200 knots indicated airspeed (KIAS), the flight data recorder (FDR) recorded a full-up deflection of the left aileron and a full-down deflection of the right aileron, causing a sharp roll to the left. The right aileron was fully-deflected for three seconds before, over the next seven seconds, the deflection gradually decreased by about five degrees. Over the same 10-second period, the left aileron was nearly fully deflected for the first eight seconds, then decreased by about five degrees during the next two seconds. By this time, the aircraft had rolled through approximately 460 degrees and the nose had dropped 20 to 30 degrees below the horizon. The ailerons returned to a neutral position and remained there for the flight's last three seconds. The bank angle remained at approximately 90 degrees of left bank with a maximum vertical g of 4.7 recorded. The aircraft struck the ground at an airspeed of approximately 290 KIAS after a heading change of about 75 degrees left of the cruise heading. At impact, the bank angle was nearly 90 degrees left and the pitch angle was 41 degrees down. The time from initial aileron deflection to ground impact was approximately 18 seconds.[citation needed]
  • 12 January 1989 - A Bradley Air Services HS-748 (C-GDOV) climbed to 1300 feet, turned right and descended into the ground after takeoff from Dayton International Airport Runway 24R. The aircraft became airborne again and continued 0,75 mile where it collided with trees. During several training flights and two check flights, the co-pilot had demonstrated difficulty with instrument flight due to disorientation, narrow focus of attention, or lack of instrument scan especially during high workload.[42]
  • 10 November 1993 – Nothland Air Manitoba. Hawker Siddeley HS-748-234 Srs. 2A. Registration C-GQTH. Departure airport Sandy Lake Airport, (ZSJ/CZSJ), Ontario, Canada "about 600 km northeast of Winnipeg.". The aircraft took off from runway 29 at Sandy Lake at approximately 1805 and entered a right turn. Witnesses indicate that the aircraft appeared to fly at a lower than normal height throughout the turn. After turning through approximately 120 degrees, the aircraft descended into 100-foot trees and crashed. The aircraft struck the ground about 1 nm northwest of the airport. A contributing factor was the loss of AC power to some of the flight instruments, the reason for which could not be determined. All 3 crew members and 4 passengers perished.
  • 28 April 1995 – Sri Lanka Air Force Avro 748 CR835 an HS 748 serial CR835 (4R-HVB) was hit by an SA-7 missile fired by the Liberation Tigers of Tamil Eelam (LTTE) immediately after takeoff from Palaly. All 45 occupants were killed. Crew managed to return the aircraft for landing but the starboard wing collapsed on short final 295 meters from the threshold due to an extensive fire in the No-2 engine.[43]
  • 29 April 1995 - Sri Lanka Air Force Avro 748 CR834 na HS 748 serial CR834 was hit by na SA-7 missile fired by the Liberation Tigers of Tamil Eelam (LTTE) while on an approach to landing. All 52 Passengers and crew members with investigetor were killed.
  • 11 January 1999 – ASTE HAL-748 ASP/H-2175, an HAL 748 crashed into the ground after the pilots lost control of the aircraft. The aircraft crashed at Attur, Tamil Nadu, India, killing the 2 crew and 6 passengers.
  • 5 September 1999 – Necon Air Flight 128 from Pokhara to Kathmandu, a BAe 748-501 Super 2B (9N-AEG) collided with a communication tower of Nepal Telecommunication Corporation and crashed in a wooded area 25 km west of Kathmandu, while approaching Tribhuvan International Airport. All 10 passengers and 5 crew were killed.[citation needed]
  • 1 June 2002[44] – Former South African cricket captain Hansie Cronje's scheduled flight home from Bloemfontein to George had been grounded, so he hitched a ride as the only passenger on a cargo flight in an HS 748. Near George airport, the pilots lost visibility in clouds and were unable to land, partly due to unserviceable navigational equipment. While circling, the plane crashed into the Outeniqua mountains northeast of the airport. Cronje, aged 32, and the two pilots died. South Africa's High Court reached the conclusion that "the death of the deceased Wessel Johannes (Hansie) Cronje was brought about by an act or omission prima facie amounting to an offence on the part of the pilots."[45][46] However, with Cronje's involvement in match-fixing, theories that Cronje was murdered on the orders of a cricket betting syndicate flourished after his death.[47]
  • On June 8, 2004, Gabon Express Flight 221, an HS 748, crashed after a engine failure. 19 of the 30 people on board died.
  • 12 June 2012[48] – A Wasaya Airways Hawker Siddeley 748 caught fire during ground operations at Sandy Lake First Nation in Northwestern Ontario. No injuries were reported. The aircraft burned completely; only the left wing and nacelle survived.
  • 17 February 2014 – an HS 748-371 Srs 2B crash landed at Rubkona Airport in South Sudan killing one crew member and injuring the other three. The cargo plane was carrying humanitarian Aid to South Sudan.[49]
  • 14 November 2014[50] – A BAe HS-748 crashed on approach to Panyagor airstrip in South Sudan, killing two crew members and seriously injuring a third crew member. The cargo plane was on a charter flight for the Lutheran World Federation and carrying relief supplies from Juba, South Sudan.

