Activation Group 1 for landing gear and Activation Group 2 for flaps.
The de Havilland DH.114 Heron was a small propeller-driven British airliner that first flew on 10 May 1950. It was a development of the twin-engine de Havilland Dove, with a stretched fuselage and two more engines. It was designed as a rugged, conventional low-wing monoplane with tricycle undercarriage that could be used on regional and commuter routes. 150 were built, exported to around 30 countries. Herons later formed the basis for various conversions, such as the Riley Turbo Skyliner and the Saunders ST-27 and ST-28.
Specifications
General Characteristics
- Created On iOS
- Wingspan 156.4ft (47.7m)
- Length 112.4ft (34.3m)
- Height 31.7ft (9.7m)
- Empty Weight 9,777lbs (4,434kg)
- Loaded Weight 82,394lbs (37,373kg)
Performance
- Horse Power/Weight Ratio 0.097
- Wing Loading 27.3lbs/ft2 (133.2kg/m2)
- Wing Area 3,020.0ft2 (280.6m2)
- Drag Points 34684
Parts
- Number of Parts 243
- Control Surfaces 7
- Performance Cost 878
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