Rotax 912 iSc Maintenance Manual page 27

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
1 04-00-00 all
This chapter 04-00-00 provides information about "Airworthiness Limita-
Introduction
tions".
- NONE
Airworthiness
Limitations
For the ROTAX type engine 912 i Series the airworthiness limitations are
not applicable.
NOTE:
Scheduled inspections of the engine including replacement and overhaul
Continued Air-
worthiness
of defined components are required in order to ensure the Continued Air-
worthiness of ROTAX aircraft engines.
Effectivity: 912 i Series
Edition 1/Rev. 1
BRP-Powertrain
MAINTENANCE MANUAL
Chapter: 04-00-00
AIRWORTHINESS LIMITATIONS
Approval
date of remark for
change approval
07 01 2012
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.
date of ap-
date of
proval from
issue
authorities
EASA approved
04-00-00
signature
page 1
July 01/2012