Surviving aircraft

[edit]
A10-601 covered in a protective spray coating at the RAAF Museum
SCM-3101 at SLAF Koggala
Cockpit of G-OPFW on display at the South Yorkshire Aircraft Museum

Australia

[edit]

Brazil

[edit]

Canada

[edit]

Ecuador

[edit]

South Africa

[edit]

Sri Lanka

[edit]

Thailand

[edit]

United Kingdom

[edit]

Specifications (Super 748)

[edit]

Data from Jane's Civil and Military Aircraft Upgrades, 1994–95,[56] BAE Systems[3]

General characteristics

  • Crew: 2 plus 1 passenger attendant (if required)
  • Capacity: 40–58 passengers / 11,323 lb (5,136 kg) payload
  • Length: 67 ft 0 in (20.42 m)
  • Wingspan: 102 ft 5.5 in (31.229 m)
  • Height: 24 ft 10 in (7.57 m)
  • Wing area: 829 sq ft (77.0 m2)
  • Aspect ratio: 11.967
  • Airfoil: root: NACA 23018; tip: NACA 4412[57]
  • Empty weight: 27,126 lb (12,304 kg)
  • Max takeoff weight: 46,500 lb (21,092 kg)
  • Fuel capacity: 1,440 imp gal (1,730 US gal; 6,500 L) in two wing integral tanks
  • Powerplant: 2 × Rolls-Royce RDa.7 Dart Mk 536-2 turboprop engines, 2,280 shp (1,700 kW) each equivalent
  • Propellers: 4-bladed Dowty Rotol constant-speed fully-feathering propellers, 12 ft 0 in (3.66 m) diameter

Performance

  • Cruise speed: 244 kn (281 mph, 452 km/h)
  • Range: 926 nmi (1,066 mi, 1,715 km) (with max payload)
  • Service ceiling: 25,000 ft (7,600 m)
  • Wing loading: 56.1 lb/sq ft (274 kg/m2)
  • Power/mass: 0.0981 hp/lb (0.1613 kW/kg)
  • Take-off distance to 50 ft (15 m): 3,800 ft (1,200 m)
  • Landing distance from 50 ft (15 m): 2,034 ft (620 m)
  • Take-off distance: 2,624 ft (800 m)
  • Landing distance: 1,968 ft (600 m)

See also

[edit]

References

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The HS 748 (later 748) is a medium-sized originally designed by in the late 1950s as a replacement for the Douglas DC-3. The project began as the Avro 748, with the first flying on 24 June 1960; following Avro's merger into , series production started in 1961 and continued until 1988. A total of 381 aircraft were manufactured, including 89 licence-built by in . The HS 748 was employed primarily in regional passenger and cargo operations, with military variants serving in transport and maritime roles for air forces including the Royal Air Force and .

Design and development

Origins and background

In the aftermath of , the British aviation industry grappled with substantial challenges, including the reorientation from wartime military production to , intense competition from American manufacturers like Douglas, and the need for government-guided consolidation to sustain competitiveness. The , convened in 1942 under Lord Brabazon of Tara, played a pivotal role by outlining future civil aircraft requirements, emphasizing the development of short- and medium-haul feeder airliners to support regional networks and replace outdated piston-engine types such as the Douglas DC-3. This recommendation highlighted the demand for versatile, economical aircraft capable of operating from unprepared airstrips in the expanding markets. Responding to these imperatives, and spurred by the which cancelled several military projects, A.V. Roe and Company () launched initial design studies in the late 1950s for a twin- , envisioned as a direct successor to the DC-3 with a capacity for 40 to 50 passengers. The core design prioritized ruggedness and operational flexibility, featuring a high-wing configuration to facilitate short takeoffs and landings on rough fields, a pressurized for comfort on routes up to 1,000 miles, and accommodation for 48 passengers in a standard layout. Power was to be provided by two engines, selected for their proven reliability and efficiency in similar applications. These choices reflected Avro's strategic shift toward civil and export-oriented production amid industry pressures. The 748's conception was shaped by emerging competitors, notably the DH.114 derivative known as the Herald and the Dutch , both high-wing turboprops targeting the same feeder market; Avro's team incorporated lessons from these designs to emphasize structural integrity and multi-role potential, including freighter adaptations. In July 1963, as part of broader industry mergers mandated by the government to streamline operations, was fully integrated into Aviation, leading to the redesignation of the project as the HS 748 while retaining the original technical foundations. To penetrate key export regions, particularly , granted a production license to (HAL) in in 1960, enabling local assembly and customization for and civil needs.

