AD/M20/38 - Fuselage Tubular Structure - Modification
1AD/M20/38 - Fuselage Tubular Structure - Modification
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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 Mooney M20 Series Aeroplanes
AD/M20/38 Fuselage Tubular Structure - Modification 2/80
Applicability: All model M20K with S/Nos. 25-0001 to 25-0247. Document: Mooney SB No. M20-220.
Compliance: Before 1 July 1980.
Background: The manufacturer advises of the possibility of the lower fuselage longeron buckling under severe positive gust conditions.