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McDONNELL DOUGLAS F/A-18 HORNET

US Navy/Marine Corps designations: F/A-18A, B, C, D

View video clip of a F/A-18 Hornet carrier launch.
See other video clips at our Film/Video Gallery

TYPE:

Carrier-borne and land-based attack/fighter.

Combat Actions:

The Navy deployed 90 F/A-18 A/C's from four aircraft carriers. The Marines had 36 F/A-18A's and 36 F/A-18Cs deployed. The aircraft was used in both an attack and fighter role. Three USMC F/A-18s were damaged by SAMs and one to anti-air artillery, but all returned to base and were back in service within two days. One Navy F/A-18 was lost in combat. The Marines also deployed 12 F/A-18D's, with two sustaining battle damage, but both returning. These aircraft were used as tactical air coordinators and airborne forward control roles.


PROGRAMME:

US Navy study of VFAX low cost, lightweight multi-mission fighter accepted Spring 1974; VFAX study terminated August 1974 and replaced by derivative of either General Dynamics YF-16 or Northrop YF-17 lightweight fighter prototypes; McDonnell Douglas proposed F-17 derivative with Northrop as associate; resultant Navy Air Combat Fighter called Hornet accepted in two versions, F-18 fighter and A-18 attack aircraft; single F/A-18 selected to fill both roles; McDonnell Douglas prime contractor and Northrop principal subcontractor for all versions agreed 1985; first Hornet flight (160775) 18 November 1978; 11 development aircraft flying by March 1980; delivery of F/A-18A/B (TA designation dropped) to US Navy and Marines began May 1980 and completed 1987; millionth flying hour achieved 10 April 1990; two-millionth on 17 September 1993.


DESIGN FEATURES:

Sharp-edged, cambered leading-edge extensions (LEX), slots at fuselage junction and outward-canted twin fins are designed to produce high agility and docile performance at angles of attack over 50 degrees; wings have 20 degrees sweepback at quarter-chord; wings fold up 90 degrees at inboard end of ailerons, even on land-based F/A-18s; landing gear designed for unflared landings on runways as well as on carriers.


STRUCTURE:

Multi-spar wing mainly of light alloy, with graphite/epoxy inter-spar skin panels and trailing-edge flaps; tail surfaces mainly graphite/epoxy skins over aluminium honeycomb core; graphite/epoxy fuselage panels and doors; titanium engine firewall. Northrop Grumman produces rear and centre fuselages; assembly and test at McDonnell Douglas St Louis factory; CASA produces horizontal tail surfaces, flaps, leading-edge extensions, speedbrakes, rudders and rear side panels for all F/A-18s.


LANDING GEAR:

Dowty retractable tricycle type, with twin-wheel nose and single-wheel main units. Nose unit retracts forward, surface of the engine air ducts. Bendix wheels and brakes. Nosewheel tyres size 22 x 6.6-10, 20 ply, pressure 24.13 bars (350 lb/sq in) for carrier operations, 10.34 bars (150 lb/sq in) for land operations. Mainwheel tyres size 30 x 11.5-14.5, 24 ply, pressure 24.13 bars (350 lb/sq in) for carrier operations, 13.79 bars (200 lb/sq in) for land operations.


POWER PLANT:

Two General Electric F404-GE-400 low bypass turbofans initially, each producing approx 71.2 kN (16,000 lb st) with afterburning. F404-GE-402 EPE (Enhanced Performance Engine) standard from early 1992; rated at approx 78.3 kN (17600 lb st). Self-sealing fuel tanks and fuel lines; foam in wing tanks and fuselage voids. Internal fuel capacity (JP5) approx 6061 litres (1600 US gallons; 1333 Imp gallons). Provision for up to three 1250 litre (330 US gallon; 275 Imp gallon) external tanks.


ACCOMMODATION:

Pilot only, on Martin-Baker SJU-5/6 ejection seat, in pressurised, heated and air-conditioned cockpit. Upward opening canopy, with separate windscreen, on all versions. Two pilots in F/A-18B and USN F/A-18D; pilot and Naval Flight Officer in USMC F/A-18D.


