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                                  Type:	           Fighter
                                     
                                     Manufacturer:      Grumman Aircraft Engineering Corporation
                                     
                                     Designed by:	   Bob Kress engineering manager[1]
                                     
                                     Maiden flight:     1970-12-21
                                     
                                     Introduced:	   September 1974
                                     
                                     Retired:	   2006, USN
                                     
                                     Status:	           active service, Iran
                                     
                                     Primary users:	   United States Navy
                                     
                                                        Islamic Republic of Iran Air Force
                                     
                                     Number built:	   675
                                     
                                     Unit cost:	   US$38 million in 1998
                                  
                                 		
                                 GENERAL CHARACTERISTICS
                                     
                                     Crew: 2 (Pilot and Radar Intercept Officer)
                                     Length: 18.6 m (61 ft 9 in)
                                     Wingspan: 64 ft unswept, 38 ft swept (19 m / 11.4 m)
                                     Height: 16 ft (4.8 m)
                                     Wing area: 565 ft² (54.5 m²)
                                     Airfoil: NACA 64A209.65 mod root, 64A208.91 mod tip
                                     Empty weight: 19,000 kg (42,000 lb)
                                     Loaded weight: 28,000 kg (61,000 lb)
                                     Max takeoff weight: 32,805 kg (72,900 lb)
                                     ; Powerplant: 2× General Electric F110-GE-400 afterburning turbofans, 13,810 lbf dry, 27,800 lbf with afterburner (72
                                    kN / 126 kN) each
                                     
                                     PERFORMANCE
                                     
                                     Maximum speed: Mach 2.34, 1,544 mph at high altitude (2,485 km/h)
                                     Range: 576 mi combat (927 km)
                                     Service ceiling: 50,000+ ft (16,000+ m)
                                     Rate of climb: 45,000+ ft/min (230+ m/s)
                                     Wing loading: 113.4 lb/ft² (553.9 kg/m²)
                                     Thrust/weight: 0.88
                                     
                                     ARMAMENT
                                     
                                     13,000 lb (5,900 kg) of ordnance including:
                                     Guns: 1× M61 Vulcan 20 mm Gatling Gun
                                     Missiles: AIM-54 Phoenix, AIM-7 Sparrow and AIM-9 Sidewinder air-to-air
                                     Loading configurations:
                                     2× AIM-9 + 6× AIM-54
                                     2× AIM-9 + 2× AIM-54 + 3× AIM-7
                                     2× AIM-9 + 4× AIM-54 + 2× AIM-7
                                     2× AIM-9 + 6× AIM-7
                                     4× AIM-9 + 4× AIM-54
                                     4× AIM-9 + 4× AIM-7
                                     Bombs: GBU-10, GBU-12, GBU-16, GBU-24, GBU-24E Paveway I/II/III LGB, GBU-31, GBU-38 JDAM, Mk-20 Rockeye II, Mk-82, Mk-83
                                    and Mk-84 series iron bombs
                                     Avionics:Hughes AN/APG-71 radar,AN/ASN-130 INS, IRST,TCS
                                     Unit Cost: US$38 million 
                                  
                                 VARIANTS
                                     
                                     YF-14A : Prototypes and pre-production aircraft. 12 built.
                                     
                                     F-14A : The original production two-seat all-weather interceptor fighter version for the US Navy. Modifications late in
                                    its service life added precision strike munitions to its armament
                                     
                                     F-14A + Plus or F-14B : Upgraded version of the F-14A with GE F110-400 engines. Much of the avionics as well as the AWG-9
                                    radar were retained. Later redesignated F-14B.
                                     
                                     F-14D Super Tomcat : The final incarnation of the F-14. The troublesome TF-30 engines were replaced with GE F110-400 engines,
                                    giving the F-14 the thrust the airframe was originally designed for (F-14Bs also received the GE F110). Also "Digitized"
                                    and fitted with a "Glass" cockpit as well as the new AGP-71 radar
                                     
                                  
                                 
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