Aviation Safety Network > ASN Aviation Safety Database > Aircraft type index > HS-125 > Hawker Siddeley HS-125 Srs. 1, 2, 3, 400 specs
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Hawker Siddeley HS-125 Srs. 1, 2, 3, 400 specs
 
Manufacturer:Hawker Siddeley Aviation
Country: United Kingdom
First flight:9 January 1962
Production ended: 19..
Production total:290
Series: Series 1: First version, powered by Viper 20 or 520 engines
Series 1A: Upgraded Series 1 with Bristol Siddeley Viper 521 or 522 engines
Series 3A/B: Viper 522-powered variant with increased MTOW
Series 400A/B: Increased weights; addition of a outward-opening main entry door
Propulsion:2 jet engines
Maximum number of passengers:8
Maximum take-off mass:10795 kg
ICAO Mass group:3

Hawker Siddeley HS-125 Srs. 1, 2, 3, 400 photo

Hawker Siddeley HS-125 Srs. 1, 2, 3, 400 file photo (photo: Aviation Safety Network archives)

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