Air Power Series>1:72 die-cast display model>F-18>HA3523
McDonnell Douglas F/A-18C Hornet No. 428, 25 Squadron, Kuwait Air Force, 1990s
General Background
The McDonnell Douglas (now Boeing) F/A-18 Hornet is a supersonic twin engine all-weather night fighter and attack aircraft. The F/A-18s first flew in November 1978 and the first production flight on April 12, 1980. The first 380 aircraft were F/A-18As and in September 1987 production switched to the F/A-18C. Variants A and C are single-seat aircraft while B and D are tandem-seats. The Hornet can operate from either aircraft carriers or land bases with the capability of in flight refueling. A total of 1,480 A-D variants were built.
The Aircraft
After the first Gulf War the Kuwaiti Air Force acquired the modern McDonnell Douglas single-seat F-18C and two-seat D variants. Delivery of the F-18s to Kuwait began in the first half of 1992 with 31 F-18/Cs and 8 F-18/Ds being added to the inventory by 2005. F-18/C # 428 MSN 1179 operates with the KAF 25 Fighter and Attack Squadron located at Ahmed al Jaber AB along with the 9 FAS. Even numbered serials belong to 25 Squadron and odd numbered serials belong to the 9 Squadron.
Specifications :
| Role: | supersonic twin engine all-weather night fighter and attack aircraft |
| Crew: | 1 x F/A-18C, 2 x F/A-18D (Pilot and Weapons Systems Officer – WSO) |
| Dimensions | |
| Length: | 56 ft (17.1 m) |
| Wingspan With AAMs: | 40 ft 5 in (12.31 m) |
| Folded: | 27 ft 6 in (8.38 m) |
| Height: | 15 ft 4 in (4.7 m) |
| Weight: | |
| Empty: | 23,000 lb (10,400 kg) |
| Loaded: | 36,970 lb (16,770 kg) |
| Maximum Take off: | 51,900 lb (23,500 kg) |
| Performance | |
| Power Plant: | 2 x General Electric F404-GE-402 turbofan |
| Dry Thrust: | 11,000 lbf (48.9 kN) per engine |
| After Burner Thrust: | 17,750 lbf (79.2 kN) per engine |
| Maximum Speed: | Mack 1.8 (1,190 mph) (1,915 km/h) @ 40,000 ft (12,190 m) |
| Range: | 1,089 nmi (1,250 miles) (2,000 km) with 2 x AIM-9s |
| Combat Radius: | 400 nmi (460 miles) (740 km) air-to-air missions |
| Ferry Range: | 1,800 nmi (2,070 miles) (3,330 km) |
| Service Ceiling: | 50,000 ft (15,240 m) |
| Rate of Climb: | 50,000 ft/min (254 m/s) |
| Armament: | 1 x 20 mm M61 Vulcan cannon mounted in nose with 578 rounds |
| 9 x Hardpoints - a capacity of 13,700 lb (6,215 kg) with external fuel tanks and ordnance | |
| 2 x wingtip missile launch rails | |
| 4 x under-wing | |
| 3 x under-fuselage | |
| Rockets: | 2.75 inch (70 mm) Hydra 70 rockets |
| 5 inch (127 mm) Zuni rockets | |
| Missiles: | Air-To-Air |
| 4 x AIM-9 Sidewinders or | |
| 4 x AIM-132 ASRAAM or | |
| 4 x IRIS-T or 4 x AIM-120 AMRAAM and 2 x AIM-7 Sparrow or | |
| Additional - 2 x AIM-120 AMRAAM | |
| Air-To-Surface: | AGM-65 Maverick |
| Standoff Land Attack Missiles (SLAM-ER) | |
| AGM-88 HARM Anti-radiation Missile (ARM) | |
| AGM-154 Joint Standoff Weapon (JSOW) | |
| Taurus Missile (Cruise Missile) | |
| Anti-ship: | AGM-84 Harpoon |
| Bombs: | JDAM Precision-Guided Munition (PGM) |
| Paveway series of Laser-guided bombs | |
| Mk. 80 series of unguided iron bombs | |
| CBU-87 cluster bombs | |
| CBU-89 gator mine | |
| CBU-97 | |
| Mk. 20 Rockeye II | |
| B61/Mk. 57 nuclear bombs | |
| Others: | SUU-42A Flares/Infrared decoys dispenser pod and chaff pod Or |
| Electronic countermeasures (ECM) pod Or | |
| AN/AAS-38 Nite Hawk targeting pod (USN only) to be replaced by AN/ASQ-228 ATFLIR Or | |
| LITENING targeting pod (only used by USMC, Royal Australian Air Force, Spanish Air Force and Finnish Air Force) Or | |
| Up to 3 x 330 US gallons (270 imp gallons / 1,200 liters) Sargent Fletcher drop tanks for ferry flight Or Extended range/loitering time | |
| Avionics: | Hughes APG-73 radar |
| ROVER (Remotely Operated Video Enhanced Receiver) antenna for use by USN F/A-18C strike fighter squadrons | |
| Inertial Navigation System (INS) | |
| GPS | |
| 2 x mission computers | |
| HUD (Head Up Display) cockpit display | |
| Very High Frequency (VHF) omni-directional landing system | |
| Multiple-functioning Cathode Ray Tube (CRT) display |