AD/M20/11 - Main Landing Gear Retraction Truss - Modification
1AD/M20/11 - Main Landing Gear Retraction Truss - 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/M20/11 Main Landing Gear Retraction Truss - Modification 9/67
Applicability: All model M20C with S/Nos. 2807 to 3466 and Model M20E with S/Nos. 470 to 1270.
Document: Mooney SB M20-143.
Compliance: Within 100 hours time in service after 7 September 1967.