Bell AH-1 Cobra vs Eurocopter EC225 Super Puma

Attack helicopter^[source]

Passenger transport helicopter^[source]

United States^[source]

Multinational^[source]

Bell Helicopter^[source]

Eurocopter Airbus Helicopters^[source]

In service^[source]

United States Army (historical) Japan Ground Self-Defense Force Republic of Korea Army Royal Jordanian Air Force^[source]

1,116^[source]

170+ (as of 2016 )^[source]

1967–2019^[source]

1999–present^[source]

1967^[source]

December 2004^[source]

7 September 1965^[source]

27 November 2000^[source]

2001 (US Army)^[source]

Bell UH-1 Iroquois^[source]

Eurocopter AS332 Super Puma^[source]

Bell AH-1 SeaCobra/SuperCobra Bell 309 KingCobra^[source]

44 ft 5 in (13.5 m)^[source]

1,520 sq ft (141 m 2 )^[source]

206.15 m 2 (2,219.0 sq ft)^[source]

NACA 0009.3 mod^[source]

190 kn (220 mph, 350 km/h)^[source]

324 km/h (201 mph, 175 kn)^[source]

single-engined attack helicopter^[source]

long-range passenger transport helicopter^[source]

While some officials within the Pentagon, particularly those within the US Army, had recognized the potential value of purpose-built armed rotary aircraft as early as 1962 and were keen to see such a vehicle developed promptly, the issue was complicated in part due to inter-service politics. The United States Air Force (USAF) largely held the opinion that most forms of US military aircraft should be operated only by their service, and that the US Army would be intruding into their domain by developing a complex armed aerial combatant, and ought to be largely restricted to transport aircraft. Meanwhile, some Army officials were concerned that the USAF did not take the close air support (CAS) mission as seriously as it ought to, and that response times of 30 minutes or more for fixed-wing aircraft would be unacceptable.^[source]Bell AH-1 Cobra · Development / Background; only the objects and conditions stated in this passage

Bell had been investigating helicopter gunships since the late 1950s, paying particular attention to the Algerian War , in which French forces mounted weapons on helicopters to fight the growing insurgency. The company created a mockup of its D-255 helicopter gunship concept, named "Iroquois Warrior". The Iroquois Warrior was planned to be a purpose-built attack aircraft based on UH-1B components with a new, slender airframe and a two-seat, tandem cockpit. It featured a grenade launcher in a ball turret on the nose, a 20 mm belly-mounted gun pod, and stub wings for mounting rockets or SS.10 anti-tank missiles.^[source]Bell AH-1 Cobra · Development / Iroquois Warrior, Sioux Scout and AAFSS; only the objects and conditions stated in this passage

The Army's solution to the shortcomings of the Sioux Scout was to launch the Advanced Aerial Fire Support System (AAFSS) competition. This called for a heavily armed helicopter capable of at least 200 miles per hour (320 km/h). A total of seven companies, including Bell, opted to respond to the requirement. It was out of the AAFSS program that the Lockheed AH-56 Cheyenne emerged, a heavy attack helicopter with high speed capability. During testing, it proved to be too sophisticated and costly, and was ultimately canceled in 1972 after ten years of development. In its place, the Advanced Attack Helicopter program was launched. Under this initiative, the Army sought a conventional attack helicopter with a greater level of survivability.^[source]Bell AH-1 Cobra · Development / Iroquois Warrior, Sioux Scout and AAFSS; only the objects and conditions stated in this passage

As the Vietnam War proceeded, pressure accumulated in favor of the Model 209. Attacks on US forces were increasing and, by the end of June 1965, there were already 50,000 US ground troops in Vietnam. 1965 was also the deadline for AAFSS selection, but the program would become stuck in technical difficulties and political bickering. The US Army needed an interim gunship for Vietnam and it approached five separate companies with its request to provide a quick solution. Submissions came in for armed variants of the Boeing-Vertol ACH-47A , Kaman HH-2C Tomahawk , Piasecki 16H Pathfinder , Sikorsky S-61 , and the Bell 209.^[source]Bell AH-1 Cobra · Development / Model 209; only the objects and conditions stated in this passage

