|British Merlin HM1 in August 2012|
|Role||Anti-submarine warfare (ASW) and medium-lift transport / Utility helicopter|
|First flight||9 October 1987|
|Primary users||Royal Navy
Royal Air Force
Royal Danish Air Force
US$21 million (2009)
|Variants||AgustaWestland CH-149 Cormorant
Lockheed Martin VH-71 Kestrel
The AgustaWestland AW101 is a medium-lift helicopter used in both military and civil applications. It was developed by joint venture between Westland Helicopters in the UK and Agusta in Italy in response to national requirements for a modern naval utility helicopter; until 2007, the aircraft had been marketed under the designation EH101. Several operators, including the armed forces of Britain, Denmark and Portugal, use the name Merlin for their AW101 aircraft. It is manufactured at factories in Yeovil, England and Vergiate, Italy; licensed assembly work has also taken place in Japan and the United States.
In 2000, Westland Helicopters and Agusta merged to form AgustaWestland, leading to the type's redesignation as AW101. The AW101 first flew in 1987, and entered into service in 1999. Since the AW101's introduction it has replaced several older helicopter types such as the Sikorsky S-61, performing roles such as medium-sized transport, anti-submarine warfare, and ship-based utility operations.
The Royal Canadian Air Force (RCAF) operates a variant of the AW101, designated CH-149 Cormorant, in the air-sea rescue role. Another variant, designated VH-71 Kestrel, was developed to serve in the US presidential transport fleet, however the program was cancelled. Civil operators also use AW101s in roles such as passenger and VIP transportation. The type has been deployed to active combat theatres, such as in support of coalition forces during the Iraq War and the War in Afghanistan.
- 1 Development
- 2 Design
- 3 Operational history
- 4 Variants
- 5 Operators
- 6 Notable accidents and incidents
- 7 Specifications (Merlin HM1)
- 8 Notable appearances in media
- 9 See also
- 10 References
- 11 External links
In 1977, the UK Ministry of Defence issued a requirement for an anti-submarine warfare (ASW) helicopter to replace the Royal Navy's Westland Sea Kings, which were becoming inadequate in the face of advances in Soviet submarine technology. Westland Helicopters put together a proposal, designated WG.34, for a three-engined helicopter of similar dimensions to the Sea King; the WG.34 was to feature more autonomy and a greater range than its predecessor. At the same time, the Italian Navy (Marina Militare), was also considering the replacement of its fleet of Sea Kings built by the Italian company Agusta; Westland and Agusta soon began talks regarding joint development of a successor helicopter.
Agusta and Westland finalised an agreement to work on the project together, and formed a jointly-owned new company, EH Industries Limited (EHI), to pursue the development and marketing of the new helicopter to potential operators. On 12 June 1981, the UK government confirmed its participation in the project, allocated an initial budget of £20 million to develop nine pre-series examples. A major agreement, which secured funding for the majority of the EH101's development program, was signed by both the British and Italian governments in 1984. At the 1985 Paris Air Show, Agusta showed a mock-up of a utility version of the new helicopter, leading to a more generalised design that could be customised to meet the needs of various civilian or military customers. The first prototype flew on 9 October 1987.
In 1987, Canada had selected the EH101 to replace their Sea Kings in anti-submarine warfare and search and rescue roles; the EH101's third engine and increased autonomy compared favorably against rivals such as the Sikorsky Seahawk, its range and de-icing capability were also seen as vital for North Atlantic operations. The fledgling EH101, of which up to 50 were on order to replace the Canadian Armed Forces's (CAF) Sea Kings, found itself subject to a wider political battle between the Conservative and Liberal parties, the latter viewing the aircraft as too costly. Critics attacked the EH101 purchase as excessive and unnecessary after the Cold War's end in the early 1990s. Wide-ranging cost estimates were presented by both proponents and opponents of the EH101 procurement, with opponents backing life extensions of Sikorsky CH-124 Sea King and Boeing Vertol CH-113 Labrador helicopter fleets. The EH101 controversy was seen as a factor in the 1993 Canadian federal election. The order was cancelled by the new Liberal government in 1993 resulting in a $470 million cancellation fee.
