Commonwealth legislation

AD/RB211/5 Amdt 2 - Low Pressure Compressor Rotor (Fan) Axial Retention

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD amends RB211/5 to reference Rolls‑Royce Service Bulletin RB211‑72‑6574, Revision 6. It affects operators, owners and maintenance organisations for specified RB211‑22B and RB211‑524 engines and modules and requires them to carry out the inspections/modifications and timing set out in that SB.

CASA issues the AD; Rolls‑Royce supplies the technical requirements. Direct costs (labour, parts, downtime) fall to operators, and compliance depends on obtaining and implementing SB Rev. 6.

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AD/RB211/5 Amdt 2 - Low Pressure Compressor Rotor (Fan) Axial Retention

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Rolls Royce Turbine Engines - RB211 Series

AD/RB211/5

Amdt 2

Low Pressure Compressor Rotor (Fan) Axial Retention

1/83

Applicability: RB211-22B-02, RB211-524B-02, RB211-524B2-19, RB211-524B2-39, RB211-

524C2-19 engines and modules as specified in SB No. RB211-72-6574, Rev. 6.

Document: Rolls Royce SB No. RB211-72-6574, Rev. 6.

Note: FAA AD No. 82-12-05, Amdt. 39-4398 refers.

Compliance: In accordance with the requirement document.

Background: This Directive is amended in order to reference the latest revision to the manufacturer’s requirement document.

Source text

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