AD/B727/124 - Fuselage Crown Skin Circumferential Joint BS 1080
1AD/B727/124 - Fuselage Crown Skin Circumferential Joint BS 1080
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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/B727/124 Fuselage Crown Skin Circumferential
Joint BS 1080
Applicability: Model 727-100 and 727-100C aircraft listed in the Requirement document.
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Requirement: Action in accordance with the technical requirements of FAA AD 90-21-10 Amdt 39-6761.
Note: Boeing SB 727-53-0109 Rev 1, Rev 2 and Rev 3 refer.
Compliance: As specified in the Requirement document with effective date 13 November 1990.
Background: Country of origin AD. To detect delamination, cracking, and/or corrosion that may lead to depressurisation.