AD/BEECH 23/29 Amdt 2 - Wing Main Spar Corrosion
1AD/BEECH 23/29 Amdt 2 - Wing Main 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 Beechcraft 19, 23 and 24 Series Aeroplanes
AD/BEECH 23/29
Amdt 2
Wing Main Spar Corrosion 12/86
Applicability: All 19, 23 and 24 series.
Requirement: Action in accordance with Beechcraft SI No. 0824-035 Rev. II.
Compliance: Prior to the issue of the next Maintenance Release after 31 December 1986 and thereafter at intervals not exceeding 12 months.
Background: A history of Major Defect Reports has warranted an increase in the periodicity of this Directive to that originally called up by Beech.