AD/MU-2/9 - Trim Aileron Bellcrank Bracket Bolt Holes - Inspection

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

Legislation au F2006B11403 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

 


Mitsubishi MU-2 Series Aeroplanes

 

AD/MU-2/9 Trim Aileron Bellcrank Bracket Bolt Holes - Inspection

Applicability: As detailed in the requirement document. Document: Mitsubishi SB No. 164.

Compliance: Within 50 hours time in service after 28 June 1974.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


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