| C-141 Starlifter | |
|---|---|
 A United States Air Force C-141B in flight | |
| General information | |
| Type | Strategic airlifter |
| National origin | United States |
| Manufacturer | Lockheed |
| Status | Retired |
| Primary users | United States Air Force |
| Number built | 285 |
| History | |
| Manufactured | 1963 (1963)–1968 (1968) |
| Introduction date | April 1965 |
| First flight | December 17, 1963; 62 years ago (1963-12-17) |
| Retired | May 2006 |
| Variant | Kuiper Airborne Observatory |
TheLockheed C-141 Starlifter is a retired militarystrategic airlifter that served with theMilitary Air Transport Service (MATS), its successor organization theMilitary Airlift Command (MAC), and finally theAir Mobility Command (AMC) of theUnited States Air Force (USAF). The aircraft also served with airlift and air mobility wings of theAir Force Reserve (AFRES), later renamedAir Force Reserve Command (AFRC), theAir National Guard (ANG) and, later, one air mobility wing of theAir Education and Training Command (AETC) dedicated to C-141,C-5,C-17 andKC-135 training.
Introduced to replace slower propeller driven cargo planes such as theDouglas C-124 Globemaster II andDouglas C-133 Cargomaster, the C-141 was designed to requirements set in 1960 and first flew in 1963. Production deliveries of an eventual 285 planes began in 1965: 284 for the USAF, and a company demonstrator later delivered toNational Aeronautics and Space Administration (NASA) for use as an airborne observatory. The aircraft remained in service for over 40 years until the USAF withdrew the last C-141s from service in 2006, after replacing the airlifter with the C-17 Globemaster III.
Throughout the early 1960s, the United States Air Force'sMilitary Air Transport Service (MATS) relied on a substantial number of propeller-driven aircraft for strategic airlift.[1][2] As these aircraft were mostly obsolescent designs and the USAF needed the benefits of jet power, the USAF ordered 48Boeing C-135 Stratolifters as an interim step. The C-135 was a useful stop-gap, but only had side-loading doors, thus much of the bulky and oversize equipment employed by theU.S. Army would not fit.[3]
In spring 1960, the USAF releasedSpecific Operational Requirement (SOR) 182, calling for a new aircraft that would be capable of performing both strategic and tactical airlift missions.[4] The strategic role demanded that the aircraft be capable of missions with a radius of at least 3,500 nautical miles (6,500 km) with a 60,000 pounds (27,000 kg) load. The tactical role required it to be able to perform low-altitude air drops of supplies, as well as carry and drop combat paratroops.[5] The final version of SOR 182 was released in fall 1960, and requests for proposals were sent to Boeing, Douglas, Convair, and Lockheed-Georgia.[6]
Lockheed's design team produced their own unique design in response to the requirement, internally designated as theLockheed Model 300; it would be the first large jet designed from the start to carry freight. In comparison to the firm's previous utility transport, theturboprop-poweredLockheed C-130 Hercules, it was considerably bigger, as well as possessing greater speed and more power.[7] In terms of its basic configuration, the Model 300 was a large airlifter, furnished with aT-tail and a high-mountedswept wing, under which a total of four pod-mountedTF33turbofan engines were fitted.[4] The Model 300 possessed a lengthy, unobstructed cargo deck, which provided sufficient space and fittings to safely accommodate up to 154 troops or 42,869 kg (94,510 lb) of cargo.[4]
During March 1961, Lockheed's submission was selected as the winner.[4] PresidentJohn F. Kennedy's first official act after his inauguration was to order the development of the Lockheed 300 on 13 March 1961, placing an initial contract for five aircraft for test and evaluation, to be designated theC-141. One unusual aspect of the aircraft was that it was designed to meet both military and civil airworthiness standards. The prototypeC-141A serial number61-2775 was manufactured and assembled in record time, having been rolled out of Lockheed's factory at Marietta, Georgia on 22 August 1963. It was also the first aircraft to be designed and produced at the plant that would go into full-rate production.[8] The prototype performed itsmaiden flight on 17 December of that year, coinciding with the 60th anniversary of theWright brothers' first flight.[4]
