North American Sabreliner

Airplanes

Length

13.41 m

Flat Wing Span

13.56 m

Height

4.88 m

Flat Wing Area

31.79 m²

Cruise Speed

800 km/h

Max Speed

885 km/h

Max Ceiling

12200 m

Number of Engines

First Flight

1958-09-16

Entry Into service

1962-01-01

Number Built

800

Maximum Take-Off Weight

8.056 t (paragliders: kg)

Maximum Range

4020 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
North American Sabreliner	8.056	4020

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Piaggio PD.808	Armstrong Siddeley Viper	12.85	13.2	10	Compare
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Grumman OV-1 Mohawk	Lycoming T53	12.4968	14.6304		Compare
Bolkhovitinov S	Klimov M-103	13.2	13.8		Compare
Dornier Do 335		13.85	13.8		Compare
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All data (24 fields)

Name: North American Sabreliner
Manufacturer: North American Aviation
Description: The North American Sabreliner, later sold as the Rockwell Sabreliner, is a mid-sized business jet designed and produced by American aircraft manufacturer North American Aviation.
ICAO Code: SBR1
First Flight: 1958-09-16
Entry Into service: 1962-01-01
Production End: 1982-01-01
Designer: North American Aviation
Type: Trainer aircraft , Business jet
Length (m): 13.41
Height (m): 4.88
Max Speed (km/h): 885
Cruise Speed (km/h): 800
Max Ceiling (m): 12200
Capacity Description: five–seven passengers
Number Built: 800
Powerplant Description: 2 × Pratt & Whitney J60-P-3 turbojet, 13.3 kN thrust each
Primary Users: United States Air Force, United States Navy , United States Marine Corps
Status: In active service
Wikipedia Article (URL): en.wikipedia.org/wiki/North_American_Sabreliner
Flat Wing Span (m): 13.56
Flat Wing Area (m²): 31.79
Wake Category: M
Number of Engines: 2