Saab-MFI 15/17 Safari-Supporter

1971

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Saab-MFI 17 Supporter

On 11 July 1969 Saab flew the prototype (SE-301) of a two/three-seat civil/military trainer or general utility aircraft to which it had allocated the designation Saab-MFI 15. As then flown it was powered by a 119kW Avco Lycoming IO-320-B2 flat-four engine and had a conventional low-set tailplane, but this was modified subsequently to T-tail configuration to minimise damage when operating from rough airfields.

The prototype was flown on 26 February 1971 with a more powerful Avco Lycoming engine, which became the standard powerplant for the production version, which was re-designated Saab Safari. A braced shoulder-wing monoplane with fixed tricycle landing gear, available optionally with tailwheel landing gear, it provides side-by-side enclosed accommodation for two and has dual controls as standard.

A military version designated originally Saab-MFI 17 was flown on 6 July 1972 and differed from the Safari by being equipped more specifically for use as a military trainer, or for such duties as artillery observation, forward air control and liaison; this version was later named Saab Supporter.

In August 1978 Saab flew a version of the Safari with a 157kW Continental flat-six turbocharged engine; designated Safari TS it did not progress beyond the prototype stage.

Saab built a combined total of about 250 Safari/Supporter aircraft before production ended in the late 1970s. Military Supporters were supplied to the Pakistan air force and army (45), Royal Danish air force (32, which designated it T-17) and Zambian air force (20). Licence-production of this aircraft was started in Pakistan during 1976, initially from kits supplied by Saab, but there has been a gradual change to indigenous manufacture from raw materials. Designated Mushshak in Pakistan, more than 150 have been built.

3-View 
Saab-MFI 15/17 Safari-SupporterA three-view drawing (800 x 684)

Specification 
 MODELSaab-Safari
 ENGINE1 x Avco Lycoming IO-360-A1B6 piston engine, 149kW
 WEIGHTS
  Take-off weight1200 kg2646 lb
  Loaded weight646 kg1424 lb
 DIMENSIONS
  Wingspan8.85 m29 ft 0 in
  Length7.0 m23 ft 12 in
  Height2.6 m9 ft 6 in
  Wing area11.9 m2128.09 sq ft
 PERFORMANCE
  Max. speed235 km/h146 mph
  Ceiling4100 m13450 ft

Comments1-20 21-40 41-60
Lin Light, e-mail, 28.01.2007 05:31

Would like to construct a smaller version. Just a two place under U.S. experimental rules and some help from EAA.

reply

1-20 21-40 41-60

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