Commonwealth legislation

AD/F2000/28 - Rivets between Frames 9 and 10, and Stringer Reinforcements

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires the owner/operator of Dassault Falcon 2000EX serial number 82 to carry out the corrective actions specified in EASA AD 2006-0320-E (install missing rivets and stringer reinforcements) by 31 December 2007; it takes effect 20 December 2007.

It affects the aircraft’s maintenance budget and downtime: the operator pays for inspections and structural work, must schedule maintenance before the deadline, and must follow technical instructions from an overseas regulator.

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Current sections

Direct links to the current provisions in AD/F2000/28 - Rivets between Frames 9 and 10, and Stringer Reinforcements.

Dassault Aviation Falcon 2000 Series Aer

Dassault Aviation Falcon 2000 Series Aeroplanes

AD/F2000/28	Rivets between Frames 9 and 10, andStringer Reinforcements	13/2007

Applicability:	Model Falcon 2000EX aircraft, serial number 82.
Requirement:	Action in accordance with the requirements of EASA AD 2006-0320-E.
Compliance:	Before 31 December 2007.
	This Airworthiness Directive becomes effective on 20 December 2007.
Background:	The manufacturer has determined that some stringer reinforcements and some rivets are missing from the skin panels on each side of the fuselage between frames 9 and 10 on certain Falcon 2000EX aircraft.

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David Villiers
Delegate of the Civil Aviation Safety Authority

7 November 2007

AD/F2000/28

Rivets between Frames 9 and 10, andStrin

Rivets between Frames 9 and 10, andStringer Reinforcements

Rivets between Frames 9 and 10, and

Stringer Reinforcements

13/2007

Source text

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

Dassault Aviation Falcon 2000 Series Aer Dassault Aviation Falcon 2000 Series Aeroplanes

Dassault Aviation Falcon 2000 Series Aeroplanes

AD/F2000/28	Rivets between Frames 9 and 10, andStringer Reinforcements	13/2007

Applicability:	Model Falcon 2000EX aircraft, serial number 82.
Requirement:	Action in accordance with the requirements of EASA AD 2006-0320-E.
Compliance:	Before 31 December 2007.
	This Airworthiness Directive becomes effective on 20 December 2007.
Background:	The manufacturer has determined that some stringer reinforcements and some rivets are missing from the skin panels on each side of the fuselage between frames 9 and 10 on certain Falcon 2000EX aircraft.

David Villiers
Delegate of the Civil Aviation Safety Authority

7 November 2007

AD/F2000/28 AD/F2000/28

AD/F2000/28

Rivets between Frames 9 and 10, andStrin Rivets between Frames 9 and 10, andStringer Reinforcements

Rivets between Frames 9 and 10, and

Stringer Reinforcements

Deep dive

Current sections

Dassault Aviation Falcon 2000 Series Aeroplanes

Dassault Aviation Falcon 2000 Series Aeroplanes

AD/F2000/28

AD/F2000/28

Rivets between Frames 9 and 10, andStringer Reinforcements

Rivets between Frames 9 and 10, and

13/2007

13/2007

Source text

Dassault Aviation Falcon 2000 Series Aer Dassault Aviation Falcon 2000 Series Aeroplanes

Dassault Aviation Falcon 2000 Series Aeroplanes

AD/F2000/28 AD/F2000/28

AD/F2000/28

Rivets between Frames 9 and 10, andStrin Rivets between Frames 9 and 10, andStringer Reinforcements

Rivets between Frames 9 and 10, and

13/2007 13/2007

13/2007