Document ID: chunk:federal_register_of_legislation:F2007L02127:body:0:p2
Version: federal_register_of_legislation:F2007L02127
Segment Type: other
Provision Reference: 
Character Range: 3644–4750

series engines, use paragraphs 3.A. through 3.C.(1)(b)2, of GE SB No. CF6-80E1 S/B 73-0075, Revision 1, dated 27 November 2006, to do the replacements.

             This AD requires no further action if the fuel shroud retaining snap rings were installed in the CF6-80C2 series engines before the effective date of this AD using GE SB No. CF6-80C2 S/B 73-0337, Revision 2, dated 11 January 2007; Revision 1, dated 19 April 2005; or the Original, dated 30 November 2004.

             Note 3:  FAA AD 2007-11-20 Amdt 39-15077 dated 24 May 2007 refers.
Compliance:  At the next engine shop visit for any reason after the effective date of this AD, unless the actions have already been done.
             This Airworthiness Directive becomes effective on 2 August 2007.
Background:  This AD results from two events of external engine fuel leakage and a subsequent under-cowl engine fire.  The issuing of this AD is intended to prevent an under-cowl engine fire and damage to the aeroplane during an engine high vibration event.

David Punshon
Delegate of the Civil Aviation Safety Authority

12 June 2007