During April 1966, Bell's submission emerged victorious in an evaluation against the other rival helicopters. The US Army promptly signed the first production contract, ordering an initial batch of 110 aircraft. By the end of the year, rapid follow-on orders had increased this to 500 Cobras. Bell added "Cobra" to the UH-1's Huey nickname to produce its HueyCobra name for the 209. The Army applied the Cobra name to its AH-1G designation for the helicopter. The Bell 209 demonstrator was used for the next six years to test weapons and fit of equipment. An additional use for the demonstrator was participating in marketing initiatives. It was also modified to match the AH-1 production standard by the early 1970s. The demonstrator was retired to the Patton Museum at Fort Knox , Kentucky and converted to approximately its original appearance.^[source]Bell AH-1 Cobra · Development / Model 209; only the objects and conditions stated in this passage

Typically, the Cobra would avoid hovering at any point in an active engagement; instead, emphasis was placed on maintaining speed and mobility. The gunner often fired the chin-mounted cannon with the intention of suppressing hostile targets in between barrages of 2.75-inch rockets, held in pods upon the stub wings, which were fired by the back-seater. It was unusual for Cobras to operate alone; instead, two or more would be dispatched and teamwork encouraged, leading to hunter-killer tactics being used to flush out and eliminate ground targets. Pairings with other helicopters, such as the Bell OH-58 Kiowa scout helicopter, were also common occurrences. Radio communications were handled by the gunner. Regardless of mission profile, low altitude flying was commonplace.^[source]Bell AH-1 Cobra · Design; only the objects and conditions stated in this passage

By June 1967, the first AH-1G HueyCobras had been delivered. Originally designated as UH-1H, the "A" for attack designation was soon adopted and when the improved UH-1D became the UH-1H, the HueyCobra became the AH-1G. The AH-1 was initially considered a variant of the H-1 line, resulting in the G series letter.^[source]Bell AH-1 Cobra · Operational history / United States; only the objects and conditions stated in this passage

On 12 September 1968, Capt. Ronald Fogleman was flying an F-100 Super Sabre when the aircraft was shot down and he ejected 200 miles (320 km) north of Bien Hoa. Fogleman became the only pilot to be rescued by holding on to an Army AH-1G's deployed gun-panel door. Bell built 1,116 AH-1Gs for the U.S. Army between 1967 and 1973, and the Cobras chalked up over a million operational hours in Vietnam; the number of Cobras in service peaked at 1,081. In 1971 during Operation Lam Son 719 in Southeastern Laos , 26 U.S. Army AH-1Gs were destroyed and 158 sustained some level of damage. Out of nearly 1,110 AH-1s that were delivered between 1967 and 1973, approximately 300 were lost to a combination of combat and accidents during the conflict. Approximately one third of this number were operational or non-combat losses.^[source]Bell AH-1 Cobra · Operational history / United States; only the objects and conditions stated in this passage

The U.S. Marine Corps also operated the AH-1G Cobra in Vietnam for a short time before acquiring the twin-engine AH-1J Cobras . The AH-1Gs had been adopted by the Marines as an interim measure, a total of 38 helicopters having been transferred from the U.S. Army to the Marines in 1969.^[source]Bell AH-1 Cobra · Operational history / United States; only the objects and conditions stated in this passage

By 2013, Pakistan reportedly operated a fleet of 35 AH-1F helicopters. Maintaining these aircraft has been difficult, but possible through commercial channels. Additionally, the US government provided $750,000 (~$993,036 in 2024) through 2013 to update the existing AH-1F/S Cobra fleet. However, controversy over how much of this funding has actually been spent on Pakistan's Cobras has also been present throughout the 2010s. Turkey has also become a key supplier of spare parts for the Cobra, often free of cost, to Pakistan. During the 2010s, Pakistan lost a total of three aircraft in separate incidents.^[source]Bell AH-1 Cobra · Operational history / Pakistan; only the objects and conditions stated in this passage

Pakistan repeatedly sought the Bell AH-1W SuperCobra from the US to supplement and replace its current AH-1 Cobras. Attempts to acquire the AH-1Z Viper or AH-64E Apache from the US were rejected, so Pakistan turned to buying other foreign attack helicopters. Possible candidates have included the Turkish T129 , the Chinese CAIC Z-10 , and the Russian Mi-35 Hind . In November 2014, Russia approved the sale of Mi-35M helicopters to Pakistan. In April 2015, China delivered three Z-10s to Pakistan. During the same month, the US Department of State approved the sale of 15 AH-1Zs and associated equipment to Pakistan. During October 2017, the T129 was also reported to be a contender for further orders.^[source]Bell AH-1 Cobra · Operational history / Pakistan; only the objects and conditions stated in this passage

