INDIAFOXTECHO - NORTHOP GRUMMAN F-14D TOMCAT FOR (FSX & P3D)
The final variant of the F-14 was the F-14D Super Tomcat. The F-14D variant was first delivered in 1991. The original TF-30 engines were replaced with GE F110-400 engines, similar to the F-14B. The F-14D also included newer digital avionics systems including a glass cockpit and replaced the AWG-9 with the newer AN/APG-71 radar. Other systems included the Airborne Self Protection Jammer (ASPJ), Joint Tactical Information Distribution System (JTIDS), SJU-17(V) Naval Aircrew Common Ejection Seats (NACES) and Infra-red search and track (IRST).
Although the F-14D was to be the definitive version of the Tomcat, not all fleet units received the D variant. In 1989, Secretary of Defense Dick Cheney refused to approve the purchase of any more F-14D model aircraft for $50 million each and pushed for a $25 million modernization of the F-14 fleet instead. Congress decided not to shut production down and funded 55 aircraft as part of a compromise. A total of 37 new aircraft were completed, and 18 F-14A models were upgraded to D-models, designated F-14D(R) for rebuild. An upgrade to the F-14D's computer software to allow AIM-120 AMRAAM missile capability was planned but was later terminated.
While upgrades had kept the F-14 competitive with modern fighter aircraft technology, Cheney called the F-14 1960s technology. Despite an appeal from the Secretary of the Navy for at least 132 F-14Ds and some aggressive proposals from Grumman for a replacement, Cheney planned to replace the F-14 with a fighter that was not manufactured by Grumman. Cheney called the F-14 a "jobs program", and when the F-14 was canceled, an estimated 80,000 jobs of Grumman employees, subcontractors, or support personnel were affected. Starting in 2005, some F-14Ds received the ROVER III upgrade.
General characteristics
Crew: 2 (Pilot and Radar Intercept Officer)
Length: 62 ft 9 in (19.1 m)
Wingspan:
Spread: 64 ft (19.55 m)
Swept: 38 ft (11.58 m)
Height: 16 ft (4.88 m)
Wing area: 565 ft² (54.5 m²)
Airfoil: NACA 64A209.65 mod root, 64A208.91 mod tip
Empty weight: 43,735 lb (19,838 kg)
Loaded weight: 61,000 lb (27,700 kg)
Max. takeoff weight: 74,350 lb (33,720 kg)
Powerplant: 2 × General Electric F110-GE-400 afterburning turbofans
Dry thrust: 16,610 lbf (73.9 kN) each
Thrust with afterburner: 30,200 lbf (134 kN) each
Maximum fuel capacity: 16,200 lb internal; 20,000 lb with 2x 267 gallon external tanks[36]
Performance
Maximum speed: Mach 2.34 (1,544 mph, 2,485 km/h) at high altitude
Combat radius: 500 nmi (575 mi, 926 km)
Ferry range: 1,600 nmi (1,840 mi, 2,960 km)
Service ceiling: 50,000+ ft (15,200 m)
Rate of climb: >45,000 ft/min (229 m/s)
Wing loading: 96 lb/ft²[164] (468.7 kg/m²)
Thrust/weight: 0.88[166]
Armament
Guns: 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, with 675 rounds
Hardpoints: 10 total: 6× under-fuselage, 2× under nacelles and 2× on wing gloves[167][N 2] with a capacity of 14,500 lb (6,600 kg) of ordnance and fuel tanks[168]
Missiles:
Air-to-air missiles: AIM-54 Phoenix, AIM-7 Sparrow, AIM-9 Sidewinder
Loading configurations:
2× AIM-9 + 6× AIM-54 (Rarely used due to weight stress on airframe)
2× AIM-9 + 2× AIM-54 + 3× AIM-7 (Most common load during Cold War era)
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:
JDAM precision-guided munition (PGMs)
Paveway series of laser-guided bombs
Mk 80 series of unguided iron bombs
Mk 20 Rockeye II
Others:
Tactical Airborne Reconnaissance Pod System (TARPS)
LANTIRN targeting pod
2× 267 US gal (1,010 l; 222 imp gal) drop tanks for extended range/loitering time
Avionics
Hughes AN/APG-71 radar
AN/ASN-130 Inertial navigation system, Infra-red search and track, TCS
Remotely Operated Video Enhanced Receiver (ROVER) upgrade.
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