Boeing CH-47 Chinook
|A U.S. Army CH-47D with two underslung containers comes in to offload supplies at Kunsan Air Base, South Korea in March 2008.|
|National origin||United States|
|Manufacturer||Boeing Rotorcraft Systems|
|First flight||21 September 1961|
|Primary users||United States Army
Japan Ground Self-Defense Force
Royal Netherlands Air Force
See CH-47 operators for others
|Number built||Over 1,200 as of 2012|
US$38.55 million (CH-47F, FY13)
|Developed from||Vertol Model 107|
|Variants||Boeing Chinook (UK variants)|
The Boeing CH-47 Chinook is an American twin-engine, tandem rotor heavy-lift helicopter. Its primary roles are troop movement, artillery placement and battlefield resupply. It has a wide loading ramp at the rear of the fuselage and three external-cargo hooks. With a top speed of 170 knots (196 mph, 315 km/h) the helicopter is faster than contemporary 1960s utility and attack helicopters. The CH-47 is among the heaviest lifting Western helicopters. Its name is from the Native American Chinook people.
The Chinook was designed and initially produced by Boeing Vertol in the early 1960s; it is now produced by Boeing Rotorcraft Systems. It is one of the few aircraft of that era – along with the fixed-wing Lockheed C-130 Hercules cargo aircraft – that remain in production and frontline service, with over 1,200 built to date. The helicopter has been sold to 16 nations with the U.S. Army and the Royal Air Force (see Boeing Chinook (UK variants)) being its largest users.
- 1 Design and development
- 2 Operational history
- 3 Variants
- 4 Operators
- 5 Notable accidents
- 6 Specifications (CH-47F)
- 7 See also
- 8 References
- 9 External links
Design and development
In late 1956, the United States Department of the Army announced plans to replace the Sikorsky CH-37 Mojave, which was powered by piston engines, with a new, turbine-powered helicopter. Turbine engines were also a key design feature of the smaller UH-1 "Huey" utility helicopter. Following a design competition, in September 1958, a joint Army–Air Force source selection board recommended that the Army procure the Vertol medium transport helicopter. However, funding for full-scale development was not then available, and the Army vacillated on its design requirements. Some in the Army aviation corps thought that the new helicopter should be a light tactical transport aimed at taking over the missions of the old piston-engined H-21 and H-34 helicopters, and be consequently capable of carrying about fifteen troops (one squad). Another faction in the Army aviation corps thought that the new helicopter should be much larger to be able to airlift a large artillery piece, and have enough internal space to carry the new MGM-31 "Pershing" Missile System.
Vertol began work on a new tandem-rotor helicopter designated Vertol Model 107 or V-107 in 1957. In June 1958, the U.S. Army awarded a contract to Vertol for the aircraft under the YHC-1A designation. The YHC-1A had a capacity for 20 troops. Three were tested by the Army for deriving engineering and operational data. However, the YHC-1A was considered by most of the Army users to be too heavy for the assault role and too light for the transport role. The decision was made to procure a heavier transport helicopter and at the same time upgrade the UH-1 "Huey" as a tactical troop transport. The YHC-1A would be improved and adopted by the Marines as the CH-46 Sea Knight in 1962. The Army then ordered the larger Model 114 under the designation HC-1B. The pre-production Boeing Vertol YCH-1B made its initial hovering flight on 21 September 1961. In 1962 the HC-1B was redesignated the CH-47A under the 1962 United States Tri-Service aircraft designation system. It was named "Chinook", which alludes to the Chinook people of the Pacific Northwest.
The CH-47 is powered by two turboshaft engines, mounted on each side of the helicopter's rear pedestal and connected to the rotors by driveshafts. Initial models were fitted with Lycoming T-53 jet engines with a combined rating of 2,200 shaft horsepower. Subsequent versions of the Chinook were configured with improved Lycoming engines and later with General Electric turbines. The counter-rotating rotors eliminate the need for an anti-torque vertical rotor, allowing all power to be used for lift and thrust. The ability to adjust lift in either rotor makes it less sensitive to changes in the center of gravity, important for the cargo lifting role. If one engine fails, the other can drive both rotors. The "sizing" of the Chinook was directly related to the growth of the Huey and the Army's tacticians' insistence that initial air assaults be built around the squad. The Army pushed for both the Huey and the Chinook, and this focus was responsible for the acceleration of its air mobility effort.
