Air Power Series>1:72 die-cast display model>F-18>HA3535
F/A-18A Hornet A21-27, 75 Squadron, RAAF, 2003
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
The RAAF ordered 75 F-18 Hornets made up of 57 single-seat “A” variant serials A21-1 to A21-
57 and 18 two-seater F-18 “B” serials A21-101 to A21-118. F/A-18A A21-27 c/n 514 AF-27 was
first delivered to 75 Sqn./81 Wing on May 10, 1988. 75 Sqn. deployed to Qatar from February
2003 to May 2003 for Operation Bastille and Operation Falconer, RAAF names for their
participation in OIF. During their time in Qatar 75 Sqn. flew 350 combat missions delivering 122
LGBs before returning to home base Tindal.
Specifications :
| Role: | Fighter/Attack |
| Manufactured: | 1980 to 1987 |
| Numbers Produced: | A – 371 |
| B – 40 | |
| Crew: | A – 1 |
| B – 2 | |
| Dimensions | |
| Length: | 56 ft 0 in (17.07 m) |
| Wingspan: | 40 ft 8 in (12.4 m) |
| Folded: | 27 ft 6 in (8.38 m) |
| Height: | 15 ft 4 in (4.66 m) |
| Weight: | |
| Empty: | 28,000 lbs (12,700 kg) |
| Gross: | 38,000 lbs (17,240 kg) |
| Maximum Take off: | 56,000 lb (25,400 kg) |
| Performance | |
| Engines: | 2 X GE F404-GE turbofans producing 10,600 lb.s.t. dry & 15,800 lb.s.t with afterburning per engine |
| Fuel: | |
| Internal: | 1,670 U.S. gal (6,322 l) |
| External: | As many as 3 X 330 U.S. gal (1,249 l) drop tanks |
| Maximum Fuel: | 2,660 U.S. gal (10,070 l) |
| Maximum Speed: | Mach 1.8 1,190 mph (1,915 km/h) @ 35,000 ft (10,670 m) |
| Landing Speed: | 150 mph (241.4 km/h) |
| Combat Ceiling: | 50,000 ft (15,240 m) |
| Maximum Range: | 2,875 miles (4,627 km) |
| Armament: | 1 X 20 mm M61A1 cannon in nose Plus |
| Hard Points: | 4 X under-wing |
| 2 X fuselage corner stations | |
| 1 X center-line | |
| 2 X wing-tip | |
| To carry AIM-9 Sidewinder Missiles Or | |
| AIM-7 Sparrow Missiles Plus | |
| Up to 3 external fuel tanks and other assorted ordnance |