Document ID: chunk:federal_register_of_legislation:F2009L00221:body:0:p2
Version: federal_register_of_legislation:F2009L00221
Segment Type: other
Provision Reference: 
Character Range: 2878–3401

to include a replacement of the rail pressure control valve.  Failure of this part could result in in-flight shut down(s) of the engine(s).

             This AD requires replacement of the rail pressure control valve, modification of the VRail Plug and the implementation of the instructions, limitations, inspections and corrective measures, as specified in TAE SB TM 125-1008 P1 and in issue 1 revision 2 of the chapter 5 of the OM-02-02.

James Coyne
Delegate of the Civil Aviation Safety Authority

22 December 2008