Improved and later versions
Improved and more powerful versions of the CH-47 have been developed since the helicopter entered service. The U.S. Army's first major design leap was the now-common CH-47D, which entered service in 1982. Improvements from the CH-47C included upgraded engines, composite rotor blades, a redesigned cockpit to reduce pilot workload, improved and redundant electrical systems, an advanced flight control system and improved avionics. The latest mainstream generation is the CH-47F, which features several major upgrades to reduce maintenance, digitized flight controls, and is powered by two 4,733-horsepower Honeywell engines.
A commercial model of the Chinook, the Boeing-Vertol Model 234, is used worldwide for logging, construction, fighting forest fires, and supporting petroleum extraction operations. On 15 December 2006, the Columbia Helicopters company of the Salem, Oregon, metropolitan area, purchased the Type certificate of the Model 234 from Boeing. The Chinook has also been licensed to be built by companies outside the United States, such as Elicotteri Meridionali (now AgustaWestland) in Italy, and Kawasaki in Japan.
The Army finally settled on the larger Chinook as its standard medium transport helicopter and as of February 1966, 161 aircraft had been delivered to the Army. The 1st Cavalry Division had brought their organic Chinook battalion with them when they arrived in 1965 and a separate aviation medium helicopter company, the 147th, had arrived in Vietnam on 29 November 1965. This latter company was initially placed in direct support of the 1st Infantry Division.
The most spectacular mission in Vietnam for the Chinook was the placing of artillery batteries in perilous mountain positions inaccessible by any other means, and then keeping them resupplied with large quantities of ammunition. The 1st Cavalry Division found that its CH-47s were limited to a 7,000-pound (3,200 kg) payload when operating in the mountains, but could carry an additional 1,000 pounds (450 kg) when operating near the coast. The early Chinook design was limited by its rotor system which did not permit full use of the installed power, and users were anxious for an improved version which would upgrade this system.
As with any new piece of equipment, the Chinook presented a major problem of "customer education". Commanders and crew chiefs had to be constantly alert that eager soldiers did not overload the temptingly large cargo compartment. It would be some time before troops would be experts at using sling loads. The Chinook soon proved to be such an invaluable aircraft for artillery movement and heavy logistics that it was seldom used as an assault troop carrier. Some of the Chinook fleet were used for casualty evacuation, due to the very heavy demand for the helicopters they were usually overburdened with wounded. Perhaps the most cost effective use of the Chinook was the recovery of other downed aircraft.
The CH-47s are generally armed with a single 7.62-millimeter M60 machine gun on a pintle mount on either side of the machine for self-defense, with stops fitted to keep the gunners from firing into the rotor blades. Dust filters were also added to improve engine reliability. At its peak employment in Vietnam, there were 22 Chinook units in operation. Of the nearly 750 Chinook helicopters in the U.S. and South Vietnam fleets, about 200 were lost in combat or wartime operational accidents. The U.S. Army CH-47s supported the 1st Australian Task Force as required.
During the 1970s, the United States and Iran had a strong relationship, in which the Iranian armed forces began to use many American military aircraft, most notably the F-14 Tomcat, as part of a modernization program. After an agreement signed between Boeing and Elicotteri Meridionali, the Imperial Iranian Air Force purchased 20 Elicotteri Meridionali-built CH-47Cs in 1971. The Imperial Iranian Army Aviation purchased 70 CH-47Cs from Elicotteri Meridionali between 1972 and 1976. In late 1978, Iran placed an order for an additional 50 helicopters with Elicotteri Meridionali, but that order was canceled immediately after the revolution.
In the 1978 Iranian Chinook shootdown, four Iranian CH-47Cs penetrated 15–20 km into Soviet airspace in the Turkmenistan Military District. They were intercepted by a MiG-23M which shot down one, killing eight crew members, and forced a second one to land. Chinook helicopters were used in efforts by the Imperial Iranian loyalist forces to resist the 1979 Iranian revolution.
During the Iran–Iraq War, Iran made heavy use of its US-bought equipment, and lost at least 8 CH-47s during the 1980–1988 period; most notably during a clash on 15 July 1983, when an Iraqi Mirage F1 destroyed three Iranian Chinooks transporting troops to the front line, and on 25–26 February 1984, when Iraqi MiG-21 fighters shot down two examples.
