Fuji T-1

Airplanes

Length

12.12 m

Flat Wing Span

10.5 m

Height

4.08 m

Flat Wing Area

22.22 m²

Flat Wing Aspect Ratio

4.96

Cruise Speed

620 km/h

Max Speed

925 km/h

Max Ceiling

14400 m

Number of Engines

Aircraft Engine

First Flight

1958-01-01

Number Built

Maximum Take-Off Weight

5 t (paragliders: kg)

Maximum Range

1300 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Fuji T-1	5	1300

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Soko J-21 Jastreb		10.88	10.56		Compare
Gulfstream American Hustler	Honeywell TPE331	12.4968	10.3632	7	Compare
Aero L-39 Albatros		12.13	9.46		Compare
FMA IA-63 Pampa		10.93	9.69		Compare
Martin-Baker MB 5		11.2776	10.668		Compare
CASA C-101 Aviojet		12.5	10.6		Compare

All data (27 fields)

Name: Fuji T-1
Manufacturer: Fuji Heavy Industries, Ltd.
Description: The Fuji T-1 Hatsutaka was a jet-powered trainer aircraft designed and produced by the Japanese conglomerate Fuji Heavy Industries.
ICAO Code: T1
First Flight: 1958-01-01
Production End: 1963-01-01
Service End: 2006-03-03
Designer: Fuji Heavy Industries, Ltd.
Type: Intermediate trainer aircraft
Length (m): 12.12
Height (m): 4.08
Cockpit Crew: 2
Max Speed (km/h): 925
Cruise Speed (km/h): 620
Max Ceiling (m): 14400
Rate of Climb (m/s): 33.02
Armament: Provision for 1 × 12.7 mm Browning M53-2 machine gun in nose; 2
Number Built: 66
Powerplant Description: 1 × Bristol Siddeley Orpheus Mk 805 turbojet
Primary Users: Japan Air Self Defense Force (JASDF)
Wikipedia Article (URL): en.wikipedia.org/wiki/Fuji_T-1
Flat Wing Span (m): 10.5
Flat Wing Area (m²): 22.22
Flat Wing Aspect Ratio: 4.96
Wake Category: L
Aircraft Engine: Bristol Siddeley Orpheus
Number of Engines: 1