AD/Z 526/2 - Main Wing Spar Corrosion
1AD/Z 526/2 - Main Wing Spar Corrosion
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.