Rotax 912 Series Operator's Manual

2) Operating instructions
Topics in this chapter
2.1 Operating limits (912 A/F/UL)...................................................................2
2.2 Operating limits (912 S/ULS) ...................................................................5
2.3 Operating media-Coolant........................................................................ 8
2.4 Operating media – Fuel...........................................................................9
2.5 Operating media-Lubricants.................................................................. 10
Introduction
The data of the certified engine are based on the type
certificate of type 912 A JAR 22 (TC No. EASA.E.121), 912 F/S
FAR 33 (TC No. E00051 EN), JAR-E (TC No. EASA.E. 121).
This chapter of the Operators Manual contains the operating
limits that must be observed to ensure the ROTAX® aircraft
engine and standard systems operate safely.
Effectivity: 912 Serie
Edition 4 / Rev. 0
BRP-Rotax Page 2-1
November 01/2016

Rotax 912 Series Specifications

General

Redline	5800 rpm
TBO	2000 hours
Displacement	1211 cc
Bore	79.5 mm
Stroke	61 mm
Power Output	80 hp (59.6 kW)
Compression Ratio	9.0:1
Fuel Type	Avgas 100LL
Ignition System	Dual electronic ignition
Fuel System	Fuel Injected
Oil System	Dry sump
Engine Type	4-cylinder, horizontally opposed, 4-stroke