Raytheon T-1 Jayhawk

Airplanes

Length

14.6304 m

Flat Wing Span

13.1064 m

Height

3.9624 m

Flat Wing Area

22.4268 m²

Flat Wing Aspect Ratio

7.5

Max Seating

Cruise Speed

725.9834 km/h

Max Speed

866.7353 km/h

Max Ceiling

12496.8 m

Number of Engines

Aircraft Engine

First Flight

1991-07-05

Entry Into service

1992-01-17

Number Built

180

Maximum Take-Off Weight

7.3028 t (paragliders: kg)

Maximum Range

5370.8 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Raytheon T-1 Jayhawk	7.3028	5370.8

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Hawker 400		14.6304	13.1064	9	Compare
Learjet 31	Garrett TFE731	14.6304	13.1064	8	Compare
Aérospatiale Corvette	Pratt & Whitney Canada JT15D	13.83	12.87	6	Compare
SyberJet SJ30	Williams FJ44	14.2646	12.893	7	Compare
Learjet 28		14.51	13.35	8	Compare
FMA IA 58 Pucará	Turbomeca Astazou	14.25	14.5		Compare

All data (29 fields)

Name: Raytheon T-1 Jayhawk
Manufacturer: Beechcraft
Description: The Raytheon T-1 Jayhawk is a twin-engined jet aircraft used by the United States Air Force for advanced pilot training.
ICAO Code: BE40
First Flight: 1991-07-05
Entry Into service: 1992-01-17
Production End: 1997-01-01
Designer: Beechcraft
Type: Trainer aircraft
Length (m): 14.6304
Height (m): 3.9624
Cockpit Crew: 3
Max Seating: 4
Max Speed (km/h): 866.7353
Cruise Speed (km/h): 725.9834
Min Speed (km/h): 172.2359
Max Ceiling (m): 12496.8
Capacity Description: 4 passengers
Number Built: 180
Powerplant Description: 2 × Pratt & Whitney Canada JT15D-5B turbofan
Primary Users: United States Air Force, Japan Air Self-Defense Force
Status: Active service
Wikipedia Article (URL): en.wikipedia.org/wiki/Raytheon_T-1_Jayhawk
Flat Wing Span (m): 13.1064
Flat Wing Area (m²): 22.4268
Flat Wing Aspect Ratio: 7.5
Wake Category: M
Aircraft Engine: Pratt & Whitney Canada JT15D
Number of Engines: 2