AD/P68/6 - Rudder Trim Tab Control Rod P/N 68-506053 - Inspection

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

Legislation au F2006B05381 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

 


Partenavia P68 Series Aeroplanes

 

AD/P68/6 Rudder Trim Tab Control Rod P/N 68-506053 - Inspection

Applicability: All models P68 and P68B.

 

Requirement: 1. Inspect rudder trim tab control rod for correct installation according to the instructions contained in the Partenavia SB No. 32.


10/77

 

2. If rudder trim tab control rod installation is incorrect remove rod and inspect rod visually for distortion and the rod and rod-ends for cracks using a magnetic particle technique.

 

Compliance: Unless already accomplished, before further flight and thereafter at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.