Commonwealth legislation

AD/PT6A/15 - Reversing Linkage Front End Clevis - Incorporation of Inspection Hole - 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This Act has been repealed and is no longer in force. It is retained for historical reference.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

This cancels the 1974 airworthiness directive AD/PT6A/15 that had required inspection/modification (adding an inspection hole) of the reversing linkage front end clevis on certain Pratt & Whitney Canada PT6A turbine engines.

Owners and operators of affected PT6A-powered aircraft no longer must follow the cited service bulletins; they should update maintenance records to reflect the directive’s removal.

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Current sections

Direct links to the current provisions in AD/PT6A/15 - Reversing Linkage Front End Clevis - Incorporation of Inspection Hole - CANCELLED.

Pratt and Whitney Canada Turbine Engines

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD/PT6A/15	Reversing Linkage Front EndClevis - Incorporation of Inspection Hole	7/2009

Requirement:	CANCELLED.
	This AD is cancelled on 2 July 2009.
Background:	This unique Australian AD specified action in accordance with UACL SB No. 166 or SB No. 1119 within 100 hours time in service after October 1974. The AD is no longer required.

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James Coyne
Delegate of the Civil Aviation Safety Authority

18 May 2009

AD/PT6A/15

Reversing Linkage Front EndClevis - Inco

Reversing Linkage Front EndClevis - Incorporation of Inspection Hole

Reversing Linkage Front End

Clevis - Incorporation of Inspection Hole

7/2009

Source text

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

Pratt and Whitney Canada Turbine Engines Pratt and Whitney Canada Turbine Engines - PT6A Series

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD/PT6A/15	Reversing Linkage Front EndClevis - Incorporation of Inspection Hole	7/2009

Requirement:	CANCELLED.
	This AD is cancelled on 2 July 2009.
Background:	This unique Australian AD specified action in accordance with UACL SB No. 166 or SB No. 1119 within 100 hours time in service after October 1974. The AD is no longer required.

James Coyne
Delegate of the Civil Aviation Safety Authority

18 May 2009

AD/PT6A/15 AD/PT6A/15

AD/PT6A/15

Reversing Linkage Front EndClevis - Inco Reversing Linkage Front EndClevis - Incorporation of Inspection Hole

Reversing Linkage Front End

Clevis - Incorporation of Inspection Hole

Deep dive

Current sections

Pratt and Whitney Canada Turbine Engines - PT6A Series

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD/PT6A/15

AD/PT6A/15

Reversing Linkage Front EndClevis - Incorporation of Inspection Hole

Reversing Linkage Front End

7/2009

7/2009

Source text

Pratt and Whitney Canada Turbine Engines Pratt and Whitney Canada Turbine Engines - PT6A Series

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD/PT6A/15 AD/PT6A/15

AD/PT6A/15

Reversing Linkage Front EndClevis - Inco Reversing Linkage Front EndClevis - Incorporation of Inspection Hole

Reversing Linkage Front End

7/2009 7/2009

7/2009