AD/MU-2/34 - Engine Air Intake Bleed Air Tubing Coupling Nut Retorque, Inspection, Modification

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Legislation au F2006B11364 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-2/34 Engine Air Intake Bleed Air Tubing Coupling Nut

Retorque, Inspection, Modification


7/84

 

Applicability: All models MU-2B/-10/-15/-20/-25/-26 with S/Nos. 008 to 347 (except S/Nos. 313SA and 321SA) and MU-2B-30/-35/ -36 with S/Nos. 501 to 696 (except S/Nos. 652SA and 661SA).

 

Document: Mitsubishi SB No. 196 Rev A.

 

Note: JCAB AD No. TCD-2342-84 refers.

 

Compliance: Before further flight after 31 July 1984.

 

Background: Loss of engine bleed air at the intake anti-ice coupling nut can cause malfunction of the engine air intake anti-ice system. The manufacturer has therefore introduced an inspection and a minor modification to ensure permanent security of the coupling nut.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.