Document ID: chunk:federal_register_of_legislation:F2009L03433:body:0:p4
Version: federal_register_of_legislation:F2009L03433
Segment Type: other
Provision Reference: 
Character Range: 9935–10912

FAA AD retained the initial inspection compliance of 'within 250 hours time in service after 28 August 2008' and also allowed credit for inspections accomplished in accordance with the superseded Directives.
             The original issue of this Directive was issued to detect and correct chafing of electrical wires, components, and tube assemblies.  This condition, if not corrected, could result in arcing of exposed wires with consequent burning of a hole in a hydraulic line or the bleed air line.  This failure could lead to a hydraulic fluid leak and a possible fire in the engine nacelle compartment.
             This Amendment continues the requirements of the original issue but corrects a typographical error in the Applicability Statement by correctly identifying a
             SA226-TC model aeroplane.

   The original issue of this Directive became effective on 30 July 2009.

James Coyne
Delegate of the Civil Aviation Safety Authority

14 August 2009