Prototypes and first flight

Two prototypes of the Avro 748 were constructed at the factory in , as part of the initial development effort to validate the design's short take-off and landing () capabilities. The first flying prototype, registered G-APZV and powered by two Mk 514 engines, underwent ground testing before its . The maiden flight occurred on 24 June 1960 from , lasting approximately two hours and piloted by Avro's chief , J.G. "Jimmy" Harrison, with observers on board. Initial impressions highlighted the aircraft's stable handling characteristics and smooth integration of the Dart engines, confirming promising low-speed performance during the short test sortie. The second flying , G-ARAY, followed with its first flight on 10 April 1961, further expanding the evaluation of the airframe's aerodynamic qualities. Flight testing progressed rapidly, with the prototypes accumulating over 1,000 hours between them by early 1962, encompassing a range of maneuvers to assess operations, engine reliability, and systems integration. Key milestones included hot-and-high altitude trials conducted at , , and , , which demonstrated the aircraft's ability to perform in challenging environmental conditions. Early tests also revealed minor aerodynamic issues, leading to adjustments such as refinements to the wing leading edges to improve behavior and enhance overall at low speeds. In 1963, following the merger of A.V. Roe and Company (Avro) into Hawker Siddeley Aviation, the program transitioned under the new branding, with the aircraft officially redesignated the Hawker Siddeley HS 748 to reflect the consolidated . This shift occurred amid ongoing prototype evaluations, ensuring continuity in the development timeline toward certification.

Certification and production

The Hawker Siddeley HS 748 received its British transport category certificate of airworthiness on 9 January 1962, following extensive testing that confirmed its suitability for short-haul operations on unprepared airstrips. This certification enabled the type's entry into commercial service later that year, with the Series 1 variant featuring Rolls-Royce Dart R.Da.6 Mk 514 turboprop engines rated at 1,400 kW (1,880 ehp) each. The U.S. Federal Aviation Administration issued its type certificate in 1963, broadening the aircraft's market access in North America. Production commenced with the Series 1 in , with 24 units built between and at Hawker Siddeley's facilities in Woodford, , including initial assemblies under license in . In , manufacturing shifted to the improved Series 2, which incorporated uprated R.Da.7 Mk 531 engines providing 1,420 kW (1,910 ehp), enhanced , and optional stretched configurations for increased capacity. This transition addressed performance demands in diverse environments, with Series 2 and later models emphasizing ruggedness for regional routes. Overall production totaled 382 aircraft by 1988, comprising approximately 267 civil units and 89 variants across all series. Hindustan Aeronautics Limited (HAL) in produced 89 HS 748s between 1961 and 1988 at its facility, supporting local needs and exports while adhering to specifications. The program's economics reflected 1960s challenges, with unit costs around £176,000 for early Series 1 models, though exports faced stiff competition from American and continental European turboprops like the Fokker F27 and Fairchild F-27. Despite this, the HS 748's versatility sustained steady output until the final assembly in December 1988.

Operational history

Civil operations

The Hawker Siddeley HS 748 entered commercial service on April 1, 1962, with launch customer Skyways Coach-Air Limited (later part of the group), operating on short-haul routes across such as to . The aircraft's rugged design and short takeoff and landing () performance made it suitable for regional operations from smaller airfields, quickly establishing a niche in feeder services. By the early 1970s, over 100 HS 748s had been sold to airlines in more than 30 countries, with strong adoption in developing regions due to its ability to serve remote and unpaved airstrips. Key civil operators included , which used the type for domestic feeder routes in challenging terrain, and , which operated HAL-built versions for regional connectivity in . In , operators like those in utilized the HS 748 for similar short-haul services to isolated areas, leveraging its reliability in hot-and-high environments. The HS 748 began phasing out from major passenger fleets in the 1980s and 1990s, displaced by more efficient regional jets and turboprops such as the Fokker F28 and Embraer EMB-120. Following the retirement of the last civil operator, , in May 2025, no airworthy civil HS 748s remain in service globally as of November 2025. In the 2000s, many surplus HS 748s underwent conversion to freighter configurations, incorporating large cargo doors for palletized loads, which extended their utility for regional cargo operations in and . Operators such as in employed these converted aircraft for short-haul freight until their retirement in the mid-2020s, capitalizing on the type's advantages in underdeveloped infrastructure.

