TheBeechcraft King Air is a line of Americanutility aircraft produced byBeechcraft. The King Air line comprises a number of twin-turboprop models that have been divided into two families. The Model 90 and 100 series developed in the 1960s are known as King Airs, while the laterT-tail Model 200 and 300 series were originallymarketed asSuper King Airs, with the name "Super" being dropped by Beechcraft in 1996 (although it is still often used to differentiate the 200 and 300 series King Airs from their smaller stablemates).
The Model 90 King Air was conceived as theModel 120 in 1961. In its original planned configuration, the Model 120 was to have been powered by two 917 shp (684 kW)Turbomeca Bastan VI engines.[4] On May 15, 1963, Beechcraft began test flights of the proof-of-conceptModel 87, a modifiedQueen Air withPratt & Whitney Canada PT6A-6 engines. On July 14, Beech announced a new type, and a month later began accepting orders for the "King Air", with deliveries to commence in Autumn 1964.[5] On January 24, 1964, the first definitive prototype, by now designatedModel 65-90 and also fitted with PT6A-6 engines,[6] flew for the first time. After 10 months of test flying, in 1964 the Model 87 was delivered to theUnited States Army as the NU-8F. The first production aircraft was delivered on October 8, and by the end of the month, 152 aircraft had been ordered;[7] by year's end, seven had been built.[8]
In 1966, after 112 65-90s were completed,[8] production switched to theModel 65-A90 with PT6A-20 engines. As a measure of the type's popularity, 206 65-A90s were built in less than two years when production switched to theModel B90, the first of these rolling off the production line in 1968.[8] Military versions built during these years included the65-A90-1,65-A90-2,65-A90-3, and65-A90-4, all being unpressurised models based on the Model 87. These were produced for the US Army which designated them U-21s of various sub-models; many were fitted out for electronic battlefield surveillance. A total of 162 of these were built between 1967 and 1971.[9]
A total of 184 B90 models were produced before theModel C90 was introduced in 1971,[8] with wingspan increased over earlier models by 4 ft 11 in (1.50 m) to 50 ft 3 in (15.32 m), Maximum Take-Off Weight (MTOW) increased by 350 lb (160 kg) to 9,650 lb (4,378 kg), and PT6A-20A engines. The broadly similarModel E90 was introduced the following year, with PT6A-28 engines; the two were produced in parallel. Further refinement of the 90 series resulted in theModel F90 and follow-onModel F90-1. The F-models featured theT-tail of theModel 200 mated to the fuselage and wings of the E90, with PT6A-135 engines of 750 shp (560 kW) driving four-bladed propellers. The F90 prototype flew on January 16, 1978, and 203 production versions followed between 1979 and 1983, when the F90 was superseded by the F90-1.[8] The F90 prototype was re-engined withGarrett AiResearch TPE-331 engines to test the feasibility of aModel G90, but this model was not put into production.
TheModel C90-1 entered production in 1982 after 507 C90s and 347 E90s had been built,[8] and featured PT6A-21 engines and improvements to the pressurization system. 54 were built.[8][10] The following year the F90-1 was put into production with redesigned engine cowlings, upgraded PT6A-135A engines, hydraulic landing gear, and triple-fed electrical bus; only 33 were built by the time production terminated in 1985.[8] The C90-1 was soon followed by theModel C90A, which featured the redesigned engine cowlings of the F90-1. The C90A received an increase in MTOW in 1987, being certified to 10,100 lb (4,580 kg). The C90A model was in production until 1992, by which time 235 had been built, all but 74 with the increased MTOW.
