AD/B727/129 - Fuselage Circumferential Joint Doubler BS259, 360, 441, 481 and 681
1AD/B727/129 - Fuselage Circumferential Joint Doubler BS259, 360, 441, 481 and 681
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.