Commonwealth legislation

AD/B727/96 Amdt 1 - Wing Rear Spar Terminal Fitting

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Commonwealth

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legislative instrument

Plain English Summary

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This AD makes compliance with FAA AD 87-04-15 and Boeing Service Bulletin 727-57-103 Revision 4 mandatory for Boeing 727s listed in that service bulletin, requiring the inspections and corrective actions it prescribes. It targets cracking in wing rear spar terminal fittings reported on 21 fittings in service.

Owners/operators of affected aircraft must obtain and follow the referenced FAA and Boeing documents, bearing inspection, repair/replacement and downtime costs; Amendment 1 updates the AD to reference the latest FAA AD.

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AD/B727/96 Amdt 1 - Wing Rear Spar Terminal Fitting

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Boeing 727 Series Aeroplanes

AD/B727/96

Amdt 1

Wing Rear Spar Terminal Fitting 11/87

Applicability: All models with S/Nos. specified in Boeing SB 727-57-103 R4.

Requirement: Action in accordance with FAA AD 87-04-15 and Boeing SB 727-57-103 R4. Compliance: As per Requirement documents.

Background: Cracks have been reported in 21 fittings on aircraft in service. Amdt 1 of this Directive references the latest FAA AD.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.