Document ID: chunk:federal_register_of_legislation:F2006B11331:body:0
Version: federal_register_of_legislation:F2006B11331
Segment Type: other
Provision Reference: 
Character Range: 0–904

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

 Aerospatiale Rallye Series Aeroplanes

AD/MSR/31 Nose Landing Gear - Yoke Pivot Assembly 5/95

            Applicability: All models, all serial numbers Morane Saulnier and Rallye aeroplanes except Rallye 235F model.

 Requirement: Inspect the yoke pivot assembly for cracks using dye penetrant.

            Inspect in accordance with Socata Service Bulletin 151.

            Note: DGAC AD 93-143(A) refers.

             Compliance: 1. Inspect in accordance with Requirement within 50 hours time in service from 27 April 1995.

            Background: Reports have been received that fatigue cracks could form in the nose landing gear yoke pivot assembly due to a manufacturing defect.

            This AD requires a once only inspection for cracks.