Hobby Master HA3017 RAAF General Dynamics F-111C "Aardvark" Strike Aircraft - "RAAF Farewell", No.82 Wing, December 2010 (1:72 Scale)
"It's quite an historic day from an Air Force perspective particularly for the guys who've worked on the F-111 ... to see the last one just about to depart."
- Wing Commander Clive Wells, Royal Australian Air Force, as the final F-111 leaves for the Pacific Air Museum, September 4th, 2013
The General Dynamics F-111 "Aardvark" is a medium-range interdictor and tactical strike aircraft that also fills the roles of strategic bomber, reconnaissance, and electronic warfare in its various versions. Developed in the 1960s and first entering service in 1967, the United States Air Force (USAF) variants were officially retired by 1998. The Royal Australian Air Force (RAAF) is the sole remaining operator of the F-111.
The F-111 pioneered several technologies for production military aircraft including variable-sweep wings, afterburning turbofan engines, and automated terrain following radar for low-level, high-speed flight. Its design was influential, being reflected in later Soviet aircraft such as the Sukhoi Su-24, and some of its advanced features have since become commonplace. During its inception, however, the F-111 suffered a variety of development problems, and several of its intended roles, such as naval interception through the F-111B, failed to materialize.
In USAF service the F-111 has been effectively replaced by the F-15E Strike Eagle for medium-range precision strike missions, while the supersonic bomber role has been assumed by the B-1B Lancer. In 2007, the RAAF decided to replace its 21 F-111s in 2010 with 24 F/A-18F Super Hornets.
Pictured here is a 1:72 scale rendition of a Royal Australian Air Force General Dynamics F-111C "Aardvark" strike aircraft that was attached to No.82 Wing during December 2010.
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Dimensions:
Wingspan: 12-1/4-inches
Length: 10-1/2-inches
Release Date: August 2016
Historical Account: "Pigs No Longer Fly" - In 2007, the Australian government decided to retire all of its F-111s by 2010, and acquire 24 F/A-18F Super Hornets as an interim replacement, pending the arrival of the F-35 Lightning JSF then under development. The F-111 fleet was considered to be at risk due to fatigue issues, and too expensive to operate as each aircraft required 180 hours of maintenance for every hour of flying time. No.82 Wing began re-equipping with the Super Hornet in 2010, and the last F-111s were retired on December 3rd that year. FACDU was combined with the RAAF Special Tactics Project in July 2009 to form No.4 Squadron. The following year, No.82 Wing became home to No.5 Flight, which was responsible for training personnel to operate the RAAF's two IAI Heron unmanned aerial vehicles based at Kandahar in Afghanistan. The Air Force acquired a third Heron in 2011, based in Australia and operated by No.5 Flight. As of that year, the F-35 was not expected to enter Australian service until 2018.
The RAAF hoped to be able to sell off its Super Hornets "with very low kilometers on the clock" by 2020, but this would depend on delivery of the replacement F-35s. In April 2013, No.5 Flight was transferred from No.82 Wing to Surveillance and Response Group's No.92 Wing. The following month, the Federal government announced plans to purchase twelve Boeing EA-18G Growlers to supplement the Super Hornet fleet. No.6 Squadron is expected to begin taking delivery of the Growlers in 2017, at which point its Super Hornets will be transferred to No.1 Squadron.
- General characteristics
- Crew: 2 (pilot and weapons system operator)
- Length: 73 ft 6 in (22.4 m)
- Wingspan:
- Spread: 63 ft (19.2 m)
- Swept: 32 ft (9.75 m)
- Height: 17.13 ft (5.22 m)
- Wing area:
- Spread: 657.4 ft² (61.07 m²)
- Swept: 525 ft² (48.77 m²)
- Airfoil: NACA 64-210.68 root, NACA 64-209.80 tip
- Empty weight: 47,200 lb (21,400 kg)
- Loaded weight: 82,800 lb (37,600 kg)
- Max takeoff weight: 100,000 lb (45,300 kg)
- Powerplant: 2× Pratt & Whitney TF30-P-100 turbofans
- Dry thrust: 17,900 lbf (79.6 kN) each
- Thrust with afterburner: 25,100 lbf (112 kN) each
- Zero-lift drag coefficient: 0.0186
- Drag area: 9.36 ft² (0.87 m²)
- Aspect ratio: spread: 7.56, swept: 1.95
- Performance
- Maximum speed: Mach 2.5 (1,650 mph, 2,655 km/h)
- Combat radius: 1,330 mi (1,160 nmi, 2,140 km)
- Ferry range: 4,200 mi (3,700 nmi, 6,760 km)
- Service ceiling: 66,000 ft (20,100 m)
- Rate of climb: 25,890 ft/min (131.5 m/s)
- Wing loading:
- Spread: 126.0 lb/ft² (615.2 kg/m²)
- Swept: 158 lb/ft² (771 kg/m²)
- Thrust/weight: 0.61
- Lift-to-drag ratio: 15.8
- Armament
- Guns: 1× M61 Vulcan 20 mm (0.787 in) gatling cannon (seldom fitted)
- Hardpoints: 9 in total (8× under-wing, 1× under-fuselage between engines)
- Armament capacity: 31,500 lb (14,300 kg) ordnance mounted externally on hardpoints and internally in fuselage weapons bay
- Bombs:
- Free-fall general-purpose bombs
- Mk 82 (500 lb/227 kg)
- Mk 83 (1,000 lb/454 kg)
- Mk 84 (2,000 lb/907 kg)
- Mk 117 (750 lb/340 kg)
- Cluster bombs
- BLU-109 (2,000 lb/907 kg) hardened penetration bomb
- Paveway laser-guided bombs, including:
- GBU-10 (2,000 lb/907 kg)
- GBU-12 (500 lb/227 kg)
- GBU-28, specialized 4,800 lb (2,200 kg) penetration bomb
- BLU-107 Durandal runway-cratering bomb
- GBU-15 electro-optical bomb
- AGM-130 stand-off bomb
Wingspan: 12-1/4-inches Length: 10-1/2-inches
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