Commonwealth legislation

AD/RB211/6 Amdt 4 - Low Pressure Compressor Rotor (Fan) Axial Retention

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD makes compliance with Rolls‑Royce Service Bulletin RB211‑72‑6576, Revision 7 mandatory for specified RB211‑524 engines and listed modules, requiring operators to follow the manufacturer’s procedures addressing low‑pressure compressor (fan) axial retention. It updates effectivity to reflect the SB’s latest revision. Affected owners/operators must arrange and pay for the inspections, repairs or modifications the SB prescribes; the AD enforces the SB by reference and cites a related FAA AD.

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AD/RB211/6 Amdt 4 - 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/RB211/6

Amdt 4

Low Pressure Compressor Rotor (Fan) Axial Retention

9/87

Applicability: RB211-524 series engines and modules as listed in Rolls Royce SB RB211-72-6576 R7.

Requirement: Rolls Royce SB RB211-72-6576 Rev 7.

Note: FAA AD 82-12-05 Amdt 39-4398 refers.

Compliance: In accordance with the Requirement Document.

Background: This Directive has been amended to reflect the manufacturers latest revision to the Requirement Document. This revision amends the engine models and modules effectivity listing.

Source text

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