Airbus A400M Atlas

As of July 2012 the A400M is undergoing flight testing. Orders totalled 174 aircraft from eight nations as of July 2011. Airbus Military is expected to deliver the first aircraft in early 2013.

Top 5 Important Pictures That Shaped America

On July 20, 1969, the United States Apollo 11 space flight landed on the moon. It was the third lunar mission of NASA’s Apollo program and the vessel was crewed by Commander Neil Armstrong, Command Module Pilot Michael Collins, and Lunar Module Pilot Buzz Aldrin Jr.

Nokia Lumia 900 review

The Nokia Lumia 900 is a good-looking phone that boasts a bright 4.3in screen that shows off the software’s distinctive live tiles

Samsung Galaxy Note 2 release rumoured for August 30th

Further blurring the lines between smartphones and tablets, Samsung is rumoured to be preparing a Samsung Galaxy Note 2 release for IFA 2012

Addis Ababa’s Future National Stadium And Sports Village In Ethiopia

Entertainment is an essential part of our lives; without entertainment, sports or games, our lives would be like a barren land.

Tampilkan postingan dengan label Aircraft. Tampilkan semua postingan
Tampilkan postingan dengan label Aircraft. Tampilkan semua postingan

Minggu, 22 Juli 2012

Airbus A400M Atlas ~ Fourtriangle





As of July 2012 the A400M is undergoing flight testing. Orders totalled 174 aircraft from eight nations as of July 2011. Airbus Military is expected to deliver the first aircraft in early 2013. The Airbus A400M Atlas,is a multi-national four-engine turboprop military transport aircraft. It was designed by Airbus Military as a tactical airlifter with strategic capabilities.The aircraft's maiden flight, originally planned for 2008, took place on 11 December 2009 in Seville, Spain.

As of July 2012 the A400M is undergoing flight testing. Orders totalled 174 aircraft from eight nations as of July 2011.Airbus Military is expected to deliver the first aircraft in early 2013.

Development

Origins

The project began as the Future International Military Airlifter (FIMA) group, set up in 1982 by Aérospatiale, British Aerospace (BAe), Lockheed, and Messerschmitt-Bölkow-Blohm (MBB) to develop a replacement for the C-130 Hercules and Transall C-160.Varying requirements and the complications of international politics caused slow progress. In 1989 Lockheed left the grouping and went on to develop an upgraded Hercules, the C-130J Super Hercules. With the addition of Alenia of Italy and CASA of Spain the FIMA group became Euroflag.

The A400M is positioned as an intermediate size between the Lockheed C-130, and the Boeing C-17. Originally the SNECMA M138 turboprop (based on the M88 core) was selected to power the A400M. Airbus Military issued a new request for proposal (RFP) in April 2002, after which Pratt & Whitney Canada with the PW180 and Europrop International answered; the latter was a new design. Airbus Military preferred the PWC engine, but political interference resulted in the selection of the Europrop TP400-D6 in May 2003.

The partner nations – France, Germany, Italy, Spain, the United Kingdom, Turkey, Belgium, and Luxembourg – signed an agreement in May 2003 to buy 212 aircraft. These nations decided to charge the Organisation for Joint Armament Cooperation (OCCAR) with the management of the acquisition of the A400M.

Following the withdrawal of Italy and revision of procurement totals the revised requirement was for 180 aircraft, with first flight in 2008 and first delivery in 2009. On 28 April 2005, South Africa joined the partnership programme with the state-owned Denel Saab Aerostructures receiving a contract for fuselage components.

Into production


The A400M assembly at the Seville plant of EADS Spain started in the first quarter of 2007. Airbus plans to manufacture thirty aircraft per year.The major assemblies arrive by Airbus Beluga transporters. The four Europrop TP400-D6 flight test engines were delivered in late February 2008 for the first A400M.Static structural testing of a A400M test airframe began on 12 March 2008 in Spain.

The first flight, originally scheduled for the first quarter of 2008, was postponed due to program delays, schedule adjustments and financial pressures. EADS announced in early January 2008 that continued development problems with the engines had resulted in a delay to the second quarter of 2008 before the first engine test flights on a C-130 testbed aircraft. The first flight of the aircraft, previously scheduled for July 2008, had again been postponed. Civil certification under European Aviation Safety Agency (EASA) CS-25 will be followed later by certification for military purposes. The A400M was "rolled out" in Seville on 26 June 2008 at an event presided by King Juan Carlos I of Spain.On 12 January 2011, serial production of the A400M for its first customers started.

Development problems

On 9 January 2009, EADS announced that the first delivery has been postponed until at least 2012. EADS also indicated that it wanted to renegotiate "certain technical characteristics" of the aircraft.EADS has long maintained the first deliveries would begin three years after the A400M's first flight. The German newspaper Financial Times Deutschland has closely followed the A400M program and reported on 12 January 2009 that the aircraft is overweight by 12 tons and may not be able to achieve a critical performance requirement, the ability to airlift 32 tons. Sources told FTD at the time that the aircraft could only lift 29 tons, which is insufficient to carry a modern armored infantry fighting vehicle (like the Puma).The FTD report prompted the chief of the German Air Force to say, "That is a disastrous development," and could delay deliveries to the Luftwaffe until 2014.The Initial Operational Capability (IOC) for the Luftwaffe is delayed at least until 2017. This leads the political planning to potential alternatives in the shape of a higher integration of European airlift capabilities.The OCCAR reminded the participating countries that they can terminate the contract before 31 March 2009.

On 29 March 2009, Airbus CEO Thomas Enders told Der Spiegel magazine that the program may need to be abandoned without changes.Then on 3 April 2009 the South African Air Force announced that it would start considering alternatives to the A400M due to postponed production and increased cost.On 5 November 2009, South Africa announced it was cancelling the order citing increased cost and delivery delays.On 12 June, The New York Times reported that Germany and France have delayed the decision whether or not to cancel their orders for another six months, while the UK still plans to decide at the end of June. The NYT also quotes a report to the French Senate from February 2009, according to which "the A400M is €5 billion over budget, 3 to 4 years behind schedule, [...] aerospace experts estimate it is also costing Airbus between €1 billion and €1.5 billion a year."

The shortage of military transports caused by the A400M delay forced the UK to lease, and subsequently purchase, six C-17s. France and Germany have also been considering other planes, as all three countries need to support their operations in Afghanistan.The ADS Group has warned that shifting the British orders to American aircraft for the short term budget savings would cost much more over time in missed civil and military aerospace business, because they say that the technologies used in the A400M would be a bridge to the next generation of civilian aircraft.In June 2009, Lockheed Martin said that both United Kingdom and France had asked for technical details on the C-130J as an alternative to the A400M.

Airbus acknowledged in 2009 that the program is expected to lose at least €2.4 billion and cannot break even without sales outside NATO countries.A PricewaterhouseCoopers audit of the program projected that it would run €11.2 billion over budget unless corrective measures were taken, which would result in an overrun of only €7.6 billion.On 24 July 2009, the seven European nations announced that they would continue with the A400M program, and form a joint procurement agency to renegotiate the contract with EADS.The ministers of the seven European launch customers were supposed to meet 15 October 2009 in Germany to approve a new timetable, configuration and financial terms for the A400M airlifter.On 14 October 2009, French Ministry of Defense spokesman Laurent Teisseire, announced this meeting had been postponed.

On 9 December 2009, the Financial Times reported that Airbus has asked for an additional €5 billion subsidy to complete the project.On 5 January 2010, Airbus repeated that the A400M program may be scrapped, costing Airbus €5.7 billion unless €5.3 billion was added by partner governments.On 11 January 2010, Tom Enders, Airbus chief executive, stated that he was prepared to cancel production of the A400M if European governments did not provide more funding. Delays to the A400M project had already increased its budget by 25%.On 5 November 2010, Belgium, Britain, France, Germany, Luxembourg, Spain and Turkey finalised the contract and agreed to lend Airbus Military €1.5 billion. The program is at least three years behind schedule. The deal, however, meant also that the UK reduced its order from 25 to 22 aircraft and Germany from 60 to 53, decreasing the total order from 180 to 170.

Flight testing

Before the first flight, the company obtained the required hours of airborne test time on the engines using a C-130 testbed aircraft.The first flight of the C-130 testbed occurred on 17 December 2008.The A400M's maiden flight was carried out from Seville on 11 December 2009.The first A400M had flown 39 hours of test flights as of 9 March 2010.The second test aircraft's engines were tested on 18 March 2010 prior to it beginning test flights.The second A400M completed its first flight on 8 April 2010.The third A400M took to the air in July 2010. With this flight the three A400Ms have taken more than 100 flights, totaling 400 hours.

In July 2010, the A400M passed a key test: ultimate-load testing of the wing.On 28 October 2010, Airbus Military announced that it was about to start refuelling and air-drop tests.By late October 2010 the A400M had flown 672 hours of the 2,700 hours expected to reach certification. Cold weather testing is to be performed in either Canada or Sweden.In November 2010, the first paratroop jumps were performed from the A400M.In December 2010 the A400M fleet's flight time has risen to 965 hours.A400M number four joined the test fleet with its first flight of over five hours on 20 December 2010.

Winter tests were done in Kiruna, Sweden during February 2011.By April 2011 a total of 1,400 flight hours over 450 flights had been achieved.In May 2011 the A400M's EPI TP400-D6 engine received certification from the European Aviation Safety Agency (EASA).In May 2011, the A400M fleet had totaled 1,600 hours over 500 flights; by September 2011, the total increased to 2,100 hours and 684 flights.

Due to a problem with the gearbox the A400M did not fly demonstrations at the 2011 Paris Air Show. It was shown on static display insteadBy October 2011, the total flight hours had reached 2,380 over 784 flights. A minor problem that occurred during wet landing test led to reconstruction of parts of the main landing gear door.

High altitude start and landing tests were performed at La Paz at 4,061.5 m (13,325 ft) and Cochabamba at 2,548 m (8,360 feet) in Bolivia in March 2012.

Design


The Airbus A400M will increase the airlift capacity and range compared with the aircraft it was originally set to replace, the older versions of the Hercules and Transall. Cargo capacity is expected to double over existing aircraft, both in payload and volume, and range is increased substantially as well. The cargo box is 17.71 m long excluding ramp, 4.00 m wide, and 3.85 m high (or 4.00 m aft of the wing).and the ramp is 5.40 m long.

The A400M will operate in many configurations including cargo transport, troop transport, Medical evacuation, aerial refuelling, and electronic surveillance. The aircraft is intended for use on short, soft landing strips and for long-range, cargo transport flights.

It features a fly-by-wire flight control system with sidestick controllers and flight envelope protection. Like other Airbus aircraft, the A400M will have a full glass cockpit (all information accessed through large colour screens) and as such will represent a technological leap compared to the older C-130s and C-160s that many countries now operate.

