| Modern Drawings/Air/UK/Fighters/Others/Seafire-FRMk46.htm | Update: - |
Station Flight
Lossiemouth, FAA - RNAS Lossiemouth, 1947. Equiped with extra 145 L fuel tank in the rear fuselage. The wings were plumbed to allow for a 102 L combat tank to be carried underneath each wing. In addition a 227 L drop tank could be carried under the fuselage. In April 1947, a decision was made to replace the Griffon 61s or 64s driving a five bladed Rotol propeller unit with Griffon 85s or 87s driving two three bladed Rotol contra-rotating propellers. |
Spitfire
Mk.21-24 Specifications |
| General |
Type:
Fighter |
| Engine |
| 1 × Rolls-Royce Merlin 65 | 2050 hp | Pistons |
| Dimensions/Masses |
| Length: 10.04 m |
Width: 11.26 m | Height:
3.86 m Weight: 3247 kg | Max. Combat Weight: 5121 kg |
| Performances |
| Max. Speed: 731 km/h
| Ceiling: 13563 m | Range: 740, 1368 km (ferry range) |
| Armament |
MG:
4 × 20 mm Hispano Mk II Gun |
