Aviation Safety Network > ASN Aviation Safety Database > Aircraft type index > Short S.45 > Short S.45 Solent specs
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Short S.45 Solent specs
Country: United Kingdom
First flight:11 November 1946
Production ended: 1949
Production total:22
Propulsion:4 piston engines
Maximum number of passengers:34
Maximum take-off mass:35400 kg
ICAO Mass group:4

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