| 1 | A | B | C | D | E | F |
| --- | --- | --- | --- | --- | --- | --- |
| 2 | General Electric CF6 - Specifications |  |  |  |  |  |
| 3 | Variant | CF6-6 | CF6-50 | CF6-80A | CF6-80C2 | CF6-80E1 |
| 4 | Type | Dual rotor, axial flow, high bypass ratio turbofan, annular combustor | Dual rotor, axial flow, high bypass ratio turbofan, annular combustor | Dual rotor, axial flow, high bypass ratio turbofan, annular combustor | Dual rotor, axial flow, high bypass ratio turbofan, annular combustor | Dual rotor, axial flow, high bypass ratio turbofan, annular combustor |
| 5 | Compressor | Fan & 1LP + 16HP | Fan & 3LP + 14HP | Fan & 3LP + 14HP | Fan & 4LP + 14HP | Fan & 4LP + 14HP |
| 6 | Turbine | 2HP + 5LP | 2HP + 4LP | 2HP + 4LP | 2HP + 5LP | 2HP + 5LP |
| 7 | Length | 188 in (478 cm) | 183 in (465 cm) | 167 in (424 cm) | 168 in (427 cm) | 168 in (427 cm) |
| 8 | Diameter | 105 in (267 cm) | 105 in (267 cm) | 105 in (267 cm) | 106 in (269 cm) | 114 in (290 cm) |
| 9 | Blade Count | 38 | 38 | 38 | 38 | 34 |
| 10 | Takeoff thrust | 41,500 lbf 185 kN | 51,500–54,000 lbf 229–240 kN | 48,000–50,000 lbf 210–220 kN | 52,200–61,960 lbf 232.2–275.6 kN | 65,800–69,800 lbf 293–310 kN |
| 11 | Pressure ratio | 25–25.2 | 29.2–31.1 | 27.3–28.4 | 27.1–31.8 | 32.4–34.8 |
| 12 | Bypass ratio | 5.76–5.92 | 4.24–4.4 | 4.59–4.66 | 5–5.31 | 5–5.1 |
| 13 | Max. power TSFC | 0.35 lb/lbf/h 9.9 g/kN/s | 0.368–0.385 lb/lbf/h 10.4–10.9 g/kN/s | 0.355–0.357 lb/lbf/h 10.1–10.1 g/kN/s | 0.307–0.344 lb/lbf/h 8.7–9.7 g/kN/s | 0.332–0.345 lb/lbf/h 9.4–9.8 g/kN/s |
| 14 | Application | DC-10-10 | B747, DC-10-15/30 A300 | A310, B767 | A300/310, B747-400 B767, MD-11, C-5M | A330 |
| 15 | TCDS | CF6-6 | CF6-50 | CF6-80A | CF6-80C2 | CF6-80E1 |
| 16 | Weight | 8,176 lb 3,709 kg | 8,825–9,047 lb 4,003–4,104 kg | 8,760–8,776 lb 3,973–3,981 kg | 9,480–9,860 lb 4,300–4,470 kg | 11,225 lb 5,092 kg |
| 17 | Max. LP RPM | 3,810 | 4,102 | 4,016 | 3,854 | 3,835 |
| 18 | Max. HP RPM | 9,925 | 10,761 | 10,859 | 11,055 | 11,105 |
| 19 | Thrust-to-weight ratio | 5.08 | 5.84–5.97 | 5.48–5.7 | 5.51–6.28 | 5.86–6.22 |

Question: What is the thrust range of the CF6-80A and to which aircraft is is applicable?
Answer: The CF6-80A has a thrust of 48,000 to 50,000 lb, which is applicable for Airbus A310.