The A400M's wings are primarily carbon fibre reinforced plastic. The eight-bladed Scimitar propeller is also made from a woven composite material. The aircraft is powered by four Europrop TP400-D6 engines rated at 8,250 kW (11,000 hp) each.The TP400-D6 engine is to be the most powerful turboprop engine in the West to enter operational use.One of the few propeller powered aircraft with swept wings, the turboprops provide an efficient cruise speed of 780 km/h (480 mph) which falls between the C-130 and the jet-powered C-17.

The pair of propellers on each wing of the A400M turn in opposite directions, with the tips of the propellers advancing from above towards the midpoint between the two engines. This is in contrast to the overwhelming majority of multi-engine propeller driven aircraft where all propellers on the same wing turn in the same direction. The counter-rotation is achieved by the use of a gearbox fitted to two of the engines, and only the propeller turns the opposite direction; all four engines are identical and turn in the same direction which eliminates the need to have two different "handed" engines on stock for the same aircraft, which simplifies maintenance and supply costs. This configuration, dubbed DBE (Down Between Engines), allows the aircraft to produce more lift and lessens the torque and prop wash on each wing. It also reduces yaw in the event of an outboard engine failure.

EADS and Thales will provide the new Multi-Colour Infrared Alerting Sensor (MIRAS) missile warning sensor for the A400M.

Operational history

Exports

South Africa

In December 2004, South Africa announced it would purchase eight A400Ms at a cost of approximately €837 million, with the nation joining the Airbus Military team as an industrial partner. Deliveries were expected from 2010 to 2012.In 2009, South Africa cancelled all eight aircraft, citing increasing costs. On 29 November 2011 Airbus Military reached an agreement to refund pre-delivery payments worth €837 million to Armscor.

Canada

Airbus Military made a bid in 2006 to supply Canada with the A400M to meet a tender request for 17 new tactical airlifters to replace their old C-130E models.The Canadians ordered four C-17 Globemaster IIIs and 17 C-130J Super Hercules instead.

Others

In July 2005, the Chilean Air Force signed a Memorandum of understanding for three aircraft,but no order has been placed.

In December 2005, the Royal Malaysian Air Force ordered four A400Ms to supplement its fleet of Lockheed C-130 Hercules.

In 2009 the United States Air Force Air Mobility Command requested information on the A400M and the company responded with a proposal for 118 A400Ms.

In June 2010, EADS suggested a possibility that the Royal Australian Air Force might consider buying the A400M.

Specifications

Data from Airbus Military specifications

General characteristics

Crew: 3 or 4 (2 pilots, 3rd optional, 1 loadmaster)
Capacity: 37,000 kg (81,600 lb)
116 fully equipped troops / paratroops,
up to 66 stretchers accompanied by 25 medical personnel
Length: 45.1 m (148 ft 0 in)
Wingspan: 42.4 m (139 ft 1 in)
Height: 14.7 m (48 ft 3 in)
Empty weight: 76,500 kg (168,654 lb) ; operating weight[84]
Max takeoff weight: 141,000 kg (310,852 lb)
Fuel capacity: 50,500 kg (111,330 lb) internal fuel
Max landing weight: 122,000 kg (268,963 lb)
Powerplant: 4 × Europrop TP400-D6 turboprop, 8,250 kW (11,060 hp) each
Propellers: 8-bladed, 5.3 m (17 ft 5 in) diameter

Performance

Cruising speed: 780 km/h (485 mph; 421 kn) (Mach 0.68-0.72)
Initial cruise altitude: at MTOW: 9,000 m (29,000 ft)
Range: 3,298 km (2,049 mi; 1,781 nmi) at max payload (long range cruise speed; reserves as per MIL-C-5011A)
Range at 30-tonne payload: 4,540 km (2,450 nmi)






Source: http://id.wikipedia.org/wiki/Airbus_A400M

Minggu, 01 Juli 2012

Lockheed C-5 Galaxy ~ Fourtriangle



The Lockheed C-5 Galaxy is a large military transport aircraft built by Lockheed. It provides the United States Air Force (USAF) with a heavy intercontinental-range strategic airlift capability, one that can carry outsize and oversize cargos, including all air-certifiable cargo. The Galaxy has many similarities to its smaller C-141 Starlifter predecessor, and the later C-17 Globemaster. The C-5 is among the largest military aircraft in the world.

The C-5 Galaxy had a complicated development; significant cost overruns were experienced and Lockheed suffered significant financial difficulties. Shortly after entering service, fractures in the wings of many aircraft were discovered and the C-5 fleet were restricted in capability until corrective work was conducted. The C-5M Super Galaxy is an upgraded version with new engines and modernized avionics designed to extend its service life beyond 2040.

The C-5 Galaxy has been operated by USAF since 1969. In that time, it has been used to support US military operations in all major contingencies including Vietnam, Iraq, Yugoslavia and Afghanistan; as well as in support of allies, such as Israel during the Yom Kippur War and NATO operations in the Gulf War. The C-5 has also been used to distribute humanitarian aid and disaster relief, and in support of the US Space Shuttle program run by NASA.

Development

CX-X and Heavy Logistics System

In 1961, several aircraft companies began studying heavy jet transport designs that would replace the Douglas C-133 Cargomaster and complement Lockheed C-141 Starlifters. In addition to higher overall performance, the United States Army wanted a transport aircraft with a larger cargo bay than the C-141, whose interior was too small to carry a variety of their outsized equipment. These studies led to the "CX-4" design concept, but in 1962 the proposed six-engine design was rejected, because it was not viewed as a significant advance over the C-141.By late 1963, the next conceptual design was named CX-X. It was equipped with four engines, instead of six engines in the earlier CX-4 concept. The CX-X had a gross weight of 550,000 pounds (249,000 kg), a maximum payload of 180,000 lb (81,600 kg) and a speed of Mach 0.75 (500 mph/805 km/h). The cargo compartment was 17.2 ft (5.24 m) wide by 13.5 feet (4.11 m) high and 100 ft (30.5 m) long with front and rear access doors.To provide required power and range with only four engines required a new engine with dramatically improved fuel efficiency.

The criteria were finalized and an official request for proposal was issued in April 1964 for the "Heavy Logistics System" (CX-HLS) (previously CX-X). In May 1964, proposals for aircraft were received from Boeing, Douglas, General Dynamics, Lockheed, and Martin Marietta. General Electric, Curtiss-Wright, and Pratt & Whitney submitted proposals for the engines. After a downselect, Boeing, Douglas and Lockheed were given one-year study contracts for the airframe, along with General Electric and Pratt & Whitney for the engines.All three of the designs shared a number of features; all three placed the cockpit well above the cargo area to allow for cargo loading through a nose door. The Boeing and Douglas designs used a pod on the top of the fuselage containing the cockpit, while the Lockheed design extended the cockpit profile down the length of the fuselage, giving it an egg-shaped cross section. All of the designs had swept wings, as well as front and rear cargo doors allowing simultaneous loading and unloading. Lockheed's design featured a T-tail, while the designs by Boeing and Douglas had conventional tails.

The Air Force considered Boeing's design better than that of Lockheed, although Lockheed's proposal was the lowest total cost bid.Lockheed was selected the winner in September 1965, then awarded a contract in December 1965.General Electric's TF-39 engine was selected in August 1965 to power the new transport plane.At the time GE's engine concept was revolutionary, as all engines beforehand had a bypass ratio of less than two-to-one, while the TF-39 promised and would achieve a ratio of eight-to-one, which had the benefits of increased engine thrust and lower fuel consumption.

Into production


The first C-5A Galaxy (serial number 66-8303) was rolled out of the manufacturing plant in Marietta, Georgia, on 2 March 1968.On 30 June 1968, flight testing of the C-5A began with the first flight, flown by Leo Sullivan, with the call sign "eight-three-oh-three heavy". Flight tests revealed that the aircraft exhibited a higher drag divergence Mach number than predicted by wind tunnel data. The maximum lift coefficient measured in flight with the flaps deflected 40 degree was higher than predicted (2.60 vs. 2.38), but was lower than predicted with the flaps deflected 25 degrees (2.31 vs. 2.38) and with the flaps retracted (1.45 vs. 1.52).

Aircraft weight was a serious issue during design and development. At the time of the first flight, the weight was below the guaranteed weight, but by the time of the delivery of the 9th aircraft, had exceeded guarantees.In July 1969, during a fuselage upbending test, the wing failed at 128% of limit load, which is below the requirement that it sustain 150% of limit load. Changes were made to the wing, but in a later test, in July 1970, it failed at 125% of limit load. A passive load reduction system, involving uprigged ailerons was incorporated, but the maximum allowable payload was reduced from 220,000 pounds to 190,000 pounds. At the time, it was predicted that there was a 90% probability that no more than 10% of the fleet of 79 airframes would reach their fatigue life of 19,000 hours without cracking of the wing.

Cost overruns and technical problems of the C-5A were the subject of a congressional investigation in 1968 and 1969.The C-5 program has the dubious distinction of being the first development program with a one billion dollar overrun.Due to the C-5's troubled development, the Department of Defense abandoned Total Package Procurement.In 1969 Henry Durham raised concerns about the C-5 production process with Lockheed, his employer; subsequently Durham was transferred and subjected to abuse until he resigned. The Government Accountability Office (GAO) substantiated some of his charges against Lockheed; later the American Ethical Union honored Durham with the Elliott-Black Award.

Upon completion of testing in December 1969, the first C-5A was transferred to the Transitional Training Unit at Altus Air Force Base, Oklahoma. Lockheed delivered the first operational Galaxy to the 437th Airlift Wing, Charleston Air Force Base, SC, in June 1970. Due to higher than expected development costs, in 1970 there were public calls for the government to split the substantial losses that Lockheed were experiencing.Production was nearly brought to a halt in 1971 due to Lockheed going through financial difficulties, partly down to the C-5 Galaxy's development but also a civilian jet liner, the Lockheed L-1011.The U.S. government gave loans to Lockheed to keep the company operational.

In the early 1970s, NASA considered the C-5 for the Shuttle Carrier Aircraft role, to transport the Space Shuttle to Kennedy Space Center. However, they rejected it in favor of the Boeing 747, in part due to the 747's low-wing design.In contrast, the Soviet Union chose to transport its shuttles using the high-winged An-225,which derives from the An-124, which is similar in design and function to the C-5.

During static and fatigue testing cracks were noticed in the wings of several aircraft,and as a consequence the C-5A fleet was restricted to 80% of maximum design loads. To reduce wing loading, load alleviation systems were added to the aircraft.By 1980, payloads were restricted to as low as 50,000 lb (23,000 kg) for general cargo during peacetime operations. A $1.5 billion program, known as H-Mod,to re-wing the 76 completed C-5As to restore full payload capability and service life began in 1976.After design and testing of the new wing design, the C-5As received their new wings from 1980 to 1987.During 1976, numerous cracks were also found in the fuselage along the upper fuselage on the centerline, aft of the refueling port, extending back to the wing. The cracks required a redesign to the hydraulic system for the visor, the front cargo entry point.

