Commonwealth legislation

AD/ERJ-190/17 - Internal Wing Spars and Rib Flanges

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires operators of Embraer ERJ-190 aeroplanes (serial numbers 19000002, 19000004 and 19000006–19000062) to carry out inspections and any corrective action on internal wing spars and rib flanges in accordance with ANAC AD 2008-10-03 Amdt39-1246 (and Embraer Service Bulletin 190-57-0023 where referenced). CASA issued the AD with an effective date of 20 November 2008; operators bear the cost and must follow the referenced documents and update maintenance records to show compliance.

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Current sections

Direct links to the current provisions in AD/ERJ-190/17 - Internal Wing Spars and Rib Flanges.

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/17	Internal Wing Spars and Rib Flanges	12/2008

Applicability:	Model ERJ 190 aircraft, serial numbers 19000002, 19000004, and 19000006 through 19000062.
Requirement:	Action in accordance with the requirements of ANAC AD 2008-10-03 Amdt39-1246.Note: Embraer Service Bulletin No. 190-57-0023 original issue, or later ANAC approved revision, refers.
Compliance:	As specified in the Requirement document, with a revised effective date of20 November 2008.
	This Airworthiness Directive becomes effective on 20 November 2008.
Background:	The manufacturer has determined that the possibility exists of the development of cracks and deformation during assembly of the internal wing spars and rib flanges.

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David Villiers
Delegate of the Civil Aviation Safety Authority

9 October 2008

AD/ERJ-190/17

Internal Wing Spars and Rib Flanges

12/2008

Source text

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

Embraer ERJ-190 Series Aeroplanes Embraer ERJ-190 Series Aeroplanes

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/17	Internal Wing Spars and Rib Flanges	12/2008

Applicability:	Model ERJ 190 aircraft, serial numbers 19000002, 19000004, and 19000006 through 19000062.
Requirement:	Action in accordance with the requirements of ANAC AD 2008-10-03 Amdt39-1246.Note: Embraer Service Bulletin No. 190-57-0023 original issue, or later ANAC approved revision, refers.
Compliance:	As specified in the Requirement document, with a revised effective date of20 November 2008.
	This Airworthiness Directive becomes effective on 20 November 2008.
Background:	The manufacturer has determined that the possibility exists of the development of cracks and deformation during assembly of the internal wing spars and rib flanges.

AD/ERJ-190/17 - Internal Wing Spars and Rib Flanges

Plain English Summary

Deep dive

Current sections

Embraer ERJ-190 Series Aeroplanes

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/17

AD/ERJ-190/17

Internal Wing Spars and Rib Flanges

Internal Wing Spars and Rib Flanges

12/2008

12/2008

Source text

Embraer ERJ-190 Series Aeroplanes Embraer ERJ-190 Series Aeroplanes

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/17 AD/ERJ-190/17

AD/ERJ-190/17

Internal Wing Spars and Rib Flanges Internal Wing Spars and Rib Flanges

Internal Wing Spars and Rib Flanges

12/2008 12/2008

12/2008