The Chinook was used both by Argentina and the United Kingdom during the Falklands War in 1982. The Argentine Air Force and the Argentine Army each deployed two CH-47C helicopters, which were widely used in general transport duties. Of the Army's aircraft, one was destroyed on the ground by a Harrier while the other was captured by the British and reused after the war. Both Argentine Air Force helicopters returned to Argentina and remained in service until 2002.
Afghanistan and Iraq wars
The CH-47D has seen wide use in Operation Enduring Freedom in Afghanistan and Operation Iraqi Freedom in Iraq. The Chinook is being used in air assault missions, inserting troops into fire bases and later bringing food, water, and ammunition. It is also the casualty evacuation (casevac) aircraft of choice in the British Armed Forces. In combat theaters, it is typically escorted by attack helicopters such as the AH-64 Apache for protection. Its lift capacity has been found of particular value in the mountainous terrain of Afghanistan where high altitudes and temperatures limit the use of helicopters such as UH-60 Black Hawk; reportedly, one Chinook can replace up to five UH-60s in the air assault transport role.
The Chinook helicopters of several nations have participated in the Afghanistan War, including aircraft from Britain, Italy, the Netherlands, Spain, Canada, and Australia. Despite the age of the Chinook, it is still in heavy demand, in part due its proven versatility and ability to operate in demanding environments such as Afghanistan.
On 6 August 2011, a Chinook crashed near Kabul killing all of the 38 aboard. It was reportedly shot down with a rocket-propelled grenade by the Taliban. The 38 were members of NATO and allied forces, including about 30 U.S. special forces and seven Afghan troops. The previous biggest single-day loss for American forces in Afghanistan involved a Chinook that was shot down near Kabul in Kunar Province in June 2005 with the death of all aboard, including a 16-member U.S. Special Operations team.
In May 2011 an Australian Army CH-47D crashed during a resupply mission in Zabul Province, resulting in one fatality and five survivors. The helicopter was unable to be recovered and was destroyed in place. To compensate for the loss, the ADF added two ex-U.S. Army CH-47Ds to the fleet which are expected to be in service until the introduction of the CH-47Fs in 2016.
Disaster relief and other roles
|This section requires expansion. (May 2013)|
Since the type's inception, the Chinook has carried out secondary missions including medical evacuation, disaster relief, search and rescue, aircraft recovery, fire fighting, and heavy construction assistance. According to Suresh Abraham, the Chinook's ability to carry large underslung loads has been of significant value in relief operations in the aftermath of natural disasters. Chinooks operators have often deployed their fleets overseas to support humanitarian efforts in stricken nations; Chinooks of the Republic of Singapore Air Force assisted in relief operations in neighboring Indonesia following the 2004 Asian Tsunami, and after the 2005 Kashmir earthquake the Royal Air Force dispatched Chinooks to Northern Pakistan to assist in recovery efforts.
Three Japanese CH-47s were used to cool Reactors 3 and 4 of the Fukushima Nuclear power-plant with sea water after the 9.0 earthquake in 2011; to protect the crew from heightened radiation levels, lead plates were attached to the floor.
The pre-1962 designation for Model 114 development aircraft that would be re-designated CH-47 Chinook.
The all-weather, medium-lift CH-47A Chinook was powered initially by Lycoming T55-L-5 engines rated at 2,200 horsepower (1,640 kW) but then replaced by the T55-L-7 rated at 2,650 hp (1,980 kW) engines or T55-L-7C engines rated at 2,850 hp (2,130 kW). The CH-47A had a maximum gross weight of 33,000 lb (15,000 kg). allowing for a maximum payload of approximately 10,000 lb (4,500 kg) Initial delivery of the CH-47A Chinook to the U.S. Army was in August 1962. A total of 349 were built.
The ACH-47A was originally known as the Armed/Armored CH-47A (or A/ACH-47A). It was officially designated ACH-47A by U.S. Army Attack Cargo Helicopter and unofficially Guns A Go-Go. Four CH-47A helicopters were converted to gunships by Boeing Vertol in late 1965. Three were assigned to the 53rd Aviation Detachment in South Vietnam for testing, with the remaining one retained in the U.S. for weapons testing. By 1966, the 53rd was redesignated the 1st Aviation Detachment (Provisional) and attached to the 228th Assault Support Helicopter Battalion of the 1st Cavalry Division (Airmobile). By 1968, only one gunship remained, and logistical concerns prevented more conversions. It was returned to the United States, and the program stopped.