Continued production and development

In 1974, Iran, then holding good relations with the United States, offered $160 million to restart C-5 production to enable Iran to purchase aircraft for their own air force;in a similar climate as to their acquisition of F-14 Tomcat fighters.However no C-5 aircraft were ever ordered by Iran, as the prospect was firmly halted by the Iranian Revolution in 1979.

As part of President Ronald Reagan's military policy, funding was made available for expansion of the USAF's airlift capability; however as the C-17 program was still some years from completion a new version of the C-5, the C-5B, was approved by Congress in July 1982 for purchase instead.The first C-5B was delivered to Altus Air Force Base in January 1986. In April 1989, the last of 50 C-5B aircraft was added to the 77 C-5As in the Air Force's airlift force structure. The C-5B includes all C-5A improvements and numerous additional system modifications to improve reliability and maintainability.

In 1998, the Avionics Modernization Program (AMP) began upgrading the C-5's avionics to include a glass cockpit, navigation equipment, and a new autopilot system.Another part of the C-5 modernization effort is the Reliability Enhancement and Re-engining Program (RERP). The program will mainly replace the engines with newer, more powerful ones. Three C-5s underwent RERP as a test with full production in May 2008.

A total of 52 C-5s are contracted to be modernized, consisting of 49 B-, two C- and one A-model aircraft through the Reliability Enhancement and Re-Engining Program (RERP). Over 70 changes and upgrades are incorporated in the program, including the newer General Electric engines. Five C-5M Super Galaxies have been produced.The RERP upgrade program is to be completed in 2016.

Design

Overview

The C-5 is a large high-wing cargo aircraft. It has a distinctive high T-tail, 25 degree wing sweep, and four TF39 turbofan engines mounted on pylons beneath the wings. The C-5 is similar in layout to its smaller predecessor, the C-141 Starlifter. The C-5 has 12 internal wing tanks and is equipped for aerial refueling.
It has both nose and aft doors for "drive-through" loading and unloading of cargo.The C-5 is also known as FRED (fucking, sometimes written as "fantastic", ridiculous, economic/environmental disaster)by its crews due to its maintenance/reliability issues and large consumption of fuel.

It has an upper deck seating area for 73 passengers and 2 loadmasters. The passengers face the rear of the aircraft, rather than forward. Its takeoff and landing distances, at maximum gross weight, are 8,300 ft (2,500 m) and 4,900 ft (1,500 m) respectively. Its high flotation main landing gear has 28 wheels to share the weight. The rear main landing gear is steerable for a smaller turning radius and it rotates 90 degrees horizontally before it is retracted after takeoff. The "kneeling" landing gear system permits lowering of the parked aircraft so the cargo floor is at truck-bed height to facilitate vehicle loading and unloading.

The C-5 has a Malfunction Detection Analysis and Recording (MADAR) system to identify errors throughout the aircraft. Some Galaxies have a Low Pressure Pneumatic System (LPPS) that utilizes a turbo compressor driven by bleed air to provide up to 150 psi pressure for inflating the aircraft's tires. One of the unique features of the aircraft is the crosswind landing system that allows the landing gear to be offset up to 20 degrees either side of centerline; when the main landing gear was down (MLG) all the other 28 wheels would be slaved to the MLG and driven by hydraulic actuators to the same offset.

The C-5 features a cargo compartment 121 ft (37 m) long, 13.5 ft (4.1 m) high, and 19 ft (5.8 m) wide, or just over 31,000 cu ft (880 m3). The compartment can accommodate up to 36 463L master pallets or a mix of palletized cargo and vehicles. The cargo hold of the C-5 is a foot longer than the entire length of the first powered flight by the Wright Brothers at Kitty Hawk.The nose and aft doors open the full width and height of the cargo compartment to permit faster and easier loading. Ramps are full width at each end for loading double rows of vehicles.

The Galaxy is capable of carrying nearly every type of the Army's combat equipment, including bulky items such as the 74 short tons (67 t) armored vehicle launched bridge (AVLB), from the United States to any location on the globe.A C-5 is capable of transporting up to six Boeing AH-64 Apaches or five Bradley Fighting Vehicles.

Operational history

The first C-5A was delivered to the USAF on 17 December 1969. Wings were built up in the early 1970s at Altus AFB, Oklahoma, Charleston AFB, Dover AFB, Delaware, and Travis AFB, California. The C-5's first mission was on 9 July 1970, in Southeast Asia during the Vietnam War.C-5s were used to transport equipment and troops, including Army tanks and even some small aircraft, throughout the later years of the US action in Vietnam.In the final weeks of the war, prior to the Fall of Saigon, several C-5s were involved in evacuation efforts; during one such mission a C-5A crashed while transporting a large number of orphans.

C-5s have also been used to deliver support and reinforce various US allies over the years. During the Yom Kippur war in 1973, multiple C-5s and C-141 Starlifters delivered critical supplies of ammunition, replacement weaponry and other forms of aid to Israel, the US effort was named as Operation Nickel Grass.The C-5 Galaxy's performance in Israel was such that the Pentagon began to consider further purchases.The C-5 was regularly made available to support American allies, such as the British-led peacekeeper initiative in Zimbabwe in 1979.

On 24 October 1974, the Space and Missile Systems Organization successfully conducted an Air Mobile Feasibility Test where a C-5A Galaxy aircraft air dropped a 86,000 lb Minuteman ICBM from 20,000 ft over the Pacific Ocean. The missile descended to 8,000 ft before its rocket engine fired. The 10-second engine burn carried the missile to 20,000 ft again before it dropped into the ocean. The test proved the feasibility of launching an intercontinental ballistic missile from the air. Operational deployment was discarded due to engineering and security difficulties, though the capability was used as a negotiating point in the Strategic Arms Limitation Talks.

The C-5 has been used for several unusual functions; during the development of the secretive stealth fighter, the Lockheed F-117 Nighthawk, Galaxies were often used to carry partly disassembled aircraft, leaving no exterior signs as to their cargo.It remains the largest aircraft to ever operate in the Antarctic;Williams Field near McMurdo Station is capable of handling C-5 aircraft, the first of which landed there in 1989.The C-5 Galaxy was a major supply asset in the 1991 international coalition operations against Iraq's invasion of Kuwait, known as the First Gulf War.C-5s have routinely delivered relief aid and humanitarian supplies to areas afflicted with natural disasters or crisis, multiple flights were made over Rwanda in 1994.


The wings on the C-5As were replaced during the 1980s to restore full design capability.The USAF took delivery of the first C-5B on 28 December 1985 and the final one in April 1989.The reliability of the C-5 fleet has been a continued issue throughout its lifetime,however the C-5M upgrade program seeks in part to address this issue.Their strategic airlift capacity has been a key logistical component of U.S. military operations in Afghanistan and Iraq; following an incident during Operation Iraqi Freedom where one C-5 was damaged by a projectile, the installation of defensive systems has become a stated priority.

The C-5 AMP and RERP modernization programs plan to raise mission-capable rate to a minimum goal of 75%.Over the next 40 years, the U.S. Air Force estimates the C-5M will save over $20 billion.The first C-5M conversion was completed on 16 May 2006; C-5Ms began test flights at Dobbins Air Reserve Base in June 2006.The USAF decided to convert remaining C-5Bs and C-5Cs into C-5Ms with avionics upgrades and re-engining in February 2008.The C-5As will receive only the avionics upgrades.

In response to Air Force motions towards the retirement of the C-5 Galaxy, Congress implemented legislation that placed set limits upon retirement plans for C-5A models in 2003.By 2005, 14 C-5As were retired.One was sent to the Warner Robins Air Logistics Center (WR-ALC) for tear down and inspection to evaluate structural integrity and estimate the remaining life for the fleet. 13 C-5As were sent to the Air Force's Aerospace Maintenance and Regeneration Group (AMARG) for inspection of levels of corrosion and fatigue.

The U.S. Air Force began to receive refitted C-5M aircraft in December 2008;full production of C-5Ms began in the summer of 2009.In 2009, the Congressional ban on the retirement of C-5s was overturned.The Air Force seeks to retire one C-5A for each 10 new C-17s ordered.In October 2011, the 445th Airlift Wing based at Wright-Patterson Air Force Base retired or reassigned all of its remaining C-5s; it has since reequipped with C-17s.In early February 2012, it was announced that the remaining 27 C-5As at Kelly Field, Texas; Memphis, Tennessee; and Martinsburg, West Virginia would be retired in fiscal years 2013 and 2014. Kelly is to receive C-5Ms currently assigned to Westover, Massachusetts and the other two wings are scheduled to receive C-17s.

On 13 September 2009, a C-5M set 41 new records; flight data was submitted to the National Aeronautic Association for formal recognition. The C-5M had carried a payload of 176,610 lb (80,110 kg) to over 41,100 ft (12,500 m) in 23 minutes, 59 seconds. Additionally, 33 time to climb records at various payload classes were set, and the world record for greatest payload to 6,562 ft (2,000 m) was broken. The aircraft was in the category of 551,160 to 661,390 lb (250,000 to 300,000 kg) with a takeoff weight of 649,680 lb (294,690 kg) including payload, fuel, and other equipment.

Variants

C-5A

The C-5A is the original version of the C-5. From 1969 to 1973, 81 C-5As were delivered to U.S. Air Force bases. Due to cracks found in the wings in the mid-1970s, the cargo weight was restricted. To restore the C-5's full capability, the wing structure was redesigned. A program to install new strengthened wings on 77 C-5As was conducted from 1981 to 1987. The redesigned wing made use of a new aluminum alloy that did not exist during the original production.

C-5B

The C-5B is an improved version of the C-5A. It incorporated all modifications and improvements made to the C-5A with improved wings, simplified landing gear, upgraded TF-39-GE-1C turbofan engines and updated avionics. From 1986 to 1989, 50 of the new variant were delivered to the U.S. Air Force.

C-5C

The C-5C is a specially modified variant for transporting large cargo. Two C-5s (68-0213 and 68-0216) were modified to have a larger internal cargo capacity to accommodate large payloads, such as satellites for use by NASA. The major modifications were the removal of the rear passenger compartment floor, splitting the rear cargo door in the middle, and installing a new movable aft bulkhead further to the rear.The official C-5 technical manual refers to the version as C-5A(SCM) Space Cargo Modification. Modifications also included adding a second inlet for ground power, which can feed any power-dependent equipment that may form part of the cargo. The two C-5Cs are operated by U.S. Air Force crews on the behalf of NASA, and are stationed at Travis AFB, California. 68-0216 completed the Avionics Modernization Program in January 2007.

