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BLERIOT-SPAD S.50 Civil Aircraft Model Details

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Our dedication to quality does not end there, as every part of civil aircraft model BLERIOT-SPAD S.50 is subjected to rigorous quality assurance testing by our expert team to ensure our customers only receive the best. If you are ready for a competitive quote, submit an RFQ today and a dedicated account manager will be in touch.

General Information of BLERIOT-SPAD S.50
First Flight : 12 December, 1920

Manufacturer : BlEriot

Number Built : ca. 41

Primary Users : Franco-Roumaine, CMA; SNETA

Role : Airliner

Variants : BlEriot-SPAD S.46

General characteristics of BLERIOT-SPAD S.50
Capacity : 5 passengers

Crew : one pilot

Empty Weight : 1,050 kg (2,315 lb)

Gross Weight : 2,062 kg (4,546 lb)

Height : 3.20 m (10 ft 6 in)

Length : 9.08 m (29 ft 10 in)

Powerplant : 1 × Salmson CM.9 water-cooled radial engine, 194 kW (260 hp)

Wing Area : 42.2 m2 (454 ft2)

Wingspan : 11.66 m (38 ft 3 in)

Performance of BLERIOT-SPAD S.50
Cruise Speed : 160 km/h (100 mph)

Maximum Speed : 180 km/h (112 mph)

Range : 1,060 km (670 miles)

Service Ceiling : 3,800 m (12,470 ft)

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