Home>FAA AC 33.14-1:2001

FAA AC 33.14-1:2001

FAA AC 33.14-1:2001 Damage Tolerance For High Energy Turbine Engine Rotors Explains an acceptable means for showing compliance with the requirements of Section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requireme

More details

Download

PDF AVAILABLE FORMATS IMMEDIATE DOWNLOAD
$35.20 tax incl.

$80.00 tax incl.

(price reduced by 56 %)

1000 items in stock

Table of Contents

1PURPOSE
2RELATEDREADINGMATERIAL
3DEFINITIONS
4BACKGROUND
5APPLICABILITY

Abstract

Explains an acceptable means for showing compliance with the requirements of Section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.

Contact us