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AD/FA-200/27 - Wing Spar Flange Corrosion
Fuji FA-200 Series AeroplanesFuji FA-200 Series Aeroplanes
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Fuji FA-200 Series Aeroplanes
| AD/FA-200/27 | Wing Spar Flange Corrosion | 9/2009 |
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| Applicability: | Model FA-200 series aircraft. |
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| Requirement: | Carry out the fabrication of inspection holes, an inspection of the wing spar flange for corrosion, repair of any corrosion if necessary, and removal of sealing compound; in accordance with Fuji Heavy Industries Ltd. Service Bulletin No. 200-015, dated28 February 2006, or later JCAB approved revision.Note: JCAB AD TCD-6832-2006 refers. |
| Compliance: | Unless the initial requirements are already accomplished, within three months after27 August 2009. Inspect thereafter at intervals not to exceed 5 calendar years. |
| This Airworthiness Directive becomes effective on 27 August 2009. | |
| Background: | The JCAB requires the actions of this Directive to prevent the deterioration of wing structural integrity by corrosion of the wing spar flange. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
30 June 2009