AD/MU-2/10 Amdt 1 - Flap Control System Flexible Shafts - Inspection

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Legislation au F2006B11338 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

 


Mitsubishi MU-2 Series Aeroplanes

 

AD/MU-2/10

Amdt 1


Flap Control System Flexible Shafts - Inspection 12/84

 

Applicability: All models MU-2B aircraft referred to in the requirement document. Document: Mitsubishi MU-2 S.B. No. 162 Rev. A.

Compliance: At intervals not exceeding 100 hours time in service after 28 February 1975.

 

Background:  This directive is amended to clarify the aircraft applicability and amend the revision status of the requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.