Military service

The Royal Air Force adopted the Hawker Siddeley Andover, a militarized variant of the HS 748, in 1965 to fulfill tactical transport requirements, with the first production aircraft delivered for trials at RAF Boscombe Down that year. The type entered operational service in 1966 with No. 46 Squadron at RAF Abingdon, later serving with units such as No. 52 Squadron in the Far East Air Force for short take-off and landing operations from forward bases. A total of 37 Andover aircraft were built for the RAF, comprising 31 C.1 tactical transports delivered by 1968, six CC.2 VIP transports, and conversions including nine E.3 navigator trainers and two C.1(PR) for photo-reconnaissance duties. Military adaptations distinguished the Andover from its civil HS 748 origins, including a hydraulic "" undercarriage to lower the rear for easier loading, a strengthened floor capable of handling heavy pallets, paratroop doors for airborne operations, and a rear ramp for rapid freight or troop deployment. Some examples were fitted with electronic countermeasures equipment for protection in contested environments, enhancing their utility in tactical support roles. The aircraft supported in regions such as and during the 1970s, providing reliable short-field performance for expeditionary missions. Export sales expanded the Andover's military footprint, with the Indian Air Force receiving over 50 HS 748 aircraft—many license-built by —configured for transport, navigation training, and VIP duties from the late 1960s onward. The acquired five HS 748s between 1970 and 1976 for transport roles. The RAF began phasing out the Andover in the late 1970s for tactical transports, with remaining E.3 and CC.2 variants retired by 1991, replaced by more modern types like the . In contrast, the maintained operational HS 748s into the 2020s for VIP transport and training, though several were placed in storage by 2025.

Variants

HS 748 series

Total production of the HS 748 family reached 381 aircraft, including civil and military variants. The HS 748 series comprised the initial civil production models of the twin-turboprop airliner, introduced as a medium-range feederliner capable of operating from short and unprepared runways. These variants established the core design before subsequent enhancements like the Super 748. Production emphasized reliability for regional routes, with a focus on low operating costs and versatility in passenger configuration. The Series 1 was the first production version, with 20 aircraft assembled between 1961 and 1964. Configured for up to 48 passengers in a pressurized cabin, it was powered by two RDa.6 Mk 514 engines, each rated at 1,400 kW (1,874 ehp), driving four-bladed propellers. The was limited to 36,800 lb (16,690 kg), enabling short-field performance suitable for smaller airports. The Series 2 entered service in 1962 and continued until 1988, with 192 units built featuring a stretch that increased seating to 52 passengers. It incorporated uprated R.Da.11 Mk 534 engines at 1,450 shp each for improved climb and hot/high performance, along with enhanced pressurization maintaining a 7,000 ft cabin altitude at operational ceilings. This allowed greater comfort on longer sectors compared to the Series 1. Sub-variants of the Series 2 included the 2A and 2B models, which added modern suites for better and instrument approaches, as well as quick-change interiors permitting rapid reconfiguration between passenger and cargo roles via removable seats and a large aft door. (HAL) in produced versions under , including the Series 2 for civil applications and the Series 2M adapted for military transport. In total, approximately 279 civil aircraft from the HS 748 series were manufactured, with approximately 80% delivered to export customers outside the , reflecting strong international demand in developing markets. The Series 2 achieved a cruise speed of 220 knots and a range of 1,000 nautical miles with full payload, prioritizing efficiency for regional networks.

