Aircraft Alternator
Maintenance Manual
ES1031
24-30-01
Rev. B: 20 Apr. 2022
Page: A-1
© 2022 - Hartzell Engine Technologies - All rights reserved
Revision Number Description of Revision
Airworthiness Limitation Revisions Log
AIRWORTHINESS LIMITATIONS
A.1 General Information
CAUTION:
THE AIRWORTHINESS LIMITATIONS HEREIN ARE THOSE MANDATED BY
HARTZELL ENGINE TECHNOLOGIES. THESE LIMITATIONS ARE THE MINIMUM
REQUIRED TO MEET CONTINUED AIRWORTHINESS BUT MAY BE SUPERSEDED
BY MORE STRINGENT REQUIREMENTS AS PUBLISHED BY THE FAA, AIRCRAFT,
ROTORCRAFT OR OTHER MANUFACTURERS THAT USE THESE COMPONENTS
IN THEIR APPLICATIONS. FAILURE TO OBSERVE THESE LIMITATIONS MAY
COMPROMISE THE COMPONENT OR THE APPLICATION IT IS USED IN.
A.2 Airworthiness Limitations Statement
A.
The Airworthiness Limitations section is FAA accepted and specifies maintenance required under
§ 43.16 and § 91.403 of the Federal Aviation Regulations unless an alternative program has been
FAA approved.
AIRW
OR
THINESS
LIMIT
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TIONS