C-5 AMP and C-5M Super Galaxy

Following a study showing 80% of the C-5 airframe service life remaining,AMC began an aggressive program to modernize all remaining C-5Bs and C-5Cs and many of the C-5As. The C-5 Avionics Modernization Program (AMP) began in 1998 and includes upgrading avionics to Global Air Traffic Management compliance, improving communications, new flat panel displays, improving navigation and safety equipment, and installing a new autopilot system. The first flight of a C-5 with AMP (85-0004) occurred on 21 December 2002.

The Reliability Enhancement and Re-engining Program (RERP) began in 2006. It includes new General Electric F138-GE-100 (CF6-80C2) engines, pylons and auxiliary power units, upgrades to aircraft skin and frame, landing gear, cockpit and pressurization systems.The CF6 engine produces 22% more thrust (for 50,000 lbf/220 kN) from each engine,[88] providing a 30% shorter takeoff, a 38% higher climb rate to initial altitude, an increased cargo load and a longer range.Upgraded C-5s are designated C-5M Super Galaxy.

L-500

Lockheed also planned a civilian version of the C-5 Galaxy, the L-500, the company designation also used for the C-5 itself. Both passenger and cargo versions of the L-500 were designed. The all-passenger version would have been able to carry up to 1,000 travelers, while the all-cargo version was predicted to be able to carry typical C-5 volume for as little as 2 cents per ton-mile (in 1967 dollars).[91] Although some interest was expressed by carriers, no orders were placed for either L-500 version, due to operational costs caused by low fuel efficiency, a significant concern for a profit-making carrier, even before the oil crisis of the 1970s, keen competition from Boeing's 747, and high costs incurred by Lockheed in developing the C-5 and later, the L-1011 which led to the governmental rescue of the company.

Specifications (C-5B)
*Data from Quest for Performance,International Directory of Military Aircraft,and USAF fact sheet

General characteristics

  • Crew: 8 typical (pilot, first pilot, 1st Officer, two flight engineers, three loadmasters)
  • 4 minimum (pilot, copilot, two flight engineers)
  • Payload: 270,000 lb (122,470 kg)
  • Length: 247 ft 1 in (75.31 m)
  • Wingspan: 222 ft 9 in (67.89 m)
  • Height: 65 ft 1 in (19.84 m)
  • Wing area: 6,200 ft2 (576 m2)
  • Empty weight: 380,000 lb (172,370 kg)
  • Loaded weight: 769,000 lb (348,800 kg)
  • Max. takeoff weight: 840,000 lb (381,000 kg)
  • Powerplant: 4 × General Electric TF39-GE-1C high-bypass turbofan, 43,000 lbf (190 kN) each


Performance

  • Maximum speed: Mach 0.79 (503 kn, 579 mph, 932 km/h)
  • Cruise speed: Mach 0.77 (919 km/h)
  • Range: 2,400 nmi (2,760 mi, 4,440 km) with a 263,200 lb (119,400 kg) payload
  • Service ceiling: 35,700 ft (10,600 m) at 615,000 lb (279,000 kg) gross weight
  • Rate of climb: 1,800 ft/min (9.14 m/s)
  • Wing loading: 120 lb/ft2 (610 kg/m2)
  • Thrust/weight: 0.22
  • Takeoff roll: 8,400 ft (2,600 m)
  • Landing roll: 3,600 ft (1,100 m)
  • Fuel capacity: 51,150 US gal (193,600 L)


Senin, 11 Juni 2012

Antonov An-225 ~ Fourtriangle




The Antonov An-225 Mriya (Ukrainian: Антонов Ан-225 Мрія, Dream, NATO reporting name: 'Cossack') is a strategic airlift cargo aircraft, designed by the Antonov Design Bureau in the 1980s. It is the world's heaviest aircraft. The design, built in order to transport the Buran orbiter, was an enlargement of the successful Antonov An-124. The An-225's name, Mriya (Мрiя) means "Dream" (Inspiration) in Ukrainian.

The first An-225 was completed in 1988 and a second An-225 has been partially completed. The completed An-225 is in commercial operation with Antonov Airlines carrying oversized payloads.

Development

The Antonov An-225 was designed to airlift the Energia rocket's boosters and the Buran space shuttle for the Soviet space program. It was developed as a replacement for the Myasishchev VM-T. The An-225's original mission and objectives are almost identical to that of the United States' Shuttle Carrier Aircraft.

The An-225 first flew on 21 December 1988. The aircraft was on static display at the Paris Air Show in 1989 and it flew during the public days at the Farnborough air show in 1990. Two aircraft were ordered, but only one An-225 (tail number UR-82060) was finished. It can carry ultra-heavy and oversize freight, up to 250,000 kg (550,000 lb) internally,or 200,000 kg (440,000 lb) on the upper fuselage. Cargo on the upper fuselage can be 70 metres (230 ft) long.

A second An-225 was partially built during the late 1980s for the Soviet space program. The second An-225 included a rear cargo door and a redesigned tail with a single vertical stabilizer. It was planned to be more effective for cargo transportation.Following the collapse of the Soviet Union in 1991 and the cancellation of the Buran space program, the lone operational An-225 was placed in storage in 1994.The six Ivchenko Progress engines were removed for use on An-124s, and the second uncompleted An-225 airframe was also stored. The first An-225 was later re-engined and put into serviceBy 2000, the need for additional An-225 capacity had become apparent, so the decision was made in September 2006 to complete the second An-225. The second airframe was scheduled for completion around 2008, then delayed. By August 2009, the aircraft had not been completed and work had been abandoned.In May 2011 Antonov CEO is reported to have said that the completion of a second An-225 Mriya transport aircraft with a carrying capacity of 250 tons requires at least $300 million, but if the financing is provided, its completion could be achieved in three years.According to different sources, the second jet is 60-70% complete.

Design


Based on Antonov's earlier An-124, the An-225 has fuselage barrel extensions added fore and aft of the wings, which received root extensions to increase span. Two more Ivchenko Progress D-18T turbofan engines were added to the new wing roots, bringing the total to six, and an increased-capacity landing gear system with 32 wheels was designed. The An-124’s rear cargo door and ramp were removed to save weight, and the empennage was changed from a single vertical stabilizer to a twin tail with an oversized horizontal stabilizer. The twin tail was essential to enable the plane to carry large, heavy external loads that would disturb the aerodynamics of a conventional tail. Unlike the An-124, the An-225 was not intended for tactical airlifting and is not designed for short-field operation.

Initially the 225 had a maximum gross weight of 600 tonnes (1,320,000 lb) but the aircraft was modified in 2000–01, at a cost of US$20M, with a reinforced floor that increased the maximum gross weight to 640 tonnes (1,410,000 lb).
Both the earlier and later takeoff weights establish the An-225 as the world's heaviest aircraft, being heavier than the double-deck Airbus A380 even though Airbus plans to pass the An-225's maximum landing weight with 591.7 tonnes (1,304,000 lb) for the A380. The Hughes H-4 Hercules, known as the "Spruce Goose", had a greater wingspan and a greater overall height, but was 20% shorter, and due to the materials used in its construction, also lighter. In addition, the Hercules only flew once, making the An-225 the largest aircraft in the world to fly multiple times. The An-225 is larger than the Airbus A380 airliner, and also bigger than the Antonov An-124, Boeing 747 Large Cargo Freighter, and Lockheed C-5 Galaxy, the nearest equivalent heavy cargo aircraft.

Operational history

In the late 1970s, efforts were begun by the Soviet government to generate revenue from its military assets. In 1989, a holding company was set up by the Antonov Design Bureau as a heavy airlift shipping corporation under the name "Antonov Airlines", based in Kiev, Ukraine and operating from London Luton Airport in partnership with Air Foyle HeavyLift.



As the Soviet space program was in its last years, the An-225 was employed as the prime method of transporting the Buran Shuttle.

The company initiated operations with a fleet of four An-124-100s and three Antonov An-12s, but by the late 1990s a need for aircraft larger than the An-124 became apparent. In response, the original An-225 was re-engined, modified for heavy cargo transport, and placed back in service under the management of Antonov Airlines.

On 23 May 2001, the An-225 received its type certificate from the Interstate Aviation Committee Aviation Register (IAC AR). In September 2001, carrying 4 main battle tanks at a record load of 253.82 tonnes (279.79 short tons) of cargo, the An-225 flew at an altitude of 2 km (6,600 ft) over a closed circuit of 1,000 km (620 mi) at a speed of 763.2 km/h (474.2 mph).

The type's first flight in commercial service departed from Stuttgart, Germany on 3 January 2002, and flew to Thumrait, Oman with 216,000 prepared meals for American military personnel based in the region. This vast number of ready meals was transported on some 375 pallets and weighed 187.5 tons.

The An-225 has since become the workhorse of the Antonov Airlines fleet, transporting objects once thought impossible to move by air, such as locomotives and 150-ton generators. It has become an asset to international relief organizations for its ability to quickly transport huge quantities of emergency supplies during disaster relief operations.

The An-225 has been contracted by the Canadian and U.S. governments to transport military supplies to the Middle East in support of Coalition forces.In November 2004, FAI placed the An-225 in the Guinness Book of Records for its 240 records. An example of the cost of shipping cargo by An-225 was €266,000 for flying a chimney duct from Denmark to Kazakhstan in 2008.

On 11 August 2009, the heaviest single cargo item ever sent via air freight was loaded onto the Antonov 225. At 16.23 metres (53.2 ft) long and 4.27 metres (14.0 ft) wide, the consignment–a generator for a gas power plant in Armenia and its loading frame–weighed in at a record 189 tonnes (420,000 lb).[Also during 2009, the An-225 was painted in a new blue and yellow paint scheme,after Antonov ceased cooperation with AirFoyle and partnered with Volga-Dnepr in 2006.

On 11 June 2010, the An-225 carried the world's longest piece of air cargo, when it flew two new 42-meter test wind turbine blades from Tianjin, China to Denmark.

Specification

SPECIFICATIONS
Official Name:
An-225, Mriya
Wingspan:
290 ft.
Length:
275 ft. 7 in.
Height:
59 ft. 8-1/2 in.
Cargo Hold:
Length: 141 ft.;
Width: 21 ft.;
Height: 14 ft. 5-1/4 in.
Engines:
Six ZMKB Progress Lotarev D-18T turbofans each producing 51,590 lb. of thrust
Crew:
7
Max Takeoff Weight:
1,322,750 lb.
Max Payload:
551,150 lb.
Cruising Speed:
497 mph
Max Speed:
528 mph
Range With Max Payload:
2813 miles
Range With Max Fuel:
9625 miles


Kamis, 07 Juni 2012

Boeing 747 ~ Fourtriangle



The Boeing 747 is a wide-body commercial airliner and cargo transport aircraft, often referred to by its original nickname, Jumbo Jet, or Queen of the Skies. It is among the world's most recognizable aircraft, and was the first wide-body ever produced. Manufactured by Boeing's Commercial Airplane unit in the United States, the original version of the 747 was two and a half times the size of the Boeing 707,one of the common large commercial aircraft of the 1960s. First flown commercially in 1970, the 747 held the passenger capacity record for 37 years.

