Document ID: chunk:federal_register_of_legislation:F2006B03025:body:0
Version: federal_register_of_legislation:F2006B03025
Segment Type: other
Provision Reference: 
Character Range: 0–833

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

 Boeing 747 Series Aeroplanes

AD/B747/124 H-11 Steel Bolts 7/94

            Applicability: Model 747 series aircraft with line numbers 641 through 708, excluding Model 747- 400 series aircraft.

            Requirement: Action in accordance with the technical requirements of FAA AD 94-07-06 Amendment 39-8864.

            Note: Boeing SB 747-51-2048 refers.

 Compliance: As specified in the Requirement Document.

            Background: Reports were received of cracked and fractured H-11 steel bolts installed at certain locations of the airframe structure. The actions specified in this Directive are intended to prevent the failure of attachment bolts at critical locations.