Air Power Series>1:72 die-cast display model>F-5>HA3351
Northrop F-5F Tiger II 30127, 401 TFW, ROCAF
General Background
The Northrop F-5 tactical fighter was designed as an extremely maneuverable, supersonic fighter with a high rate of reliability at a low operating cost. The F-5 first flew on July 30, 1959 with the first customer delivery in 1964. The last of more than 2,600 F-5’s was produced in 1989 and about two-thirds of these are still in service with 26 countries more than 4 decades later. The F-5 was manufactured by Northrop Grumman and under license in Canada, Taiwan, South Korea, Spain and Switzerland.
The Aircraft
F-5F 83-0127 c/n VN.1024 was delivered to the RoCAF 5th TFW, 4th TRS as 5401 but
eventually went to the 12th TRS, 401st TFW "Red Fox". On Tuesday September 13, 2011
F-5F 5401 along with RF-5E 5506 departed on a routine flight. Thirteen minutes after
departure at 19:52 both aircraft disappeared from radar. Civilians reported a huge
explosion and fires in the mountains of Yilan County. Both aircraft had flown into the
mountain killing all 3 pilots and spewing wreckage over the mountain and a nearby highway.
Specifications :
Specification for the Northrop F-5E/ F-5F Tiger II | |
Number Built: | 1,400 + E/F |
Role F-5F: | Two-seat Combat Trainer Version Of The F-5E Tiger II |
Dimensions | |
Length (F-5E): | 47 feet 4.75 inch (14.65 m) |
Length (F-5F): | 51 feet 4 inch (15.65 m) |
Wingspan F-5E & F-5F: | 26 ft 8 in) |
Height (F-5E): | 13 feet 4 inch (4.06 m) |
Height (F-5F): | 13 feet 1.75 inch (4.01 m) |
Weight | |
Empty Weight (F-5E): | 9,723 lb (4,410 kg) |
Empty Weight (F-5F): | 10,576 lb (4,797 kg) |
Max Take-off Weight (F-5E): | 24,722 lb (11,214 kg) |
Max Take-off Weight (F-5F): | 25,152 lb (11,409 kg) |
Performance | |
Powerplant: | 2 x General Electric J85-GE-21B Turbojets With 5,000 lb.s.t. With Afterburning |
Maximum Speed F-5E: | Mach 1.64 @ 36,000 ft |
Maximum Speed F-5F: | Mach 1.55 @ 36,000 ft |
Range (F-5E): | 1,545 nm (2,863 km) |
Range (F-5F): | 1,270 nm (2,353 km) |
Service Ceiling (F-5E): | 51,800 ft (15,780 m) |
Service Ceiling (F-5F): | 50,800 ft (15,484 m) |
Max Rate of Climb (F-5E): | 34,500 feet/min |
Max Rate of Climb (F-5F): | 32,900 feet/min |
Armament | 1 x In-Nose 20mm M39A2 Cannon With 140 Rounds |
2 x AIM-9 Sidewinder Missiles On Wing Tips | |
5 x Pylons Capable Of Carrying Up To 7,000 lbs. Of Ordnance Or Fuel | |
1 x Under Fuselage Center-line | |
4 x Under Wing (2/Wing) |