Document ID: chunk:federal_register_of_legislation:F2009L03120:body:0:p2
Version: federal_register_of_legislation:F2009L03120
Segment Type: other
Provision Reference: 
Character Range: 4811–5720

may both interfere with the frame 8 of the aeroplane structure.  A subsequent design review of the oxygen lines routing has confirmed that, on certain aeroplanes, equipped with a 115 cu-ft oxygen cylinder in the RH mid-cabin, may have been installed in such a way as to cause interference with the structure.  This condition, if not corrected, could lead to an oxygen leak.

             As a result, the original issue of this Directive required inspection of the oxygen lines, replacement of any damaged lines and modification of their support assembly.
             This Amendment, whilst continuing the requirements of the original issue, requires compliance in accordance with revision 1 of the service bulletin and revises the applicability.
             The original issue of this Directive became effective on 30 July 2009.

James Coyne
Delegate of the Civil Aviation Safety Authority

30 June 2009