DE HAVILLAND DH.114 HERON Civil Aircraft Model Details

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General Information of DE HAVILLAND DH.114 HERON

Developed From : DH.104 Dove

First Flight : 18393

Introduction : 1950

Manufacturer : de Havilland

Number Built : 150

Primary Users : Garuda Indonesian Airways; Prinair; See Operators

Role : Airliner

Status : retired

Variants : Saunders ST-27

General characteristics of DE HAVILLAND DH.114 HERON

Capacity : 14 passengers

Crew : two (pilot and co-pilot)

Empty Weight : 8,150 lb (3,705 kg)

Height : 15 ft 7 in (4.75 m)

Length : 48 ft 6 in (14.79 m)

Max Takeoff Weight : 13,500 lb (6,136 kg)

Powerplant : 4 × de Havilland Gipsy Queen 30 Mk.2 6-cylinder inverted inline air-cooled piston engine, 250 hp (186 kW) each

Wing Area : 499 ft² (46.4 m²)

Wingspan : 71 ft 6 in (21.80 m)

Performance of DE HAVILLAND DH.114 HERON

Cruise Speed : 159kn(183 mph, 295 km/h)

Range : 795nmi(915 mi, 1,473 km)

Rate Of Climb : 1,140 ft/min (5.8 m/s)

Service Ceiling : 18,500 ft (5,600 m)

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