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914 UL | F

Product catalog summary

Overview: The document provides technical specifications and features of the Rotax 914 UL | F engine, emphasizing its power-to-weight ratio and reliability for aviation use.

Specifications:

Power Output: 115 HP (84.5 kW) at 5800 RPM.
Torque: 144 Nm (106 ft. lb.) at 4900 RPM.
Engine Type: 4-cylinder, 4-stroke liquid-/air-cooled with opposed cylinders.
Displacement: 1211.2 cm³ (73.91 cu in).
Fuel Compatibility: Leaded, unleaded, AVGAS 100LL, Ethanol 10, with minimum MON 85 RON 95 and AKI 91.
Weight: Total engine weight with components is approximately 75.5 kg (166.4 lb).

Key Features:

Turbocharger with automatic waste gate control for enhanced performance at high altitudes.
Dual electronic ignition and electric starter for reliability and ease of use.
Propeller speed reduction gearbox and engine mount assembly included.
Dry sump forced lubrication with separate oil tank and automatic adjustment by hydraulic valve tappet.
Two carburetors for efficient fuel management.
Exhaust system and air intake system designed for optimal performance.
Time Between Overhaul (TBO): 2,000 hours.

Certifications:

UL: ASTM compliant.
F: Certified according to FAR33 and JAR-E standards.

Conclusion: The Rotax 914 UL | F engine is designed for high performance and reliability, suitable for aviation applications requiring a lightweight and powerful engine. It is compliant with international standards and offers advanced features for enhanced operational efficiency.

Catalog excerpts

POWER MEETS RELIABILITY. The ultimate flight experience with the best power-to-weight ratio and reliability.

Open the catalog to page 1

Rotax 914 UL with options, delivery state Turbo charged low weight engine with more performance on high altitudes. Engine with propeller speed reduction gearbox i = 2.43 4-cylinder 4-stroke liquid-/air-cooled engine with opposed cylinders Turbo charger 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 gearbox Engine mount assembly Air intake system Exhaust system TBO 2,000 hrs Exhaust system Overload clutch Engine suspension frame External...

Open the catalog to page 2

All Rotax Aircraft Engines catalogs and technical brochures

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