Only two C90As were built in 1992, theModel C90B followed that year with airframe improvements, four-bladed propellers, and propeller synchrophasing,[11] all in an effort to reduce cabin noise. This model also had PT6A-21s; the first production C90B was fitted with the 10,000th PT6 engine delivered to Beechcraft. In 1994 a cheaper version was introduced as theC90SE (Special Edition), with three-bladed propellers, standardised interior and mechanical instruments instead of theElectronic Flight Instrument System (EFIS) fitted to the C90B.[12] A total of 456 C90Bs and C90SEs were delivered by the time production of these models ended in late 2005.[8]
In July 2005, during theOshkosh Airshow, Beechcraft introduced theC90GT. The C90GT was fitted with 750 shp (560 kW) PT6A-135As,flat rated to the same 550 shp (410 kW) as the earlier King Airs. This engine change increased performance due to lower operating temperatures, improving both cruise speed and climb rate. With a 275 kt (509 km/h, 316 mph) cruise speed, the C90GT was highly competitive with the new generation ofVery Light Jets over short to medium distances, while providing a larger and more luxurious cabin. C90GT deliveries commenced at the beginning of 2006.[8] On May 21, 2007, during the 7th Annual European Business Aviation Convention & Exhibition in Geneva, Beechcraft announced theModel C90GTi updated version of the C90GT,[13] featuring theRockwell Collins Proline 21avionics package previously only offered for the B200 and B300 King Airs. Deliveries commenced in 2008 after 97 C90GTs were delivered to customers over the previous two years.[8] In 2015, theC90GTx was introduced with additional upgrades. In 2019, the C90 unit cost wasUS$2.75M, and $4.2M (~$5.07 million in 2024) for the C90GTi.[14]
In March 2021, Beechcraft discontinued the C90GTx, thus ending the Model 90 production run.Textron, Beechcraft's parent company, stated that it intends to support the existing 90 series fleet indefinitely given the large number of aircraft being actively operated.[15]
TheModel 100 is a stretched derivative of the Model 90 featuring five cabin windows instead of the Model 90's three; MTOW increased by 1,300 lb (590 kg) over the 90, to 10,600 lb (4,810 kg). The 100 used the wings, tail, and engines (two PT6A-28 engines, although rated at 680 shp)[16] from theModel 99 airliner, itself a development of the Queen Air (as was the Model 90).
The Model 100 was flown for the first time on March 17, 1969, and unveiled to the public in May. A total of 89 Model 100s were built before it was superseded by theModel A100 in 1972, with a further increase in MTOW to 11,500 lb (5,220 kg), fuel capacity increased by 94 US gallons (360 L), and four-bladed propellers.[17] A total of 157 A100s were built by the time production of this model ceased in 1979. The next in the series was theB100, which featured 715 shp (533 kW) Garrett AiResearch TPE-331 engines as an alternative to the Pratt & Whitneys offered on other King Airs, and another increase in MTOW to 11,800 lb (5,350 kg). The B100 was introduced in 1976 and was produced concurrently with the A100 for several years; manufacture ceased in 1983 after 137 were built. TheModel 200 Super King Air was developed from the Model 100, with the same fuselage design being used for both models (with some differences, mainly associated with the different tails). The Model 200 had different wings and a T-tail and entered service in 1974.
TheJapan Maritime Self-Defense Force (JMSDF) has operated a total of 40 C90 and C90A King Airs, with deliveries beginning in 1973. These have been given various designations by the JMSDF and consist of 34TC-90 trainers, fiveLC-90 transports, and a singleUC-90 which is configured for photographic aerial survey. The TC-90s and the UC-90 are operated by the202nd Naval Air Training Squadron (JMSDF) based atTokushima Air Base, while the LC-90s are attached to various Lockheed P-3Kokutai (Squadrons) andAir Transport Squadron 61[18] as liaison aircraft. In late 2005, the JMSDF marked 500,000 accident-free flying hours of the TC-90 trainer fleet. Philippine maintenance staff will also be trained.[19]
The JMSDF made plans to lease at least five TC-90 aircraft to the Philippines to conduct maritime patrols.[20][21][22][23] Two aircraft were transferred free of charge in March 2017.[24] From November 2016 to November 2017, sixPhilippine Navy pilots were trained to fly the aircraft atTokushima Airport. Maintenance staff are also being trained.[25][26][27] There are plans to transfer three more aircraft.[24]
The U.S. military has used King Air 90s in various roles, primarily VIP and liaison transport, with designations including theVC-6A, theT-44 Pegasus, and theU-21 Ute. The U-21 Ute used by the US Army was the most common version.
