Saab MFI-15 Safari / MFI-17 Supporter

The Saab MFI-15 Safari and its armed sibling the MFI-17 Supporter are Swedish primary trainer/utility aircraft designed by Bjorn Andreasson at Malmo Flygindustri (MFI), which was absorbed into Saab in 1968. The airplane first flew on 26 February 1971 and entered service in 1972. A total of 462 were built — 250 at Saab's Malmskoga plant in Sweden (1971–1979), and 212 license-built in Pakistan by the Pakistan Aeronautical Complex (PAC) as the Mushshak and later upgraded Shahbaz.

Its most distinctive feature is a forward-swept shoulder-mounted wing — the wing root sits behind the pilots' heads, yielding a panoramic, unobstructed downward view from the bubble canopy that rivals a helicopter. Two seats sit side-by-side with a third jump/baggage seat aft, all under the one-piece sliding canopy. The tricycle gear is fixed, the construction is all-metal, and despite the training mission the airplane is fully aerobatic (+6/-3 g). The MFI-17 Supporter adds six underwing hardpoints for light weapons or stores (up to 300 kg external) and is the dominant operator variant worldwide.

Principal military users are/were the Royal Danish Air Force (32 T-17s, retired 2016), Royal Norwegian Air Force (16, retired 2016), Pakistan Air Force and Army (120+ Mushshaks still active), Zambia, Sierra Leone, and Iran. Civil registrations are extremely rare; perhaps a dozen fly in Europe (mostly Sweden, Denmark, Norway) and only a handful in the US after Danish T-17 surplus disposals around 2016–2018.

The Safari's 200 hp over roughly 2,650 lb gross gives it a power loading near 13 lb/hp — genuinely sprightly for a trainer. Real-world cruise is 110–115 KTAS at roughly 9.5 gph; book max cruise of 127 KIAS is rarely seen in practice because drag from the fat canopy and external appendages bleeds off the top. Climb performance is excellent from sea level (~800 fpm at gross; 1,100+ fpm solo) and holds up well at density altitude thanks to fuel injection.

STOL numbers are legitimate: the forward-swept wing with slotted flaps gives a published 385 m (1,263 ft) over a 15 m obstacle at max gross, and solo with half fuel, operators routinely see ground rolls under 500 ft. Stall is docile and well-telegraphed — a key reason the Scandinavians picked it as a primary trainer. The airplane is aerobatic to +6/-3 g in the utility category (seat, rudder pedal, and harness provisions), and Danish and Norwegian air forces used it for upset and spin training.

Endurance is exceptional: 50 US gal and ~9.5 gph yields well over 5 hours with reserves. The forward-swept wing is purely a visibility and CG-compatibility trick, not a performance feature — it does not confer supersonic-style benefits.

With 50 US gal usable (~300 lb fuel) and 1,222 lb useful load, the Safari/Supporter can carry two 200 lb adults, full fuel, and ~620 lb of baggage — or fill the third seat with a 170 lb passenger, two 200 lb front-seaters, full fuel, and still have 350 lb of margin. This is exceptional load capability for a 200 hp trainer and reflects the airframe's military utility heritage.

At full fuel and two-up, still-air range is roughly 580 nm with 45-minute reserve at 112 KTAS. Three-up with full fuel remains legal and practical; with underwing stores (on Supporters retaining hardpoints) useful load decreases but the airframe is still strong. The forward CG at full load is mild due to the shoulder-wing geometry, and rearward CG with a third occupant is usually within limits without fuel trickery. In practice the airframe is payload-unlimited for typical training and fun-flying missions, and the true limit is fuel-burn endurance (~5 hours) rather than weight.

Sources:

• Saab Safari - Wikipedia
• PAC Mushshak - Wikipedia
• Saab-MFI 15/17 Safari-Supporter - Aviastar
• Saab MFI-15 Safari / MFI-17 Supporter - flugzeuginfo.net
• Andersson Aircraft MFI-15-200A listing
• Lycoming Overhaul Prices - A&E Aircraft Engines

• Flight training (6): Excellent handling, aerobatic-capable, bubble canopy visibility, and durable military-spec airframe make it a superb trainer in theory. Held back only by orphan-fleet logistics; no US flight school would touch it. Scandinavian and Pakistani air forces ran their entire primary syllabus on it. See Flight Training.
• Backcountry/bush (6): Genuine short-field numbers and rugged fixed gear help, but the low-slung fuselage, small tires, and limited prop clearance make it inferior to a Husky or Maule on unimproved strips. Shoulder wing and canopy give unmatched terrain visibility. See Backcountry / Bush Flying.
• Business travel (3): 112 KTAS cruise is Cessna 172 territory with worse payload-range when loaded with three; no IFR certification in most civil examples.
• Aerobatics (5): Certified +6/-3 g and fully aerobatic, but it is a heavy trainer, not a Pitts — rolls are slow and vertical performance is limited. Great for upset recovery and basic acro.
• Cross-country (5): Reasonable range (~580 nm) and comfortable side-by-side seating, but slow and fuel-hungry vs. a Mooney or Cirrus.
• Cargo hauling (3): 1,200+ lb useful load is strong, but the cabin is small and there is no cargo door; the jumpseat/baggage area behind is cramped.
• Local fun flying (8): Bubble canopy, aerobatic capability, military trainer pedigree, and oddball European cachet make it an exceptional weekend and fly-in airplane. See Local Fun Flying.
• Surveying (7): Canopy visibility rivals a helicopter; shoulder wing does not block downward sightlines. 5+ hour endurance and 200 hp are ideal for pipeline/wildlife/photo work — the limiter is parts supply, not suitability.

