Rotax 914 series Installation Manual

Effectivity: 914 Series
Edition 2 / Rev. 0
d04275
page 23
July 01/2008
BRP-Rotax
INSTALLATION MANUAL
Following equipment has not been tested for safety and durability to the
standards of aviation.
▲ WARNING: The user assumes all risks possibly arising by utilizing auxiliary
equipment.
The furnishing of proof in accordance to the latest FAR or EASA has
to be conducted by the aircraft manufacturer.
- intake filter
- Flydat
- mechanical tachometer
- electric tachometer
- shock mount
- oil hose

Rotax 914 series Specifications

General

Bore	79.5 mm
Stroke	61 mm
Compression Ratio	9.0:1
Cooling System	Liquid-cooled cylinder heads, air-cooled cylinders
Redline	5800 rpm
Engine Type	4-cylinder, 4-stroke
Fuel Type	Avgas 100LL
Oil System	Dry sump
Fuel System	fuel injection
TBO (Time Between Overhauls)	2000 hours
Displacement	1.211 liters (1211 cc)
Power Output	84.6 kW (115 hp) at 5, 800 rpm