Document ID: chunk:federal_register_of_legislation:F2006B04918:body:0
Version: federal_register_of_legislation:F2006B04918
Segment Type: other
Provision Reference: 
Character Range: 0–944

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

 Cessna 150, F150, 152 & F152 Series Aeroplanes

 AD/CESSNA 150/2
 Amdt 1

 Main Undercarriage "U" Bolts 11/67

 Applicability: All models fitted with "U" bolts P/N 0441161 types.

             Requirement: 1. Visual: Inspect the main undercarriage "U" bolts P/N 0441161 in situ for cracks and other damage and check that the "U" bolt retaining nuts are torqued to the values specified in the Cessna Service Manual.

             2. Magnetic Particle: Remove the main undercarriage "U" bolts P/N 0441161 and inspect by the magnetic particle method for cracks particularly in the radius of the bends and in the root of the threads.

 Compliance: Visual: At intervals not exceeding 100 hours time in service.

            Magnetic Particle: At intervals not exceeding 500 hours time in service.