AD/BEECH 23/29 Amdt 2 - Wing Main Spar Corrosion
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
View image in the official source 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.