Rotax 914 UL F Aircraft Engines

• Customization: Available
• Transport Package: Box
• Origin: China
• Model NO.: Rotax 914 UL F

Product Description

Product Description

Rotax 914 UL | F Aircraft Engines

 

Engine Data

WEIGHT	kg	lb
Engine with propeller speed reduction gearbox i = 2.43	64.0	140.8
Exhaust system	4.0	8.8
Engine suspension frame	2.0	3.7
Overload clutch	1.7	3.7
External alternator	3.0	6.6

PERFORMANCE
84.8 kW	115	5800 1/min

TORQUE
144 Nm	106 ft. lb.	4900 1/min

Max RPM

5800 1/min

BORE
79.5 mm	3.13 in

STROKE
61.0 mm	2.4 in

DISPLACEMENT
1211.2 cm³	73.91 cu in

FUEL*

min. MON 85 RON 95* min AKI 91*

Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.

* leaded, unleaded, AVGAS 100LL, Ethanol 10
** max. continuous power at 5500 1/min
*** MOGAS, no hydraulic governor
 

Low-weight engine with excellent performance at high altitudes.

• Four-stroke piston engine with four liquid and air-cooled cylinders
• Turbocharger
• Automatic wastegate 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 hrsCheck at every level: from production to testing
  one-stop service
  material selection→manufacturing→transportation→export→after-sales
  ATTENTION:
  1. You must know before buying the product: If you don't understand, consult before buying:
  2. Before buying the product, you must determine the needs, configuration, and cabinet requirements:
  3. For the transportation of special large items, please consult the freight instructions, and consult the customer service in advance for invoice requirements
  4. Customer-exclusive customized products do not support return and exchange services, regular stock is confirmed