AD/CESSNA 188/18 - Main Landing Gear Leg Attachment Bolts
1AD/CESSNA 188/18 - Main Landing Gear Leg Attachment Bolts
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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 Cessna 188 (Agwagon) Series Aeroplanes
AD/CESSNA 188/18 Main Landing Gear Leg Attachment Bolts 11/72
Applicability: All models.
Requirement: Inspect the inboard main landing gear to fuselage attachment bolts to ensure they are of NAS 152-88 type and are torqued to the correct value.
Compliance: Within 100 hours time in service after 30 November 1972 and thereafter at intervals not exceeding 100 hours time in service.