Several pre-production aircraft were assembled during the late 1980s and early 1990s. Flight tests were suspended for six months following the crash of the second pre-production aircraft on 21 January 1993. On 6 June 1993, the first EH101 flew with the Rolls-Royce/Turbomeca RTM322 turboshaft engine. Nine prototypes were built to explore military and civil applications, including a "heliliner" configuration. In February 1995, Britain formally placed its first order for a total of 22 EH101s; this was quickly followed by Italy's order for 16 EH101s in October 1995. The EH101 order was not without controversy, the RAF had declared its preference for an all-Chinook fleet; also, Boeing allegedly offered cheaper terms for the Chinook. In 1997, RAF deliveries began, RN deliveries started the following year.
In 2005, a team of AgustaWestland and Lockheed Martin was selected as the winners of the US VXX competition to replace the President's Marine One helicopters of the United States Marine Corps. A variant of the AW101, designated VH-71 Kestrel, was to be manufactured domestically and had proceeded into the flight testing stages. However the programme encountered significant cost overruns and political opposition, which led to the procurement being scrapped in June 2009. Separately, the Marine Corps had also conducted studies into the adoption of the EH101 as a fallback option to the Bell-Boeing V-22 Osprey tiltrotor during the 1990s.
Following the merger of Westland and Agusta to form AgustaWestland in 2000, there was no need for the separate EHI entity; the EH101 was formally re-branded as the AW101 in 2007. In 2008, the volume of AW101 orders was reported as having filled production capacity in excess of the following five years. By April 2009, more than 180 AW101s had been sold worldwide; the combined operational fleet had also accumulated a total of 170,000 flying hours.
In November 2007, Algeria signed a contract for 6 AW101 helicopters. In August 2012, it was reported that Algeria had signed an agreement with AgustaWestland for the provision of up to 80 helicopters, 42 of which were to be AW101s. Under the terms of this arrangement, early aircraft were to be manufactured by AgustaWestland, while Algeria was to commence the assembly of some AW101s later on.
The AW101 was a candidate in the Norwegian All Weather Search and Rescue Helicopter (NAWSARH) programme to replace the Royal Norwegian Air Force's Westland Sea King Mk.43B helicopter fleet. Other candidates included Bell Boeing V-22 Osprey, Eurocopter EC225, NHIndustries NH90, and Sikorsky S-92. Iceland cooperated with Norway on the programme and was to buy 3–4 helicopters to replace its Super Puma helicopters, but withdrew in 2012 due to limited finances. The AW101 was selected in November 2013.
On 7 June 2010, it was announced that Boeing had acquired a manufacturing license and the rights from AgustaWestland for US production of a localised AW101 variant, designated as the Boeing 101. In October 2012, the AW101 was submitted in a U.S. Air Force competition to replace the HH-60 Pave Hawk; however the bid was dropped three months later.
In September 2013, AgustaWestland was reportedly in the process of acquiring new civil certification for the AW101, target customers include long-range offshore oil platform transport operators and VIP clients. As of February 2014, AgustaWestland was considering adapting the AW101 as a heavyweight unmanned aerial vehicle, it is proposed that in this configuration an AW101 could be optionally manned.
The AW101 Merlin follows a conventional design layout but makes use of advanced technologies such as the design of the rotor blades, avionics systems, and the extensive use of composite materials. The fuselage structure is modular and comprises an aluminium-lithium alloy, designed to be both light and damage-resistant. The AW101 is designed for operating in extreme weather conditions; it is fitted with a de-icing system and rated to operate in temperatures ranging between −45 to +50 °C. The aircraft's control systems allow the AW101 to maintain a stable hover in 74 km/h (40 kn) crosswinds.
An active vibration control system, known as the active control of structural response system, reduces airframe vibration by up to 80% which increases crew comfort and minimises the buildup of stress on the airframe. The cockpit is fitted with armoured seats for the crew, and can withstand an impact velocity of over 10 m/s. Dual flight controls are provided, though the AW101 can be flown by a single person. The pilots' instrument displays include six full-colour high-definition screens and an optional mission display; a digital map or forward-looking infrared (FLIR) display can also be installed.
