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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Jan. 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 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
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 Series
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January 01 2020
