AD/CESSNA 188/18 - Main Landing Gear Leg Attachment Bolts

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B05153 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.