Super 748

The Super 748 represented an advanced evolution of the HS 748 Series 2, aimed at enhancing performance for civil regional operations with greater capacity and efficiency. Development of this variant was announced in as part of Hawker Siddeley's to extend the type's competitiveness in the short-haul market, building on the Series 2 predecessor by incorporating more powerful engines and aerodynamic refinements. The prototype achieved its first flight on 21 July 1977, leading to production that spanned 1979 to 1988, during which 8 aircraft were constructed. These featured two Mk 552 engines, each rated at 1,750 shp, providing improved power for demanding conditions. Key enhancements in the Super 748 included a maximum seating capacity of 58 passengers, a maximum takeoff weight of 46,500 lb (21,092 kg), a cruise speed of 235 knots, and a range of 1,200 nautical miles, all contributing to superior hot-and-high performance compared to earlier models. The aircraft incorporated four-bladed propellers for reduced noise and better efficiency, an increased wingspan of 102 ft 6 in (31.23 m) versus 98 ft 6 in (30.02 m) on the original series, and an optional electronic flight instrument system (EFIS) cockpit for modernized avionics. These upgrades positioned the Super 748 as a more capable feederliner for routes requiring short takeoffs and reliable operations in varied environments. Market demand focused on export sales, with primary customers including East-West Airlines in , and operators in such as . Deliveries continued under following the 1977 merger of into the new entity. Production of the Super 748 ultimately ceased in 1988 as shifted resources to the development of its successor, the ATP turboprop , which promised further advancements in speed and capacity.

Andover military variants

The Andover C.1 was the principal tactical transport variant of the HS 748 developed for the Royal Air Force, incorporating a rear loading ramp and kneeling to enable efficient loading of troops and cargo on unprepared airstrips. Thirty-seven aircraft were constructed between 1965 and 1973, each powered by two RDa.12 Mk 201 engines rated at 2,420 kW (3,245 eshp), and capable of carrying up to 48 paratroops or 52 seated troops. The Andover E.3 served as a dedicated navigator training platform, with seven aircraft converted featuring specialized radar equipment and astro-domes to support aerial navigation instruction and calibration tasks. These conversions from earlier C.1 models were employed primarily for training aircrew in radar navigation and electronic systems until their retirement in 2011. Six Andover CC.2 aircraft were converted from C.1 airframes to perform electronic intelligence (ELINT) and communications intelligence (COMINT) reconnaissance missions, outfitted with side-looking airborne radar for signals monitoring. Export military adaptations of the HS 748 included the HAL-built Series 2M variant produced under license in specifically for the , serving in transport and VIP transport roles with strengthened floors and large freight doors on later examples. The received seven C-748 aircraft based on the HS 748 design for similar tactical transport duties. Military Andover variants were distinguished from their civil HS 748 counterparts by a reinforced structure supporting a maximum take-off weight of 51,000 lb (23,133 kg), integration of military-grade , and the addition of the rear ramp for rapid deployment. Approximately 44 UK-built Andover units were manufactured for the RAF across all sub-variants, with additional licensed variants produced elsewhere.

Operators

Civil operators

The Hawker Siddeley HS 748 saw extensive civil use by airlines and operators worldwide, with more than 200 units entering service historically across passenger and freighter roles.

Current operators (as of 2025)

As of November 2025, following the retirement of the last North American civil HS 748 on May 30, 2025, very few or no airworthy examples remain in civil service worldwide. Small operators in may maintain limited freighter operations, but no specific active fleets are confirmed. Most civil HS 748s were retired by 2000, though freighter adaptations had sustained limited operations in regional cargo networks into the early .

Former major operators

  • British United Airways (United Kingdom): Launch customer with 5 HS 748s introduced in 1962 for short-haul routes; fleet retired in the 1970s following merger into .
  • (India): Largest operator with 89 HAL-built HS 748s delivered from 1962 onward for domestic services; phased out in the 2000s and replaced by jet aircraft.
  • Mount Cook Airline (New Zealand): Operated 5 HS 748s from 1971 for scenic and regional flights; retired in the 1990s amid fleet modernization.
The type had a strong regional footprint in , including operators like () and (), and in , where numerous examples underwent conversions for remote .

Military operators

The Hawker Siddeley HS 748 and its Andover military variants have been operated by forces in at least 10 countries, with maintaining the largest fleet of 56 HAL-built aircraft introduced since 1961. As of 2025, the continues to utilize over 10 HS 748s (known locally as ) primarily for storage, VIP transport, and limited operational roles, while phasing them out in favor of the C-295. Former military operators include the United Kingdom's , which procured approximately 50 Andover variants (including 31 C.1 tactical s and 6 CC.2 VIP aircraft) starting in 1965 and retired the type in 2012 after decades of service in , , and communications roles. The operated 8 HS 748s until retirement in the 1990s. The acquired 12 C-748 transports and used them for various roles until retirement in the 2010s, with several examples preserved post-service. Other historical users include the Royal New Zealand Air Force, which received 10 ex-RAF Andover C.1s in 1976 and retired them in 1998, and the Venezuelan Air Force, which operated 3 HS 748s until the 1980s. The formerly operated HS 748s for transport duties until retirement in the 1990s.

