Document ID: chunk:federal_register_of_legislation:F2009L00754:body:0:p2
Version: federal_register_of_legislation:F2009L00754
Segment Type: other
Provision Reference: 
Character Range: 2969–4106

the action detailed in Requirement 1 of this AD is carried out, whichever occurs first.

             Thereafter repeat the inspection at intervals not to exceed 100 hours TIS or 12 months, whichever occurs first.

             For Requirement 4 - Before further flight, after the inspection detailed in Requirement 3 of this AD is carried out and any displacement or damage of clamps or hoses is found.

             For Requirement 5 - From the effective date of this AD.
             This Airworthiness Directive becomes effective on 27 March 2009.
Background:  This FAA has advised of two instances of induction hose disconnection occurring while in service on the air inlet manifold circuit, resulting in a loss of turbo boost and a significant loss of engine power.  The issuing this AD is intended to detect and correct improper intercooler hose assembly installation, which could result in loss of turbo boost and a significant loss of engine power.

             This failure could lead to an inability to maintain constant altitude in flight.

James Coyne
Delegate of the Civil Aviation Safety Authority

26 February 2009