The ACH-47A carried five M60D 7.62 × 51 mm machine guns or M2HB .50 caliber machine guns, provided by the XM32 and XM33 armament subsystems, two M24A1 20 mm cannons, two XM159B/XM159C 19-Tube 2.75-inch (70 mm) rocket launchers or sometimes two M18/M18A1 7.62 × 51 mm gun pods, and a single M75 40 mm grenade launcher in the XM5/M5 armament subsystem (more commonly seen on the UH-1 series of helicopters). The surviving aircraft, Easy Money, has been restored and is on display at Redstone Arsenal, Alabama.
The CH-47B was an interim solution while Boeing worked on a more substantially improved CH-47C. The CH-47B was powered by two Lycoming T55-L-7C 2,850 shp (2,130 kW) engines. It featured a blunted rear rotor pylon, redesigned asymmetrical rotor blades, and strakes along the rear ramp and fuselage to improve flying characteristics. It could be equipped with two door-mounted M60D 7.62 mm NATO machine guns on the M24 armament subsystem and a ramp-mounted M60D using the M41 armament subsystem. Some CH-47 "bombers" were equipped to drop tear gas or napalm from the rear cargo ramp onto NLF (aka Việt Cộng) bunkers. The CH-47 could be equipped with a hoist and cargo hook. The Chinook proved especially valuable in "Pipe Smoke" aircraft recovery missions. The "Hook" recovered about 12,000 aircraft valued at over $3.6 billion during the war. 108 were built.
The CH-47C featured more powerful engines and transmissions. Three versions of the "C model" were built. The first had Lycoming T55-L-7C engines delivering 2,850 shp (2,130 kW). The "Super C" included Lycoming T55-L-11 engines delivering 3,750 shp (2,800 kW), an upgraded maximum gross weight of 46,000 lb (21,000 kg) and a pitch stability augmentation system (PSAS). Due to difficulties with the T55-L-11 engines, which were hurriedly introduced to increase payload, they were temporarily removed and the reliable Lycoming T55-L-7C's were installed. The type was distinguishable from the standard "C" by the uprated maximum gross weight.
The type was unable to receive FAA certification to engage in civil activities due to the non-redundant hydraulic flight boost system drive. A redesign of the hydraulic boost system drive was incorporated in the succeeding CH-47D, allowing that model to achieve certification as the Boeing Model 234. A total of 233 CH-47Cs were built. Canada bought a total of eight CH-47Cs, deliveries of the type began in 1974. Receiving the Canadian designation "CH-147", these were fitted with a power hoist above the crew door, other changes included a flight engineer station in the rear cabin, Boeing referred to the configuration as the "Super C". The CH-47C saw wide use during the Vietnam war, eventually replacing the older H-21 Shawnee in the combat assault support role.
The CH-47D shares the same airframe as earlier models, the main difference being the adoption of more powerful engines. Early CH-47Ds were originally powered by two T55-L-712 engines, the most common engine is the later T55-GA-714A. With its triple-hook cargo system, the CH-47D can carry heavy payloads internally and up to 26,000 pounds (12 t) (such as 40-foot or 12-metre containers) externally. The D-model was first introduced into service in 1979. In air assault operations, it often serves as the principal mover of the 155 mm M198 howitzer, accompanying 30 rounds of ammunition and an 11-man crew. The CH-47D also has advanced avionics, such as the Global Positioning System. Nearly all US Army CH-47D were conversions from previous A, B, and C models, a total of 472 converted into D-models. The last U.S. Army D-model built was delivered to the U.S. Army Reserve, located at Fort Hood, Texas, in 2002.