The Florida Division of Forestry also acquired three AH-1Ps from the US Army. These are called Bell 209 "Firesnakes" and are equipped to carry a water/fire retardant system.^[source]Bell AH-1 Cobra · Operational history / Civilian operators; only the objects and conditions stated in this passage

Original AH-1G prototype with retractable skid landing gear. This model number is also used by the FAA for the civilian registration of former U.S. Army AH-1s used in firefighting service.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

AH-1G HueyCobra^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

Initial 1966 production model gunship for the U.S. Army, with one 1,400 shp (1,000 kW ) Avco Lycoming T53-13 turboshaft.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

JAH-1G HueyCobra^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

TH-1G HueyCobra^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

The Spanish Navy purchased eight new-build AH-1Gs, designating the type the "Z-14". These were equipped with the M35 20 mm cannon system, and were used to support coastal patrol boats. Four of these were lost in accidents. The remaining helicopters were retired in 1985 with three sent back to the US, and one kept in storage in Spain.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

AH-1G powered by a T53-L-703 engine without TOW system.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

The baseline AH-1S is an AH-1Q upgraded with a 1,800 shp (1,300 kW) T53-L-703 turboshaft engine. The AH-1S is also referred to as the "Improved AH-1S", "AH-1S Modified", or "AH-1S(MOD)" prior to 1988. (Prior to 1988, all upgraded aircraft were referred to as variants of the AH-1S.)^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

98 production aircraft with the Enhanced Cobra Armament System (ECAS) featuring the M97A1 armament subsystem with a three-barreled M197 20 mm cannon. The AH-1E is also referred to as the "Upgunned AH-1S", or "AH-1S(ECAS)" prior to 1988. These improvements are considered Step 2 of the AH-1S upgrade program. AH-1E aircraft included the M147 Rocket Management Subsystem (RMS) to fire 2.75-inch (70 mm) rockets.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

143 production aircraft and 387 converted AH-1G Cobras. The AH-1F incorporates all Step 1 and 2 upgrades to the AH-1S. It also featured Step 3 upgrades: a head-up display, a laser rangefinder, an infrared jammer mounted above the engine exhaust, and an infrared suppressing engine exhaust system, and the M143 Air Data Subsystem (ADS). The AH-1F is also referred to as the "Modernized AH-1S", "AH-1S Modernized Cobra", or "AH-1S(MC)" prior to 1988.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

Experimental all-weather version based on the AH-1G single-engine and AH-1J twin-engine designs. Two Bell 309s were produced; the first was powered by a PWC T400-CP-400 Twin-Pac engine set and the second was powered by a Lycoming T55-L-7C engine.^[source]Bell AH-1 Cobra · Variants / Single-engine; only the objects and conditions stated in this passage

Length: 53 ft (16 m) including rotors^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Fuselage length: 44 ft 5 in (13.5 m)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Width: 10 ft 4 in (3.15 m) stub wings^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Height: 13 ft 6 in (4.11 m)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Empty weight: 5,810 lb (2,635 kg)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Max takeoff weight: 9,500 lb (4,309 kg)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Powerplant: 1 × Lycoming T53-L-13 turboshaft , 1,100 hp (820 kW)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Main rotor diameter: 44 ft 0 in (13.4 m)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Main rotor area: 1,520 sq ft (141 m 2 )^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Maximum speed: 149 kn (171 mph, 276 km/h)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Never exceed speed : 190 kn (220 mph, 350 km/h)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Range: 310 nmi (360 mi, 570 km)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Service ceiling: 11,400 ft (3,500 m)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

Rate of climb: 1,230 ft/min (6.2 m/s)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

2 × 7.62 mm (0.308 in) multi-barrel Miniguns , or 2 × M129 40 mm grenade launchers , or one of each, in the M28 turret . (When one of each was mounted, the minigun was mounted on the right side of the turret, due to feed requirements.)^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

2.75 in (70 mm) rockets – 7 rockets mounted in the M158 launcher or 19 rockets in the M200 launcher^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

M18 7.62 mm Minigun pod or XM35 armament subsystem with XM195 20 mm cannon^[source]Bell AH-1 Cobra · Specifications (AH-1G HueyCobra); only the objects and conditions stated in this passage

