Aircraft Alternator
Maintenance Manual
A.1
General Information
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REQUIRED TO MEET CONTINUED AIRWORTHINESS BUT MAY BE SUPERSEDED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.
Revision Number
ES1031
Rev. A: 11 Aug. 2021
AIRWORTHINESS LIMITATIONS
CAUTION:
Airworthiness Limitation Revisions Log
Description of Revision
© 2021 - Hartzell Engine Technologies - All rights reserved
24-30-01
Page: A-1