AD/B747/210 - Aileron Cable System

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

Legislation au F2006B03110 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

 


Boeing 747 Series Aeroplanes

 

AD/B747/210 Aileron Cable System 9/99

Applicability: Model 747 series aircraft, as listed in Boeing Service Bulletin 747-27-2367 Revision 1, dated December 17 1998.

 

Requirement: Inspect aileron cables and aileron cable markers in accordance with the technical requirements of FAA AD 99-11-15 Amdt 39-11186.

 

Note: Boeing Service Bulletins 747-27-2367 and 747-27-2367 Revision 1 refer.

 

Compliance: As specified in the Requirement Document with a revised effective date of 9 September 1999.

 

This Airworthiness Directive becomes effective on 9 September 1999.

 

Background: The FAA received a report of an aileron cable failure, due to improper installation onto the wrong groove of an aileron cable drum. The FAA AD issued as a result requires a one-time visual inspection to detect improperly installed or frayed aileron cables, and a one-time visual inspection to detect improper identification or location of the cable markers.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.