The Airbus Helicopters H225 (formerly Eurocopter EC225 Super Puma ) is a long-range passenger transport helicopter developed by Eurocopter as the next generation of the civilian Super Puma family. It is a twin-engined aircraft and can carry up to 24 passengers along with two crew and a cabin attendant, dependent on customer configuration. The helicopter is marketed for offshore support and VIP passenger transport duties, as well as public service missions.^[source]Eurocopter EC225 Super Puma · Lead; only the objects and conditions stated in this passage

In February 2014, Airbus Helicopters announced at Heli-Expo 2014 the development of an improved variant, the EC225e. The EC225e features numerous changes including new avionics systems, such as the TCAS II collision avoidance system, an automatic identification system, and a specialized rig-approach system; it was also intended to feature an improved Turbomeca Makila 2B engine to increase the EC225e's maximum takeoff weight by 550 kg, and an additional fuel tank in the rear baggage compartment to extend its range to 300 nautical miles with up to ten passengers on board. Some, but not all, modifications can be retrofitted onto existing EC225s. In the same announcement, in February 2014, Lease Corporation International said that they had placed a $645 million order for 15 EC225e (along with 6 Airbus Helicopters EC175 ) helicopters as the launch customer. In February 2016, the Makila 2B engine was dropped from the EC225e as a cost reduction measure, development of the other structural and avionics aspects is proceeding.^[source]Eurocopter EC225 Super Puma · Development; only the objects and conditions stated in this passage

A key safety feature of the aircraft's main gear box (MGB) is an emergency oil spraying sub-system present in the lubrication system; this is designed to exceed the JAR 29 Standard's requirements of a 30-minute running time in the event of the loss of MGB oil pressure, and has demonstrated up to 50-minute running time. The engine also incorporates a "blade shedding" system to ensure engine integrity during an overspeed instance. Energy absorbent self-sealing fuel tanks are contained in the aircraft's sponsons , along with other equipment such as downward-facing illumination and navigation lighting fixtures. The transmission can accommodate more power than the maximum output of the engines; however two aircraft were lost in 2012 due to the cracking of the bevel gear shaft, a gearbox component. In response, the design of the transmission was modified in 2013, and the onboard health and usage monitoring system (HUMS) was upgraded to provide real-time monitoring of the bevel gear shaft against the threat of crack formation.^[source]Eurocopter EC225 Super Puma · Design; only the objects and conditions stated in this passage

In terms of cockpit equipment and avionics, the H225 is equipped with a full glass cockpit with active-matrix liquid crystal displays ; these include four 6-inch by 8-inch multi-functional displays as the predominant instrumentation for key flight information, two 4-inch by 5-inch monitors for displaying aircraft parameters, and a 3-inch screen for backup. The advanced helicopter cockpit and avionics system is described as serving to reduce pilot and crew workload, being used to display flight management and sub-systems information and is complete with a four-axis digital autopilot. During a typical flight, the pilot programs the route into the aircraft and then monitors it, as opposed to direct continuous control of the flight; the need for paper charts has been eliminated by these systems. Under autopilot, the automatic flight control system acts to prevent pilot actions from exceeding the established flight envelope; the H225 remains flyable with all automatic systems disabled. From initiating the startup sequence to being ready to takeoff only takes three minutes.^[source]Eurocopter EC225 Super Puma · Design; only the objects and conditions stated in this passage

There are currently a total of four principal configurations designed by Airbus Helicopters for the H225. The passenger transport version has a crash-worthy seating arrangement for up to 19 passengers with a high-density seating arrangement accommodating up to 28 passengers available to be fitted. The VIP transport version has a large lounge with seating for up to 12 passengers and a cabin attendant. The emergency medical services (EMS) configuration has medical units for six stretchers and four seats for medical workers. The search and rescue (SAR) configuration allows space for search and rescue equipment with an operator seat, hoistman seat and up to eight rescue seats and three stretchers. While a single pilot is capable of controlling the aircraft under visual meteorical conditions, two pilots are used in a typical crew complement and, dependent on role, a cabin attendant or flight engineer may also be present.^[source]Eurocopter EC225 Super Puma · Design; only the objects and conditions stated in this passage

Icelandic Coast Guard — received 2 H225s in 2019 and 1 in 2021.^[source]Eurocopter EC225 Super Puma · Operators / Military operators; only the objects and conditions stated in this passage