Almost all surviving airframes retain their original military or 1970s-era panels: a single King KX-170 or similar comm/nav, a basic ADF, and mechanical gyros. Ex-Danish T-17s disposed in 2016 were delivered with minimal avionics and no IFR certification. Civil owners in Europe have typically upgraded to a single Garmin GTN 650 or GNC 255/GTR 225 combo, a GTX 335 ADS-B transponder, and sometimes a G5 for attitude. No glass panel retrofits are known; the shallow panel cutout and non-standard instrument layout complicate STC-free installs.

Experimental-category US owners (some Mushshaks and Supporters were imported on experimental exhibition tickets) have more freedom and a few have installed Dynon or Garmin G3X Touch systems. See Avionics Pricing Reference.

There is no meaningful STC catalog for the MFI-15/17 — the type certificate is held by Saab (now dormant for this product) and any modifications require either OEM engineering approval (rare) or a field approval. Known mods:

• IO-540 engine upgrade: Performed on the PAC Shahbaz and Super Mushshak but not available as a civil retrofit; adds 60 hp and dramatically improves hot-and-high climb.
• Tailwheel conversion: Factory option from Saab; a handful of tailwheel Supporters exist but most are trike.
• Glider tow hook: Factory option and the dominant civilian use case in Sweden; the 200 hp engine makes it a strong towplane.
• Underwing hardpoint removal: Former military Supporters typically have the hardpoints faired over for civil operation.

Parts availability is poor and getting worse. Saab exited this product line decades ago and holds but does not actively support the type certificate. PAC in Pakistan manufactures Mushshak parts but does not export to Western civil operators. Practical sources are:

• European type clubs in Sweden, Denmark, and Norway — the only real parts pipeline, primarily trading surplus from retired Danish T-17s.
• Lycoming IO-360-A1B6 engine parts are universally available through any Lycoming distributor — the engine is the one bright spot.
• Standard hardware, instruments, tires, brakes — generally interchangeable with other 1970s GA types.
• Structural parts, canopies, cowlings, wing fittings, landing gear — essentially must be salvaged from a parted-out airframe.

A&P familiarity is rare — virtually no US mechanic has worked on one. Annual inspections run USD 3,000–5,000 routine, with an "it depends" factor for any structural finding that requires sourced parts. Expect to ship parts from Europe and accept 2–4 week AOG times. See Maintenance Ecosystem.

Civil market pricing is thin. Tidy ex-Danish T-17s sold for roughly USD 55,000–70,000 at Danish Air Force disposal auctions in 2016–2018; well-imported, re-registered, freshly painted Supporters in Europe ask EUR 85,000–110,000 (~USD 90,000–120,000). Mushshaks are essentially unavailable to Western buyers. Typical US civil examples land around USD 80,000. See Aircraft Valuation Methodology.

Premium drivers: recent engine (the IO-360-A1B6 overhaul at ~USD 35,000–40,000 is a huge fraction of hull value), intact undamaged canopy, complete and translated log history, civil type certificate data and operating limitations already established by the FSDO, and low-cycle airframe. Discount drivers: cracked canopy, corrosion in wing carry-through, high-cycle landing gear, incomplete logs, and experimental-exhibition-only US airworthiness (which restricts flight to specific mission profiles).

• Wing attach fitting corrosion: The shoulder wing attach carry-through is a known inspection item on high-time airframes; Danish Air Force AD-equivalent service bulletins required recurring eddy-current inspections.
• Canopy cracking: The one-piece bubble is expensive and essentially unobtainable new; cracks propagate from latch points and are a common grounding item.
• Fuel selector wear: Original selectors develop detents and internal seal leaks; replacements must be sourced from surplus.
• Landing gear leg fatigue: Tricycle gear legs have service life limits tracked in cycles, not hours, and trainer-career airframes often have thousands of cycles.
• Lycoming IO-360-A1B6 ADs: The engine inherits the standard Lycoming AD set (crankshaft, oil pump gears, lifters) — engine ADs are the least of an MFI owner's worries.
• Documentation gaps: Ex-military airframes often arrive with incomplete or Danish/Swedish-language logbooks and require translation and re-compilation for FAA import.

Hull insurance is the hardest part of MFI-15/17 ownership in the US. Underwriters classify it as an orphan European military type with no parts pipeline and no familiar repair network, so hull premiums run roughly 2–3x a comparable-value Cessna 172 — expect USD 2,000–2,800/year on a USD 80,000 hull, with many carriers declining outright. Liability-only is more accessible (USD 600–900). Carriers will typically require 500+ hours total time, 25+ hours in make/model (difficult — there are almost no US instructors), and a checkout in a Scandinavian or European type club. See GA Insurance Underwriting.