Gulfstream specs
| Manufacturer: | Gulfstream Aerospace |
| Country: |  United States of America |
| First flight: | 2 October 1966 |
| Production ended: | in production |
| Production total: | 1616+ |
| Series: | Gulfstream G-IV: Re-engined, stretched fuselage derivative of the Gulfstream III
Gulfstream G-V: G-IV with fuselage lengthened by 7 foot, new engines, higher MTOW Gulfstream G550: G-V with enhanced avionics and other improvements Gulfstream G650: Further development based on G550 Gulfstream II: Original model Gulfstream II B: Modified version, with the wider, wingleted wings and instruments of the Gulfstream III Gulfstream II SP: Modified by the addition of winglets Gulfstream II TT: Modified version with tip tanks Gulfstream III: Improved variant of the Grumman Gulfstream II |
| Propulsion: | 2 jet engines |
| Maximum number of passengers: | 19 |
| Maximum take-off mass: | 41277 kg |
| ICAO Mass group: | 4 |
Gulfstream file photo (photo: Aviation Safety Network archives)
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