Most U-21s were unpressurized Model 87 derivatives, but there were also five U-21Fs based on the A100 King Air; and three U-21Js, which Beechcraft designatedModel A100-1, but were actually the first three production Model 200 Super King Airs (C/Ns BB-3, BB-4 and BB-5, after prototypes C/N BB-1 and BB-2 had been built). The majority of U-21s were delivered as U-21As (102 65-A90-1s), but there were also four RU-21As (65-A90-1s), three RU-21Bs (65-A90-2s), two RU-21Cs (65-A90-3s), 18 RU-21Ds (65-A90-1s), 16 RU-21Es (65-A90-4s), and 17 RU-21Gs (65-A90-1s). The RU-21Es (except one written off) were later converted to U-21Hs and RU-21Hs, with two U-21Hs and an RU-21H being further converted to JU-21Hs.[28] In 1993, the three surviving RU-21As that remained in military service were retired and sent to JW Duff Aircraft Salvage in Denver. On November 14, 2015, one of aircraft, (67-18113) was donated by Dynamic Aviation to the 138th Aviation Company Memorial to restore the aircraft to be displayed atOrlando International Airport.[29] The majority of the U-21 series were retired in the second half of the 1990s and most are now owned byDynamic Aviation ofBridgewater, Virginia. Some have been modified as spraying aircraft and are used on insect control work.[30][31]
The T-44A Pegasus is a trainer version, designated theModel H90 by Beechcraft, used to trainUnited States Navy,Marine Corps,Coast Guard, andAir Force (USAF) pilots to fly multi-engine aircraft. A total of 61 were delivered to the US Navy between 1977 and 1980. In August 2006, the Navy announced that after 29 years of operation, the T-44A fleet would be upgraded with modernized avionics systems, and redesignated T-44Cs.[32]
Two VC-6A aircraft were operated by the US military. One was a Model 65-A90 operated by the US Army and serialled 66-15361,[33] the other a B90, designated as a VC-6A (66-7943), was operated by the USAF and used byPresidentLyndon Johnson.
A B100 King Air modified with five-bladed propellers
A number of aftermarket modifications and upgrades are available for 90 and 100 Series King Airs.[35] An engine upgrade involves earlier-build 90 Series aircraft being re-engined with the PT6A-135A engines of the C90GT.[36][37] A more radical re-engining program involves the replacement of the PT6s in C90 and E90 King Airs with TPE-331s.
A King Air 90 with the full CargoLiner Conversion
Among the numerous airframe modifications available: a cargo conversion for the 90 model, the CargoLiner, which replaces the rear door with a large pallet accessible cargo door, a heavy duty floor structure and cabin cargo liner, also a crew hatch for cockpit access for the crew in the 90, 100, and 200;[38] a Wing Front Spar Reinforcement Kit for both 90 and 100 Series aircraft,[35] a modification for the entire King Air line that entails reworking and extending the nose[39] to house a baggage compartment as well as the avionics normally found in the noses of King Air aircraft. Modifications available for the King Air 100 include a belly cargo pod similar to those fitted to the Beech 99 and the Model 1300 version of the King Air 200 series.[40]
In addition to its use by military and government users, the King Air is also used by many non-governmental organizations, as well as by corporate and private users. This includes commercial use by air-taxi and air charter companies.[41]
TheRoyal Flying Doctor Service of Australia previously operated a large number of 90 Series King Airs, but retired the last example in 2006, standardizing on the King Air 200 Series and thePilatus PC-12 for its fleet requirements.
On January 19, 2017, a Beechcraft C90GT King Air crashed inParaty,Rio de Janeiro, Brazil, killingTeori Zavascki, the Minister of the Supreme Court of Brazil and 4 other people.[44][45]
On June 28, 2018, a Beechcraft King Air C90crashed in a suburb of Mumbai, India, killing all four aboard and one on the ground; three people sustained injuries.