The AW101 is powered by three turboshaft engines. Two different types of engines available for operators, the Rolls-Royce/Turbomeca RTM322 used by the UK, Japan, Denmark and Portugal; or the General Electric CT7 used by Italy, Canada, and Japan. The Rolls-Royce RTM322 engine was specifically developed for the AW101; it was subsequently adopted on the WAH-64 Apache and the NHIndustries NH90 helicopters. About 80% of AW101s use the RTM322 powerplant, according to Rolls-Royce.
The engines power an 18.59 metre diameter five-bladed main rotor. The rotor blades are constructed from carbon/glass with nomex honeycomb and rohacell foam, edged with titanium alloy in a sandwich construction. The shaping of the main rotor blades is derived from the BERP rotor blades first used on the Westland Lynx. This blade design improves aerodynamic efficiency at the blade tip and reduces the noise signature. Improved BERP IV rotors have since been developed; when installed, this increases the AW101's maximum takeoff weight.
Each engine is supplied by a separate 1,074 litre (276 US Gallon, 230 Imperial Gallon) fuel tank using dual booster pumps. Optional fourth and fifth tanks can be added to act as a reservoir supply, topping up the main tanks during flight, increasing range or endurance. The AW101 can also be outfitted with a probe for aerial refuelling. Self-sealing fuel tanks are an optional item to be selected by the customer. An inlet particle separator system can be installed, protecting the engine when operating in sandy environments.
Armament and defensive systems
Most variants of the AW101 are equipped with self-defence systems such as chaff and flare dispensers, directed infrared countermeasures (infrared jammers), ESM (electronic support measures in the form of RF heads), and a laser detection and warning system. British Merlins have been outfitted with protective armouring against small-arms fire. A chin-mounted forward looking infrared (FLIR) imaging sensor has been fitted to some variants.
Two hardpoints are present on the underside of the airframe on which the HM1 model can carry four Sting Ray torpedoes or Mk 11 Mod 3 depth charges. Some customers have chosen to deploy the Marte anti-ship missile on the AW101; as of 2011, the Royal Navy is considering equipping their Merlin fleet with an anti-surface missile. The Mk1, Mk3 and Mk3A variants can mount general purpose machine guns in up to 5 locations in the main cabin, aimed out of both door and window apertures. AgustaWestland has examined the integration of rockets and additional ground-attack weapons.
Westland and IBM formed a consortium in 1991 to perform the helicopter's complex systems integration. The AW101 features a network of helicopter management and mission systems designed to reduce pilot workload and enable the helicopter to undertake a wide variety of missions. A digital automatic flight control system (AFCS) is employed by the AW101. The AFCS allows the operation of a four-axis (pitch, roll, yaw and collective) autopilot and the automatic stabilisation system, and is linked in with the aircraft's flight management systems. The AFCS, manufactured by Smiths Aerospace, is a dual-duplex system using two flight computers to provide redundancy and fault-tolerance.
The AW101's navigation system includes a GPS receiver and inertial navigation system, VHF omnidirectional radio range (VOR), instrument landing system (ILS), TACAN, and automatic direction finding. The Mk1 and Mk3 are equipped with a Doppler velocity system (DVS) which provides relative ground velocities; the DVS is also linked into the AFCS as part of the autostabilisation system. For safety, the aircraft is equipped with obstacle and terrain avoidance warning systems, traffic collision avoidance system (TCAS), and both voice and flight data recorders.
The AW101 is equipped with the Blue Kestrel search and detection radar which is capable of 360 degree scanning and can detect small targets as far as 25 nautical miles. As part of the Royal Navy's Merlin HM2 upgrade program, Lockheed Martin implemented a series of improvements to the radar, notably allowing it to track 40 times the number of targets previously capable. Danish EH101s are fitted with the RDR-1600 search and weather radar. Royal Navy Merlins are equipped with the AQS901 anti-submarine system for processing sonographic data from sonobuoys to detect and target submerged submarines. The AQS901 was derived from the system on the earlier Hawker Siddeley Nimrod maritime patrol aircraft.
Crew and cargo
The AW101 is typically operated by a crew of three: a pilot, an observer, and a crewman/operator. The pilot is able to fly for the majority of a mission in a hands-off mode, enabled by the sophisticated autopilot. All crew members have individual access to management computers and tactical information.
