Document ID: chunk:federal_register_of_legislation:F2006B03110:body:0
Version: federal_register_of_legislation:F2006B03110
Segment Type: other
Provision Reference: 
Character Range: 0–1184

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.