AD/GENERAL/51 - Electrical External Power Connection - Inspection

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

Legislation au F2006B10282 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

 


Aircraft - General

 

AD/GENERAL/51 Electrical External Power Connection - Inspection


11/75

 

Applicability: All aircraft with a maximum take-off weight of 5700 kg and below fitted with electrical external power provision.

 

Requirement: 1. Inspect the external power system to ensure that an external power supply with reversed polarity or phase sequence cannot be connected to the electrical system of the aircraft.

 

2. Modify or disconnect any external power system which does not comply with para. 1.

 

Compliance: Within 100 hours time in service after 28 November 1975.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.