Document ID: chunk:federal_register_of_legislation:F2005L03142:body:0:p2
Version: federal_register_of_legislation:F2005L03142
Segment Type: other
Provision Reference: 
Character Range: 2642–3256

of this AD.

                   3. After the effective date of this AD.
                This Airworthiness Directive becomes effective on 24 November 2005.

Background:  This AD results from reports that certain JT8D critical life-limited rotating parts have been returned to service with cracks, corrosion pitting, or dimensions outside of manual limits.  This AD is intended to prevent failure of critical life-limited rotating engine parts, which could result in an uncontained engine failure and damage to the aeroplane.

Jayaprakashan Ambali
Delegate of the Civil Aviation Safety Authority

7 October 2005