Aircraft > Multi-Engine Piston > DeHavilland > N415SA: DeHavilland DH-114
N415SA: DeHavilland DH-114
Last Updated
Feb. 15, 2023
Details
Registration #
N415SA
Status
Off Market
Year
1954
Make
DeHavilland
Model
DH-114
Serial Number
14064
TTAF
21000
Engine 1 Time
896
Engine 2 Time
1140
Flight Rules
IFR
Location
Stockholm SWE
Price History
Dec. 15, 2022
249,000
Listings
Site
Price
Status
Updated
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
Trig VHF ADS-B Transponder LOC / Glideslope
Airframe
21000 hrs TTSN
Engines / Mods
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.