In conjunction with the USAF, Lockheed subjected the prototype to an intensive flight testing program, which would involve five testing and evaluation aircraft.[4] The first delivery of a production C-141 occurred during April 1965.[4] Over the course of three years, a total of 284 C-141s were manufactured, excluding five aircraft constructed for testing purposes. Production of new-build C-141s ended in February 1968.[4]
During the 1960s, Lockheed made efforts to market the aircraft on the civilian market; this resulted in provisional orders having been placed by bothFlying Tiger Line andSlick Airways. These were to be a stretched version, 37 feet (11 m) longer than the C-141A, which was marketed as theL-300B orL-301SuperstarLifter. Slick's order was ultimately for six firm, and Flying Tiger for eight.[9] Other changes were also incorporated to adapt the design to be more suited to the commercial sector, including the use of a different controlyoke. Following the satisfactory completion of civil testing, aFederal Aviation Administration (FAA)type certificate was awarded to the C-141 on 29 January 1965 to allow it to operate commercially.[10] In summer 1965, go ahead on a commercial version seemed likely,[11] but later that year Slick abandoned scheduled and domestic service.[12] When no commercial sales were made, Lockheed donated the aircraft toNASA.[13]
Another, more ambitious proposal, commonly designated asSC.5/40, sought to combine elements of the Starlifter with another strategic airlifter, theturboprop-poweredShort Belfast, was to be performed in partnership with theBritish aircraft manufacturerShorts.[14] For this variant, the fuselage of the Belfast would have been paired with the wing of the Starlifter, which would have readily enabled the adoption ofturbojet engines; speculated engines to power the envisioned airlifter included thePratt & Whitney JT3D-3 (18,000 lb) or JT3D-8 (21,000 lb),Rolls-Royce Conway 550 (21,825 lb) orBristol Siddeley BS.100 (27,000 lb approximately).[14][15] A broadly similar but improved proposal, designated asSC.5/45, was heavily promoted by Shorts forOperational Requirement ASR.364, partly on the basis that it would also enable a near-identical civil-orientated model to be produced for home and export use, designated asSC.5/41.[16] Detailed presentations on theSC.5/41 andSC.5/45 proposals were reportedly made to bothBritish Overseas Airways Corporation (BOAC) and to theRoyal Air Force (RAF) respectively, but no orders were placed.[17]
The Lockheed C-141 Starlifter is a long range strategic airlifter, designed for transporting large quantities of either cargo or passengers. It is powered by an arrangement of fourTF33turbofan engines, each capable of generating up to 21,000 pounds-force (93 kN) of thrust; these were installed in pods beneath the high-mountedswept wing.[4] The underside accommodates the retractabletricycle landing gear, consisting of a twin-wheel nose unit and four-wheel main units, the latter of which retract forward into fairings set onto each side of fuselage. The flight deck is typically operated by a crew of four.[4]
The use of a high-mounted wing enabled internal clearance in the cargo compartment of 10 feet (3.0 m) wide, 9 ft (2.7 m) high and 70 ft (21 m) long. Accordingly, the C-141 was capable of carrying, for example, a completeLGM-30 Minutemanintercontinental ballistic missile (ICBM) in its container; it was capable of carrying a maximum of 70,847 pounds (32,136 kg) over short distances, and carry up to 92,000 pounds (42,000 kg) when appropriately configured to carry the Minuteman, which lacked other equipment. In terms of personnel, the aircraft could carry a maximum of 154 fully-equipped troops, 123 paratroops or 80 litter patients at a time.[4] In practice, it was discovered that, under typical conditions, the cargo deck of the C-141A would run out of volume before the maximum weight value could be reached.[18]
