Commonwealth legislation

AD/B727/201 - Trailing Edge Flap Foreflap

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

3/10 complexity

This rule requires operators of Boeing 727-series aircraft to inspect and, if needed, replace the trailing edge foreflap carriage attach fittings after cracked or broken fittings were found, which could allow foreflap failure and affect safety. It adopts FAA AD 2005-14-07’s instructions and compliance dates (effective 13 April 2006), ensuring Australian-registered 727, 727C, 727-100/100C, 727-200/200F aircraft meet the same safety standards.

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Current sections

Direct links to the current provisions in AD/B727/201 - Trailing Edge Flap Foreflap.

Boeing 727 Series Aeroplanes

AD/B727/201	Trailing Edge Flap Foreflap	4/2006

Applicability:	Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series aircraft, as listed in Boeing Alert Service Bulletin 727-57A0135 Revision 3, or later FAA approved revision.
Requirement:	Action in accordance with the technical requirements of FAA AD 2005-14-07Amdt 39-14184.Note: Boeing Service Bulletin 727-27-133, and Boeing 727 Service Bulletins57-59 and 57-72; or later FAA approved revisions, refer.
Compliance:	As specified in the Requirement document, with a revised effective date of13 April 2006.
	This Airworthiness Directive becomes effective on 13 April 2006.
Background:	The FAA received reports of damaged or failed outboard foreflaps with a cracked or failed carriage attach fitting of the foreflap sequencing carriage.

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David Punshon
Delegate of the Civil Aviation Safety Authority

1 March 2006

AD/B727/201

Trailing Edge Flap Foreflap

4/2006

Source text

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

Boeing 727 Series Aeroplanes Boeing 727 Series Aeroplanes

Boeing 727 Series Aeroplanes

AD/B727/201	Trailing Edge Flap Foreflap	4/2006

Applicability:	Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series aircraft, as listed in Boeing Alert Service Bulletin 727-57A0135 Revision 3, or later FAA approved revision.
Requirement:	Action in accordance with the technical requirements of FAA AD 2005-14-07Amdt 39-14184.Note: Boeing Service Bulletin 727-27-133, and Boeing 727 Service Bulletins57-59 and 57-72; or later FAA approved revisions, refer.
Compliance:	As specified in the Requirement document, with a revised effective date of13 April 2006.
	This Airworthiness Directive becomes effective on 13 April 2006.
Background:	The FAA received reports of damaged or failed outboard foreflaps with a cracked or failed carriage attach fitting of the foreflap sequencing carriage.

AD/B727/201 - Trailing Edge Flap Foreflap

Plain English Summary

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Current sections

Boeing 727 Series Aeroplanes

Boeing 727 Series Aeroplanes

AD/B727/201

AD/B727/201

Trailing Edge Flap Foreflap

Trailing Edge Flap Foreflap

4/2006

4/2006

Source text

Boeing 727 Series Aeroplanes Boeing 727 Series Aeroplanes

Boeing 727 Series Aeroplanes

AD/B727/201 AD/B727/201

AD/B727/201

Trailing Edge Flap Foreflap Trailing Edge Flap Foreflap

Trailing Edge Flap Foreflap

4/2006 4/2006

4/2006