Commonwealth legislation

AD/B727/51 - Right Hand Inboard Midflap Trailing Edge Upper Chord Support Angle - Reinforcement

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Mandates reinforcement of the right‑hand inboard midflap trailing‑edge upper‑chord support angle on all Boeing 727 series aircraft, to be carried out using Boeing Service Bulletin No. 27‑97, with compliance required forthwith.

All operators, owners and maintenance organisations must implement the bulletin immediately; operators will bear parts, labour and downtime costs and no deferral or alternative compliance is stated.

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AD/B727/51 - Right Hand Inboard Midflap Trailing Edge Upper Chord Support Angle - Reinforcement

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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/B727/51 Right Hand Inboard Midflap Trailing Edge Upper

Chord Support Angle - Reinforcement

6/67

Applicability: All models. Document: Boeing SB No. 27-97. Compliance: Forthwith.

Source text

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