Grumman Gulfstream II

E544969

The Grumman Gulfstream II is a twin-engine business jet introduced in the 1960s that became one of the early iconic long-range corporate aircraft.

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Statements (49)

Predicate Object
instanceOf business jet
long‑range corporate aircraft
twin‑engine jet aircraft
aircraftCategory transport category airplane
cabinConfiguration rear airstair door
stand‑up cabin
countryOfOrigin United States of America
surface form: United States
crew 2
cruiseSpeed approximately 460 knots
approximately Mach 0.80
developedFrom Grumman Gulfstream I NERFINISHED
engineModel Rolls‑Royce Spey NERFINISHED
Rolls‑Royce Spey Mk 511‑8 NERFINISHED
engineMounting rear‑fuselage mounted
engineType turbofan
enteredService 1967
faaTypeCertificateDesignation G-1159
firstFlightDate 1966-10-02
fuselageMaterial aluminum alloy
icaoAircraftTypeDesignator G1159
introducedInDecade 1960s
landingGearType tricycle retractable landing gear
manufacturer Grumman NERFINISHED
Grumman Aerospace Corporation NERFINISHED
maximumPassengerCapacity 19
maximumRange approximately 4000 nautical miles
notableFor being one of the early iconic long‑range corporate jets
establishing Gulfstream as a major business jet brand
numberBuilt over 250
numberOfEngines 2
powerplantLocation aft fuselage
pressurizedCabin yes
primaryUse corporate aviation
private business transport
productionEnd late 1970s
productionStart late 1960s
role business transport
corporate jet
special mission aircraft
vip transport
serviceCeiling approximately 45000 ft
successor Gulfstream III NERFINISHED
tailConfiguration T‑tail
typicalPassengerCapacity 14
typicalTakeoffWeight around 65000 lb
usedBy corporate operators
government operators
military operators
wingConfiguration low‑wing

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Grumman notableProduct Grumman Gulfstream II
Rolls-Royce Spey turbofan usedIn Grumman Gulfstream II
subject surface form: Rolls-Royce Spey