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MAINTENANCE MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 1
04-00-00
page 1
July 01/2012
Chapter: 04-00-00
AIRWORTHINESS LIMITATIONS
Introduction
This chapter 04-00-00 provides information about “Airworthiness Limita-
tions“.
Airworthiness
Limitations
- NONE
For the ROTAX type engine 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 descriped in
chapter 05 and are a required by the authority in order to ensure
the Continued Airworthiness!
See chapt. 05-00-00.
Continued Air-
worthiness
Scheduled inspections of the engine including replacement and overhaul
of defined components are required in order to ensure the Continued Air-
worthiness of ROTAX aircraft engines.
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 EACH
MANDATORY REPLACEMENT TIME, INSPECTION INTERVAL, AND
RELATED PROCEDURE CONTAINED IN THIS AIRWORTHINESS
LIMITATIONS SECTION MUST ALSO BE APPROVED.
no.
chapter
page
date of
change
remark for
approval
date of ap-
proval from
authorities
date of
issue
signature
1
04-00-00
all
07 01 2012
EASA approved
Summary of Contents for 912 iS Sport
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