Commonwealth legislation

AD/B767/250 Amdt 1 - Lower Wing Skin

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This amendment corrects the compliance effective date for an Airworthiness Directive requiring inspections and corrective action on the lower wing skin of certain Boeing 767 models where cracks were found at forward tension bolt holes of the aft pitch load fitting. It applies to owners/operators of Model 767-200, -300, -300F and -400ER aircraft who must carry out the FAA-prescribed technical actions (FAA AD 2009-06-08Amdt 39-15844) by the revised effective date of 2 July 2009.

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Current sections

Direct links to the current provisions in AD/B767/250 Amdt 1 - Lower Wing Skin.

Boeing 767 Series Aeroplanes

AD/B767/250 Amdt 1	Lower Wing Skin	7/2009

Applicability:	Model 767-200, -300, -300F and -400ER series aircraft, as identified in Boeing Service Bulletin 767-57A0097 Revision 1, or later FAA approved revision.
Requirement:	Action in accordance with the technical requirements of FAA AD 2009-06-08Amdt 39-15844.
Compliance:	As specified in the Requirement document, with a revised effective date of2 July 2009.
	This Amendment becomes effective on 2 July 2009.
Background:	The FAA received reports of cracks in the lower wing skin that had originated at the forward tension bolt holes of the aft pitch load fitting. Such cracking, unless detected and corrected, could result in a fuel leak and reduced structural integrity of the aircraft.Amendment 1 is issued to correct the compliance section revised effective date.

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David Villiers
Delegate of the Civil Aviation Safety Authority

22 May 2009

AD/B767/250 Amdt 1

Lower Wing Skin

7/2009

Source text

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

Boeing 767 Series Aeroplanes Boeing 767 Series Aeroplanes

Boeing 767 Series Aeroplanes

AD/B767/250 Amdt 1	Lower Wing Skin	7/2009

Applicability:	Model 767-200, -300, -300F and -400ER series aircraft, as identified in Boeing Service Bulletin 767-57A0097 Revision 1, or later FAA approved revision.
Requirement:	Action in accordance with the technical requirements of FAA AD 2009-06-08Amdt 39-15844.
Compliance:	As specified in the Requirement document, with a revised effective date of2 July 2009.
	This Amendment becomes effective on 2 July 2009.
Background:	The FAA received reports of cracks in the lower wing skin that had originated at the forward tension bolt holes of the aft pitch load fitting. Such cracking, unless detected and corrected, could result in a fuel leak and reduced structural integrity of the aircraft.Amendment 1 is issued to correct the compliance section revised effective date.

AD/B767/250 Amdt 1 - Lower Wing Skin

Plain English Summary

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Current sections

Boeing 767 Series Aeroplanes

Boeing 767 Series Aeroplanes

AD/B767/250 Amdt 1

AD/B767/250 Amdt 1

Lower Wing Skin

Lower Wing Skin

7/2009

7/2009

Source text

Boeing 767 Series Aeroplanes Boeing 767 Series Aeroplanes

Boeing 767 Series Aeroplanes

AD/B767/250 Amdt 1 AD/B767/250 Amdt 1

AD/B767/250 Amdt 1

Lower Wing Skin Lower Wing Skin

Lower Wing Skin

7/2009 7/2009

7/2009