AD/M20/10 - Main Landing Gear Retraction Truss - Inspection
1AD/M20/10 - Main Landing Gear Retraction Truss - Inspection
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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/M20/10 Main Landing Gear Retraction Truss - Inspection 9/67
Applicability: All model M20C with S/Nos. 3351 to 3466 and 470001; Model M20E with S/Nos. 1050 to 1308 and 670001, and Model M20F with S/Nos. 660003, 670001 to 670040.
Document: Mooney SB M20-142.
Compliance: Within 100 hours time in service after 7 September 1967.