Learjet 25

· Learjet · 2 × General Electric CJ610

Airplanes

Length

14.3256 m

Flat Wing Span

10.668 m

Height

3.6576 m

Flat Wing Area

21.5321 m²

Flat Wing Aspect Ratio

5.01

Max Seating

Cruise Speed

859.3897 km/h

Max Ceiling

13716 m

Number of Engines

Aircraft Engine

First Flight

1966-08-12

Entry Into service

1967-11-01

Number Built

369

Maximum Take-Off Weight

6.8039 t (paragliders: kg)

Total Fuel Capacity

2706.569

Maximum Range

2843.711 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Learjet 25	6.8039	2706.569	2843.711

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Canadair CL-84 Dynavert	Lycoming T53	14.3256	10.3632	12	Compare
Learjet 24	General Electric CJ610	13.1064	10.668	6	Compare
HESA Yasin	General Electric J85	12.25	10.4		Compare
Convair F2Y Sea Dart		15.5448	10.668		Compare
North American Rockwell OV-10 Bronco		13.4112	12.192		Compare
AIDC T-5 Brave Eagle		14.5085	9.2354		Compare

All data (30 fields)

Name: Learjet 25
Manufacturer: Learjet
Description: The Learjet 25 is an American ten-seat (two crew and eight passengers), twin-engine, high-speed business jet aircraft manufactured by Learjet.
ICAO Code: LJ25
First Flight: 1966-08-12
Entry Into service: 1967-11-01
Production End: 1982-01-01
Designer: Learjet
Type: Business jet
Length (m): 14.3256
Height (m): 3.6576
Cockpit Crew: 2
Max Seating: 8
Cruise Speed (km/h): 859.3897
Min Speed (km/h): 168.9811
Max Ceiling (m): 13716
Rate of Climb (m/s): 30.734
Capacity Description: 8 passengers
National Origin: United States of America
Number Built: 369
Powerplant Description: 2 × General Electric CJ610-6 turbojets
Primary Users: Bolivian Air Force, Mexican Navy
Status: Active
Wikipedia Article (URL): en.wikipedia.org/wiki/Learjet_25
Flat Wing Span (m): 10.668
Flat Wing Area (m²): 21.5321
Flat Wing Aspect Ratio: 5.01
Wake Category: L
Aircraft Engine: General Electric CJ610
Number of Engines: 2