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Learjet 55

From Wikipedia, the free encyclopedia
1979 executive business jet aircraft
Learjet 55
A Learjet 55 on final approach
General information
TypeBusiness jet
National originUnited States
ManufacturerLearjet
StatusIn service
Number built147
History
Manufactured1979–1987
Introduction date1981
First flight19 April 1979
Developed intoLearjet 60

TheLearjet 55 "Longhorn" is an Americanbusiness jet manufactured byLearjet.

Development and design

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The Learjet 50 series was first announced at the 1977Paris Air Show with larger cabins than existing Learjets.[1] The series was to have three variants, the Learjet 54, 55 and 56 but only the Learjet 55 was built.[1] The Learjet 55 was a low-wing cantilever monoplane withNASA-developedwinglets. The aircraft has a T-tail and is powered by twoGarrett TFE731 turbofans mounted each side of the rear fuselage.[1] It has a retractable tricycle landing gear and an enclosed cabin for up to ten passengers and a cockpit for the two crew.[1] Construction of the Learjet 55 began in April 1978 after extensive testing and work on the wing design which came, initially, from the Learjet 25. The Learjet 55 first flew on 19 April 1979. The first production aircraft were produced starting 18 March 1981. In total, 147 Learjet 55 aircraft were delivered.

Variants

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Learjet 54
Proposed 11-seat variant; not built.[2]
Learjet 55
Production variant; 126 built.[2]
Learjet 55B
1986 - Improved version with a glass cockpit, improved take-off performance and increased range, 8 built.[2]
Learjet 55C
1987 - New rear underfuselage design, withDelta Fins to improve lateralDutch roll stability, and reduce takeoff and landing speeds.
Learjet 55C/ER
Extended-range version of the Learjet 55C.
Learjet 55C/LR
Long-range version of the Learjet 55C, fitted with an extra tank, carrying an extra 259 lb (117 kg) of fuel in the tail cone.
Learjet 56
Proposed eight-seat version, not built.[2]
VU-55
Brazilian Air Force designation for a VIP transport variant of the Learjet 55.[3]

Operators

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 Dominican Republic

Accidents and incidents

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Specifications

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Data fromIllustrated Encyclopedia of Aircraft[1]

General characteristics

  • Crew: 2
  • Capacity: 10
  • Length: 55 ft 1 in (16.80 m)
  • Wingspan: 43 ft 10 in (13.35 m)
  • Height: 14 ft 8 in (4.48 m)
  • Wing area: 264.5 sq ft (24.57 m2)
  • Empty weight: 13,000 lb (5,897 kg)
  • Max takeoff weight: 21,500 lb (9,752 kg)
  • Powerplant: 2 ×Garrett TFE731-3A-2B turbofan aero-engine, 3,700 lbf (16 kN) thrust each

Performance

  • Maximum speed: 541 mph (871 km/h, 470 kn) at 30,000 ft (9,145 m)
  • Cruise speed: 462 mph (744 km/h, 402 kn) at 49,000 ft (14,935 m)
  • Range: 2,492 mi (4,010 km, 2,165 nmi) with four passengers and fuel reserves
  • Service ceiling: 51,000 ft (15,544 m)

References

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Notes

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  1. ^abcdeOrbis 1985, p. 1935
  2. ^abcdSimpson 1991, pp. 187-188
  3. ^"Brazilian Military Aircraft Designations".designation-systems.net. Retrieved2025-03-17.
  4. ^"SAP Group - Aircrafts [sic]". Archived fromthe original on 2014-10-22. Retrieved2014-09-29.
  5. ^Deliso, Meredith."Small plane crashes near Roosevelt Mall in Philadelphia in fiery explosion".ABC News. Retrieved2025-02-01.

Bibliography

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  • The Illustrated Encyclopedia of Aircraft (Part Work 1982–1985). Orbis Publishing.
  • Simpson, R.W. (1991).Airlife's General Aviation. England: Airlife Publishing.ISBN 1-85310-194-X.

External links

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Wikimedia Commons has media related toLearjet 55.
Learjet aircraft
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Military designations
Brazilian Air Force aircraft designations
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Designations carried over fromAmerican designation systems are not included unless the designations were modified.
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