Document ID: chunk:federal_register_of_legislation:F2005L00193:body:0:p2
Version: federal_register_of_legislation:F2005L00193
Segment Type: other
Provision Reference: 
Character Range: 3380–4695

at 55-hour intervals TIS, or 6 months since the previous torque check inspection, whichever occurs first, until the accumulation of 110 hours TIS since the inspection with the torque remaining within the SB specifications.

                   3. Repetitively, at 55 hours intervals TIS, after satisfying the requirement 2.

                Note 3:  Replacement of a rotary fuel pump series RG9080, RG9570, or RG17980, with an unmodified pump (without the "/M" after the part number) requires repeating the initial and follow-up inspections in accordance with the requirement 1, 2 and 3 of this Directive.
                This Amendment becomes effective on 17 March 2005.
Background:     The amendment 1 is issued in response to a review of an AD application. The application requested an inspection interval of 55 hours or 10% tolerance.

                The actions specified by this AD are intended to prevent rotary fuel pump leaks, which could result in an engine failure, engine fire, and damage to or loss of aircraft.

                The original issue of this AD is based on FAA AD 2003-14-03 and supersedes CASA AD/FSM/25 Amendment 4.

   The original issue of this Directive became effective on 17 February 2005.

James Coyne
Delegate of the Civil Aviation Safety Authority

4 February 2005