Commonwealth legislation

AD/PA-34/22 - Fuselage Structure Rivets - Inspection - CANCELLED

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

1/10 complexity

What this does: This document officially scraps a previous aviation safety rule (Airworthiness Directive AD/PA-34/22) that required owners of Piper PA-34 Seneca aircraft to inspect their fuselage rivets for defects.

Who it affects: Owners and operators of Piper PA-34 Seneca series aeroplanes.

What changed: As of 23 October 2008, you no longer need to perform the rivet inspection that was previously required by Piper Service Bulletin No. 545. The original rule (which mandated an inspection within 100 hours of flight time after May 1977) is now completely cancelled and no longer legally enforceable.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/PA-34/22 - Fuselage Structure Rivets - Inspection - CANCELLED.

Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/22	Fuselage Structure Rivets - Inspection	11/2008

Requirement:	CANCELLED.
	This AD is cancelled on 23 October 2008.
Background:	This unique Australian AD specified inspection of fuselage structure rivets in accordance with Piper SB No. 545. Compliance was required within 100 hours time in service after May 1977. The AD is no longer required.

View image in the official source

David Villiers
Delegate of the Civil Aviation Safety Authority

9 September 2008

AD/PA-34/22

Fuselage Structure Rivets - Inspection

11/2008

Source text

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

Piper PA-34 (Seneca) Series Aeroplanes Piper PA-34 (Seneca) Series Aeroplanes

Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/22	Fuselage Structure Rivets - Inspection	11/2008

Requirement:	CANCELLED.
	This AD is cancelled on 23 October 2008.
Background:	This unique Australian AD specified inspection of fuselage structure rivets in accordance with Piper SB No. 545. Compliance was required within 100 hours time in service after May 1977. The AD is no longer required.

AD/PA-34/22 - Fuselage Structure Rivets - Inspection - CANCELLED

Plain English Summary

Deep dive

Current sections

Piper PA-34 (Seneca) Series Aeroplanes

Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/22

AD/PA-34/22

Fuselage Structure Rivets - Inspection

Fuselage Structure Rivets - Inspection

11/2008

11/2008

Source text

Piper PA-34 (Seneca) Series Aeroplanes Piper PA-34 (Seneca) Series Aeroplanes

Piper PA-34 (Seneca) Series Aeroplanes

AD/PA-34/22 AD/PA-34/22

AD/PA-34/22

Fuselage Structure Rivets - Inspection Fuselage Structure Rivets - Inspection

Fuselage Structure Rivets - Inspection

11/2008 11/2008

11/2008