AD/PA-31/32 - Electrical Power Indicators - Modification

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

Legislation au F2006B05737 Not 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

 


Piper PA-31 Series Aeroplanes

 

AD/PA-31/32 Electrical Power Indicators - Modification 8/74

Applicability: All models.

 

Requirement:  Install an ammeter in each generator feeder line so that the flight crew are provided with means to continually monitor the current essential for the safe operation of the system.

 

Note: An ammeter that can be switched into the battery line and each generator feeder line may be used provided that the switch can be selected to a generator feeder line throughout the flight.

 

Compliance: Within 200 hours time in service after 30 August 1974.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.