AVIONICS:

Include an automatic carrier landing system (ACLS) for all-weather carrier operations; a Hughes Aircraft AN/APG-65 multi-mode digital air-to-air and air-to-ground tracking radar, with air-to-air modes which include velocity search (VS), range while search (RWS), track while scan (TWS), which can track 10 targets and display eight to the pilot, and raid assessment mode (RAM). Hughes AN/APG-73 radar in C/Ds for USN, USMC, Finland, Malaysia and Switzerland from May 1994. Smiths Industries multi-purpose colour map display; two Kaiser monochrome MFDs (colour on Night Attack Hornets). Collins AN/ARN-118 Tacan, AN/ARC-182 UHF/VHF com and DF-301E UHF/DF; Magnavox AN/ALR-50 and Litton AN/ALR-67 RWRs; GEC-Marconi Type 117 laser designator; Harris AN/ASW-25 radio data link; Eaton AN/ARA-63 receiver/decoder; GEC-Marconi FID 2035 horizontal situation display; Bendix/King HSI; J. E. T. ID-1791/A flight director indicator; General Electric quadruple-redundant fly-by-wire flight control system, with direct electrical backup to all surfaces and direct mechanical backup to tailerons; two Control Data AN/AYK-14 digital computers; Litton AN/ASN-130A inertial navigation system (plus GPS from FY 1993), but being replaced by Litton AN/ASN-139 ring laser system (including retrofits); two Kaiser multi-function CRTs, central GEC-Marconi-Bendix/King CRT and Kaiser AN/AVQ-28 HUD; Conrac communications system control; Normalair-Garrett digital data recorder for Bendix/King maintenance recording system; flight incident recording and monitoring system (FIRAMS).

ARMAMENT:

Nine external weapon stations, comprising two wingtip stations for AIM-9 Sidewinder air-to-air missiles; two outboard wing stations for an assortment of air-to-air or air-to-ground weapons, including AIM-7 Sparrows, AIM-9 Sidewinders, AIM-120 AMRAAMs (launch trials by VX-4 in 1992; cleared for squadron use mid-1993), AGM-84 Harpoons and AGM-65F Maverick missiles; two inboard wing stations for external fuel tanks, air-to-ground weapons or Brunswick ADM-141 TALD tactical air-launched decoys; two nacelle fuselage stations for Sparrows or Martin-Marietta AN/ASQ-173 laser spot tracker/strike camera (LST/SCAM) or AN/AAS-38 and AN/AAR-50 sensor pods (see Avionics); and a centreline fuselage station for external fuel or weapons. Air-to-ground weapons include GBU-10 and -12 laser-guided bombs, Mk 82 and Mk 84 general purpose bombs, and CBU-59 cluster bombs. An M61A1 20 mm six-barrel gun, with 570 rounds, is mounted in the nose and has a McDonnell Douglas director gunsight, with a conventional sight as backup.

DIMENSIONS: EXTERNAL:

Wingspan: 11.43 m (37 ft 6 in)

Wingspan over missiles: 12.31 m (40 ft 4 3/4 in)

Wing chord: at root: 4.04 m (13 ft 3 in)

at tip: 1.68 m (5 ft 6 in)

Wing aspect ratio: 3.52

Width, wings folded: 8.38 m (27 ft 6 in)

Length overall: 17.07 m (56 ft 0 in)

Height overall: 4.66 m (15 ft 3 1/2 in)

Tailplane span: 6.58 m (21 ft 7 1/4 in)

Distance between fin tips: 3.60 m (11 ft 9 1/2 in)


WEIGHTS AND LOADINGS:

Weight empty: 10,810 kg (23,832 lb)

Max fuel weight: internal (JP5): 4926 kg (10,860 lb)

external: F/A-18 (JP5): 3053 kg (6732 lb)

CF-18 (JP4): 4246 kg (9360 lb)

Max external stores load: 7031 kg (15,500 lb)

T-O weight: fighter mission: 16,651 kg (36,710 lb)

attack mission: 23,541 kg (51,900 lb)

max: approx 25,401 kg (56,000 lb)

Max wing loading

(attack mission): 600.83 kg/m/2 (123.06 lb/sq ft)

Max power loading

(attack mission): 156.80 kg/kN (1.54 lb/lb st)


PERFORMANCE:

Max level speed: more than Mach 1.8

Max speed, intermediate power: more than Mach 1.0

Approach speed: 134 knots (248 km/h; 154 mph)

Combat ceiling: approx 15240 m (50,000 ft)


LENGTH (m): 17.07

HEIGHT (m): 4.66

WINGSPAN (m): 12.31

MAX WING LOAD (kg/m/2/): 600.83

MAX LEVEL SPEED (knots): 1032

T-O RUN (m): 427

Data from FAS, Jane's All the World's Aircraft, and Aerospace/Defense Companies.

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