Commonwealth legislation

AD/TBM 700/42 - Rivets at Frames C18 BIS and C19

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates owners/operators of Aerospatiale (Socata) TBM 700 A, B, and C aircraft to inspect rivets at tail frames C18 BIS and C19 per Service Bulletin No. 70‑129 at the next 100‑hour or annual inspection after 29‑Sep‑2005 and at every subsequent 100‑hour/annual check. Any loose rivets must be repaired per the bulletin. The measure addresses reported loose rivets that could weaken the tail structure and risk loss of control.

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Current sections

Direct links to the current provisions in AD/TBM 700/42 - Rivets at Frames C18 BIS and C19.

Aerospatiale (Socata) TBM 700 Series Aer

Aerospatiale (Socata) TBM 700 Series Aeroplanes

AD/TBM 700/42	Rivets at Frames C18 BIS and C19	10/2005

Applicability:	Model TBM 700 A, B, and C variants, all serial numbers.
Requirement:	Action in accordance with EADS SOCATA TBM 700 Service Bulletin No. 70-129, or later EASA approved revision.Note: DGAC AD F-2005-132 refers.
Compliance:	At the next scheduled 100-hour inspection or annual inspection after 29 September 2005. Thereafter at each 100-hour inspection or annual inspection.
	This Airworthiness Directive becomes effective on 29 September 2005.
Background:	The manufacturer received reports of loose rivets on frames C18 BIS and C19. Uncorrected, this condition could result in reduced structural integrity of the tail area.

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David Villiers
Delegate of the Civil Aviation Safety Authority

9 August 2005

AD/TBM 700/42

Rivets at Frames C18 BIS and C19

10/2005

Source text

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

Aerospatiale (Socata) TBM 700 Series Aer Aerospatiale (Socata) TBM 700 Series Aeroplanes

Aerospatiale (Socata) TBM 700 Series Aeroplanes

AD/TBM 700/42	Rivets at Frames C18 BIS and C19	10/2005

Applicability:	Model TBM 700 A, B, and C variants, all serial numbers.
Requirement:	Action in accordance with EADS SOCATA TBM 700 Service Bulletin No. 70-129, or later EASA approved revision.Note: DGAC AD F-2005-132 refers.
Compliance:	At the next scheduled 100-hour inspection or annual inspection after 29 September 2005. Thereafter at each 100-hour inspection or annual inspection.
	This Airworthiness Directive becomes effective on 29 September 2005.
Background:	The manufacturer received reports of loose rivets on frames C18 BIS and C19. Uncorrected, this condition could result in reduced structural integrity of the tail area.

AD/TBM 700/42 - Rivets at Frames C18 BIS and C19

Plain English Summary

Deep dive

Current sections

Aerospatiale (Socata) TBM 700 Series Aeroplanes

Aerospatiale (Socata) TBM 700 Series Aeroplanes

AD/TBM 700/42

AD/TBM 700/42

Rivets at Frames C18 BIS and C19

Rivets at Frames C18 BIS and C19

10/2005

10/2005

Source text

Aerospatiale (Socata) TBM 700 Series Aer Aerospatiale (Socata) TBM 700 Series Aeroplanes

Aerospatiale (Socata) TBM 700 Series Aeroplanes

AD/TBM 700/42 AD/TBM 700/42

AD/TBM 700/42

Rivets at Frames C18 BIS and C19 Rivets at Frames C18 BIS and C19

Rivets at Frames C18 BIS and C19

10/2005 10/2005

10/2005