Commonwealth legislation

AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires operators of Falcon 10 series aircraft whose Aircraft Maintenance Manual (AMM) Chapter 5-40 is below Revision 08 to insert EASA AD 2006-0147 into that AMM. It updates the overwing emergency-exit maintenance regime (extending the opening-test interval to 24 months) and must be complied with within 30 days after 3 August 2006; once AMM Chapter 5-40 is updated to Revision 08 the insertion requirement ends.

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Current sections

Direct links to the current provisions in AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit.

AMD Falcon 10 Series Aeroplanes

AD/AMD 10/22 Amdt 1	Overwing Emergency Exit	8/2006

Applicability:	All Falcon 10 aircraft for which the Aircraft Maintenance Manual (AMM) Airworthiness Limitation Section, Chapter 5-40, is not at Revision 08 or above.
Requirement:	Insert a copy of EASA AD 2006-0147 into Chapter 5-40 of the Aircraft Maintenance Manual.Note: Updating Chapter 5-40 with Revision 08 terminates the requirement of this Directive, upon which the copy of this Directive may then be removed from the AMM.
Compliance:	Within 30 days after 3 August 2006.
	This Amendment becomes effective on 3 August 2006.
Background:	During an attempted operation of a Falcon 50 emergency exit, interference was reported between interior trim and the exit.Amendment 1 is issued in response to a new EASA AD, which supersedes DGAC AD 1999-211-023(B) (the original issue of this Directive), and extends the repetitive overwing emergency exit opening test interval to 24 months.

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David Villiers
Delegate of the Civil Aviation Safety Authority

23 June 2006

AD/AMD 10/22 Amdt 1

Overwing Emergency Exit

8/2006

Source text

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

AMD Falcon 10 Series Aeroplanes AMD Falcon 10 Series Aeroplanes

AMD Falcon 10 Series Aeroplanes

AD/AMD 10/22 Amdt 1	Overwing Emergency Exit	8/2006

Applicability:	All Falcon 10 aircraft for which the Aircraft Maintenance Manual (AMM) Airworthiness Limitation Section, Chapter 5-40, is not at Revision 08 or above.
Requirement:	Insert a copy of EASA AD 2006-0147 into Chapter 5-40 of the Aircraft Maintenance Manual.Note: Updating Chapter 5-40 with Revision 08 terminates the requirement of this Directive, upon which the copy of this Directive may then be removed from the AMM.
Compliance:	Within 30 days after 3 August 2006.
	This Amendment becomes effective on 3 August 2006.
Background:	During an attempted operation of a Falcon 50 emergency exit, interference was reported between interior trim and the exit.Amendment 1 is issued in response to a new EASA AD, which supersedes DGAC AD 1999-211-023(B) (the original issue of this Directive), and extends the repetitive overwing emergency exit opening test interval to 24 months.

AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit

Plain English Summary

Deep dive

Current sections

AMD Falcon 10 Series Aeroplanes

AMD Falcon 10 Series Aeroplanes

AD/AMD 10/22 Amdt 1

AD/AMD 10/22 Amdt 1

Overwing Emergency Exit

Overwing Emergency Exit

8/2006

8/2006

Source text

AMD Falcon 10 Series Aeroplanes AMD Falcon 10 Series Aeroplanes

AMD Falcon 10 Series Aeroplanes

AD/AMD 10/22 Amdt 1 AD/AMD 10/22 Amdt 1

AD/AMD 10/22 Amdt 1

Overwing Emergency Exit Overwing Emergency Exit

Overwing Emergency Exit

8/2006 8/2006

8/2006