Effective Date: July 16, 2007.
Affected ADs: Supersedes AD 88-08-02, Amendment 39-5889. NOTE: This AD applies to our DHC-2 aircraft in the AK Wing. Reason: The mandatory continuing airworthiness information (MCAI) states: A report has been received of stress corrosion cracking occurring in the wing left strut lower clevis fitting, part number C2W-1097A. See AD for affected aircraft.