1AD/GENERAL/51 - Electrical External Power Connection - Inspection

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

Image unavailable in extracted text 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.