AD/MU-2/37 - Flap Flexible Shaft Sealing and Torque Check

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

Legislation au F2006B11367 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-2/37 Flap Flexible Shaft Sealing and Torque Check 12/85

Applicability: All models MU-2B/-10/-15/-20/-25/-26 with S/Nos. 008 to 347 except S/Nos. 313 and 321. All models MU-2B-30/-35/- 36 with S/Nos.501 to 696 except S/Nos. 652

and 661.

 

Requirement: Action in accordance with Mitsubishi SB No. 198.

 

Note: JCAB AD No. TCD-2451-85 refers.

 

Compliance: At the next scheduled inspection for Maintenance Release issue after 31 December 1985.

 

Background: The manufacturer reports failures of the flexible drive shaft attributable to ingress of moisture.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.