Power Plant F-14B/D
Two General Electric F-110-GE-400 turbo fans rated at 71.56 kN and 120.1 kN with afterburn . Garret ATS 200-50 air turbine starter. F110 engine has 43 % more reheated thrust and 37% more military thrust (no after burn) than TF-20-P-414A in F-14A resulting in 20% more specific excess energy and 30% lower fuel consumption . The engine also have 62% greater launch deck intercept radius and 34 % more combat air patrol time .
Total fuel capacity is 9,029l liters plus 2 external tank each capable of carrying 1,011 liters .
| Dimensions, External |
| Wing Span |
| Unswept | 19.54m |
| Swept | 11.65 |
| Overswept | 10.15 |
| Wing aspect ratio | 7.28 |
| Length Overall | 19.10 |
| Height Overall | 4.88m |
| Tailplane Span | 9.97m |
| Distance Between fin tips | 4.88m |
Weights and Landing
F-14D with F110-GE-400 |
| Weight Empty | 18,951kg |
| Max. Fuel Capacity (usable) |
| Internal | 7,348kg |
| External | 1,724kg |
| Max. External Weapon load | 6,577 kg |
| T-O weight |
| fighter/escort mission | 29,072 kg |
| fleet air defence mission | 33,157 kg |
| Max | 22,724 kg |
| Max Wing Loading | 642.5kg/m square |
| Max power loading | 140.4kg/kN |
| Performance (F110 engines) |
| Max Level Speed | Mach 1.88 |
| Max Normal operating speed | Mach 0.72 |
| Carrier approach speed | 125 knots |
| Service Ceiling | above 16,150m |
| T-0 (Field) | 762m |
| Landing run (field) | 732m |
| Range (with external fuel) | approx 1,600nm |