In terms of ground logistics, an important aspect of the C-141 was the floor height of the cabin being only 50 inches (130 cm) above the ground, enabling easy access to the cabin via the large rear doors incorporated into the upwards-sweeping rear fuselage. This section is furnished with a large single-piecehydraulically-actuated loading ramp for simplified loading/unloading of both vehicles and general cargo.[4] The two side-facing rear doors were designed to allow the type to be used for droppingparatroops (in August 1965, the C-141 performed the first such drop from a jet-powered aircraft). The rear cargo doors could be also opened in flight to perform airborne cargo drops.[4]
The prototype and development aircraft were involved in an intensive operational testing program, along with the first C-141 to be delivered to MATS (63-8078) on 19 October 1964 to the 1707th Air Transport Wing, Heavy (Training),Tinker Air Force Base, Oklahoma.[19][20] The first delivery to an operational unit (63-8088) was conducted on 23 April 1965 to the 44th Air Transport Squadron, 1501st Air Transport Wing,Travis Air Force Base, California.[21]
Although operational testing was still underway, as a consequence of the United States' military involvement inSouth Vietnam, the C-141 was quickly dispatched to the region to commence operational sorties within the combat zone. The type became heavily used throughout the latter stages of theVietnam War, its transport capabilities being in high demand.[22] Even following the arrival of large numbers of C-141s in the Vietnam theatre, the type was never able to replace theC-124 Globemaster II fully due to its inability to transportoutsize equipment in-theatre; this situation was later addressed by the introduction of the even largerC-5 Galaxy.[2][23] The final duties performed by the C-141 in the conflict were repatriation flights, bringing home thousands of Americanprisoners of war (POWs).[24]
Despite some operational issues experienced, the C-141 formed the backbone of the USAF's strategic airlift capability during the late 1960s; it continued to hold this status through to the late 1990s.[25] On 8 January 1966, following the disestablishment of MATS, all C-141s were transferred to the newly establishedMilitary Airlift Command (MAC).[26]
During October 1973, both the C-141 and the larger C-5 Galaxy airlifted supplies from the United States to Israel during the 1973Yom Kippur War as part ofOperation Nickel Grass. Over the course of the operation, C-141s flew 422 missions and carried a total of 10,754 tons of cargo.[27] By 1975, the C-141 fleet had reportedly accumulated an average of 20,000 flight hours each, two-thirds of their original rated life span.[25]
Despite an early belief that the advantages of theturbojet over preceding propeller-driven cargo aircraft would render the latter obsolete, service experiences with the C-141 found that there was still a useful role forturboprop-driven utility transports such as theLockheed C-130 Hercules. Capabilities such as short-field takeoff performance and suitability for austere airstrips meant that such aircraft proved useful, while the C-141 proved to be anything but robust, suffering numerous instances of structural failures.[28] Specifically, the C-141 fleet was troubled by seemingly random cracking through the wing area, which was, according to a report compiled by theGovernment Accountability Office (GAO), sometimes attributable to stresses imposed under certain types of missions undertaken. A planned remedial program during the 1980s to repair C-141wing boxes uncovered significant corrosion and cracking, necessitating the replacement of all wing boxes across the fleet instead of making repairs.[29]
During the late 1970s, the USAF opted to commence a series of major upgrades to the C-141 fleet; not only was work started on a life extension program but, in 1977, the service also accepted a proposal from Lockheed to stretch several aircraft.[25] The first of these stretched airlifters, re-designatedC-141B to differentiate it from unmodified members of the fleet, was delivered during December 1979. The final C-141B was delivered in 1982.[25] A total of 270 C-141As were modified to the C-141B standard, comprising nearly the entire original production run.[30]
The first strategic airlift flight ofOperation Desert Shield was flown by a MAC C-141 of the437th Military Airlift Wing out ofCharleston AFB, SC, on 7 August 1990. The C-141 proved to be a workhorse airlifter of Operations Desert Shield andDesert Storm, flying 159,462 short tons (144,661 t) of cargo and 93,126 passengers during 8,536 airlift missions.[31] In order to provide sufficient C-141s to meet intense demands, all scheduled maintenance activities were postponed, while the planned peacetime flight hours of the fleet were doubled. According to a GAO report, weight-related operational restrictions imposed upon the fleet have little effect on performance overall.[32] This airlift effort has been referred to as the largest in history.[32]
