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

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

Legislation au F2006B11331 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.