Rotax 912 i series Service Manual

BRP-Rotax
MAINTENANCE MANUAL LINE
Chapter: 04–00–00
AIRWORTHINESS LIMITATIONS
TOPICS IN THIS CHAPTER
Approval
THE AIRWORTHINESS LIMITATIONS SECTION IS APPROVED BY THE EUROPEAN
AVIATION SAFETY AGENCY (EASA) IN ACCORDANCE WITH PART 21A.31(a)(3)
AND FAR 33.4. ANY CHANGE TO MANDATORY REPLACEMENT TIME,
INSPECTION INTERVAL, AND RELATED PROCEDURES CONTAINED IN THIS
AIRWORTHINESS LIMITATIONS SECTION MUST ALSO BE APPROVED.
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Sept. 01
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EASA approved
Introduction This chapter 04-00-00 provides information about “Airworthiness Limitations“.
Airworthiness
Limitations
— NONE
For the ROTAX® engine type 912 i Series the airworthiness limitations are not applicable.
NOTE
Regarding engine operating limitations see the relevant chapter “Limits of
Operation“ in the relevant Operators Manual.
Maintenance checks and replacement of defined components are required on this
engine! These procedures are described in chapter 05 and are required by the
authorities in order to ensure Continued Airworthiness!
See Chapter 05-00-00 Maintenance.
Continued
Airworthiness
Scheduled inspections of the engine including replacement and overhaul of defined
components are required in order to ensure Continued Airworthiness of ROTAX® aircraft
engines.
Effectivity: 912 i Series
Edition 2/Rev. 0
04–00–00
Page 1
September 01/2018

Rotax 912 i series Specifications

General

Number of Cylinders	4
Max Power	100 hp (73.5 kW)
Max Power Output RPM	5800 rpm
Ignition System	Dual electronic ignition
Oil System	Dry sump, forced lubrication with separate oil tank
Reduction Gear Ratio	2.43:1
TBO	2000 hours
Engine Type	4-stroke, horizontally opposed
Displacement	1352 cm³
Bore x Stroke	84 mm x 61 mm
Max Torque	128 Nm
Fuel Type	Avgas 100LL or unleaded automotive gasoline
Fuel System	Electronic fuel injection
Cooling System	Liquid/air-cooled