Commonwealth legislation

AD/B747/102 - P180-1 Terminal Strip Nuts

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Commonwealth

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legislative instrument

Plain English Summary

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This AD requires operators of the Boeing 747 aeroplanes covered by FAA AD 91‑23‑09 to carry out the inspections and corrective work specified in that FAA directive—adopted by the Civil Aviation Safety Authority—and to complete it before 10 January 1992.

It addresses a reported loose battery power‑feeder terminal that could cause fire or loss of electrical power to flight‑critical systems; responsibility for costs and execution falls to operators and maintenance organisations.

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AD/B747/102 - P180-1 Terminal Strip Nuts

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Boeing 747 Series Aeroplanes

AD/B747/102 P180-1 Terminal Strip Nuts 2/92 DM

Applicability: As specified in the requirement document.

Requirement: Action in accordance with the technical requirements of FAA AD 91-23-09. Compliance: Prior to 10 January 1992.

Background: The FAA have advised that a report has been received of loss of battery power due to a loose power feeder terminal connection. This condition, if not corrected, could result in fire and/or loss of electrical power to flight critical systems in the event of failure of the aircraft primary electrical power system.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.