Commonwealth legislation

AD/F28/45 Amdt 5 - Structural Integrity Program

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This instrument revokes AD/F28/45 Amdt 4 and issues AD/F28/45 Amdt 5 under subregulation 39.1(1) of CAR 1998, titled "Structural Integrity Program 5/2000", and applies to all models. It mandates the corrective actions and compliance timings set out in the AD to address an identified unsafe condition.

Operators, owners and maintainers of the affected aircraft must carry out the prescribed inspections, repairs or modifications and bear the associated operational and financial costs. Specific technical steps and deadlines are in the AD’s requirement and compliance sections.

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Current sections

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AIRWORTHINESS DIRECTIVE

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For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/F28/45 Amdt 4 and issues the following 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/F28/45

Amdt 5

Applicability: All models.

Structural Integrity Program 5/2000

AD/F28/45

Amdt 5

Applicability: All models.

Structural Integrity Program 5/2000

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 revokes Airworthiness Directive (AD) AD/F28/45 Amdt 4 and issues the following 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/F28/45 AD/F28/45

AD/F28/45

Amdt 5

Applicability: All models.

Structural Integrity Program 5/2000 Structural Integrity Program 5/2000

AD/F28/45

Amdt 5

Applicability: All models.

Structural Integrity Program 5/2000