Document ID: chunk:federal_register_of_legislation:F2009L00214:body:0:p2
Version: federal_register_of_legislation:F2009L00214
Segment Type: other
Provision Reference: 
Character Range: 3077–3720

21 January 2008. They are obtained by modifying (reworking) older P/N LPT frames.

             Before the issue of the CFM56-7B Engine Shop Manual (ESM) Temporary Revisions (TR) 05-0097, 05-0098, and 05-0099 on September 19, 2008, the concerned LPT rear frames were neither subject to a life limit nor to a mandatory inspection.

             This AD is issued to make sure that all operators are informed about the Low Cycle Fatigue (LCF) life limits or mandatory inspections affecting these new P/N and revise their aircraft maintenance programs accordingly.

James Coyne
Delegate of the Civil Aviation Safety Authority

23 January 2009