Document ID: chunk:federal_register_of_legislation:F2006B02651:body:0
Version: federal_register_of_legislation:F2006B02651
Segment Type: other
Provision Reference: 
Character Range: 0–761

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

 Boeing 727 Series Aeroplanes

 AD/B727/129 Fuselage Circumferential Joint Doubler
                       BS259, 360, 441, 481 and 681

 Applicability: 727-100 line position 1 through 547.

            727-200 line position 433 through 549.

3/91

            Requirement: Action in accordance with the technical requirements of FAA AD 90-26-09 Amdt 39- 6835.

Note: Boeing SB 727-53-0084 Rev. 4 refers.

Compliance: As specified in the Requirement Document.

            Background: Country of origin AD. Delamination, corrosion and/or cracking if not corrected, could result in loss of cabin pressurisation.