Accidents and incidents

Notable civil accidents

The Hawker Siddeley HS 748 has been involved in 62 civil hull-loss accidents, resulting in 589 fatalities across its operational history. Common contributing factors included adverse weather conditions, pilot error, and challenges associated with short takeoff and landing (STOL) operations on unprepared or rough fields, which were frequent in the aircraft's regional and remote service roles. The first hull loss of an HS 748 occurred on 11 July 1965, when Skyways Coach-Air flight G-ARMV, an Avro 748 Series 1, attempted a heavy landing at Lympne Airport, UK, on a grass runway that could not support the aircraft's weight, causing the nose landing gear to dig in and collapse; all 52 occupants survived with injuries, attributed to pilot error in runway selection. On 15 August 1967, two Channel Airways HS 748 Series 2 aircraft, G-ATEK and G-ATEH, overran the wet grass runway during landings at Airport, , due to low coefficient of friction and inadequate braking performance; both aircraft sustained substantial damage but there were no fatalities among the occupants. One of the deadliest civil accidents involving the HS 748 was on 26 June 1987, when the Series 2 aircraft, registration RP-C1015, flew into Mount Ugo near , , during approach in poor visibility and bad weather, resulting in a that killed all 50 people on board. On 4 August 1979, flight VT-DXJ, a HAL-built HS 748 Series 2, crashed into hilly terrain 12 km from , , after a loss of electrical power led to instrument failure and in clouds; all 45 occupants perished. In , a HS 748 Series 2A, registration PP-VDP, was involved in an accident on 24 April 1974 at Iguatu Airport, where it overran the runway during landing, resulting in minor damage but no fatalities; the cause was not publicly detailed but aligned with common issues of rough field operations. A notable non-fatal incident occurred on 17 February 1998, when Wasaya Airways HS 748 Series 2A C-GTAD made a hard landing at Kasabonika Airport, Ontario, Canada, due to pilot mismanagement of approach speed and configuration, causing substantial damage to the landing gear and fuselage but no injuries to the three occupants.

Military incidents

The military variants of the Hawker Siddeley HS 748, including the Andover and HAL-748, experienced several notable incidents during operations, often linked to mechanical issues or operational hazards in training and conflict environments. One significant event occurred on April 8, 1972, when RAF Andover C.1 XS609 of No. 46 Squadron crashed shortly after takeoff from Siena-Ampugnano Airport in Italy. The aircraft, carrying members of the RAF Falcons parachute display team, suffered a left engine failure, leading to a loss of control, cartwheel, and fire; four people were killed, including the two pilots and two passengers, while 19 others survived with injuries. In a tragic on March 25, 1991, an HAL-748 (H-1513) stalled and crashed moments after departing near Bangalore, , killing all 28 aboard—comprising 25 trainee pilots and three crew members. The aircraft reached only about 165 feet before plunging to the ground and bursting into flames; investigations pointed to possible control difficulties during initial climb, potentially exacerbated by technical factors or procedural errors under high-workload conditions. Sri Lanka Air Force Avro 748 operations faced threats from insurgent activity during the civil conflict. On April 28, 1995, Avro 748 CR835 was struck by a Liberation Tigers of Tamil Eelam (LTTE)-fired SA-7 surface-to-air missile while approaching Palaly Air Base, causing it to crash with the loss of all three crew members. The following day, April 29, 1995, another Avro 748 (CR834) met a similar fate on approach to the same base, shot down by an SA-7 missile and resulting in 52 fatalities among the passengers and crew, many of whom were military personnel. These shootdowns underscored vulnerabilities in low-level operations over contested areas. Across military services, such incidents were frequently attributed to stresses like engine reliability challenges during demanding takeoffs, stall risks in profiles, or exposure to hostile in zones, prompting reviews of maintenance protocols and tactical procedures.

Preserved aircraft

Australia

In , the Hawker Siddeley HS 748 is represented among preserved aircraft primarily through former examples. A10-601, a Series 2 variant (c/n 1589), is preserved on static display at the in Point Cook, Victoria. Originally delivered to the RAAF in July 1968 for navigation duties with No. 32 Squadron, it was retired in 2002 and relocated to the museum for preservation in 2004, where it remains coated in protective latex pending indoor housing. An additional airframe, the fuselage of A10-607 (Series 2, c/n 1707), is stored outdoors at in Victoria. Formerly operated by the RAAF for transport roles until retirement in 1998, it was sold to International Air Parts Pty Ltd in 1999 and transported by road to Avalon, serving as a spares source for maintenance of other HS 748s.

