AD/LEARJET 35/29 - Retirement Life - Fatigue Critical Components
1AD/LEARJET 35/29 - Retirement Life - Fatigue Critical Components
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/LEARJET 35/29 - Retirement Life - Fatigue Critical Components.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Gates Learjet 35 and 36 Series Aeroplanes
AD/LEARJET 35/29 Retirement Life - Fatigue Critical Components
Applicability: All Learjet 35 & 36 series aeroplanes.
7/95
Requirement: Retire from service, at or before the times specified therein, all components listed in the Learjet 35 & 36 series Maintenance Manual, Revision 61, Chapter 5, Section
5-11-00.
Compliance: This Directive is effective 22 June 1995.
Background: This Directive reflects the manufacturer’s mandatory retirement life schedule for fatigue critical components.