The Netherlands acquired all seven of the Canadian Forces' surviving CH-147s and upgraded them to CH-47D standard. Six more new-build CH-47Ds were delivered in 1995 for a total of 13. The Dutch CH-47D feature a number of improvements over U.S. Army CH-47Ds, including a long nose for Bendix weather radar, a "glass cockpit", and improved T55-L-714 engines. As of 2011, the Netherlands shall upgrade 11 of these which will be updated to the CH-47F standard at a later date. As of 2011, Singapore has 18 CH-47D/SDs, which includes twelve "Super D" Chinooks, in service. In 2008, Canada purchased 6 CH-47Ds from the U.S. for the Canadian Helicopter Force Afghanistan for $252 million. With 1 CH-47D loss, the remaining 5 CH-47D were returned by Canada in 2011 after their mission in Afghanistan was over.[clarification needed]
The MH-47D variant was developed for special forces operations and has inflight refueling capability, a fast rope-rappelling system and other upgrades. The MH-47D was used by U.S. Army 160th Special Operations Aviation Regiment. 12 MH-47D helicopters were produced. Six were conversions from CH-47A models and six were conversions from CH-47C models.
The MH-47E has been used by U.S. Army Special Operations. Beginning with the E-model prototype manufactured in 1991, there were a total of 26 Special Operations Aircraft produced. All aircraft were assigned to 2–160th SOAR(A) "Nightstalkers", home based at Fort Campbell Kentucky. E models were conversions from existing CH-47C model airframes. The MH-47E has similar capabilities as the MH-47D, but includes an increased fuel capacity similar to the CH-47SD and terrain following/terrain avoidance radar.
In 1995, the Royal Air Force ordered eight Chinook HC3s, effectively a low-cost version of the MH-47E for the special operations role. They were delivered in 2001 but never entered operational service due to technical issues with their avionics fit, unique to the HC3. In 2008, work started to downgrade the HC3s to HC2 standard, to enable them to enter service.
The first CH-47F, an upgraded D model, made its maiden flight in 2001; the first production rolled out on 15 June 2006 at Boeing's facility in Ridley Park, Pennsylvania, and first flew on 23 October 2006. Upgrades included new 4,868-shaft-horsepower (3,630 kW) Honeywell engines, an upgraded airframe featuring greater single-piece construction for lower maintenance requirements. The milled construction reduces vibrations, eliminate flexing points, and reduces inspection and repair needs; it is also expected to increase service life. The CH-47F can fly at speeds of over 175 mph (282 km/h) with a payload of more than 21,000 lb (9.5 t). New avionics include a Rockwell Collins Common Avionics Architecture System (CAAS) cockpit, and BAE Systems' Digital Advanced Flight Control System (DAFCS).
Boeing delivered 48 F-model helicopters to the U.S. Army through August 2008; at that time Boeing announced a $4.8 billion contract with the Army for 191 Chinooks. In February 2007, the Netherlands became the first international customer, ordering six CH-47Fs, expanding their fleet to 17. The Netherlands also plans to upgrade its current 11 CH-47Ds to the CH-47F configuration. On 10 August 2009, Canada signed a contract to purchase 15 CH-47Fs for delivery in 2013–14, entering service with the Royal Canadian Air Force. On 15 December 2009, Britain announced its Future Helicopter Strategy, including the purchase of 24 new CH-47Fs to be delivered from 2012. Australia ordered seven CH-47Fs in March 2010 to replace its six CH-47Ds between 2014 and 2017. AgustaWestland also domestically assembles the CH-47F under license, known as the Chinook ICH-47F, for several customers.
A CH-47F Block 2 is planned to be introduced after 2020. The Block 2 aims for a payload of 22,000 lb with 4,000 ft/95 °F high/hot hover performance, eventually increased up to 6,000 ft/95 °F, to carry the Joint Light Tactical Vehicle. It features the advanced Chinook rotor blade (ACRB), derived from the canceled RAH-66 Comanche, 20 percent more powerful Honeywell T55-715 engines, and the active parallel actuator system (APAS); the APAS enhances the digital advanced flight-control system, and provides an exact torque split between the rotors for greater efficiency. A new fuel system that combines the three fuel cells in each sponson into one larger fuel cell, reducing weight, eliminating fuel transfer hardware between each fuel cell and increasing fuel capacity. A redesigned electrical system is also planned that will include three 60kVA generators for increased electrical capacity for future growth.
Upgrades to the Chinook have made Boeing consider a CH-47H variant to keep the helicopter relevant for several more decades. Budget issues have caused suggested upgrades to be changed to cheaper and more immediate features, like a strengthened airframe and propulsion system to lift 24,500 kg (54,000 lb), about 1,810 kg (3,990 lb) greater than the previous model.
