The de Havilland DH.54 Highclere was a single-engined biplane airliner designed to replace the DH.34, built to Air Ministry specification 40/22 as a larger version of that successful aircraft. Compared with the DH.34 its passenger complement rose from nine to twelve, its all-up weight by 56 percent and its wing area by 70 percent, and full-span flaps were fitted in response to criticism of the earlier type's high landing speed. For safety over water the undercarriage could be jettisoned and the fuselage was watertight. A 650 hp Rolls-Royce Condor IIIA engine drove a four-bladed propeller. It was first flown by H.S. Broad on 18 June 1925 and received its certificate of airworthiness on 23 April 1926, but Imperial Airways had decided to carry passengers only in multi-engined types. The sole aircraft was used for experimental work and as a freighter before a hangar collapsed on it in heavy snow at Croydon on 1 February 1927.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineRolls-Royce Condor IIIA water-cooled inline 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source De Havilland DH.54 Highclere (Wikipedia)
Of Make
Source De Havilland DH.54 Highclere (Wikipedia)
Sources
1. De Havilland DH.54 Highclere (Wikipedia)
Operational history
The Highclere was first flown by H.S. Broad on 18 June 1925
Description
so the Highclere used a 650 hp (485 kW) Rolls-Royce Condor IIIA water-cooled inline engine
Specifications, empty weight
Empty weight: 6,768 lb (3,070 kg)
Specifications, maximum weight
Gross weight: 11,250 lb (5,103 kg)
Specifications, maximum speed
Maximum speed: 110 mph (177 km/h, 96 kn)
Operational history, units built
the sole Highclere was transferred to RAE Farnborough on 7 March 1926 for experimental work
Lead
The de Havilland DH.54 Highclere was a single-engined 15-passenger biplane airliner designed to replace the DH.34.
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