Gulfstream II

Grumman / Gulfstream American · USA · first flew 1966 · transport aircraft

The Gulfstream II was the first jet-powered Gulfstream, evolving the turboprop GI airframe into a transatlantic-capable executive transport powered by Rolls-Royce Spey turbofans.

Recognition (WEFT)

W — WingsLow-mounted, swept
E — Engines2 × turbofan, tail-mounted
F — FuselageEarly classic T-tail twin with large oval portholes along a cylindrical fuselage — the definitive 1960s executive jet look
T — TailT-tail

WEFT is AircraftIQ's four-point recognition method — how it works.

Spot it by:

The GII is larger and longer than the contemporary Learjet family and shows a more cylindrical, porthole-equipped fuselage versus the slender Learjet. Against the GIII it lacks the supercritical wing's noticeable leading-edge sweep change and has blunter engine nacelles.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

First flown in October 1966, the GII entered service in 1967 and was produced until 1979 with 258 aircraft built. It established Gulfstream as the pre-eminent large-cabin bizjet brand. Many were later re-engined under the GIIIB programme with Spey Mk 511 engines for improved performance.

Variants

The GII was offered in standard form; operators later fitted winglets in the 1980s as an STC modification to improve fuel efficiency, creating what became informally known as the GIIB.

Where you'll see it

Essentially retired from European operations; occasional examples still fly with government and legacy operators in Africa and the Americas, and historically were familiar at Farnborough and Heathrow in the 1970s.

Related aircraft

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