The MH-47G Special Operations Aviation (SOA) version is currently being delivered to the U.S. Army. It is similar to the MH-47E, but features more sophisticated avionics including a digital Common Avionics Architecture System (CAAS). The CAAS is a common glass cockpit used by different helicopters such as MH-60K/Ls, CH-53E/Ks, and ARH-70As. The MH-47G also incorporates all of the new sections of the CH-47F.
The new modernization program improves MH-47D and MH-47E Special Operations Chinook helicopters to the MH-47G design specs. A total of 25 MH-47E and 11 MH-47D aircraft were upgraded by the end of 2003. In 2002 the army announced plans to expand the Special Operations Aviation Regiment. The expansion would add 12 additional MH-47G helicopters. On 10 February 2011, leaders and employees from the H-47 program gathered for a ceremony at Boeing's helicopter facility in Ridley Park, PA, to commemorate the delivery of the final MH-47G Chinook to U.S. Army Special Operations Command. Modernization of MH-47D/E Chinooks to MH-47G standard is due for completion in 2015.
The CH-47J is a medium-transport helicopter for the Japan Ground Self-Defense Force (JGSDF), and the Japan Air Self-Defense Force (JASDF). The differences between the CH-47J and the CH-47D are the engine, rotor brake and avionics, for use for general transportation, SAR and disaster activity like U.S. forces. The CH-47JA, introduced in 1993, is a long-range version of the CH-47J, fitted with an enlarged fuel tank, an AAQ-16 FLIR in a turret under the nose, and a partial glass cockpit. Both versions are built under license in Japan by Kawasaki Heavy Industries, who produced 61 aircraft by April 2001.
The Japan Defense Agency ordered 54 aircraft of which 39 were for the JGSDF and 15 were for the JASDF. Boeing supplied flyable aircraft, to which Kawasaki added full avionics, interior, and final paint. The CH-47J model Chinook (N7425H) made its first flight in January 1986, and it was sent to Kawasaki in April. Boeing began delivering five CH-47J kits in September 1985 for assembly at Kawasaki.
On 9 November 2006, the HH-47, a new variant of the Chinook based on the MH-47G, was selected by the U.S. Air Force as the winner of the Combat Search and Rescue (CSAR-X) competition. Four development HH-47s were to be built, with the first of 141 production aircraft planned to enter service in 2012. However, in February 2007 the contract award was protested and the GAO ordered the CSAR-X project to be re-bid. However, the CSAR-X program was again terminated in 2009. In February 2010, the U.S. Air Force announced plans to replace aging HH-60G helicopters. The Air Force is deferring secondary combat search and rescue requirements that called for a larger helicopter.
Other export models
The Royal Air Force variant of the CH-47C is known as the Chinook HC1. The export version of the CH-47C Chinook for the Italian Army was designated "CH-47C Plus". The Royal Air Force versions of the CH-47D are known as the Chinook HC2 and HC2A.
The HH-47D is a search and rescue version for the Republic of Korea Air Force. The CH-47DG is an upgraded version of the CH-47C for Greece. While the CH-47SD (also known as the "Super D") is a modified variant of the CH-47D, with extended range fuel tanks and higher payload carrying capacity; the CH-47SD is currently in use by the Republic of Singapore Air Force, Hellenic Army and the Republic of China Army.
Eight CH-47Cs were delivered to the Canadian Forces in 1974. These helicopters were in Canadian service until 1991, with the designation CH-147. These aircraft were subsequently sold to the Netherlands and are now operated by the Royal Netherlands Air Force as CH-47Ds. Plans are to completely replace the current fleet of 17 CH-47Ds with the F-model and enlarge the fleet to 20 aircraft, pending funding.
- Model 234LR (long range): Commercial transport helicopter. The Model 234LR can be fitted out as an all-passenger, all-cargo, or cargo/passenger transport helicopter.
- Model 234ER (extended range): Commercial transport version.
- Model MLR (multi-purpose long range): Commercial transport version.
- Model 234UT (utility transport): Utility transport helicopter.
- Model 414: The Model 414 is the international export version of the CH-47D. It is also known as the CH-47D International Chinook.
In 1969, work on the experimental Model 347 was begun. It was a CH-47A with a lengthened fuselage, four-blade rotors, detachable wings mounted on top of the fuselage and other changes. It first flew on 27 May 1970 and was evaluated for a few years.