On 1 June 1992, following the disestablishment of Military Airlift Command, all C-141s and the airlift wings to which they were assigned were transferred to the newly established Air Mobility Command (AMC).Air Force Reserve Command (AFRC) andAir National Guard (ANG) C-141s and units were also transferred to AMC.[26]
By 1992, shortly following the end of Desert Storm, according to a GAO report, the C-141 fleet had, on average, nearly reached its 30,000 flight hour rated service life.[33] While the USAF was in the process of putting the fleet through a life extension program, numerous aircraft had reached well into their extended service life already, necessitating large numbers of C-141s to be withdrawn accompanied by tight limitations on the remaining fleet's flying hours being implemented during the 1990s. The GAO warned that, should another event on the scale of Desert Storm break out, the USAF would probably experience a significant shortage in airlift capabilities due to the high fatigue state of the fleet, and noted that theC-17 Globemaster III intended to eventually replace the C-141 was experiencing delays.[34]
During 1994, one of the aircraft based at Wright-Patterson AFB was identified by its crew chief as theHanoi Taxi (AF Serial Number 66-0177), the first aircraft to land in North Vietnam in 1973 forOperation Homecoming in the final days of theVietnam War, torepatriateAmericanPOWs fromNorth Vietnam.[35]
Between 1996 and 1998, a C-141A was used as a towing aircraft in theEclipse project to demonstrate the possibility of using aerotow systems to bring towed winged vehicles to sufficient altitude to launch small satellites, the ultimate goal was to lower the cost of space launches. Six successful tests were flown with a modifiedConvair F-106 Delta Dart, the QF-106 variant, in tow.[36] A similar system can be seen inSpaceShipTwo, whereby atmospheric engines carry a rocket-engined "second stage" to high altitude for launch.
On 16 September 2004, the C-141 left service with all active USAF units, being confined to Air Force Reserve and Air National Guard units for the final two years of its operational service life. Between 2004 and 2006, multiple C-141s assigned to the Air Force Reserve's445th Airlift Wing (445 AW) atWright-Patterson AFB were deployed toIraq andAfghanistan, where they were typically engaged in themedical evacuation (MEDEVAC) mission to repatriate wounded service members.[37]
In 2005,Hanoi Taxi and other aircraft were marshalled by the USAF to provide evacuation for those seeking refuge fromHurricane Katrina. This aircraft and others evacuated thousands of people, including the MEDIVAC of hundreds of ill and injured. With the 5 May 2005 announcement of the retirement of the last eight C-141s, theHanoi Taxi embarked on a series of flights, giving veterans, some of whom flew out of POW captivity in Vietnam in this aircraft, the opportunity to experience one more flight before retirement.[citation needed] On 6 May 2006, theHanoi Taxi landed for the last time and was received in a formal retirement ceremony at the National Museum of the United States Air Force, located at Wright-Patterson Air Force Base nearDayton, Ohio.[38]
There are 15 C-141s, including the "Hanoi Taxi", now on static display at various air museums around the United States, all other airframes were retired to the "boneyard" at Davis-Monthan AFB, Arizona, where they were scrapped.[39]
The originalStarlifter model, designatedC-141A, could carry 154 passengers, 123 paratroopers or 80 litters for wounded with seating for 16. A total of 284 A-models were built. The C-141A entered service in April 1965. It was soon discovered that the aircraft's volume capacity was relatively low in comparison to its lifting capacity; it generally ran out of physical space before it hit its weight limit.[40] The C-141A could carry ten standard463L master pallets and had a total cargo capacity of 62,700 pounds (28,400 kg). It could also carry specialized cargoes, such as theMinuteman missile.
