CTHRepealedLegislation
AD/TBM 700/42 - Rivets at Frames C18 BIS and C19
Aerospatiale (Socata) TBM 700 Series AerAerospatiale (Socata) TBM 700 Series Aeroplanes
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Aerospatiale (Socata) TBM 700 Series Aeroplanes
| AD/TBM 700/42 | Rivets at Frames C18 BIS and C19 | 10/2005 |
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| Applicability: | Model TBM 700 A, B, and C variants, all serial numbers. |
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| 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