McDonnell CF-188D CF-18 outside a hardened aircraft In the 1970s, the Air Force decided that a single multi-role fighter type would replace its CF-101 Voodoos , CF-104 Starfighters and CF-116 Freedom Fighters. The resulting New Fighter Aircraft competition culminated in the selection of the McDonnell-Douglas F/A-18 Hornet. Canada became the first export customer for the type in a contract worth $2.34 (Cdn) billion. A number of Canadian-unique modifications were incorporated into the aircraft design. These included changes for Canadian unique weapons, a 600,000 candle power searchlight in the starboard nose for night intercepts, a modified survival kit and a land based ILS system replacing the USN automatic carrier landing system. Deployed to Canadian air defence (NORAD) and NATO squadrons, the CF-18 Hornet has lived up to all expectations. The multi-role capability of the Hornet has been repeatedly proven in CF use and the aircraft have been operationally employed in the Gulf War and more recently, in the NATO campaign over Kosovo. In the Gulf War, the aircraft were employed in both CAP and conventional strikes. Flying from Aviano, Italy, in the skies over Kosovo and Serbia, the aircraft was primarily employed in the attack role dropping both conventional and precision guided
The two CF-18 fighter squadrons are assigned the air defence role in North America. They maintain limited air-to-surface capability to provide support to maritime operations, as well as support to land operations in defence of Canada. They are also available for contingency operations anywhere in the world.
Note: Current operational aircraft strength is 60 aircraft with the additional 60 aircraft undergoing upgrading and rotation.
| Manufacturer: | McDonnell-Douglas Aircraft Corporation |
| Crew/Passengers: | 1 pilot (CF-18A) or 2 pilots (CF-18B) |
| Power Plant: | 2 x General Electric F404-GE-400 low-bypass turbofans @ 16,000 lb (7,258 kg) thrust |
| Performance: | Max Speed: Mach 1.8 Service Ceiling: 49,000 ft (15,000 m) Unrefuelled Range: 2,300 mi (3,704 km) * * (retractable air-to-air refueling probe fitted) |
| Weights: | Empty: 23,400 lb (10,614 kg) Gross: 37,000 lb (16,783 kg) Maximum Take-off: 49,355 lb (22,387 kg) |
| Dimensions: | Unfolded Span: 40 ft 5 in (12.32 m) (with missiles) Folded Span: 27 ft 6 in (8.38 m) Length: 56 ft 0 in (17.07 m) Height: 15 ft 3 in (4.66 m) Wing Area: 400 sq ft (37.16 sq m) |
| Armament: | Internally mounted M61A1 20mm cannon & provisions for AIM9 Sidewinder and AIM7 Sparrow air-to-air missiles, Maverick air-to-ground missiles, conventional bombs and precision-guided bombs, unguided CRV7 rockets, fuel tanks etc |
| Cost: | Approximately $24 M (Cdn) per aircraft |