NASA obtained Lockheed's C-141 demonstrator, designated L-300.[41][42] The airplane was modified to house theKuiper Airborne Observatory (KAO) telescope for use at very high altitudes. This aircraft, NC-141A is in storage atNASA Ames Research Center,Moffett Federal Airfield, California.[41] The KAO was retired in 1995 and was replaced by the 747SP-basedStratospheric Observatory for Infrared Astronomy (SOFIA).[43]
In service, the C-141 proved to "bulk out" before it "grossed out", meaning that it often had additional lift capacity that went wasted because the cargo hold was full before the plane's weight capacity had been reached. To correct the perceived deficiencies of the original model and utilize the C-141 to the fullest of its capabilities, 270 in-service C-141As (vast majority of the fleet) were stretched, adding needed payload volume. The conversion program took place between 1977 and 1982, with first delivery taking place in December 1979.[4] These modified aircraft were designatedC-141B. It was estimated that this stretching program was equivalent to buying 90 new aircraft, in terms of increased capacity. Also added was a boom receptacle forinflight refueling.[44] The fuselage was stretched by adding "plug" sections forward and aft of the wings, lengthening the fuselage a total of 23 feet 4 inches (7.11 m) and allowing the carriage of 103 litters for wounded, 13 standard pallets, 205 troops, 168paratroopers, or an equivalent increase in other loads.
In 1994, a total of 13 C-141Bs were givenSOLL II (Special Operations Low-Level II) modifications, which gave the aircraft a low-level night flying capability, enhanced navigation equipment, and improved defensive countermeasures. These aircraft were operated by AMC in conjunction withAir Force Special Operations Command (AFSOC).
A total of 63 C-141s were upgraded throughout the 1990s toC-141C configuration, with improved avionics and navigation systems, to keep them up to date. New capabilities, includingtraffic collision avoidance system (TCAS) andGlobal Positioning System (GPS), were added to aircraft that received this upgrade package.[4] This variant introduced some of the firstglass cockpit technology to the aircraft, as well as improving reliability by replacing some mechanical and electromechanical components with more modern electronic equivalents. The final C-141C were delivered during late 2001.[4]
21 C-141s were lost to accidents in the plane's 41-year service life.
| Date | Type | Tail | Unit | Location | Fatalities | Cause | Refs |
|---|---|---|---|---|---|---|---|
| 7 Sep 1966 | C-141A | 65-0281 | 62 MAW | McChord AFB, WA | 3 ground crew | Ground accident (explosion and fire) during fuel systems maintenance work not performed in accordance with procedures. | [45][46] |
| 23 Mar 1967 | C-141A | 65-9407 | 62 MAW | Da Nang, Republic of Vietnam (South Vietnam) | 5 crew | Ground collision after air traffic control cleared aUSMC fighter jet for takeoff, but also cleared the C-141 to cross the runway. One C-141 crew member and both USMC pilots survived. | [47][46][48] |
| 13 Apr 1967 | C-141A | 66-0127 | 62 MAW | Cam Ranh Bay, Republic of Vietnam (South Vietnam) | 7 crew | Crashed just after takeoff due to checklist deviation. | [49][46] |
| 28 Aug 1973 | C-141A | 63-8077 | 438 MAW | Hueva Castile-La Mancha,Spain (nearTorrejon AB) | 7 crew, 17 passengers | Ground impact in level flight due to miscommunication with Torrejon AB air traffic control and checklist deviation. One crew member survived. | [50][46] |
| 18 Aug 1974 | C-141A | 65-0274 | 437 MAW | Mount Potosi, about 17 miles (27 km) fromLa Paz,Bolivia | 7 crew | Crashed at the 19,000 feet (5,800 m) level of a 20,000 feet (6,100 m) mountain due to navigation error in reporting position to air traffic control. | [51][46][52] |
