Saab 105

· Saab

Airplanes

Length

10.8 m

Flat Wing Span

9.5 m

Height

2.7 m

Flat Wing Area

16.3 m²

Max Speed

970 km/h

Max Ceiling

13700 m

Number of Engines

First Flight

1963-06-29

Entry Into service

1967-07-17

Number Built

192

Maximum Take-Off Weight

4.635 t (paragliders: kg)

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Saab 105	4.635

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Focke-Wulf F 19 Ente		10.53	10		Compare
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Nakajima Kikka	Ishikawajima Ne-20	9.25	10		Compare
NASA AD-1	Microturbo TRS 18	11.83	9.85		Compare
Williams V-Jet II		10.668	10.668		Compare
Morane-Saulnier MS.760 Paris		10.05	10.15	2	Compare

All data (27 fields)

Name: Saab 105
Manufacturer: Saab
Description: The Saab 105 is a Swedish high-wing, twinjet trainer aircraft developed in the early 1960s as a private venture by Saab AB.
ICAO Code: SB05
First Flight: 1963-06-29
Entry Into service: 1967-07-17
Production End: 1972-01-01
Service End: 2020-12-31
Designer: Saab
Type: Jet trainer and light attack aircraft
Length (m): 10.8
Height (m): 2.7
Cockpit Crew: 2
Max Speed (km/h): 970
Max Ceiling (m): 13700
Rate of Climb (m/s): 70
Armament: 6 hardpoints, AAMs, ASMs, gun pods, bombs, rockets
National Origin: Sweden
Number Built: 192
Powerplant Description: 2 × General Electric J85-17B turbojets, 12.68 kN thrust each
Primary Users: Swedish Air Force (historical), Austrian Air Force (historical)
Status: retired in military service, Active in Swedish Air Force Historic Flight
Wikipedia Article (URL): en.wikipedia.org/wiki/Saab_105
Flat Wing Span (m): 9.5
Flat Wing Area (m²): 16.3
Wake Category: L
Number of Engines: 2