The fuselage has a volume of 31.91 cubic metres (1,127 cu ft) and the cargo compartment is 6.5 metres (21 ft) in length, 2.3 metres (7 ft 7 in) wide and 1.91 metres (6 ft 3 in) high. The military version of the AW101 can accommodate up to 24 seated or 45 standing combat troops and their equipment. Alternative loads include a medical team and 16 stretchers, and cargo pallets.
The ramp, 1.91 by 2.3 metres (6 ft 3 in × 7 ft 7 in), can take a 3,050-kilogram (6,720 lb) load, allowing it to carry vehicles such as Land Rovers. The ramp and cabin floor are fitted with flush tie-down points. A cargo hook under the fuselage can carry external loads of 5,440 kilograms (11,990 lb) via the use of a semi-automatic cargo release unit (SACRU). A rescue hoist and a hover trim controller are fitted at the cargo door. An optional cargo winch can be installed near to the rear ramp.
The RN's final order was for 44 ASW aircraft, originally designated Merlin HAS.1 but soon changed to Merlin HM1. The first fully operational Merlin was delivered on 17 May 1997, entering service on 2 June 2000. All aircraft were delivered by the end of 2002, and are operated by four Fleet Air Arm squadrons: 814 NAS, 820 NAS, 824 NAS and 829 NAS, all based at RNAS Culdrose in Cornwall. 700 NAS was the Merlin Operational Evaluation Unit from 2000 to 2008. In March 2004, Navy Merlins were temporarily grounded following an incident at RNAS Culdrose in which a tail rotor failed due to a manufacturing defect. An improved tail rotor was designed and adopted on most AW101s; according to AgustaWestland the redesigned rotor also significantly reduced associated maintenance.
The Merlin HM1 has been cleared to operate from the Royal Navy's aircraft carriers, amphibious assault ships, Type 23 frigates and several Royal Fleet Auxiliary (RFA) vessels including the Fort Victoria class; it is also to equip the Type 45 destroyer. 30 aircraft are being upgraded to Merlin HM2 standard under the £750m Merlin Capability Sustainment Programme which runs to 2015. The HM2 has a new mission system, digital cockpit, electro-optical camera and multi-static processing for the sonar system. The HM2 performed its first ship-borne test flight in September 2012 and achieved IOC on 30 June 2014, after nine HM2 had flown 480 hours from Illustrious during Exercise Deep Blue earlier that month. At the same time it was reported that some of the eight airframes not previously scheduled to get the upgrade for financial reasons, may now be updated.
Five of the 30 HM2 will be in maintenance at any one time, leaving 25 available at readiness, of which 14 will be assigned to the new Queen Elizabeth-class aircraft carrier. In addition to its anti-submarine role, the HM2 will be able to carry an airborne early warning (AEW) pod under procurement through the Crowsnest programme to replace the Sea King ASaC7. In September 2011, Thales UK proposed re-using Sea King ASaC7 equipment, such as the Searchwater 2000, on the Merlin; Lockheed Martin has proposed developing a new multi-functional sensor for either the AW101 or other aircraft. Lockheed originally planned to use a derivative of the F-35's APG-81 radar but is now believed to be using an Elta system; both it and the Thales system will begin flight trials in the summer of 2014 with Main Gate in 2016. Ten pods are planned with IOC in 2019.
On 15 December 2009, plans were announced to transfer RAF Merlin HC3s and HC3As to the Commando Helicopter Force to replace retiring Sea King HC4 helicopters. The Sea King is to retire in 2016, after which the Navy will operate a combination of the Wildcat and Merlin. It is intended that 846 NAS will reform with ex-RAF Merlin HC3s in 2015. 845 NAS will follow in 2017, operating the fully navalised Merlin HC4.
In 1995, it was announced the Navy's Westland Lynx helicopters would be retired in favour of an all-Merlin fleet. however, the subsequent 2010 SDSR stated the future naval helicopters to be the Merlin and the Wildcat, a derivative of the Lynx.
Royal Navy Merlins have seen action in the Caribbean, on counter-narcotics and hurricane support duties, as well as maritime security duties in the Persian Gulf. Merlins have also seen active duty in Iraq, providing support to British and coalition forces based in the region.
