The 747-100 with a range of 4,620 nautical miles (8,556 km), was the original variant launched in 1966. The 747-200 soon followed, with its launch in 1968 and the shorter 747SP launched in 1973. The 747-300 was launched in 1980 and was followed by the 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 introduced it on January 22, 1970 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 an upper deck with ten windows on either side as an option. Some early -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, but many 747-100s were converted into freighters as 747-100(SF). The first 747-100(SF) was delivered to Flying Tiger Line in 1974. A total of 168 747-100s were built; 167 were delivered to customers, while Boeing kept the prototype,
City of Everett. In 1972, its unit cost was ( million today).
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 version of the with lower fuel capacity and greater payload capability. With increased economy class seating, up to 498 passengers could be carried in early versions and up to 550 in later models. Extra structural support was built into the wings, fuselage, and the landing gear along with a 20% 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 flights within Japan. Seven -100SRs were built between 1973 and 1975, each with a MTOW and
Pratt & Whitney JT9D-7A engines derated to 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 MTOW and was powered by the same JT9D-7A or
General Electric CF6-45 engines used on the -100SR. ANA operated this variant on domestic Japanese routes with 455 or 456 seats until retiring its last aircraft in March 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.
747-100B , the last in passenger service|alt=Top view of quadjet on apron The 747-100B model was developed from the -100SR, using its stronger airframe and landing gear design. The type had an increased fuel capacity of , allowing for a range with a typical 452-passenger payload, and an increased MTOW of was offered. The first -100B order, one aircraft for
Iran Air, was announced on June 1, 1978. This version 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
Saudi Arabian Airlines. Unlike the original -100, the -100B was offered with Pratt & Whitney JT9D-7A, CF6-50, or
Rolls-Royce RB211-524 engines. However, only RB211-524 (Saudia) and JT9D-7A (Iran Air) engines were ordered. The last 747-100B, EP-IAM was retired by Iran Air in 2014, the last commercial operator of the 747-100 and -100B.
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 shorter than the . Fuselage sections were eliminated fore and aft of the wing, and the center section of the fuselage was redesigned to fit mating fuselage sections. 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 type certificate on February 4, 1976, and entered service with launch customers Pan Am and Iran Air that same year. A total of 45 747SPs were built, Iran Air, the last civil operator of the type, retired its final 747-SP (EP-IAC) in June 2016.
747-200 , had ten windows per side on the upper deck While the 747-100 powered by Pratt & Whitney
JT9D-3A engines offered enough payload and range for medium-haul operations, it was marginal for long-haul 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 747-200 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. The convertible version, the 747-200C, could be converted between a passenger and a freighter or used in mixed configurations, The
combi aircraft model, the 747-200M (originally designated 747-200BC), 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. Of these, 225 were -200B, 73 were -200F, 13 were -200C, 78 were -200M, and 4 were military. Iran Air retired the last passenger in May 2016, 36 years after it was delivered. , five 747-200s remain in service as freighters.
747-300 took the first delivery on March 23, 1983. After being made standard on the 747-300, the SUD was offered as a retrofit, and as an option to earlier variants still in-production. An example for a retrofit were two
UTA -200 Combis being converted in 1986, and an example for the option were two brand-new JAL -100 aircraft (designated -100BSR SUD), the first of which was delivered on March 24, 1986. The 747-300 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. 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. 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 series aircraft 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,
Japan Airlines,
Pakistan International Airlines, and
Qantas were some of the last major carriers to operate the . On December 29, 2008, Qantas flew its last scheduled 747-300 service, operating from Melbourne to Los Angeles via
Auckland. In July 2015, Pakistan International Airlines retired their final 747-300 after 30 years of service.
Mahan Air was the last passenger operator of the 747-300. In 2022, one of their 747-300Ms was leased by
Emtrasur Cargo. The 747-300M was later seized by the
US Department of Justice in 2024.