The four-engine 747 uses a double deck configuration for part of its length. It is available in passenger, freighter and other versions. Boeing designed the 747's hump-like upper deck to serve as a first class lounge or (as is the general rule today) extra seating, and to allow the aircraft to be easily converted to a cargo carrier by removing seats and installing a front cargo door. Boeing did so because the company expected supersonic airliners (whose development was announced in the early 1960s) to render the 747 and other subsonic airliners obsolete, while believing that the demand for subsonic cargo aircraft would be robust into the future.The 747 in particular was expected to become obsolete after 400 were sold ,but it exceeded its critics' expectations with production passing the 1,000 mark in 1993.By December 2011, 1,427 aircraft had been built, with 97 of the 747-8 variants remaining on order.

The 747-400, the most common passenger version in service, is among the fastest airliners in service with a high-subsonic cruise speed of Mach 0.85–0.855 (up to 570 mph, 920 km/h). It has an intercontinental range of 7,260 nautical miles (8,350 mi or 13,450 km).The 747-400 passenger version can accommodate 416 passengers in a typical three-class layout, 524 passengers in a typical two-class layout, or 660 passengers in a high density one-class configuration.The newest version of the aircraft, the 747-8, is in production and received certification in 2011. Deliveries of the 747-8F freighter version to launch customer Cargolux began in October 2011; deliveries of the 747-8I passenger version to Lufthansa began in May 2012. The 747 is to be replaced by the Boeing Y3 (part of the Boeing Yellowstone Project) in the future.

Development

Background

In 1963, the United States Air Force started a series of study projects on a very large strategic transport aircraft. Although the C-141 Starlifter was being introduced, they felt that a much larger and more capable aircraft was needed, especially the capability to carry outsized cargo that would not fit in any existing aircraft. These studies led to initial requirements for the CX-Heavy Logistics System (CX-HLS) in March 1964 for an aircraft with a load capacity of 180,000 pounds (81,600 kg) and a speed of Mach 0.75 (500 mph/805 km/h), and an unrefueled range of 5,000 nautical miles (9,260 km) with a payload of 115,000 pounds (52,200 kg). The payload bay had to be 17 feet (5.18 m) wide by 13.5 feet (4.11 m) high and 100 feet (30.5 m) long with access through doors at the front and rear.

Featuring only four engines, the design also required new engine designs with greatly increased power and better fuel economy. On May 18, 1964, airframe proposals arrived from Boeing, Douglas, General Dynamics, Lockheed and Martin Marietta; while engine proposals were submitted by General Electric, Curtiss-Wright, and Pratt & Whitney. After a downselect, Boeing, Douglas and Lockheed were given additional study contracts for the airframe, along with General Electric and Pratt & Whitney for the engines.

All three of the airframe proposals shared a number of features. As the CX-HLS needed to be able to be loaded from the front, a door had to be included where the cockpit usually was. All of the companies solved this problem by moving the cockpit to above the cargo area; Douglas had a small "pod" just forward and above the wing, Lockheed used a long "spine" running the length of the aircraft with the wing spar passing through it, while Boeing blended the two, with a longer pod that ran from just behind the nose to just behind the wing.In 1965 Lockheed's aircraft design and General Electric's engine design were selected for the new C-5 Galaxy transport, which was the largest military aircraft in the world at the time.The nose door and raised cockpit concepts would be carried over to the design of the 747.

Airliner proposal

The 747 was conceived while air travel was increasing in the 1960s.The era of commercial jet transportation, led by the enormous popularity of the Boeing 707 and Douglas DC-8, had revolutionized long-distance travel.Even before it lost the CX-HLS contract, Boeing was pressed by Juan Trippe, president of Pan American World Airways (Pan Am), one of its most important airline customers, to build a passenger aircraft more than twice the size of the 707. During this time, airport congestion, worsened by increasing numbers of passengers carried on relatively small aircraft, became a problem that Trippe thought could be addressed by a large new aircraft.

In 1965, Joe Sutter was transferred from Boeing's 737 development team to manage the design studies for a new airliner, already assigned the model number 747.Sutter initiated a design study with Pan Am and other airlines, in order to better understand their requirements. At the time, it was widely thought that the 747 would eventually be superseded by supersonic transport aircraft.Boeing responded by designing the 747 so that it could be adapted easily to carry freight and remain in production even if sales of the passenger version declined. In the freighter role, the clear need was to support the containerized shipping methodologies that were being widely introduced at about the same time. Standard containers are 8 ft (2.4 m) square at the front (slightly higher due to attachment points) and available in 20 and 40 ft (6.1 and 12 m) lengths. This meant that it would be possible to support a 2-wide 2-high stack of containers two or three ranks deep with a fuselage size similar to the earlier CX-HLS project.

In April 1966, Pan Am ordered 25 747-100 aircraft for US$525 million. During the ceremonial 747 contract-signing banquet in Seattle on Boeing's 50th Anniversary, Juan Trippe predicted that the 747 would be "... a great weapon for peace, competing with intercontinental missiles for mankind's destiny", according to Malcolm T. Stamper, who led the 747 program.As launch customer,and because of its early involvement before placing a formal order, Pan Am was able to influence the design and development of the 747 to an extent unmatched by a single airline before or since.

Design effort

Ultimately, the high-winged CX-HLS Boeing design was not used for the 747, although technologies developed for their bid had an influence.The original design included a full-length double-deck fuselage with rows of eight-across seating and two aisles on the lower deck and seven-across seating and two aisles on the upper deck.However, concern over evacuation routes and limited cargo-carrying capability caused this idea to be scrapped in early 1966 in favor of a wider single deck design.The cockpit was, therefore, placed on a shortened upper deck so that a freight-loading door could be included in the nose cone; this design feature produced the 747's distinctive "bulge".In early models it was not clear what to do with the small space in the pod behind the cockpit, and this was initially specified as a "lounge" area with no permanent seating.

One of the principal technologies that enabled an aircraft as large as the 747 to be conceived was the high-bypass turbofan engine.The engine technology was thought to be capable of delivering double the power of the earlier turbojets while consuming a third less fuel. General Electric had pioneered the concept but was committed to developing the engine for the C-5 Galaxy and did not enter the commercial market until later.Pratt & Whitney was also working on the same principle and, by late 1966, Boeing, Pan Am and Pratt & Whitney agreed to develop a new engine, designated the JT9D to power the 747.

The project was designed with a new methodology called fault tree analysis, which allowed the effects of a failure of a single part to be studied to determine its impact on other systems.To address concerns about safety and flyability, the 747's design included structural redundancy, redundant hydraulic systems, quadruple main landing gear and dual control surfaces.Additionally, some of the most advanced high-lift devices used in the industry were included in the new design, in order to allow it to operate from existing airports. These included leading edge flaps running almost the entire length of the wing, as well as complex three-part slotted flaps along the rear.The wing's complex three-part flaps increase wing area by 21 percent and lift by 90 percent when fully deployed compared to their non-deployed configuration.

Boeing agreed to deliver the first 747 to Pan Am by the end of 1969. The delivery date left 28 months to design the aircraft, which was two-thirds of the normal time.The schedule was so fast paced that the people who worked on it were given the nickname "The Incredibles".Developing the aircraft was such a technical and financial challenge that management was said to have "bet the company" when it started the project.

Production plant

As Boeing did not have a plant large enough to assemble the giant airliner, they chose to build a new plant. The company considered locations in about 50 cities,and eventually decided to build the new plant some 30 miles (48 km) north of Seattle on a site adjoining a military base at Paine Field near Everett, Washington.It bought the 780-acre (3.2 km2) site in June 1966.

Developing the 747 had been a major challenge, and building its assembly plant was also a huge undertaking. Boeing president William M. Allen asked Malcolm T. Stamper, then head of the company's turbine division, to oversee construction of the Everett factory and to start production of the 747.To level the site, more than 4 million cubic yards (3.1 million m³) of earth had to be moved.Time was so short that the 747's full-scale mock-up was built before the factory roof above it was finished.The plant is the largest building by volume ever built, and has been substantially expanded several times to permit construction of other models of Boeing wide-body commercial jets.

Development and testing

Before the first 747 was fully assembled, testing began on many components and systems. One important test involved the evacuation of 560 volunteers from a cabin mock-up via the aircraft's emergency chutes. The first full-scale evacuation took two and a half minutes instead of the maximum of 90 seconds mandated by the Federal Aviation Administration (FAA), and several volunteers were injured. Subsequent test evacuations achieved the 90-second goal but caused more injuries. Most problematic was evacuation from the aircraft's upper deck; instead of using a conventional slide, volunteer passengers escaped by using a harness attached to a reel.Tests also involved taxiing such a large aircraft. Boeing built an unusual training device known as "Waddell's Wagon" (named for a 747 test pilot, Jack Waddell) that consisted of a mock-up cockpit mounted on the roof of a truck. While the first 747s were still being built, the device allowed pilots to practice taxi maneuvers from a high upper-deck position.

On September 30, 1968, the first 747 was rolled out of the Everett assembly building before the world's press and representatives of the 26 airlines that had ordered the airliner.Over the following months, preparations were made for the first flight, which took place on February 9, 1969, with test pilots Jack Waddell and Brien Wygle at the controls and Jess Wallick at the flight engineer's station. Despite a minor problem with one of the flaps, the flight confirmed that the 747 handled extremely well. The 747 was found to be largely immune to "Dutch roll", a phenomenon that had been a major hazard to the early swept-wing jets.

During later stages of the flight test program, flutter testing showed that the wings suffered oscillation under certain conditions. This difficulty was partly solved by reducing the stiffness of some wing components. However, a particularly severe high-speed flutter problem was solved only by inserting depleted uranium counterweights as ballast in the outboard engine nacelles of the early 747s.This measure caused anxiety when these aircraft crashed, as did China Airlines Flight 358 at Wanli in 1991 and El Al Flight 1862 at Amsterdam in 1992.

The flight test program was hampered by problems with the 747's JT9D engines. Difficulties included engine stalls caused by rapid movements of the throttles and distortion of the turbine casings after a short period of service.The problems delayed 747 deliveries for several months and stranded up to 20 aircraft at the Everett plant while they awaited engine installation.The program was further delayed when one of the five test aircraft suffered serious damage during a landing attempt at Renton Municipal Airport, site of the company's Renton factory. On December 13, 1969 the test aircraft was being taken to have its test equipment removed and a cabin installed when pilot Ralph C. Cokely undershot the airport's short runway. The 747's right, outer landing gear was torn off and two engine nacelles were damaged.However, these difficulties did not prevent Boeing from taking one of the test aircraft to the 28th Paris Air Show in mid-1969, where it was displayed to the general public for the first time.The 747 achieved its FAA airworthiness certificate in December 1969, making it ready for introduction into service.

