| 
       
        
      
      
      General Dynamics F-111 
      
        
      The first warplane with variable 
      geometric wings to be mass produced, the F-111 was built by General 
      Dynamics at the beginning of the 1960s against an initial contract for 
      delivery of eighteen planes to the USAF and five to the US Navy. Although 
      the prototype had already flown on December 21, 1964, subsequent phases of 
      development were fraught with difficulties, leading to the abandonment of 
      the program by the US Navy. Production, therefore, was reserved for the 
      USAF, which took delivery of the first machines in 1968. The first variant 
      was the F-111A, and after seventeen pre-production models, 141 of these 
      planes were built. Then followed 76 FB-111As, with more powerful engines, 
      larger wings and more sophisticated electronics, which went into service 
      in 1969. Successive variants were the E (94 planes in service from 
      September 1970); the D for tactical support (96 machines, operational from 
      October 1971); and the F, the final version which appeared as prototype in 
      May 1973 and of which 106 were made, the last in November 1976. Total 
      production of General Dynamics F-111 was 562 aircraft, including 24 
      F-111Cs which were exported to Australia. 
      The first F-111As, hot off the assembly 
      lines, were sent to Vietnam in March 1968 for the Combat Lancer operation. 
      Six tactical bombers of the 428th TFS had the chance to prove their worth 
      in the battle zone, but the experiment was disastrous: three of the six 
      were destroyed during unescorted missions at various times. Initially it 
      was assumed they had been shot down by the enemy, but it later became 
      clear that they had crashed because of structural faults. The detachment, 
      having carried out 55 missions, was recalled to the US, where criticism of 
      this already controversial aircraft reached a new peak. Yet the F-111A did 
      eventually prove itself, again in Vietnam. On September 27, 1972, 48 
      F-111As of the 429th and 430th TFS of the 474th TFW arrived in Southeast 
      Asia; they immediately went into action to help check the accelerating 
      advance of the North Vietnamese. In five months, that is up to the end of 
      the hostilities, they carried out over 4,000 sorties dropping about 74,000 
      tons of bombs with high results, and the loss of only six machines. It is 
      worth noting that 3,980 of these 4,000 missions were effected by means of 
      TFR (Terrain Following Radar), a radar system capable of guiding the plane 
      at a height of only a few meters, encompassing the slightest unevenness of 
      terrain, without intervention by the pilot, and flying beneath the net of 
      the SAM missile radar systems. Such feats in Southeast Asia were crucial 
      in establishing and later restoring the reputation for quality which this 
      variable-sweep wing fighter-bomber from General Dynamics was intended to 
      possess from the start. In action once more in April 1986, attacking 
      targets in Tripoli and Benghazi, Libya, the F-111s confirmed their right 
      to be considered the spearhead of the USAF tactical bombing operations. 
      
      
        
      
        
      
        
      
      
        
      
      Technical Specifications 
      
      
      Aircraft: 
      General Dynamics 
      F-111A 
      Year: 1964 
      Type: fighter-bomber 
      Manufacturer: General Dynamics 
      Engine: 2 x Pratt & Whitney TF30-P-1 
      Power: 18,000 lb (8,165 kg) 
      Wingspan: 63ft (19.20m) 
      Length: 73ft 5 1/2in (22.40m) 
      Height: 17ft 1/2in (5.18m) 
      Wing area: 525sq ft (48.77mē) 
      Max take-off weight: 98,850 lb (44,838 kg) 
      Empty weight: 46,172 lb (20,944 kg) 
      Max speed: 1,435mph at 53,450ft (2,338km/h at 16,292m) 
      Service ceiling: 56,650ft (17,267m) 
      Range: 1,330mi (2,140km) 
      Crew: 2 
      Load-armament: 1x20mm cannon; 30,000 lb (13,608 kg) 
      
          |