Royal Air Force
The RAF ordered 22 transport helicopters designated Merlin HC3, the first of which entered service in January 2001 with No. 28 Squadron RAF based at RAF Benson. The type is equipped with extended-range fuel tanks and is capable of air-to-air refuelling; however as of 2012, aerial refuelling has not entered operational usage. The Merlin is frequently utilised for troop transport duties and for the transport of bulky objects, either internally or underslung, including vehicles and artillery. Depth maintenance of the Merlin HC3 is carried out at the Merlin Depth Maintenance Facility at RNAS Culdrose.
The Merlin's first operational deployment was to the Balkans region in 2003. RAF Merlins were first deployed to Iraq as part of Operation Telic in 2004, supporting coalition forces and were operated as the main medevac asset in southern Iraq; both Flight Lieutenant Kev Harris and Flight Lieutenant Michelle Goodman were awarded the DFC during this period. Merlins routinely operated around Basra until Britain's withdrawal in June 2009.
In 2002, Westland made an unsuccessful unsolicited offer to the British Ministry of Defence, proposing an enhanced Merlin variant intended to satisfy the demand for additional lift capacity. An alternative measure was the acquisition of six AW101s from Denmark in 2007; designated Merlin HC3A, these were assigned to the RAF, allowing Merlins to be deployed in Afghanistan. The HC3A is used for training and not for frontline operations due to various configuration differences. In December 2007, a second Merlin squadron, No. 78 Squadron was formed at Benson.
In 2009, five Merlin Mk3s were operating in Afghanistan, transporting troops and supplies. The deployment to Afghanistan was criticized as the aircraft reportedly lacked protective Kevlar armour. By July 2010, the Merlin fleet was fully fitted with ballistic armour. The deployment of Merlins to Afghanistan allowed the detachment of Sea Kings to be withdrawn from the region in October 2011. As part of the UK drawdown in Afghanistan Merlins were withdrawn from theatre in June 2013.
In 2012, RAF Merlins began the transition process over the Royal Navy's Commando Helicopter Force, due to be finalised by 2016 after modifications for extended maritime operations. Royal Navy personnel worked alongside the Royal Air Force at RAF Benson to build experience before the fleet is handed over to the Commando Helicopter Force. A £454m Merlin Life Sustainment Programme will see 25 HC3/HC3A airframes fitted with the cockpit electronics of the HM2, folding tails and main rotor heads, strengthened landing gear, deck lashing mounting points, obsolescence updates, fast-roping points and a common emergency egress system. The first HC4 will begin flight trials in September 2017 with IOC in early 2018; an interim folding main rotor head will be fitted to some HC3 for shipborne operations prior to the HC4 upgrade.
In 1997, the Italian government ordered 20 EH101 helicopters with four options for the Italian Navy. These EH101s included 10 of the anti-surface/submarine (ASuW/ASW) version, 4 airborne early warning (AEW), 4 utility, and 4 amphibious support helicopters (ASH). As of June 2011, the AW101 has also been chosen to meet an Italian Air Force (Aeronautica Militare) requirement for up to 12 helicopters in the combat search and rescue role to replace several ageing Sea King HH-3F; deliveries are expected from 2014 onwards.
The first Italian Navy production helicopter (MM81480) flew on 4 October 1999 and was officially presented to the press on 6 December 1999. Italy accepted delivery of the 21st AW101, configured for anti-submarine warfare, on 4 August 2009. Italian EH101s have operated from a variety of ships and have seen service overseas; in 2009 the Italian Navy used its AW101 fleet as executive transports for visiting heads of state and officials during the 35th G8 summit.
In 2010, the Italian Navy deployed three AW101s to Afghanistan where they were flown in both the transport and utility roles. In 2011, it was reported that the Italian contingent in Afghanistan, consisting of AW101s, had been providing coverage of a wide area of the country.
Royal Canadian Air Force
In 1997, in light of the declining condition of its helicopter fleet, Canada launched the Canadian Search and Rescue Helicopter competition. It was won by the EH101 which was designated CH-149 Cormorant in Canadian service.
