Lockheed JetStar

· AAI Corporation · 4 × Garrett TFE731

Airplanes

Length

18.41 m

Flat Wing Span

16.59 m

Height

6.22 m

Flat Wing Area

50.4 m²

Max Seating

Cruise Speed

811 km/h

Max Speed

883 km/h

Max Ceiling

13105 m

Number of Engines

Aircraft Engine

First Flight

1957-09-04

Entry Into service

1961-01-01

Number Built

202

Maximum Take-Off Weight

20.185 t (paragliders: kg)

Maximum Range

4820 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Lockheed JetStar	20.185	4820

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
McDonnell 119	Westinghouse J34	20.27	17.55	29	Compare
Curtiss-Wright XF-87 Blackhawk		18.8976	18.288		Compare
Heinkel He 343	Heinkel HeS 011	15.5	18		Compare
Potez 840	Turbomeca Astazou	15.89	19.6	24	Compare
Handley Page Marathon	De Havilland Gipsy Queen	15.8496	19.812	20	Compare

All data (26 fields)

Name: Lockheed JetStar
Manufacturer: AAI Corporation
Description: The Lockheed JetStar (company designations L-329 and L-1329; designated C-140 in US military service) is a business jet designed and produced by the American aerospace manufacturer Lockheed.
First Flight: 1957-09-04
Entry Into service: 1961-01-01
Production End: 1980-01-01
Designer: AAI Corporation
Type: Transport
Length (m): 18.41
Height (m): 6.22
Max Seating: 10
Max Speed (km/h): 883
Cruise Speed (km/h): 811
Max Ceiling (m): 13105
Rate of Climb (m/s): 21.1
Capacity Description: 8–10 passengers
National Origin: United States of America
Number Built: 202
Powerplant Description: 4 × Garrett TFE731-3 turbofan, 16.5 kN thrust each
Primary Users: United States Air Force (historical), Mexican Air Force , Islamic Republic of Iran Air Force
Status: In limited service
Wikipedia Article (URL): en.wikipedia.org/wiki/Lockheed_JetStar
Flat Wing Span (m): 16.59
Flat Wing Area (m²): 50.4
Aircraft Engine: Garrett TFE731
Number of Engines: 4