Description
The Slepcev Storch ultralight version is a 3/4 scale replica of the Second World War Fieseler Fi 156.
The Slepcev Storch (English: Stork) is a Serbian ultralight STOL aircraft, designed by Yugoslavian-Australian Nestor Slepcev.
Design and development
The aircraft was first flown in 1994. It was originally manufactured by Slepcev’s company, Slepcev Aircraft Industry of Beechwood, New South Wales, Australia. The company was later renamed Storch Aviation Australia. The aircraft was type-certified in 1999 to the Joint Airworthiness Requirements – Very Light Aircraft (JAR-VLA) standard, with contributions from aeronautical engineer C. W. “Bill” Whitney. Production then moved to Serbia where a Fédération Aéronautique Internationale microlight category model was developed.
Like the original Fi 156, the Slepcev Storch features a strut-braced high-wing, a two-seats-in-tandem enclosed cockpit, with extensive glazing, fixed conventional landing gear and a single engine in tractor configuration. It is made from welded steel tubing with its flying surfaces fashioned from sheet aluminium and covered in doped aircraft fabric. The ultralight version has a 10 m (32.8 ft) span wing with an area of 15 m2 (160 sq ft), large flaps and leading edge slots. The wings are supported by V-struts and jury struts. Engines fitted vary by model.
Operational history
The designer has a keen interest in Second World War history and wanted to use an example of his Storch design to re-enact the 12 September 1943 rescue of Benito Mussolini by Otto Skorzeny and his SS commandos from his imprisonment by Italian partisans on the Gran Sasso mountain. It took Slepcev a year to gain Italian approvals for the flight and on 24 August 1996, he landed a Storch Mk 4 at the site, 53 years after the original dramatic rescue had taken place.
General characteristics
Crew: one
Capacity: one passenger
Wingspan: 10 m (32 ft 10 in)
Wing area: 15 m2 (160 sq ft)
Gross weight: 450 kg (992 lb)
Fuel capacity: 40 litres (8.8 imp gal; 11 US gal)
Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
Performance
Maximum speed: 150 km/h (93 mph; 81 kn)
Cruise speed: 133 km/h (83 mph; 72 kn)
Stall speed: 40 km/h (25 mph; 22 kn)
Rate of climb: 6 m/s (1,200 ft/min)