"Proof-of-concept" test aircraft based on the Model A80 with PT6A-6 turboprops; one built.[49]
Model 65-90
Based on the Model 88 with two PT6A-6 turboprops and a 9000lb Take Off Gross Weight (TOGW); 112 built.[49]
Model 65-A90
Model 90 with TOGW increased to 9300lb, two 550shp PT6A-20 engines, redesigned flightdeck and a new engine de-ice system, 206 built.[49]
Model 65-A90-1
Based on the Model 87, unpressurised with square windows and 550shp PT6A-20 engines, 141 built and delivered to the US Army with the designation U-21A.[49]
Model 65-A90-2
Specialised electronic warfare variant of the A90-1 with five seats, three built as U-21Bs (later RU-21B).[49]
Model 65-A90-3
Variant of the A90-2 with improved electronic equipment, two-built for the US Army with the designation RU-21C.[49]
Model 65-A90-4
Project Guardrail variant of the A90-2, strengthened airframes and higher gross weight, 16 built for the US Army.[49]
Model B90
based on the A90 with a 9650 TOGW, improved ailerons and increased wing span, improved instrumentation and pressurization and an extra side window, 184 built.[49]
Model C90
Based on the B90 but using the Model 100 cabin environment and pressurization system, 550shp PT6A-21 engines, 507 built.[49]
Model C90-1
Improved C90 with an E90 tailplane and improved power output, increased maximum cabin pressure differential,[12] 54 built in 1982 and 1983.[8]
Model C90A
Improved C90-1 improved landing gear retraction, improved electrical system and using F90-1 pressurization and heating system, 235 built between 1984 and 1992. Two Pratt & Whitney PT6A-21 reverse-flow, free-turbine turboprop engines; 550 shp each.[50]
C90B and C90SE
Marketing names for updated versions of C90A produced between 1992 and 2005, 456 built[51] B-model has Maximum Take-off Weight of 10 100 lb (4585 kg), quieterHartzell four-blade, constant-speed, full-reversing 90-in diameter propellers and dynamic (passively resonating) vibration absorber (DVA) system. The King Air C90SE is the 'poor man’s' version of the Beech C90B with three-bladed props and “mechanical” instruments.[50]
Model C90GT
Version with PT6A-135A engines, 750 shpflat rated to 550 shp, for better climb and cruise performance, 97 built.[8][52]
Model C90GTi
Variant of C90GT with "glass cockpit" Collins Proline 21 avionics suite; at least 90 built[8][53]
Model C90GTx
Marketing name for version of C90GTi introduced in 2010 withwinglets added as factory-standard, Maximum Take-off Weight increased to 10 485 lb (4756 kg) for better full-fuel payload flexibility.[54]
Modification of L-23 Seminole with PT6A-6 turboprops. One converted.[56]
U-21A Ute
Utility aircraft for US Army, with fuselage of Queen Air 65-80 and wings of King Air 65-90, powered by 550 hp (410 kW) PT6A-20s. Beechcraft Model 65-A90-1. 141 built.[56][57]
EU-21A
Conversion of at least five U-21As as radio relay aircraft for use overVietnam. Later re-converted to U-21A standard.[58]
JU-21A
Conversion of three U-21As withLeft JabSignals intelligence (SIGINT) system. One of the system aircraft, (67-18065) with callsign "Vanguard 216" was shot down by a Surface to Air Missile near the DMZ on March 4, 1971. All 5 crew members were declared KIA Bodies Not Recovered. Two later re-converted to U-21A standard.[58]
RU-21A
Conversion of four U-21As to carryDirection finding equipment as part ofCefirm Leader program, to work with RU-21B and RU-21C aircraft.[59]
RU-21B
Signals intercept aircraft as part ofCefirm Leader program. Powered by 620 hp (462 kW) PT6A-29s and with modified undercarriage. Beechcraft Model 65-A90-2. Three built.[60]
RU-21C
Similar to RU-21B, but carrying jamming equipment as part ofCefirm Leader. Beechcraft model 65-A90-3. Two built.[60]
RU-21D
