De Havilland Heron

Airplanes

Length

14.6304 m

Flat Wing Span

21.6408 m

Height

4.572 m

Flat Wing Area

46.3586 m²

Max Seating

Cruise Speed

294.51 km/h

Max Ceiling

5638.8 m

Number of Engines

Aircraft Engine

First Flight

1950-05-10

Entry Into service

1950-01-01

Number Built

149

Maximum Take-Off Weight

6.1235 t (paragliders: kg)

Total Fuel Capacity

1872.989

Maximum Range

1472.55 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
De Havilland Heron	6.1235	1872.989	1472.55

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Blériot 195		14.7	23.2		Compare
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Beechcraft Model 34	Lycoming GSO-580	16.15	21.34	20	Compare
SNCASE SE-1210	Renault 6Q	16.35	21.75		Compare

All data (26 fields)

Name: De Havilland Heron
Manufacturer: De Havilland
Description: The de Havilland DH.114 Heron is a small propeller-driven British airliner that first flew on 10 May 1950.
ICAO Code: HERN
First Flight: 1950-05-10
Entry Into service: 1950-01-01
Designer: De Havilland
Type: Airliner
Length (m): 14.6304
Height (m): 4.572
Max Seating: 14
Cruise Speed (km/h): 294.51
Max Ceiling (m): 5638.8
Rate of Climb (m/s): 5.7912
Capacity Description: 14 passengers
National Origin: United Kingdom
Number Built: 149
Powerplant Description: 4 × de Havilland Gipsy Queen 30 Mk.2 6-cylinder inverted inline air-cooled piston engine, 186 kW (250 hp) each
Primary Users: Garuda Indonesian Airways, See Operators
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/De_Havilland_Heron
Flat Wing Span (m): 21.6408
Flat Wing Area (m²): 46.3586
Wake Category: L
Aircraft Engine: De Havilland Gipsy Queen
Number of Engines: 4