| 21 Mar 1975 | C-141A | 64-0641 | 62 MAW | Mount Constance,Washington (near McChord AFB) | 10 crew, 6 passengers | Air traffic control confused aircraft call signs and cleared the C-141A to descend below safe minimums. | [53][46] |
| 28 Aug 1976 | C-141A | 67-0006 | 438 MAW | Peterborough, Cambridgeshire,England, nearRAF Mildenhall | 14 crew, 4 passengers | Navigating through thunderstorms with an inoperative weather radar, the aircraft encountered severe turbulence and broke up in-flight while on approach for landing. | [54][55][46][56] |
| 28 Aug 1976 | C-141A | 67-0008 | 438 MAW | Søndre Strømfjord,Greenland | 7 crew, 16 passengers | Flight crew attempted a go around after touchdown. The plane over-rotated, stalled, and crashed on the runway. One crew member and three passengers survived. | [54][55][46] |
| 18 Sep 1979 | C-141 | 64-0647 | 438 MAW | Charleston, South Carolina | 0 | Electrical failure in landing gear handle caused nose gear to retract after landing. Fire then destroyed the aircraft. | [51][46] |
| 12 Nov 1980 | C-141 | 67-0030 | 62 MAW | Cairo West Air Base,Egypt | 6 crew, 7 passengers | Crashed while on a visual approach for a night landing. During the turn to final the aircraft’s bank angle and rate of descent increased until impact. | [57][46] |
| 7 Mar 1982 | C-141B | 67-0017 | 438 MAW | Cairo West Air Base, Egypt | 0 | Ground accident (fire) caused by an APU accumulator failure. | [46] |
| 31 Aug 1982 | C-141B | 64-0652 | 437 MAW | nearKnoxville, Tennessee | 9 crew | Crashed into a mountain during a low-level airdrop training mission in marginal weather. | [58][46] |
| 12 Jul 1984 | C-141B | 64-0624 | 315 MAW | NAS Sigonella,Lentini,Sicily,Italy | 8 crew, 1 passenger | Crashed shortly after takeoff due to multiple engine failures and fire in the cargo compartment. | [59][60][46] |
| 15 Oct 1986 | C-141B | 65-0246 | 439 MAW | Travis Air Force Base,Solano County, California | 0 | While parking after landing, the left wing struck a light pole and caught fire, destroying the left wing. | [46] |
| 20 Feb 1989 | C-141B | 66-0150 | 63 MAW | nearHurlburt Field,Okaloosa County, Florida | 7 crew, 1 passenger | Controlled flight into terrain. Crashed into ground four miles from the runway while on approach for landing, and in a high rate of descent. | [61][46] |
| 1 Dec 1992 | C-141B | 66-0142 | 62 MAW | nearHarlem, Montana | 6 crew | Mid-air collision with C-141 65-0255 (below) while flying a night air refueling/airdrop training mission. | [62][63][46] |
| 1 Dec 1992 | C-141B | 65-0255 | 62 MAW | near Harlem, Montana | 7 crew | Mid-air collision with C-141 66-0142 (above) while flying a night air refueling/airdrop training mission. | [62][63][46] |
| 7 Oct 1993 | C-141B | 65-0253 | 60 AMW | Travis Air Force Base, Solano County, California | 0 | Ground accident (explosion and fire) during fuel systems maintenance work not performed to procedures. | [64][46] |
| 23 Mar 1994 | C-141B | 66-0173 | 438 MAW | Pope Air Force Base,North Carolina | 24 Army personnel | Destroyed while on the ground when struck by debris from a nearby mid-air collision between an F-16 and a C-130. The aircraft was in the process of loading Army Paratroops at the time. | [65][46] |
| 13 Sep 1997 | C-141B | 65-9405 | 305 AMW | Atlantic Ocean, 80 miles off the coast ofNamibia,Africa | 9 crew | Mid-air collision with aGerman Air ForceTu-154. | [66][46] |
| 22 Dec 2001 | C-141B | Unknown | 164 AW | Memphis International Airport | 0 | Mechanical failure of the left wing structure during ground refueling caused by an incomplete maintenance procedure. | [67][46] |
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Data fromForecast International[4]
General characteristics
Performance
Related development
Aircraft of comparable role, configuration, and era
Related lists
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| National | |
| Other | |
