Document ID: chunk:federal_register_of_legislation:F2006B03003:body:0
Version: federal_register_of_legislation:F2006B03003
Segment Type: other
Provision Reference: 
Character Range: 0–765

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

 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.