The huge cost of developing the 747 and building the Everett factory meant that Boeing had to borrow heavily from a banking syndicate. During the final months before delivery of the first aircraft, the company had to repeatedly request additional funding to complete the project. Had this been refused, Boeing's survival would have been threatened.Ultimately, the gamble succeeded, and Boeing held a monopoly in very large passenger aircraft production for many years.

Entry into service

On January 15, 1970, First Lady of the United States Pat Nixon christened Pan Am's first 747, Clipper Victor, at Dulles International Airport (later renamed Washington Dulles International Airport) in the presence of Pan Am chairman Najeeb Halaby. Instead of champagne, red, white and blue water was sprayed on the aircraft. The 747 entered service on January 22, 1970, on Pan Am's New York–London route;the flight had been planned for the evening of January 21, but engine overheating made the original aircraft unusable. Finding a substitute delayed the flight by more than six hours to the following day.

The 747 enjoyed a fairly smooth introduction into service, overcoming concerns that some airports would not be able to accommodate an aircraft that largeAlthough technical problems occurred, they were relatively minor and quickly solved.After the aircraft's introduction with Pan Am, other airlines that had bought the 747 in order to stay competitive began to put their own 747s into service.Boeing estimated that half of the early 747 sales were to airlines desiring the aircraft's long range rather than its payload capacity.While the 747 had the lowest potential operating cost per seat, this could only be achieved when the aircraft was fully loaded; costs per seat increased rapidly as occupancy declined. A moderately loaded 747, one with only 70 percent of its seats occupied, used more than 95 percent of the fuel needed by a fully occupied 747.

When economic problems in the United States and other countries after the 1973 oil crisis led to reduced passenger traffic, several airlines found they did not have enough passengers to fly the 747 economically, and they replaced them with the smaller and recently introduced McDonnell Douglas DC-10 and Lockheed L-1011 TriStar trijet wide bodies(and later the 767 and A300 twinjets). Having tried replacing coach seats on its 747s with piano bars in an attempt to attract more customers, American Airlines eventually relegated its 747s to cargo service and in 1983 exchanged them with Pan Am for smaller aircraft;Delta Air Lines also removed its 747s from service after several years.Delta would later merge with Northwest Airlines, which operates 747s.

International flights that bypassed traditional hub airports and landed at smaller cities became more common throughout the 1980s, and this eroded the 747's original market.However, many international carriers continued to use the 747 on Pacific routes.In Japan, 747s on domestic routes are configured to carry close to the maximum passenger capacity.

Improved 747 versions

After the initial 747-100 model, Boeing developed the −100B, a higher maximum takeoff weight (MTOW) variant, and the −100SR (Short Range), with higher passenger capacity.Increased maximum takeoff weight allows aircraft to carry more fuel and have longer range.The −200 model followed in 1971, featuring more powerful engines and a higher MTOW. Passenger, freighter and combination passenger-freighter versions of the −200 were produced.The shortened 747SP (special performance) with a longer range was also developed, and entered service in 1976.

The 747 line was further developed with the launch of the 747-300 in 1980. The −300 resulted from Boeing studies to increase the seating capacity of the 747, during which solutions such as fuselage plugs and extending the upper deck over the entire length of the fuselage were rejected. The first 747-300, completed in 1983, included a stretched upper deck, increased cruise speed, and increased seating capacity. The original designation of the −300 was 747SUD for "stretched upper deck", then 747-200 SUD,followed by 747EUD, before the 747-300 designation was used.Passenger, short range and combination freighter-passenger versions of the −300 were produced.

In 1985, development of the longer range 747-400 began.The variant had a new glass cockpit, which allowed for a cockpit crew of two instead of three,new engines, lighter construction materials, and a redesigned interior. Development cost soared, and production delays occurred as new technologies were incorporated at the request of airlines. Insufficient workforce experience and reliance on overtime contributed to early production problems on the 747-400.The −400 entered service in 1989.

In 1991, a record-breaking 1,087 passengers were airlifted aboard a 747 to Israel as part of Operation Solomon.The 747 remained the heaviest commercial aircraft in regular service until the debut of the Antonov An-124 Ruslan in 1982; variants of the 747-400 would surpass the An-124's weight in 2000. The Antonov An-225 cargo transport, which debuted in 1988, remains the world's largest aircraft by several measures (including the most accepted measures of maximum takeoff weight and length); one aircraft has been completed and is in service as of 2010. The Hughes H-4 Hercules is the largest aircraft by wingspan, but it only completed a single flight.

Further developments

Since the arrival of the 747-400, several stretching schemes for the 747 have been proposed. Boeing announced the larger 747-500X and -600X preliminary designs in 1996.The new variants would have cost more than US$5 billion to develop,and interest was not sufficient to launch the program.In 2000, Boeing offered the more modest 747X and 747X stretch derivatives as alternatives to the Airbus A3XX. However, the 747X family was unable to attract enough interest to enter production. A year later, Boeing switched from the 747X studies to pursue the Sonic Cruiser,and after the Sonic Cruiser program was put on hold, the 787 Dreamliner.Some of the ideas developed for the 747X were used on the 747-400ER, a longer range variant of the 747-400.

After several variants were proposed but later abandoned, some industry observers became skeptical of new aircraft proposals from Boeing.However, in early 2004, Boeing announced tentative plans for the 747 Advanced that were eventually adopted. Similar in nature to the 747-X, the stretched 747 Advanced used technology from the 787 to modernize the design and its systems. The 747 remained the largest passenger airliner in service until the Airbus A380 began airline service in 2007.

On November 14, 2005, Boeing announced it was launching the 747 Advanced as the Boeing 747-8.The last 747-400s were completed in 2009.As of 2011, most orders of the 747-8 have been for the freighter variant. On February 8, 2010, the 747-8 Freighter made its maiden flight.The first scheduled delivery of the 747-8 went to Cargolux in 2011.Eventually, the 747 may be replaced in Boeing's lineup by a new design named "Y3".

Design


The Boeing 747 is a large, wide-body (two-aisle) airliner with four wing-mounted engines. The wings have a high sweep angle of 37.5 degrees for a fast, efficient cruise of Mach 0.84 to 0.88, depending on the variant. The sweep also allows the 747 to use existing hangars.Seating capacity is more than 366 with a 3–4–3 seat arrangement (a cross section of 3 seats, an aisle, 4 seats, another aisle, and 3 seats) in economy class and a 2–3–2 arrangement in first class on the main deck. The upper deck has a 3–3 seat arrangement in economy class and a 2–2 arrangement in first class.

Raised above the main deck, the cockpit creates a hump. The raised cockpit allows front loading of cargo on freight variants.The upper deck behind the cockpit provides space for a lounge or extra seating. The "stretched upper deck" became available as an option on the 747-100B variant and later as standard on the 747-300. The 747-400 cockpit roof section also has an escape hatch from which crew can exit in the event of an emergency if they cannot exit through the cabin.

The 747's maximum takeoff weight ranges from 735,000 pounds (333,400 kg) for the −100 to 970,000 lb (439,985 kg) for the −8. Its range has increased from 5,300 nautical miles (6,100 mi, 9,800 km) on the −100 to 8,000 nmi (9,200 mi, 14,815 km) on the −8I.

The 747 has multiple structural redundancy including four redundant hydraulic systems and four main landing gears with four wheels each, which provide a good spread of support on the ground and safety in case of tire blow-outs. The redundant main gear allows for landing on two opposing landing gears if the others do not function properly.In addition, the 747 has split control surfaces and was designed with sophisticated triple-slotted flaps that minimize landing speeds and allow the 747 to use standard-length runways.For transportation of spare engines, 747s can accommodate a non-functioning fifth-pod engine under the port wing of the aircraft between the inner functioning engine and the fuselage.

Variants

The 747-100 was the original variant launched in 1966. The 747-200 soon followed, with its launch in 1968. The 747-300 was launched in 1980 and was followed by the 747-400 in 1985. Ultimately, the 747-8 was announced in 2005. Several versions of each variant have been produced, and many of the early variants were in production simultaneously. The International Civil Aviation Organization (ICAO) classifies variants using a shortened code formed by combining the model number and the variant designator (e.g. "B741" for all −100 models).

747-100


Pan Am was the first airline to operate the 747. The 747-100 pictured shows the original size of the upper deck and window layout.

The first 747-100s were built with six upper deck windows (three per side) to accommodate upstairs lounge areas. Later, as airlines began to use the upper deck for premium passenger seating instead of lounge space, Boeing offered a ten-window upper deck as an option. Some −100s were retrofitted with the new configuration.The −100 was equipped with Pratt & Whitney JT9D-3A engines. No freighter version of this model was developed by Boeing. However, 747-100s have been converted to freighters. A total of 167 747-100s were built.

747SR


Responding to requests from Japanese airlines for a high-capacity aircraft to serve domestic routes between major cities, Boeing developed the 747SR as a short range variant of the 747-100 with lower fuel capacity and greater payload capability. With increased economy class seating, up to 498 passengers could be carried in early versions and more than 550 in later models.The 747SR had an economic design life objective of 52,000 flights during 20 years of airline operation, compared to 24,600 flights in 20 years for the standard 747.The initial 747SR model, the −100SR, had a strengthened body structure and undercarriage to accommodate the added stress accumulated from a greater number of takeoffs and landings.Extra structural support was built into the wings, fuselage, and the landing gear along with a 20 percent reduction in fuel capacity.

The initial order for the −100SR, four aircraft for Japan Air Lines (JAL, later Japan Airlines), was announced on October 30, 1972; rollout occurred on August 3, 1973, and the first flight took place on August 31, 1973. The type was certified by the FAA on September 26, 1973, with the first delivery on the same day. The −100SR entered service with JAL, the type's sole customer, on October 7, 1973, and typically operated Japanese domestic flights.Seven −100SRs were built from 1973 and 1975, each with a 520,000-pound (240,000 kg) MTOW and Pratt & Whitney JT9D-7A engines derated to 43,000 pounds-force (190,000 N) of thrust.

Following the −100SR, Boeing produced the −100BSR, a 747SR variant with increased takeoff weight capability. Debuting in 1978, the −100BSR also incorporated structural modifications for a high cycle-to-flying hour ratio; a related standard −100B model debuted in 1979. The −100BSR first flew on November 3, 1978, with first delivery to All Nippon Airways (ANA) on December 21, 1978. A total of 20 −100BSRs were produced for ANA and JAL.The −100BSR had a 600,000 lb MTOW and was powered by the same JT9D-7A engines used on the −100SR. ANA operated the type on domestic Japanese routes with 455 or 456 seats until retiring its last aircraft on March 10, 2006.

