1954 DEHAVILLAND DH-114

General Specs (cont.)

Total Time:21000

Engine 1 Time:896 SMOH

Engine 2 Time:1140 SMOH

Prop 1 Time:365 SPOH

Prop 2 Time:365 SPOH

Condition:Used

Flight Rules:BTH

# of Seats:16

Additional Classifications

Antique/Classic

Utility

Warbird

Detailed Description

Single Pilot Certified, No type rating required, 12,499 lbs Max Gross Weight, 16 Passenger seats and picture windows, Passenger seats are quickly changeable for executive seating or spacing. US registered. Currently hangared in Sweden.  Can be ferried worldwide.

Avionics / Equipment

Trig VHF
ADS-B Transponder
LOC / Glideslope

Airframe

21000 hrs TTSN

Engines / Mods / Prop

Lycoming IO-540
This Heron is a conversion to American engines. This conversion made the aircraft a real winner. Faster and much more reliable than the old Gypsy engines. These engines run and run and run without problems
Engine #1 - 896 SMOH
Engine #2 - 1,140 SMOH
Engine #3 - 1,654 SMOH
Engine #4 - 864 SMOH
All compression 70 or better
TBO is 2,000

Interior / Exterior

16 Passenger seats and picture windows
Passenger seats are quickly changeable for executive seating or spacing

Remarks

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.
A number of Herons were fitted with 290 hp (216 kW) Lycoming IO-540 flat-six piston engines.The modifications were carried out by the Riley Turbostream Corporation of the USA.
The DH-114 Heron served with several European countries with both the military and airlines as well as Australia and globally.