
General Dynamics F-111C | |
|---|---|
| Country | USA |
| Role | Fighter-bomber and reconnaissance aircraft |
| First flight | July 1968 |
| Built | 28 |
The General Dynamics F-111C (nicknamed “Pig”) is a variant of the F-111 Aardvark medium-range interdictor and tactical strike aircraft, developed by General Dynamics to meet Australian requirements. The design was based on the F-111A model but included longer wings and strengthened undercarriage. The Australian government ordered 24 F-111Cs to equip the Royal Australian Air Force (RAAF) in 1963, but the aircraft were not delivered until 1973 because of long-running technical problems.
Source: General Dynamics F-111C on Wikipedia
| F-111C Walk Around | |
|---|---|
| Photographer | Fotios Rouch |
| Localisation | Unknow |
| Photos | 54 |
See also:
General Characteristics and Role
The General Dynamics F-111C is a variant of the F-111 Aardvark swing-wing interdictor and tactical strike aircraft, specifically developed for the Royal Australian Air Force (RAAF). It combined the F-111A’s fuselage with the larger, longer-span wings of the FB-111A strategic bomber, along with a strengthened undercarriage to handle heavier weights. Known affectionately as the “Pig” by RAAF crews for its long snout and terrain-following capability, the F-111C served as Australia’s primary long-range strike and reconnaissance platform from 1973 until its retirement in 2010. Its key features were the variable-sweep wings, terrain-following radar, and an escape crew capsule.
| Property | Typical Value |
|---|---|
| Role | Tactical Strike, Interdiction, Reconnaissance (RF-111C) |
| National Origin | United States (Variant for Australia) |
| Manufacturer | General Dynamics |
| Service Entry (RAAF) | 1973 |
| Crew | 2 (Pilot and Weapon Systems Officer, side-by-side) |
| Length | 22.41 m (73 ft 6 in) |
| Wingspan (Extended/Max Sweep) | 19.2 m (63 ft) / 9.73 m (31 ft 11 in) |
| Maximum Takeoff Weight | Approx. 41,504 kg (91,500 lb) |
Powerplant and Performance
- Engines: Two Pratt & Whitney TF30-P-100/109RA afterburning turbofans.
- Maximum Thrust (P-100/P-109RA): Approx. 80 kN dry / 112 kN afterburner (P-100); 92.7 kN dry / 121 kN afterburner (P-109RA).
- Maximum Speed (High Altitude): Mach 2.5 (2,655 km/h / 1,650 mph).
- Maximum Speed (Sea Level): Mach 1.2 (1,390 km/h / 865 mph).
- Combat Radius (Hi-Lo-Hi): Approx. 2,140 km (1,330 mi) with combat load.
- Ferry Range (Max Fuel): Approx. 6,115 km (3,800 mi).
- Key Technology: Terrain-Following Radar (TFR) coupled to the autopilot for automatic, high-speed, low-level flight penetration.
Armament and Avionics
- Internal Weapons Bay: Could carry two M117 750 lb bombs, one nuclear weapon, auxiliary fuel, or the 20 mm M-61A1 Vulcan rotary cannon (seldom fitted).
- External Hardpoints: 9 total (8 under-wing, 1 under-fuselage).
- Capacity: Up to 14,288 kg (31,500 lb) of ordnance.
- Swiveling Pylons: Four underwing pylons pivot with the wing sweep to maintain alignment.
- Armament Capability:
- Conventional Bombs: General purpose bombs (Mk-82, Mk-84).
- Guided Munitions: Laser-Guided Bombs (LGBs) using the AN/AVQ-26 Pave Tack pod (fitted in the weapons bay).
- Missiles: AGM-84 Harpoon anti-ship missile, AGM-142 Stand-Off Weapon, and AIM-9 Sidewinder air-to-air missiles for self-defense.
- Reconnaissance Role: Four aircraft were converted to the RF-111C variant, carrying a pallet of cameras and sensors (like the panoramic KA-56E and AN/AAD-5 Infrared Linescanner) in the weapons bay.
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