747-400 s, entered service in February 1989 with
Northwest Airlines The 747-400 is an improved model with increased range. It has wingtip extensions of and
winglets of , 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. A 747-400 loaded with of fuel flying consumes an average of . Powerplants include the
Pratt & Whitney PW4062, General Electric CF6-80C2, and Rolls-Royce RB211-524. As a result of the Boeing 767 development overlapping with the 747-400's development, both aircraft can use the same three powerplants and are even interchangeable between the two aircraft models. The was offered in passenger (-400), freighter (-400F), combi (-400M), domestic (-400D), extended range passenger (-400ER), and extended range freighter (-400ERF) versions. Passenger versions retain the same upper deck as the , while the freighter version does not have an extended upper deck. The 747-400D was designed for short-range operations with maximum seating for 624. So winglets were not included though they can be retrofitted. Cruising speed is up to Mach 0.855 on different versions of the . 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 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. Japan Airlines, , 331 Boeing 747-400s were in service; (originally called the 747 Large Cargo Freighter or LCF) is a Boeing-designed modification of existing 747-400s into a larger
outsize cargo freighter 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.
747-8 made its maiden flight on February 8, 2010, as a freighter|alt=Side view of quadjet over clouds Boeing announced a new 747 variant, the , on November 14, 2005. Referred to as the
747 Advanced prior to its launch, Boeing selected the designation 747-8 to show the connection with the
Boeing 787 Dreamliner, as the aircraft would use technology and the
General Electric GEnx engines from the 787 to modernize the design and its systems. The variant is designed to be quieter, more economical, and more environmentally friendly. The 747-8's fuselage is lengthened from to , marking the first stretch variant of the aircraft. The 747-8 Freighter, or 747-8F, has 16% more payload capacity than its predecessor, allowing it to carry seven more standard air cargo containers, with a maximum payload capacity of of cargo. As on previous 747 freighters, the 747-8F features a flip up nose-door, a side-door on the main deck, and a side-door on the lower deck ("belly") 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 at Mach 0.855. As a derivative of the already common , the 747-8I has the economic benefit of similar training and interchangeable parts. The type's first test flight occurred on March 20, 2011. The 747-8 has surpassed the
Airbus A340-600 as the world's longest airliner, a record it would hold until the
777X, which first flew in 2020. The first -8I was delivered in May 2012 to Lufthansa. The 747-8 received 155 total orders, including 106 for the -8F and 47 for the -8I .
Government, military, and other variants , a
Boeing VC-25, over
Mount Rushmore carrying a
Space Shuttle orbiter •
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. Partially completed aircraft from Everett, Washington, were flown to
Wichita, Kansas, for final outfitting by
Boeing Military Airplane Company. Two new aircraft, based around the , are being procured which will be designated as VC-25B. •
E-4B – This is an airborne command post designed for use in nuclear war. Three E-4As, based on the 747-200B, with a fourth aircraft, with more powerful engines and upgraded systems delivered in 1979 as an E-4B, with the three E-4As upgraded to this standard. Formerly known as the National Emergency Airborne Command Post (referred to colloquially as "Kneecap"), this type is now referred to as the National Airborne Operations Center (NAOC). •
Survivable Airborne Operations Center - In April 2024,
Sierra Nevada Corporation was awarded a contract to develop and build the
Survivable Airborne Operations Center aircraft to replace the
Boeing E-4 NAOC. Five 747-8Is were purchased from
Korean Air for conversion, with the contract calling for nine in total. •
YAL-1 – This was the experimental
Airborne Laser, a planned component of the U.S.
