| Manufacturer |
Grumman |
| Description |
The Gulfstream II (G-II) is an American twin engine business jet designed and first built by Grumman, then Grumman American and finally Gulfstream American. |
| First Flight |
1966-10-02 |
| Production End |
1980-01-01 |
| Designer |
Grumman |
| Type |
Business jet |
| Length (m) |
24.0792 |
| Height (m) |
7.3152 |
| Cockpit Crew |
2 |
| Min Speed (km/h) |
194.4598 |
| Max Ceiling (m) |
13716 |
| Rate of Climb (m/s) |
19.304 |
| Capacity Description |
19 (maximum certified) / 2900 lb maximum payload |
| National Origin |
United States of America |
| Number Built |
256 |
| Powerplant Description |
2 × Rolls-Royce Spey 511-8 turbofan engines |
| Status |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Grumman_Gulfstream_II |
| Flat Wing Span (m) |
23.4696 |
| Flat Wing Area (m²) |
86.8272 |
| Number of Engines |
2 |