AD/BEECH 18/22 - Main Landing Gear Drag Legs, Drag Leg Bolts and Retract Slide Assemblies - Inspection
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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 18 Series Aeroplanes
AD/BEECH 18/22 Main Landing Gear Drag Legs, Drag Leg Bolts
and Retract Slide Assemblies - Inspection
Applicability: All models D18S, E18S, E18S-9700, G18S & H18 with S/Nos. referenced in
12/81
Beechcraft Service Instruction No. 1183 or with S/Nos. referenced in subsequent issues of that service instruction.
Document: Beechcraft SI No. 1183. Compliance: As per requirement document.
Background: The manufacturer advises of the possibility of cracks or corrosion developing in the M.LG. drag legs, drag leg bolts and retract slide assemblies.
Federal Register of Legislative Instruments F2006B03621