Commonwealth legislation

AD/ERJ-190/9 - Wing Lower Skin Stringers

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Requires operators of specified Embraer ERJ‑190 airframes (listed serial numbers) to perform the inspections or repairs described in ANAC AD 2008‑01‑02 Amdt39‑1228 (and the referenced Embraer Service Bulletin) to address fatigue cracking in wing lower skin stringers. Work must be done before the aeroplane reaches 5,000 flight cycles. Operators pay for and schedule the inspections/repairs; the Civil Aviation Safety Authority gives legal effect to the directive and compliance may require grounding or altered maintenance timing.

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Current sections

Direct links to the current provisions in AD/ERJ-190/9 - Wing Lower Skin Stringers.

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/9	Wing Lower Skin Stringers	6/2008

Applicability:	Model ERJ-190 aircraft, serial numbers 19000004, 19000006 through 19000028, and 19000030 through 19000039.
Requirement:	Action in accordance with the requirements of ANAC AD 2008-01-02 Amdt39-1228.Note: Embraer Service Bulletin No. 190-57-0005 Revision 1, or later ANAC approved revision, refers.
Compliance:	Before the accumulation of 5,000 flight cycles.
	This Airworthiness Directive becomes effective on 5 June 2008.
Background:	During aircraft structural fatigue tests, cracks were detected in the wing lower skin stringers between ribs 7 and 10 on both wings. Undetected fatigue cracking could result in fuel leakage and reduced structural integrity of the wing.

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David Villiers
Delegate of the Civil Aviation Safety Authority

16 April 2008

AD/ERJ-190/9

Wing Lower Skin Stringers

6/2008

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-190/9	Wing Lower Skin Stringers	6/2008

Applicability:	Model ERJ-190 aircraft, serial numbers 19000004, 19000006 through 19000028, and 19000030 through 19000039.
Requirement:	Action in accordance with the requirements of ANAC AD 2008-01-02 Amdt39-1228.Note: Embraer Service Bulletin No. 190-57-0005 Revision 1, or later ANAC approved revision, refers.
Compliance:	Before the accumulation of 5,000 flight cycles.
	This Airworthiness Directive becomes effective on 5 June 2008.
Background:	During aircraft structural fatigue tests, cracks were detected in the wing lower skin stringers between ribs 7 and 10 on both wings. Undetected fatigue cracking could result in fuel leakage and reduced structural integrity of the wing.

AD/ERJ-190/9 - Wing Lower Skin Stringers

Plain English Summary

Deep dive

Current sections

Embraer ERJ-190 Series Aeroplanes

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/9

AD/ERJ-190/9

Wing Lower Skin Stringers

Wing Lower Skin Stringers

6/2008

6/2008

Source text

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

Embraer ERJ-190 Series Aeroplanes

AD/ERJ-190/9 AD/ERJ-190/9

AD/ERJ-190/9

Wing Lower Skin Stringers Wing Lower Skin Stringers

Wing Lower Skin Stringers

6/2008 6/2008

6/2008