Brazil

In Brazil, preserved examples of the Hawker Siddeley HS 748 are limited to former aircraft, designated as C-91 in military service. These twin-turboprop transports were acquired starting in 1963 to support transport and roles, with six Series 2A variants delivered between 1963 and 1975. One notable preserved aircraft is FAB 2502 (c/n 1552, HS 748 Series 2A), which was delivered on 18 April 1963 and served with the 2º/2º Grupo de Transporte at Galeão Air Base. Decommissioned after accumulating over 10,000 flight hours, it has been statically displayed outdoors at the entrance to Galeão International Airport (also known as Galeão Air Force Base) in Rio de Janeiro since the early 2000s, serving as a to highlight the type's role in Brazilian military aviation. Another example, FAB 2504 (HS 748 Series 2A, equipped with RDa.7 Mk 533-2 engines), operated until its deactivation in 2001 following extensive service in transport duties. It was subsequently transferred to the Museu Aeroespacial (MUSAL) in Rio de Janeiro's Campo dos Afonsos district, where it has been on public display indoors since 2001 as part of the museum's collection of over 100 aircraft, emphasizing Brazil's aviation heritage.

Canada

In Canada, preserved examples of the Hawker Siddeley HS 748 are housed in aviation museums, with a notable 2025 development marking the retirement of the last airworthy aircraft in the country. The Hawker Siddeley HS 748 Series 2A, registration C-FLIY, was donated by to the Canadian Aviation Museum in , in late May 2025. This aircraft, which had accumulated over 50 years of service primarily in regional and northern Canadian operations, was the final airworthy HS 748 in Canada before its retirement. It completed its last flight on May 30, 2025, landing at Windsor Airport amid a ceremonial , and is now preserved for public display to commemorate its contributions to remote community connectivity and Indigenous aviation history.

Ecuador

In Ecuador, preserved examples of the Hawker Siddeley HS 748 are primarily housed at the Museo Aeronáutico y del Espacio de la Fuerza Aérea Ecuatoriana, located at the Mariscal Sucre Air Base in . This museum serves as a repository for retired assets, showcasing the contributions of the HS 748 to the 's operations. One key exhibit is FAE-684 (civil HC-AUK), a Series 2A variant with constructor's number 1684, which was originally delivered to the in the and later repurposed for VIP , including presidential duties marked by the and the designation "001". Decommissioned in 2013 after over three decades of service, it was transferred to the museum for static display, where it remains accessible to visitors as a representative of the type's military utility. Another significant preserved aircraft is FAE-738 (HC-BAZ), a Series 2A LFD freighter variant, constructor's number 1738, later acquired by the for cargo and troop transport roles after operating with Ecuador. On June 23, 1987, while with TAME, it suffered an overrun during landing at Lago Agrio Airport (LGQ) due to an electrical system failure, rendering it beyond economic repair with substantial damage to the forward . Repaired cosmetically for display purposes, including reconstruction of the cockpit section, it has been exhibited at the museum since shortly after the incident, highlighting the operational hazards faced by HS 748 units in rugged Andean environments.

India

The HAL Heritage Centre and Aerospace Museum in Bangalore preserves examples of HAL-built Hawker Siddeley HS 748 aircraft, highlighting India's capabilities. At the Museum at Palam Air Force Station in , the tail section of an ex-IAF HS 748 (J/H-1512) is visible, representing the type's service in training roles.

Sri Lanka

In , one example of the Hawker Siddeley HS 748 is preserved on static display at the Sri Lanka Air Force Museum, located at near . This aircraft is an Avro 748 Series 1 (c/n 1587), bearing the CR-831, which was originally delivered to in 1967 and transferred to the in 1978 upon the national carrier's closure. It served in transport roles with the air force until its withdrawal from operational use, after which it was placed on exhibit at the museum in November 1996, where it remains as a historical artifact showcasing the type's contributions to Sri Lankan .

