Rockwell Sabreliner specs
| Manufacturer: | Rockwell |
| Country: |  United States of America |
| First flight: | 16 September 1958 |
| Production ended: | 1981 |
| Production total: | 671 |
| Series: | CT-39A: T-39A modified as a cargo and personnel transport
CT-39E: United States Navy cargo/transport version CT-39G: United States Navy cargo/transport version based on the stretched fuselage Sabreliner 60 Sabreliner 40: Civil production variant two cabin windows each side; 65 built. Sabreliner 40A: Model 40 with Model 75 wings, improved systems and two CF700 turbofans Sabreliner 60: Stretched Model 40 for 12 passengers with two JT12A-8 engines; 130 built. Sabreliner 65: Series 60 with TFE731-3R-1D engines and new Mark V super-critical wing, 76 built. Sabreliner 70: Renamed Sabreliner 75 after 1971 Sabreliner 75: Series 60A with a raised cabin roof for greater cabin headroom; 9 built. Sabreliner 75A: Sabreliner 75 powered by two CF700 turbofan engines; 66 built. Sabreliner 80: Same as 75A T-39A: Pilot proficiency trainer and utility transport for USAF; 143 built T-39D: Radar systems trainer for the United States Navy T-39N: Navy trainer for the Undergraduate Flight Officer Training program. |
| Propulsion: | 2 jet engines |
| Maximum number of passengers: | 10 |
| Maximum take-off mass: | 10910 kg |
| ICAO Mass group: | 3 |
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