National Missile Defense. •
Shuttle Carrier Aircraft (SCA) – Two 747s were modified to carry the
Space Shuttle orbiter. The first was a 747-100 (N905NA), and the other was a 747-100SR (N911NA). The first SCA carried the prototype
Enterprise during the
Approach and Landing Tests in the late 1970s. The two SCA later carried all five operational Space Shuttle orbiters. •
C-33 – This aircraft was a proposed U.S. military version of the 747-400F intended to augment the
C-17 fleet. The plan was canceled in favor of additional C-17s. •
KC-25/33 – A proposed 747-200F 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-10 Extender. Before the 1979
Iranian Revolution, Iran bought four 747-100 aircraft with air-refueling boom conversions to support its fleet of
F-4 Phantoms. There is a report of the Iranians using a 747 Tanker in
H-3 airstrike during
Iran–Iraq War. It is unknown whether these aircraft remain usable as tankers. Since then there have been proposals to use a 747-400 for that role. •
747F Airlifter – Proposed US
military transport version of the 747-200F intended as an alternative to further purchases of the
C-5 Galaxy. This 747 would have had a special nose jack to lower the sill height for the nose door. System tested in 1980 on a
Flying Tiger Line 747-200F. •
747 CMCA – This "Cruise Missile Carrier Aircraft" variant was considered by the U.S. Air Force 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. •
MC-747 – Two separate studies from the 1970s and 2005, the first by Boeing and the second by
ATK and
BAE Systems, to horizontally store up to four
Peacekeeper ICBMs or seven
Minutemen above bomb bay-like doors in the first study, and to vertically store twelve Minutemen or 32
JDAM-equipped conventional missiles for launch from
in situ tubes in the second. •
747 AAC – A Boeing study under contract from the USAF for an "
airborne aircraft carrier" for up to 10 Boeing Model 985-121 "
microfighters" with the ability to launch, retrieve, re-arm, and refuel. Boeing believed that the scheme would be able to deliver a flexible and fast carrier platform with global reach, particularly where other bases were not available. Modified versions of the 747-200 and Lockheed C-5A were considered as the base aircraft. The concept, which included a complementary 747 AWACS version with two reconnaissance "microfighters", was considered technically feasible in 1973. •
Evergreen 747 Supertanker – A 747-200 modified as an aerial application platform for fire fighting using of firefighting chemicals. •
Stratospheric Observatory for Infrared Astronomy (SOFIA) – A former Pan Am 747SP modified to carry a large infrared-sensitive telescope, in a joint venture of NASA and
DLR. High altitudes are needed for
infrared astronomy, to rise above infrared-absorbing water vapor in the atmosphere. • 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
747-8s have been ordered by
Boeing Business Jet for conversion to VIP transports for several unidentified customers.
Comparison Below is a list of major differences between the original 747 variants.
Proposed variants Boeing studied a number of 747 variants that did not advance beyond the concept stage.
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 Lockheed L-1011 TriStar and McDonnell Douglas DC-10. The center engine would have been fitted in the tail with an
S-duct intake similar to the L-1011's. Overall, the 747 trijet would have had more payload, range, and passenger capacity than either of the two other aircraft. However, engineering studies showed that a major 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.
747-500 In January 1986, Boeing outlined preliminary studies to build a larger, ultra-long haul version named the , which would enter service in the mid- to late-1990s. The aircraft derivative would use engines evolved from unducted fan (UDF) (
propfan) technology by
General Electric, but the engines would have shrouds, sport a
bypass ratio of 15–20, and have a propfan diameter of . The aircraft would be stretched (including the upper deck section) to a capacity of 500 seats, have a new wing to reduce drag, cruise at a faster speed to reduce flight times, and have a range of at least , which would allow airlines to fly nonstop between
London, UK and
Sydney, Australia.
747 ASB Boeing announced the 747 ASB (
Advanced Short Body) in 1986 as a response to the Airbus A340 and the
McDonnell Douglas MD-11. This aircraft design would have combined the advanced technology used on the 747-400 with the foreshortened 747SP fuselage. The aircraft was to carry 295 passengers over a range of . However, airlines were not interested in the project and it was canceled later that year.
747-500X, -600X, and -700X illustration|alt=Aircraft comparison diagram. Boeing announced the 747-500X and -600X at the 1996
Farnborough Airshow. The 747-500X concept featured a fuselage length increased by to , and the aircraft was to carry 462 passengers over a range up to , with a gross weight of over 1.0
Mlb (450 tonnes). 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 . The 747X Stretch would be extended to long, allowing it to carry 500 passengers over ranges of up to . 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.
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 , 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 was launched as the
747-8 in 2005. == Operators ==