Scheibe SF-25 Falke Civil Aircraft Model Details

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General Information of Scheibe SF-25 Falke

Developed From : Scheibe Mu-13 E

First Flight : 1963

Manufacturer : Scheibe Aircraft GmbH

National Origin : West Germany

Number Built : 1,200+ by October 1998

Role : Motor Glider

General characteristics of Scheibe SF-25 Falke

Crew : 2

Empty Weight : 435 kg (959 lb)

Fuel Capacity : 55 L (14.5 UG gal, 12.0 Imp gal) standard

Height : 1.68 m (5 ft 6 in) tailwheel undercarriage

Length : 7.60 m (24 ft 11 in)

Max Takeoff Weight : 650 kg (1,433 lb)

Powerplant : 1 × Rotax 512 A flat-4, aircooled with water cooled cylinder heads, 48 kW (65 hp)

Propellers : 2-bladed

Wing Area : 18.20 m2 (195.9 sq ft)

Wingspan : 15.30 m (50 ft 2 in)

Performance of Scheibe SF-25 Falke

Cruise Speed : 180km/h (112mph; 97kn) maximum

Maximum Glide Ratio : 23-24

Maximum Speed : 190km/h (118mph; 103kn)

Range : 700km (435mi; 378nmi)

Rate Of Sink : 1.0m/s (200ft/min) minimum

Service Ceiling : 4,580m (15,026ft) (more than)

Stall Speed : 65km/h (40mph; 35kn)

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