Document ID: chunk:federal_register_of_legislation:F2009L02864:body:0:p2
Version: federal_register_of_legislation:F2009L02864
Segment Type: other
Provision Reference: 
Character Range: 3439–4280

AD.

             Note:  FAA AD 98-06-25 Amdt 39-10403 refers.
Compliance:     1. Within 500 hours time in service after 18 June 1998.

                2. Before further flight.

                3. Within 500 hours time in service after accomplishment of the Requirement 1 inspection.
             This Amendment becomes effective on 30 July 2009.
Background:  This AD is amended to reference relationship between this AD and cancelled AD/SWSA226/37.

             The FAA requires certain actions as a result of a decompression incident during flight caused by fatigue at the bottom of the cargo door on a Model SA226-TC.  Failure of the cargo door in flight could cause decompression injury to passengers and substantial structural damage to the aircraft.

David Villiers
Delegate of the Civil Aviation Safety Authority

17 June 2009