Commonwealth legislation

AD/RB211/23 - HP Compressor Rotor Shaft to HP Turbine Rotor Disc Retaining Bolts

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires corrective action concerning the HP compressor-rotor-shaft to HP turbine rotor-disc retaining bolts on RB211-524G2, -524G3 and 524H2 series engines (Applicability). It addresses an identified unsafe condition by mandating the actions set out in the AD. The CASA delegate issues the AD under subregulation 39.1(1) of CAR 1998 and prescribes the work, timing and instructions; affected operators or maintenance organisations must carry out and fund the required actions within the AD's compliance schedule (Requirement, Compliance sections).

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Current sections

Direct links to the current provisions in AD/RB211/23 - HP Compressor Rotor Shaft to HP Turbine Rotor Disc Retaining Bolts.

AIRWORTHINESS DIRECTIVE

View image in the official source

View image in the official source
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

AD/RB211/23 HP Compressor Rotor Shaft to

AD/RB211/23 HP Compressor Rotor Shaft to HP Turbine

Rotor Disc Retaining Bolts

Applicability: RB211-524G2, -524G3 and 524H2 series engines.

8/2000

AD/RB211/23 HP Compressor Rotor Shaft to HP Turbine

Rotor Disc Retaining Bolts

Applicability: RB211-524G2, -524G3 and 524H2 series engines.

8/2000

Source text

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

AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

AD/RB211/23 HP Compressor Rotor Shaft to AD/RB211/23 HP Compressor Rotor Shaft to HP Turbine

AD/RB211/23 HP Compressor Rotor Shaft to HP Turbine

Rotor Disc Retaining Bolts

Applicability: RB211-524G2, -524G3 and 524H2 series engines.

8/2000 8/2000

AD/RB211/23 HP Compressor Rotor Shaft to HP Turbine

Rotor Disc Retaining Bolts

Applicability: RB211-524G2, -524G3 and 524H2 series engines.

8/2000