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AD/TBM 700/38 Amdt 1 - Flap Carriage Roller Pins
Aerospatiale (Socata) TBM 700 Series AerAerospatiale (Socata) TBM 700 Series Aeroplanes
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Aerospatiale (Socata) TBM 700 Series Aeroplanes
| AD/TBM 700/38 Amdt 1 | Flap Carriage Roller Pins | 4/2007 |
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| Applicability: | Model TBM 700 aircraft, serial numbers 1 through 268, and 270 through 327, which have accumulated more than 1,500 landings. |
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| Requirement: | Action in accordance with EADS Socata TBM 700 Service Bulletin No. SB 70-122 Amdt 2, or later EASA approved revision.Note 1: Incorporation of modification MOD70-0168-57 on both wings in accordance with EADS Socata Service Bulletin No. 70-138 original issue, or later EASA approved revision, is considered terminating action for the requirements of this Directive.Note 2: EASA AD 2007-0055 refers. |
| Compliance: | Unless the initial inspection is already accomplished, at the next scheduled 100 hour inspection after 12 April 2007. Repeat thereafter at intervals not to exceed 110 flight hours. |
| This Amendment becomes effective on 12 April 2007. | |
| Background: | Reports were received of two fatigue failures of flap carriage roller pins on in-service aircraft.Amendment 1 is issued in response to a new EASA AD, which expands applicability to aircraft that have accumulated more than 1,500 landings, and introduces an optional terminating action for the requirements of this Directive. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
28 February 2007