In 1986, two −100BSR SUD models, featuring the stretched upper deck (SUD) of the −300, were produced for JAL.The type's maiden flight occurred on February 26, 1986, with FAA certification and first delivery on March 24, 1986.JAL operated the −100BSR SUD with 563 seats on domestic routes until their retirement in the third quarter of 2006. While only two −100BSR SUDs were produced, in theory, standard −100Bs can be modified to the SUD certification.Overall, 29 747SRs were built,including seven −100SR, 20 −100BSR, and two −100BSR SUD models.

747-100B


The 747-100B model was developed from the −100SR, utilizing its stronger airframe and undercarriage design. The type had an increased fuel capacity of 48,070 US gallons, allowing for a 5,000-nautical-mile (9,300 km; 5,800 mi) range with a typical 452-passenger payload, and an increased MTOW of 750,000 lb (340,000 kg) was offered. The first −100B order, one aircraft for Iran Air, was announced on June 1, 1978. This aircraft first flew on June 20, 1979, received FAA certification on August 1, 1979, and was delivered the next day.Nine −100Bs were built, one for Iran Air and eight for Saudia (now Saudi Arabian Airlines).Unlike the original −100, the −100B was offered with Pratt & Whitney JT9D-7A, General Electric CF6-50, or Rolls-Royce RB211-524 engines. However, only RB211-524 (Saudia) and JT9D-7A (Iran Air) engines were ordered.

747SP


The development of the 747SP stemmed from a joint request between Pan American World Airways and Iran Air, who were looking for a high-capacity airliner with enough range to cover Pan Am's New York–Middle Eastern routes and Iran Air's planned Tehran–New York route. The Tehran–New York route, when launched, was the longest non-stop commercial flight in the world. The 747SP is 48 feet 4 inches (14.73 m) shorter than the 747-100. Fuselage sections were eliminated fore and aft of the wing, and the center section of the fuselage was redesigned. The SP's flaps used a simplified single-slotted configuration.The 747SP, compared to earlier variants, had a tapering of the aft upper fuselage into the empennage, a double-hinged rudder, and longer vertical and horizontal stabilizers.Power was provided by Pratt & Whitney JT9D-7(A/F/J/FW) or Rolls-Royce RB211-524 engines.

The 747SP was granted a supplemental certificate on February 4, 1976 and entered service with launch customer Pan Am and Iran Air that same year.The aircraft was chosen by airlines wishing to serve major airports with short runways.A total of 45 747SPs were built,with the 44th 747SP delivered on August 30, 1982. In 1987, Boeing re-opened the 747SP production line after five years to build one last 747SP for an order by the United Arab Emirates government.In addition to airline use, one 747SP was modified for NASA Dryden Flight Research Center's SOFIA experiment.

747-200


While the −100 powered by Pratt & Whitney JT9D-3A engines offered enough payload and range for US domestic operations, it was marginal for long international route sectors. The demand for longer range aircraft with increased payload quickly led to the improved −200, which featured more powerful engines, increased MTOW, and greater range than the −100. A few early −200s retained the three-window configuration of the −100 on the upper deck, but most were built with a ten-window configuration on each side.The −200 was produced in passenger (−200B), freighter (−200F), convertible (−200C), and combi (−200M) versions.

The 747-200B was the basic passenger version, with increased fuel capacity and more powerful engines; it entered service in February 1971.In its first three years of production, the −200 was equipped with Pratt & Whitney JT9D-7 engines (initially the only engine available). Range with a full passenger load started at over 5,000 nmi (9,300 km) and increased to 6,000 nmi (11,000 km) with later engines. Most −200Bs had an internally stretched upper deck, allowing for up to 16 passenger seats.The freighter model, the 747-200F, could be fitted with or without a side cargo door,and had a capacity of 105 tons (95.3 tonnes) and an MTOW of up to 833,000 lb (378,000 kg). It entered service in 1972 with Lufthansa.The convertible version, the 747-200C, could be converted between a passenger and a freighter or used in mixed configurations,and featured removable seats and a nose cargo door.The −200C could also be fitted with an optional side cargo door on the main deck.

The combi model, the 747-200M, could carry freight in the rear section of the main deck via a side cargo door. A removable partition on the main deck separated the cargo area at the rear from the passengers at the front. The −200M could carry up to 238 passengers in a three-class configuration with cargo carried on the main deck. The model was also known as the 747-200 Combi.As on the −100, a stretched upper deck (SUD) modification was later offered. A total of 10 converted 747-200s were operated by KLM.Union des Transports Aériens (UTA) also had two of these aircraft converted.

After launching the −200 with Pratt & Whitney JT9D-7 engines, on August 1, 1972 Boeing announced that it had reached an agreement with General Electric to certify the 747 with CF6-50 series engines to increase the aircraft's market potential. Rolls-Royce followed 747 engine production with a launch order from British Airways for four aircraft. The option of RB211-524B engines was announced on June 17, 1975.The −200 was the first 747 to provide a choice of powerplant from the three major engine manufacturers.

A total of 393 of the 747-200 versions had been built when production ended in 1991.Of these, 225 were −200s, 73 were −200F, 13 were −200C, 78 were −200M, and 4 were military.Many 747-200s remain in operation, although most large carriers have retired them from their fleets and sold them to smaller operators. Large carriers have sped up fleet retirement following the September 11 attacks and the subsequent drop in demand for air travel, scrapping some or turning others into freighters.

747-300


The 747-300 features a 23 feet 4 inches (7.11 m) longer upper deck than the −200.The stretched upper deck has two emergency exit doors and is the most visible difference between the −300 and previous models. Before being made standard on the 747-300, the stretched upper deck was previously offered as a retrofit, and first appeared on two Japanese 747-100SR aircraft.The −300 introduced a new straight stairway to the upper deck, instead of a spiral staircase on earlier variants, which creates room above and below for more seats.Minor aerodynamic changes allowed the −300's cruise speed to reach Mach 0.85 compared with Mach 0.84 on the −200 and −100 models, while retaining the same takeoff weight.The −300 could be equipped with the same Pratt & Whitney and Rolls-Royce powerplants as on the −200, as well as updated General Electric CF6-80C2B1 engines.

Swissair placed the first order for the 747-300 on June 11, 1980.The variant revived the 747-300 designation, which had been previously used on a design study that did not reach production. The 747-300 first flew on October 5, 1982, and the type's first delivery went to Swissair on March 23, 1983.Besides the passenger model, two other versions (−300M, −300SR) were produced. The 747-300M features cargo capacity on the rear portion of the main deck, similar to the −200M, but with the stretched upper deck it can carry more passengers.The 747-300SR, a short range, high-capacity domestic model, was produced for Japanese markets; Japan Airlines operated the type with more than 600 seats on the Okinawa–Tokyo route and elsewhere. No production freighter version of the 747-300 was built, but Boeing began modifications of used passenger −300 models into freighters in 2000.

A total of 81 aircraft of the 747-300 series were delivered, 56 for passenger use, 21 −300M and 4 −300SR versions.In 1985, just two years after the −300 entered service, the type was superseded by the announcement of the more advanced 747-400.The last 747-300 was delivered in September 1990 to Sabena.While some −300 customers continued operating the type, several large carriers replaced their 747-300s with 747-400s. Air France, Air India, Pakistan International Airlines and Qantas were some of the last major carriers to operate the 747-300. On December 29, 2008, Qantas flew its last scheduled 747-300 service, operating from Melbourne to Los Angeles via Auckland.

747-400


The 747-400 is an improved model with increased range. It has wingtip extensions of 6 ft (1.8 m) and winglets of 6 ft (1.8 m), which improve the type's fuel efficiency by four percent compared to previous 747 versions.The 747-400 introduced a new glass cockpit designed for a flight crew of two instead of three, with a reduction in the number of dials, gauges and knobs from 971 to 365 through the use of electronics. The type also features tail fuel tanks, revised engines, and a new interior. The longer range has been used by some airlines to bypass traditional fuel stops, such as Anchorage.Powerplants include the Pratt & Whitney PW4062, General Electric CF6-80C2, and Rolls-Royce RB211-524.

The −400 was offered in passenger (−400), freighter (−400F), combi (−400C), domestic (−400D), extended range passenger (−400ER), and extended range freighter (−400ERF) versions. Passenger versions retain the same upper deck as the −300, while the freighter version does not have an extended upper deck.The 747-400D was built for short range operations and does not include winglets, but can be retrofitted with them.Cruising speed is up to Mach 0.855 on different versions of the 747-400.

The passenger version first entered service in February 1989 with launch customer Northwest Airlines on the Minneapolis to Phoenix route.The combi version entered service in September 1989 with KLM, while the freighter version entered service in November 1993 with Cargolux. The 747-400ERF entered service with Air France in October 2002, while the 747-400ER entered service with Qantas, its sole customer, in November 2002. In January 2004, Boeing and Cathay Pacific launched the Boeing 747-400 Special Freighter program,later referred to as the Boeing Converted Freighter (BCF), to modify passenger 747-400s for cargo use. The first 747-400BCF was redelivered in December 2005.

In March 2007, Boeing announced that it had no plans to produce further passenger versions of the −400.However, orders for 36 −400F and −400ERF freighters were already in place at the time of the announcement.The last passenger version of the 747-400 was delivered in April 2005 to China Airlines. Some of the last built 747-400s were delivered with Dreamliner livery along with the modern Signature interior from the Boeing 777. A total of 694 of the 747-400 series aircraft were delivered.At various times, the largest operator of the 747-400 has been Singapore Airlines,Japan Airlines,or British Airways.

747 LCF Dreamlifter


The 747-400 Dreamlifter (originally called the 747 Large Cargo Freighter or LCF) is a Boeing-designed modification of existing 747-400s to a larger configuration to ferry 787 Dreamliner sub-assemblies. Evergreen Aviation Technologies Corporation of Taiwan was contracted to complete modifications of 747-400s into Dreamlifters in Taoyuan. The aircraft flew for the first time on September 9, 2006 in a test flight.Modification of four aircraft was completed by February 2010.The Dreamlifters have been placed into service transporting sub-assemblies for the 787 program to the Boeing plant in Everett, Washington, for final assembly.The aircraft is certified to carry only essential crew and not passengers.

747-8


Boeing announced a new 747 variant, the 747-8, on November 14, 2005. Referred to as the 747 Advanced prior to its launch, the 747-8 uses the same engine and cockpit technology as the 787, hence the use of the "8". The variant is designed to be quieter, more economical, and more environmentally friendly. The 747-8's fuselage is lengthened from 232 to 251 feet (70.8 to 76.4 m),marking the first stretch variant of the aircraft. Power is supplied by General Electric GEnx-2B67 engines.