In 2004, the EH101 was entered into a Canadian competition to replace the shipboard Sea King fleet, but the Sikorsky CH-148 Cyclone was selected. In 2013, following difficulties with the CH-148 procurement, the Royal Canadian Air Force (RCAF) was reported to be seriously considering canceling the contract with Sikorsky and was investigating the possibility of procuring the AW101 instead.
Royal Danish Air Force
In 2001, the Royal Danish Air Force (RDAF) announced the purchase of 8 EH101s for SAR duties and 6 tactical troop transports for 722 Squadron. The last of the 14 AW101s was delivered in March 2007 and the first SAR AW101s became operational out of Karup Airport in April 2007. In 2007, the 6 troop transport AW101s were transferred to the British MOD; in exchange, the British government ordered 6 new-build AW101s as replacements for the RDAF.
Danish AW101s have a higher gross weight capacity of 15,600 kg and were, as delivered, coated in a paint designed to reduce the aircraft's infrared signature. In the SAR role, RDAF AW101s have a crew of six and were initially painted yellow to distinguish themselves from AW101 allocated to military duties, but were later painted green, and all 14 AW101s are used for SAR and troop transport.
On 28 January 2008, the drive shaft of a Danish AW101 broke, leading to an emergency landing at Billund Airport. Following the incident the Danish fleet was grounded as a precaution, the AW101's future was publicly debated. In the first six months of 2008, the RDAF reported an operational availability of roughly 50%, well below the target of 80%, partly due to inadequate maintenance organization and staff shortages.
In January 2011, the Danish Ministry of Defence reportedly could not afford the retrofitting of the AW101 fleet for Afghanistan operations, against earlier reports of a deployment in 2012. In February 2013, Aviation Week reported that earlier reliability issues had been resolved and that a full upgrade package would be applied to Danish AW101s, these included the addition of electronic warfare pods and a new electro-optical system, in advance of a deployment in Afghanistan in 2014. In September 2013, Danish AW101s were to receive L-3 Wescam MX-15 electro-optical/infrared (EO/IR) sensors; SAR aircraft already carry the FLIR Systems Star Safire II EO/IR sensor.
Portuguese Air Force
The Portuguese Air Force had purchased a total of 12 Merlins under a €446 million contract, the first of which was delivered in 24 February 2005. The type has been used to conduct transport, search and rescue, and maritime surveillance missions, progressively replacing the Aérospatiale Puma previously tasked with these missions. The main role of Portuguese AW101s is to perform search and rescue missions within Portugal's maritime zone. They are operated by the 751 Squadron and are kept on constant alert at three bases: Montijo near Lisbon, Lajes Field on the Azores, and Porto Santo Island.
Japan Maritime Self-Defense Force
The Japan Maritime Self-Defense Force (JMSDF) ordered 14 aircraft in 2003 to use in both the airborne mine countermeasures (AMCM) and transport roles. The AW101 was modified by Kawasaki Heavy Industries, and the Japan Defense Agency designated the model MCH-101. Special features of the MCH-101 include the automated folding of the rotor and tail. The MCH-101 has also been outfitted with Northrop Grumman's AQS-24A for the mine-hunting role.
In 2002, AgustaWestland, Kawasaki and Marubeni entered a general agreement for cooperation; Kawasaki began the assembly of both the CH-101 and the MCH-101 in 2003. Kawasaki also began licenced production of the RTM322 engines in 2005. In a separate agreement between Marubeni and AgustaWestland, a supply depot was established in Japan to support the MCH-101 and CH-101 fleets. The first MCH-101 was delivered to the JMSDF on 3 March 2006.
The MCH-101 will replace the MH-53E (S-80-M-1) in the AMCM role. The CH-101 will operate in the transport/support role for Antarctic missions, replacing the Sikorsky S-61A, and will be working in coordination with the Ministry of Education, Culture, Sports, Science and Technology.
VIP and other usage
AgustaWestland developed a specialized luxury variant, the AW101 VVIP (Very Very Important Person, i.e. a head of state), aimed at business and VIP customers. As of April 2009, 15% of all AW101s sold were for VIP purposes. Customers operating the VIP variant include Saudi Arabia, Algeria, Nigeria and Turkmenistan.