18 February 2009: G-REDU, an EC225 LP operated by Bond Offshore Helicopters . During a night visual approach to the ETAP platform, the helicopter descended and impacted the surface of the sea. The crew's perception of the helicopter's position and orientation relative to the platform during the final approach was erroneous. All 18 people on board survived the controlled flight into terrain (water) .^[source]Eurocopter EC225 Super Puma · Accidents and incidents; only the objects and conditions stated in this passage

10 May 2012: G-REDW, an EC225 LP, carried out a controlled ditching following indications of a failure of the main gearbox (MGB) lubrication system and a subsequent failure indication warning on the emergency lubrication system. An investigation by the Air Accidents Investigation Branch (AAIB) identified a 360° circumferential crack in the bevel gear vertical shaft in the main gearbox, in the vicinity of a manufacturing weld, causing disengagement of the drive to both mechanical oil pumps.^[source]Eurocopter EC225 Super Puma · Accidents and incidents; only the objects and conditions stated in this passage

22 October 2012: G-CHCN, an EC225 LP of CHC Scotia, ditched in the North Sea 32 miles south west of Shetland whilst en route from Aberdeen to the West Phoenix drilling rig. All 19 on board were rescued. A special bulletin issued by the Air Accidents Investigation Branch (AAIB) said the main and standby oil pumps were not working; a 360-degree crack found on the bevel gear vertical shaft of the gearbox had prevented the oil pump gears from being driven. A worldwide grounding of the type was initiated in response. In both of the 2012 incidents, although the main gearbox lubrication system had failed, the backup system was working correctly but displaying an erroneous warning light, due to an incorrect specification of a pressure switch, which led to the helicopters being ditched.^[source]Eurocopter EC225 Super Puma · Accidents and incidents; only the objects and conditions stated in this passage

29 April 2016: LN-OJF , an EC225 LP of CHC Helikopter Service , crashed at an islet near Turøy in the Bergen archipelago, en route to Bergen Airport, Flesland , from the Gullfaks B platform in the North Sea. The helicopter was carrying 11 passengers and 2 crew members; everyone on board died. Eyewitnesses reported that the main rotor separated from the hull immediately before the crash. Due to the crash, all commercial flights by EC225 helicopters, excluding search and rescue flights, were grounded by both Norwegian and British civil aviation authorities. The subsequent investigation concluded that a gear in the main rotor gearbox had failed due to a fatigue crack that had propagated under-surface, escaping detection. As a result of the incident the German Defence Ministry had also decided to ground 3 AS532 Helicopter in government use which were manufactured by the same company.^[source]Eurocopter EC225 Super Puma · Accidents and incidents; only the objects and conditions stated in this passage

18 January 2023: an EC225 carrying the Minister of Internal Affairs of Ukraine , Denys Monastyrsky , his deputy Yevhen Yenin and state secretary Yurii Lubkovych , crashed at a kindergarten in Brovary , a suburb of Kyiv , Ukraine . The crash killed 14 people, including Monastyrsky, Yenin and Lubkovych; a child was also among the fatalities, while 25 others were injured.^[source]Eurocopter EC225 Super Puma · Accidents and incidents; only the objects and conditions stated in this passage

Capacity: 24 passengers + 1 cabin attendant^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Length: 19.5 m (64 ft 0 in)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Height: 4.97 m (16 ft 4 in)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Empty weight: 5,256 kg (11,587 lb)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Gross weight: 11,000 kg (24,251 lb)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Max takeoff weight: 11,200 kg (24,692 lb)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Powerplant: 2 × Turbomeca Makila 2A1 turboshaft engines, 1,776 kW (2,382 hp) each^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Main rotor diameter: 16.2 m (53 ft 2 in)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Main rotor area: 206.15 m 2 (2,219.0 sq ft)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Maximum speed: 275.5 km/h (171.2 mph, 148.8 kn)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Cruise speed: 260.5 km/h (161.9 mph, 140.7 kn)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Never exceed speed : 324 km/h (201 mph, 175 kn)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Range: 857 km (533 mi, 463 nmi)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Ferry range: 985 km (612 mi, 532 nmi)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Service ceiling: 5,900 m (19,400 ft)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

Rate of climb: 8.7 m/s (1,710 ft/min)^[source]Eurocopter EC225 Super Puma · Specifications (H225); only the objects and conditions stated in this passage

CHC Helicopter^[source]

Eurocopter EC725^[source]

24 passengers + 1 cabin attendant^[source]