Thailand

One preserved example of the Hawker Siddeley HS 748 is on display at the Royal Thai Air Force Museum in , . This Series 2 aircraft, bearing constructor's number 1570 and Royal Thai Air Force serial 60301 (previously registered as L5-1/08), exemplifies the type's dual civil and military applications in Thai service. Originally delivered directly to the in 1965, it operated primarily in transport roles, including troop and cargo missions that occasionally supported civil efforts, reflecting its hybrid utility in regional operations. The aircraft remained in active for over five decades, with its identification code updated to 60301 around 2005, before from operational duties. It was then relocated to the at Don Mueang Airport in 2017, where it has been maintained in static display to showcase the HS 748's contributions to Thai aviation . This preserved HS 748 serves as a key exhibit in the 's collection of , highlighting the model's reliability in Southeast Asian environments and its role in bridging civil and military air needs during the late 20th and early 21st centuries. Visitors can view it outdoors alongside other retired RTAF assets, underscoring the enduring legacy of the type in .

United Kingdom

Several examples of the Hawker Siddeley HS 748 and its military variants are preserved in the , primarily in aviation museums and private collections, showcasing the aircraft's role in civil and history. The nose section of HS 748 Series 2A G-ORAL (c/n 1756), built in 1977 at Woodford, is on static display at the in . Originally delivered to as G-BEOZ before being re-registered, this forward fuselage section was acquired by the museum in 2010 after storage and serves as a key exhibit highlighting the type's design and instrumentation. A complete Series 1 , G-BEJD (c/n 1543), is preserved by the Group near . Delivered new in 1962 to , this example has been maintained in static condition since the early and represents one of the earliest production HS 748s; in 2023, it was elevated onto new supports for better preservation and public viewing. The RAF Museum Cosford houses Andover E.3A XS639 (c/n 1715), a variant of the HS 748, on public display in its main since the early . Built in 1968 and retired from RAF service in 1997 after over 4,000 flying hours, this aircraft exemplifies the type's adaptation for electronic warfare support roles, complete with original equipment for and aid .

Specifications

General characteristics

The Hawker Siddeley HS 748 Series 2A is a twin-engine designed for short- to medium-haul operations, featuring a of two pilots. It has a typical passenger capacity of 48 in a four-abreast configuration, with high-density seating up to 52 passengers or a maximum of 11,323 lb (5,136 kg). Key dimensions include a of 67 ft 0 in (20.42 m), of 98 ft 6 in (30.02 m), height of 24 ft 10 in (7.57 m), and wing area of 811 sq ft (75.35 m²). The is 26,800 lb (12,159 kg), with a of 46,500 lb (21,092 kg) and fuel capacity of 1,441 imp gal (6,550 L). It is powered by two RDa.7 series engines (e.g., Mk 531-535), each delivering up to 2,280 equivalent shaft horsepower (1,700 kW), driving four-bladed Dowty Rotol constant-speed fully feathering reversible-pitch propellers. The later Super 748 (Series 2B) variant featured modifications including a increase to 50,000 lb (22,680 kg) and a wingspan extension to 102 ft 6 in (31.24 m) with area of 829 sq ft (77.01 m²).

Performance

The Hawker Siddeley HS 748 Series 2A demonstrated robust flight performance suited to regional operations, achieving a maximum speed of 260 knots (299 mph, 482 km/h) and a cruising speed of 244 knots (280 mph, 452 km/h) at typical operational weights. Its range with maximum payload reached 735 nautical miles (1,360 km), while the ferry range extended to 1,690 nautical miles (3,130 km) with reserves. The service ceiling stood at 25,000 ft (7,620 m), supported by an initial of 1,320 ft/min (6.7 m/s) at , ISA. Takeoff performance was a key strength, with a balanced field length of approximately 4,000 ft (1,220 m) at under standard conditions, and capabilities for rough-field operations as short as 3,200 ft (975 m). The Super 748 variant incorporated enhancements such as more efficient hush-kitted engines and aerodynamic refinements, yielding approximately 25% greater range with maximum payload at 926 nautical miles (1,715 km) and a reduced takeoff distance of around 2,800 ft (853 m) on unprepared surfaces. These upgrades maintained the cruising speed at 244 knots (280 mph, 452 km/h) while improving overall efficiency for short-haul routes. The military Andover derivative exhibited comparable baseline performance to the Series 2A but incurred penalties from added equipment and troop-carrying configurations, resulting in a reduced cruise speed of 235 knots (270 mph, 435 km/h) and a service ceiling of 24,000 ft (7,315 m). was similarly affected, dropping to about 1,200 ft/min (6.1 m/s) under typical operational loads. At economical cruise settings, each engine consumed approximately 600 lb (272 kg) of fuel per hour, contributing to the aircraft's viability for extended regional missions.

References

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