Document ID: chunk:federal_register_of_legislation:F2008L04265:body:0:p2
Version: federal_register_of_legislation:F2008L04265
Segment Type: other
Provision Reference: 
Character Range: 2900–3669

effective date of this AD whichever occurs first.
             This Airworthiness Directive becomes effective on 3 November 2008.
Background:  This AD is the result of reports of hydraulic leaks from the hydraulic pump pressure output hose assemblies.  The issuing of this AD is intended to prevent leakage of hydraulic fluid from the pump output hose within the engine compartment, which could cause an in-flight fire.

             This AD requires you to inspect hydraulic pump pressure output hose assemblies to determine if they are from the affected lots, inspect for hydraulic fluid leaks if the hose assemblies are from the affected lots, and replace all affected hose assemblies.

James Coyne
Delegate of the Civil Aviation Safety Authority

28 October 2008