The AW101 was being acquired by the United States Marine Corps under the VXX program as a replacement for the Presidential Marine One helicopters. Designated VH-71 Kestrel, the variant was heavily customized and equipped with various self-defense systems. However, in 2009 the VH-71 procurement was abruptly terminated following the withdrawal of funding. In 2010, Boeing considered an AW101 submission in the restarted VXX program.
In April 2009, India ordered 12 AW101 to serve as executive transport helicopters for the Indian President and Prime Minister. The selection followed field trial assessments between the AW101 and the Sikorsky S-92 held in 2008. However, the procurement was put on hold and subsequently cancelled due to the 2013 Indian helicopter bribery scandal, in which Finmeccanica, AgustaWestland's parent company, had allegedly used bribes to win the contract. The 3 helicopters delivered as part of the contract may be returned to the manufacturer as part of the arbitration process. 
- PP1 – Westland-built basic air vehicle prototype, first flown 9 October 1987.
- PP2 – Agusta-built Italian basic air vehicle prototype first flown on 26 November 1987 and used for deck trials but was destroyed on 21 January 1993 following a rotor brake malfunction.
- PP3 – Westland-built and the first civil configured Heliliner, used for engine vibration tests and icing trials in Canada.
- PP4 – Westland-built British naval prototype, lost in an accident on 7 April 1995 after a drive train control rod failure.
- PP5 – Westland-built Merlin development aircraft eventually equipped with Merlin avionics.
- PP6 – Agusta-built development aircraft for Italian Navy variant first flown 26 April 1989.
- PP7 – Agusta-built military utility aircraft with rear-loading ramp.
- PP8 – Westland-built civil prototype.
- PP9 – Agusta-built military utility prototype with rear-loading ramp.
- Model 110
- Italian Navy ASW/ASuW variant, eight built. Powered by T-700-GE-T6A1 engines. Fitted with Eliradar APS-784 radar and Honeywell HELRAS dipping sonar. Armed with torpedoes or Marte anti-ship missiles.
- Model 111
- Royal Navy ASW/ASuW variant, designated Merlin HM1 by customer. Powered by RTM322 engines and fitted with Blue Kestrel radar, Thomson Marconi FLASH dipping sonar and Orange Reaper ESM. 44 built.
- Model 112
- Italian Navy early warning variant with same airframe as Model 110 but with Eliradar HEW-784 radar in large underfuselage radome. Four built.
- Series 200
- Proposed military utility version with no rear-loading ranp.
- Series 300 Heliliner
- Proposed civil transport with no ramp. In 2000, British International Helicopters conducted service trials using PP8; these did not lead to a commercial service.
- Series 310
- Proposed version of Heliliner with full airline avionics for operation from oil platforms. No production.
- Model 410
- Italian Navy transport variant with folding rotors and tail boom. Four built.
- Model 411
- Royal Air Force transport variant, designated Merlin HC3 by customer, 22 built.
- Model 413
- Italian Navy special forces and amphibious assault transport with more advanced avionics.
- Model 500
- Proposed civil utility variant with rear-ramp.
- Model 510
- Civil utility variant with rear ramp, two built. One used for Tokyo Metropolitan Police Agency and one used to support US101 bid.
- Model 511
- Canadian Forces search and rescue variant, designated CH-149 Cormorant by customer, 15 built.
- Model 512
- Merlin Joint Supporter for Royal Danish Air Force. Eight acquired for search and rescue (512 SAR) and six for tactical transport (512 TTT). The six transports were sold to RAF (as Merlin HC.3As) and replaced by six new-build Merlins.
- Model 514
- Portuguese Air Force search and rescue variant, six built.
- Model 515
- Portuguese Air Force fisheries protection variant, two built.
- Model 516
- Portuguese Air Force combat search and rescue variant, four built.
- Model 518
- Japanese Maritime Self-Defense Force mine countermeasures and transport variant, two built.
- Model 519
- Presidential Transport variant for the United States Marine Corps as the VH-71 Kestrel, four test vehicles and five pilot production aircraft built.
- Model 612
- Norwegian Air Force search and rescue variant, 16 ordered with option for 6 more 
- Merlin HM1
- Royal Navy designation for the Model 111.
- Merlin HM2
- Avionics retrofit of 30 HM1s for the Royal Navy.
- Merlin HC3
- Royal Air Force designation for the Model 411.
