Aviagamma JsCo.


Type Certificate
Russian Type Certificate ST314-AMD
(PDF)



Illustrated parts catalog
Illustrated
parts catalog

for 4-stroke ROTAX Engines
(PDF)


Data sheet
Data sheet
ROTAX 914 (PDF)

Информационный листок
ROTAX has changed TBO up to 2000 hrs for engine ROTAX 914 different versions
(PDF)


Pictures
(click to enlarge)

ROTAX 914 ULS

ROTAX 914 ULS

ROTAX 914 ULS

ROTAX 914 ULS

ROTAX 914 ULS


   www.aviagamma.ru > English version > ROTAX Aircraft Engines > ROTAX 914 UL /F

 
ROTAX 914 UL /F

ROTAX 914
The turbo charged Rotax 914 series offers more performance at high altitudes while keeping weight at a low level. This series offers a time between overhauls of 2.000 hrs and is available as certified (Rotax 914 F) according to FAR 33 and JAR-E and non-certified version (Rotax 914 UL). ROTAX 914 UL and ROTAX 914 F have no any structural differences.

  • 4-cylinder
  • 4-stroke liquid/air-cooled engine with opposed cylinders
  • with turbo charger
  • with automatic waste gate control
  • dry sump forced lubrication with separate oil tank
  • automatic adjustment by hydraulic valve tappet
  • 2 carburetors
  • dual electronic ignition
  • electric starter
  • propeller speed reduction unit
  • engine mount assembly

TBO — 2000 hours or 15 years of operation.

Warranty service life — 100 operating hours or 6 months after the first run, or 1 year from the date of purchase.

In the Russian Federation ROTAX 914 engine is certified as a type (Type Certificate №-ST314 AMD).

* Picture: 914 UL 3 DCDI with options.

Engine data / Perfomance
BORE: 79.5 mm
STROKE: 61 mm
DISPLACEMENT: 1211.2 cm3
PERFORMANCE: 84.5 KW (115 hp) at 5800 1/min
TORQUE: 144 Nm at 4900  1/min
MAX RPM: 5800 1/min

WEIGHT

engine with propeller speed reduction unit i = 2.43: 64 kg
overload clutch 1.7 kg
exhaust system 4.0 kg
engine mount assembly 2.0 kg
external alternator 3.0 kg

Engine perfomance

Engine torque

Fuel consumption

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