SIGINT aircraft system known as "Laffing Eagle" "V-Scan", deployed to Vietnam, after the war many were converted to Guardrail RU-21H models, and others having their electronic equipment removed to becomeU-21D utility aircraft. Beechcraft Model 65-A90-1. 18 built.[61]
RU-21E
ELINT version withGuardrail II,IIA orIV systems. Beechcraft Model 65-A90-4.[62] 16 built.[63]
U-21F
Five King Air A100s used by US Army as transport/utility aircraft.[64]
U-21G Ute
U-21A with modified cockpit, mainly used as utility aircraft, 17 conversions.[64]
RU-21G
Three U-21Gs fitted withGuardrail I ELINT system.[64]
RU-21H
Conversion of 21 RU-21D, E and F aircraft to carryGuardrail V ELINT system. Higher gross weight.[65]
U-21H Ute
Modification of 23 RU-21E and G aircraft replaced in the ELINT role by later aircraft to utility aircraft.[65]
JU-21H
Two former RU-21Es converted as test aircraft.[65]
VC-6A
Two B90 King Airs, powered by 550 shp (410 kW) PT6A-20s. One used as transport by US Army, and one by USAF as VIP transport for PresidentLyndon B. Johnson.[66]
T-44A Pegasus
Model H90 as a Multi-engine training aircraft for US Navy, 61 built.[66]
T-44C Pegasus
T-44A upgraded with the Rockwell Collins Pro Line 21 series avionics suite. 25 upgraded.[67]
TheICAO designator, such as might be used in aPIREP or aflight plan, for the various King Airs are BE9T (F90 and F90-1), BE9L (all other model 90s), and BE10 (model 100). With the exception of the F90 and F90-1, all 90 Series King Airs have been produced under the same Type Certificate (Number 3A20) used for Queen Air production.[69] All 100 Series King Airs were produced under the same Type Certificate (Number A14CE) used for Model 99 production.[70]
^Simpson, R.W. (1995).Airlife's General Aviation: A guide to Postwar General Aviation Manufacturers and their aircraft (2nd ed.). Airlife Publishing. p. 76.ISBN1-85310-577-5.
^Green, William. "Beech 65-90 King Air",The Observer's Book of Aircraft, 1965 Edition. Frederick Warne & Co. Ltd., London. No ISBN, Library of Congress Catalog Card No. 57-4425.
^A system fitted to many twin-engined propeller-driven aircraft, it matches propeller revolutions-per-minute and also "phases" the position of the blades of each propeller relative to the other, so the cabin noise is more even.
^Unless otherwise noted, all information here is obtained from Production Lists in the bookBeechcraft - Pursuit of Perfection and the online Production Lists available atLAASdata.comArchived September 13, 2007, at theWayback Machine
^The last King Air C90GTi built as of December 2008 is shown in the available online sources (LAASdata King Air 90 listArchived July 13, 2011, at theWayback Machine and various nations' online civil aircraft Registers) as c/no. LJ-1946, however there are gaps for registered King Airs, with some above c/no. LJ-1900 not listed.
Harding, Stephen (1997).U.S. Army Aircraft Since 1947. Atglen, PA, USA: Schiffer Publishing Ltd.ISBN0-7643-0190-X.
Kaminski, Tom. "Variant File: US Military King Airs: Part 1 Beech/Raytheon U-21 and C-12".International Air Power Review. Volume 11, Winter 2003/2004.ISBN1-880588-60-9. ISSN 1473-9917. pp. 74–93.
Kaminski, Tom. "Variant File: US Military King Airs Part 2: C-12".International Air Power Review. Volume 12, Spring 2004.ISBN1-880588-77-3. ISSN 1473-9917. pp. 90–98.
Jackson, Paul. "Beech King Air B200."Jane's All the World's Aircraft 2003-2004, 2004.ISBN0-7106-2537-5.
Phillips, Edward H.Beechcraft - Pursuit of Perfection, A History of Beechcraft Airplanes. Flying Books, Eagan, Minnesota 1992.ISBN0-911139-11-7.
Simpson, R.W.Airlife's General Aviation. London: Airlife Publishing, 1991.ISBN1-85310-194-X
Taylor, M. J. H. ed.Jane's Encyclopedia of Aviation Studio Editions Ltd.ISBN1-85170-324-1
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