Commonwealth legislation

AD/A320/114 - Frame 36 - Longitudinal Beams of the Pressure Panel

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This appears to be an Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998. It applies to specific early-model Airbus A320 aircraft (manufacturer serial numbers 0002 to 0107) and concerns the structural integrity of the longitudinal beams at Frame 36 of the pressure panel (a critical fuselage structure that maintains cabin pressure).

However, the provided text is incomplete. It includes the preamble and applicability section, but cuts off mid-sentence and omits the Requirement section (what actions must be taken), the Compliance section (when they must be done), and the Background section (what the safety risk is). Without these, the specific legal obligations for aircraft operators cannot be determined.

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Current sections

Direct links to the current provisions in AD/A320/114 - Frame 36 - Longitudinal Beams of the Pressure Panel.

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/A320/114 Frame 36 - Longitudinal Beam

AD/A320/114 Frame 36 - Longitudinal Beams of the Pressure Panel

Applicability: All Model A320 aircraft, MSN 0002 to MSN 0107 without Airbus Industrie

3/2001

AD/A320/114 Frame 36 - Longitudinal Beams of the Pressure Panel

Applicability: All Model A320 aircraft, MSN 0002 to MSN 0107 without Airbus Industrie

3/2001

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/A320/114 Frame 36 - Longitudinal Beam AD/A320/114 Frame 36 - Longitudinal Beams of the Pressure Panel

AD/A320/114 Frame 36 - Longitudinal Beams of the Pressure Panel

Applicability: All Model A320 aircraft, MSN 0002 to MSN 0107 without Airbus Industrie

3/2001 3/2001

AD/A320/114 Frame 36 - Longitudinal Beams of the Pressure Panel

Applicability: All Model A320 aircraft, MSN 0002 to MSN 0107 without Airbus Industrie

3/2001