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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
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 Series the airworthiness limitations are
not applicable.
NOTES:
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 Series
Edition 2 / Rev. 1
BRP-Powertrain
MAINTENANCE MANUAL
Chapter: 04-00-00
AIRWORTHINESS LIMITATIONS
Approval
SECTION MUST ALSO BE APPROVED.
date of
remark for
change
approval
07 01 2010
Regarding engine operating limitations see the relevant
chapter "limits of operation" in the relevant Operators Man-
ual.
Maintenance checks and replacement of defined compon-
ents 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 chap. 05-00-00.
EASA approved
date of ap-
date of
proval from
issue
authorities
EASA approved
04-00-00
signature
page 1
July 01/2010
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