In 1973, the Army contracted Boeing to design a "Heavy Lift Helicopter" (HLH), designated XCH-62A. It appeared to be a scaled-up CH-47 without a conventional body, in a configuration similar to the S-64 Skycrane (CH-54 Tarhe), but the project was canceled in 1975. The program was restarted for test flights in the 1980s and was again not funded by Congress. The scaled up model of the HLH was scrapped at the end of 2005 at Fort Rucker, Alabama.
- Argentina (former)
- Saudi Arabia
- South Korea
- South Vietnam (former)
- United Kingdom - See Boeing Chinook (UK variants)
- United Arab Emirates
- United States of America
- Vietnam (former)
- On 14 July 1977, a U.S. Army CH-47 helicopter was shot down by North Korean forces after straying into the DMZ.
- On 11 September 1982, at an airshow in Mannheim, Germany, a United States Army Chinook (serial number 74-22292) carrying parachutists crashed, killing 46 people. The crash was later found to have been caused by an accumulation of ground walnut grit that had been used to clean the machinery. The accident resulted in the eventual discontinuation of the use of walnut grit as a cleaning agent.
- On 6 November 1986, a British International Helicopters Chinook crashed on approach to Sumburgh Airport, Shetland Islands resulting in the loss of 45 lives and the withdrawal of the Chinook from crew-servicing flights in the North Sea.
- On 1 March 1991, Major Marie Therese Rossi Cayton was killed when her Chinook helicopter crashed after colliding with a microwave tower during a dust storm. She was the first American woman to fly in combat during Desert Storm in 1991.
- On 2 June 1994, a British RAF CH-47 crashed killing 25 passengers and 4 crew in Scotland.
- On 29 May 2001, a ROK Army CH-47D installing a sculpture onto Olympic Bridge in Seoul, South Korea failed to unlatch the sculpture. The helicopter's rotors struck the monument; then the fuselage hit and broke into two. One section crashed onto the bridge in flames and the other fell into the river. All three crew members on board died.
- On 21 February 2002, a U.S. Army Special Forces MH-47E crashed at sea in the Philippines, killing all ten U.S. soldiers on board. No enemy fire was involved.
- On 11 September 2004, a Greek Army CH-47SD crashed into the sea off Mount Athos. All 17 people on board were killed, including four senior figures in the Greek Orthodox Church of Alexandria.
- On 7 January 2013, a BV-234 N241CH owned by Columbia Helicopters, Inc., crashed shortly after taking off from the airport in Pucallpa, Coronel Portillo Province, Peru. All seven crew members were killed.
- Crew: three (pilot, copilot, flight engineer)
- 33–55 troops or
- 24 litters and 3 attendants or
- 28,000 lb (12,700 kg) cargo
- Length: 52 ft. fuselage, 98 ft 10 in. with rotors (30.1 m)
- Rotor diameter: 60 ft 0 in (18.3 m)
- Height: 18 ft 11 in (5.7 m)
- Disc area: 5,600 ft2 (520 m2)
- Empty weight: 23,400 lb (10,185 kg)
- Loaded weight: 26,680 lb (12,100 kg)
- Max. takeoff weight: 50,000 lb (22,680 kg)
- Powerplant: 2 × Lycoming T55-GA-714A turboshaft, 4,733 hp (3,529 kW) each
- Maximum speed: 170 knots (196 mph, 315 km/h)
- Cruise speed: 130 kt (149 mph, 240 km/h)
- Range: 400 nmi (450 mi, 741 km)
- Combat radius: 200 nmi (370.4 km)
- Ferry range: 1,216 nmi (1,400 mi, 2,252 km)
- Service ceiling: 18,500 ft (5,640 m)
- Rate of climb: 1,522 ft/min (7.73 m/s)
- Disc loading: 9.5 lb/ft2 (47 kg/m2)
- Power/mass: 0.28 hp/lb (460 W/kg)
- up to 3 pintle mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally 7.62 mm (0.308 in) M240/FN MAG machine guns
- Rockwell Collins Common Avionics Architecture System (CAAS) (MH-47G/CH-47F)
M240 machine gun emplacement on the loading ramp, as well as another partly visible on the right shoulder window
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
- List of active United States military aircraft
- List of aviation shootdowns and accidents during the Iraq War
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