The 747-8 Freighter, or 747-8F, is derived from the 747-400ERF. The variant has 16 percent more payload capacity than its predecessor, allowing it to carry seven additional standard air cargo containers, with a maximum payload capacity of 154 tons (140 tonnes) of cargo.As on previous 747 freighters, the 747-8F features an overhead nose-door to aid loading and unloading. The 747-8F made its maiden flight on February 8, 2010.The variant received its amended type certificate jointly from the FAA and the European Aviation Safety Agency (EASA) on August 19, 2011.The −8F was first delivered to Cargolux on October 12, 2011.

The passenger version, named 747-8 Intercontinental or 747-8I, is designed to carry up to 467 passengers in a 3-class configuration and fly more than 8,000 nmi (15,000 km) at Mach 0.855. As a derivative of the already common 747-400, the 747-8 has the economic benefit of similar training and interchangeable parts.The type's first test flight occurred on March 20, 2011.At its introduction, the 747-8 surpassed the Airbus A340-600 as the world's longest airliner. The first −8I is was delivered in May 2012 to Lufthansa.The 747-8 has received 106 total orders, including 70 for the −8F and 36 for the −8I, as of December 2011.

Government, military, and other variants

  1. C-19 – The U.S. Air Force gave this designation to the 747-100s used by some U.S. airlines and modified for use in the Civil Reserve Airlift Fleet.
  2. VC-25 – This aircraft is the U.S. Air Force Very Important Person (VIP) version of the 747-200B. The U.S. Air Force operates two of them in VIP configuration as the VC-25A. Tail numbers 28000 and 29000 are popularly known as Air Force One, which is technically the air-traffic call sign for any United States Air Force aircraft carrying the U.S. President. Although based on the 747-200B design, they include several innovations introduced on the 747-400. Partially completed aircraft from Everett, Washington, were flown to Wichita, Kansas, for final outfitting.
  3. E-4B – Formerly known as the National Emergency Airborne Command Post (referred to colloquially as "Kneecap"), this aircraft is now referred to as the National Airborne Operations Center (NAOC).
  4. YAL-1 – This is the experimental Airborne Laser, a component of the National Missile Defense plan.
  5. Shuttle Carrier Aircraft – Two 747s were modified to carry the Space Shuttle. One is a 747-100 (N905NA), and the other is a 747-100SR (N911NA). An SCA carried the Space Shuttle Enterprise in the late 1970s, and has since carried all Space Shuttles.
  6. A number of other governments also use the 747 as a VIP transport, including Bahrain, Brunei, India, Iran, Japan, Kuwait, Oman, Pakistan, Qatar, Saudi Arabia and United Arab Emirates. Several new Boeing 747-8s have been ordered by Boeing Business Jet for conversion to VIP transport for several unidentified customers.
  7. C-33 – This aircraft was a proposed U.S. military version of the 747-400 intended to augment the C-17 fleet. The plan was canceled in favor of additional C-17 military transports.
  8. KC-33A – A proposed 747 was also adapted as an aerial refueling tanker and was bid against the DC-10-30 during the 1970s Advanced Cargo Transport Aircraft (ACTA) program that produced the KC-10A Extender. Before the Khomeini-led revolution, Iran bought four 747-100 aircraft with air-refueling boom conversions to support a fleet of F-4 Phantoms.It is unknown whether these aircraft remain usable as tankers. Since then, other proposals have emerged for adaptation of later 747-400 aircraft for this role.
  9. 747 CMCA – This variant was considered by the U.S. Air Force as a Cruise Missile Carrier Aircraft during the development of the B-1 Lancer strategic bomber. It would have been equipped with 50 to 100 AGM-86 ALCM cruise missiles on rotary launchers. This plan was abandoned in favor of more conventional strategic bombers.
  10. 747 AAC – Boeing also considered developing the 747 into an aerial aircraft carrier for up to 10 "microfighters". With a double-decker hangar and two launching bays, it was believed that the scheme might actually be cheaper than establishing a short-term land base. However nothing came of the scheme, or its complementary 747 AWACS version, which would have carried two of the "microfighters" for reconnaissance.
  11. Evergreen 747 Supertanker – A Boeing 747-200 modified as an aerial application platform for fire fighting using 20,000 US gallons (76,000 L) of firefighting chemicals.
  12. Stratospheric Observatory for Infrared Astronomy (SOFIA) - A former Pan Am Boeing 747SP modified to carry a large infrared-sensitive telescope, in a joint venture of NASA and DLR. High altitudes are needed for infrared astronomy, so as to rise above infrared-absorbing water vapor in the atmosphere.


Undeveloped variants

747 trijet

During the late 1960s and early 1970s, Boeing studied the development of a shorter 747 with three engines, to compete with the smaller L-1011 TriStar and DC-10. The 747 trijet would have had more payload, range, and passenger capacity than the L-1011 and DC-10. The center engine would have been fitted in the tail with an S-duct intake similar to the L-1011's. However, engineering studies showed that a total redesign of the 747 wing would be necessary. Maintaining the same 747 handling characteristics would be important to minimize pilot retraining. Boeing decided instead to pursue a shortened four-engine 747, resulting in the 747SP.In the 1990s, the 777, a long-range twinjet smaller than the 747-400, entered service in the market where the 747 trijet had been targeted.

747-500X, −600X, and −700X

Boeing announced the 747-500X and −600X at the 1996 Farnborough Airshow.The proposed models would have combined the 747's fuselage with a new 251 ft (77 m) span wing derived from the 777. Other changes included adding more powerful engines and increasing the number of tires from two to four on the nose landing gear and from 16 to 20 on the main landing gear.

The 747-500X concept featured an increased fuselage length of 18 ft (5.5 m) to 250 ft (76.2 m) long, and the aircraft was to carry 462 passengers over a range up to 8,700 nautical miles (10,000 mi, 16,100 km), with a gross weight of over 1.0 Mlb (450 Mg).The 747-600X concept featured a greater stretch to 279 ft (85 m) with seating for 548 passengers, a range of up to 7,700 nmi (8,900 mi, 14,300 km), and a gross weight of 1.2 Mlb (540 Mg).A third study concept, the 747-700X, would have combined the wing of the 747-600X with a widened fuselage, allowing it to carry 650 passengers over the same range as a 747-400.The cost of the changes from previous 747 models, in particular the new wing for the 747-500X and −600X, was estimated to be more than US$5 billion.Boeing was not able to attract enough interest to launch the aircraft.

747X and 747X Stretch

As Airbus progressed with its A3XX study, Boeing in 2000 offered the market a 747 derivative as an alternative. This was a more modest proposal than the previous −500X and −600X that would retain the 747's overall wing design and add a segment at the root, increasing the span to 229 ft (69.8 m).Power would have been supplied by either the Engine Alliance GP7172 or the Rolls-Royce Trent 600, which were also proposed for the 767-400ERX.A new flight deck based on the 777's would be used. The 747X aircraft was to carry 430 passengers over ranges of up to 8,700 nmi (10,000 mi, 16,100 km). The 747X Stretch would be extended to 263 ft (80.2 m) long, allowing it to carry 500 passengers over ranges of up to 7,800 nmi (9,000 mi, 14,500 km).Both would feature an interior based on the 777's signature architecture.Freighter versions of the 747X and 747X Stretch were also studied.

Like its predecessor, the 747X family was unable to garner enough interest to justify production, and it was shelved along with the 767-400ERX in March 2001, when Boeing announced the Sonic Cruiser concept.Though the 747X design was less costly than the 747-500X and −600X, it was criticized for not offering a sufficient advance from the existing 747-400. The 747X did not make it beyond the drawing board, but the 747-400X being developed concurrently moved into production to become the 747-400ER.

747-400XQLR

After the end of the 747X program, Boeing continued to study improvements that could be made to the 747. The 747-400XQLR (Quiet Long Range) was meant to have an increased range of 7,980 nmi (9,200 mi, 14,800 km), with improvements to boost efficiency and reduce noise.Improvements studied included raked wingtips similar to those used on the 767-400ER and a sawtooth engine nacelle for noise reduction.Although the 747-400XQLR did not move to production, many of its features were used for the 747 Advanced, which has now been launched as the 747-8.

Accidents and incidents

As of September 2010, the 747 has been involved in 124 accidents or incidents,including 49 hull-loss accidents,resulting in 2,852 fatalities. The 747 has been in 31 hijackings, which caused 25 fatalities.

Few crashes have been attributed to design flaws of the 747. The Tenerife disaster resulted from pilot error, air traffic control (ATC) error, and communications failure, while the Japan Airlines Flight 123 and China Airlines Flight 611 crashes stemmed from improper aircraft repair. United Airlines Flight 811, which suffered an explosive decompression mid-flight on February 24, 1989, led the National Transportation Safety Board (NTSB) to issue a recommendation that 747-200 cargo doors similar to those on the Flight 811 aircraft be modified. Korean Air Lines Flight 007 was shot down by the Soviets in 1983 after it had strayed into Soviet territory, causing U.S. President Ronald Reagan to authorize the then-strictly military Global Positioning System (GPS) for civilian use. TWA Flight 800, a 747-100 that exploded in midair on July 17, 1996, led the FAA to propose a rule requiring installation of an inerting system in the center fuel tank of most large aircraft that was adopted in July 2008, after years of research into solutions. It is expected that the new safety system will cost US$100,000 to $450,000 per aircraft and weigh approximately 200 pounds (91 kg).

Aircraft on display


As increasing numbers of "classic" 747-100 and 747-200 series aircraft have been retired, some have found their way into museums or other uses. The City of Everett, the first 747 and prototype, is at the Museum of Flight, Seattle, Washington, USA where it is sometimes leased to Boeing for test purposes.

Other 747s in museums include those at the National Aviation Theme Park Aviodrome, Lelystad, Netherlands; the Qantas Founders Outback Museum, Longreach, Queensland, Australia; Rand Airport, Johannesburg, South Africa; Technikmuseum Speyer, Speyer, Germany; Musée de l'Air et de l'Espace, Paris, France; Tehran Aerospace Exhibition, Tehran, Iran; Jeongseok Aviation Center, Jeju, South Korea,Evergreen Aviation & Space Museum, McMinnville, Oregon, and the National Air and Space Museum, Washington, D.C.

Upon its retirement from service, the 747 number two in the production line was dis-assembled and shipped to Hopyeong, Namyangju, Gyeonggi-do, South Korea where it was re-assembled, repainted in a livery similar to that of Air Force One and converted into a restaurant. Originally flown commercially by Pan Am as N747PA, Clipper Juan T. Trippe, and repaired for service following a tailstrike, it stayed with the airline until its bankruptcy. The restaurant closed by 2009,and the aircraft was demolished in 2010.A former British Airways 747-200B, G-BDXJ,is parked at the Dunsfold Aerodrome in Surrey, England and has been used as a movie set for productions such as the 2006 James Bond film, Casino Royale.The Jumbohostel, using a converted 747-200, opened at Arlanda Airport, Stockholm on January 15, 2009.

Twitter Delicious Facebook Digg Stumbleupon Favorites More