- Merlin HC3A
- Royal Air Force designation for six former Royal Danish Air Force Model 512s modified to UK standards.
- Merlin HC3i
- Royal Navy will fit seven HC3 with folding rotor heads as an Interim measure until the full HC4 upgrade is available.
- Merlin HC4/4A
- Planned conversion of 25 RAF HC3/3A for RN use. HM2 cockpit, folding tail/blades and other adaptations for naval use.
- Merlin ASaC5
- Planned conversion of 8 RN HM1 for use in carrier based airborne early warning role.
- CH-148 Petrel
- Ship-based anti-submarine helicopter for Canada. 35 originally ordered by the Canadian Forces, reduced to 28 and cancelled in 1993.
- CH-149 Chimo
- Search and rescue helicopter for Canada. 15 ordered by the Canadian forces, but later cancelled.
- CH-149 Cormorant
- Search and rescue helicopter for Canada, 15 ordered and delivered.
- Lockheed Martin VH-71 Kestrel
- Cancelled USMC variant that was intended to serve as the US Presidential helicopter.
- Italian military designation from 2012 for the MP variant.
- Italian military designation from 2012 for the AEW variant.
- Italian military designation from 2012 for the ASH variant.
- Italian military designation for the CSAR variant.
- Indian Air Force - 3 delivered out of 12 originally ordered. May be returned to manufacturer due to the 2013 Indian helicopter bribery scandal.
Law enforcement operators
Notable accidents and incidents
- 21 January 1993 – Italian development Merlin PP2 crashed near Novara-Cameri airfield in Italy after an uncommanded application of the rotor brake in flight. Four people were killed.
- 7 April 1995 – British development Merlin PP4 (ZF644) crashed while in-flight from Yeovil, England. All four crew members escaped the helicopter during its descent before it hit the ground.
- 20 August 1996 – Italian development Merlin PP7 (I-HIOI) was damaged in an accident when it turned over after the tail rotor drive failed on landing. The helicopter was repaired.
- 27 October 2000 – Royal Navy Merlin (ZH844) ditched near the Isle of Skye, Scotland after a hydraulic fire caused by the rotor brake being partially engaged.
- 30 March 2004 – Royal Navy Merlin (ZH859) crashed on take-off from RNAS Culdrose due to tail rotor hub cracking.
- 15 November 2007 – During embarkation for a medical evacuation on São Jorge Island, Azores, a Portuguese Air Force Merlin caused injuries to five people when it unexpectedly climbed by one metre before the pilot recovered control. An Air Force spokesperson later stated that this kind of incident is unheard of.
Specifications (Merlin HM1)
- Crew: 3–4
- Capacity: 26 troops (38 passengers) or 5 tonnes of payload or 4 stretchers (with sonar removed).
- Length: 19.53 m-fuselage length (64 ft 1 in)
- Rotor diameter: 18.59 m (61 ft 0 in)
- Height: 6.62 m (21 ft 8¾ in)
- Disc area: 271.51 m² (2,992.5 ft²)
- Empty weight: 10,500 kg (23,149 lb)
- Max. takeoff weight: 14,600 kg (32,188 lb)
- Powerplant: 3 × Rolls-Royce Turbomeca RTM322-01 turboshafts, 1,566 kW (2,100 shp) (take-off power) each
- Never exceed speed: 309 km/h (167 knots, 192 mph)
- Cruise speed: 278 km/h (150 knots, 167mph)
- Range: 833 km (450 nmi, 517 mi)
- Endurance: 5 hours
- Service ceiling: 4,575 m (15,000 ft)
- Smiths Industries OMI 20 SEP dual-redundant digital automatic flight control system
- Navigation systems:
- Selex Galileo Blue Kestrel 5000 maritime surveillance radar
- Racal Orange Reaper ESM
- Thomson Marconi Sonar AQS-903 acoustic processor
- Active/passive sonobuoys
- Thomson Sintra FLASH dipping sonar array
Notable appearances in media
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
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|Wikimedia Commons has media related to AgustaWestland AW101.|
- AgustaWestland AW101 page
- RAF Merlin HC3 page
- EH-101 Merlin on Portuguese Air Force Official site, in English
- Danish EH-101 Merlin page