Rotax 915 i A SERIES Maintenance Manual page 29

TOPICS IN THIS CHAPTER
THE AIRWORTHINESS LIMITATIONS SECTION IS APPROVED BY THE EUROPEAN
no.
Introduction This chapter 04-00-00 provides information about "Airworthiness Limitations".
Airworthiness — NONE
Limitations
For the ROTAX® engine type 915 i A Series the airworthiness limitations are not
applicable.
N N O O T T E E
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 Scheduled inspections of the engine including replacement and overhaul of defined
Airworthiness components are required in order to ensure Continued Airworthiness of ROTAX® aircraft
engines.
Effectivity: 915 i A Series
Edition 0/Rev. 0
MAINTENANCE MANUAL
Chapter: 04–00–00
AIRWORTHINESS LIMITATIONS
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.
page
chapter
1 04–00–00 all
Chapter 05-00-00
BRP-Rotax
Approval
remark
date of
for
change
approval
Dec. 01
2017
Maintenance.
date of
approval
date of
from
issue
authori-
ties
EASA approved
04–00–00
December 01 2017
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