Document ID: chunk:federal_register_of_legislation:F2006B07625:body:0
Version: federal_register_of_legislation:F2006B07625
Segment Type: other
Provision Reference: 
Character Range: 0–698

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Morovan Zlin Z 526 Series Aeroplanes

AD/Z 526/2 Main Wing Spar Corrosion 11/96

 Applicability: All models Z 526 aircraft.

 Requirement: Inspect in accordance with Morovan Mandatory Service Bulletin Z 526/69a.

            Note: Czech CAI AD 2-016/96 refers.

 Compliance: Before 10 November 1996, and thereafter at intervals not to exceed 12 months.

            Background:  The Czech civil aviation authority received reports of exfoliation corrosion on the main wing spar flanges which seriously degraded the structural strength of the wing.