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AD/ATR 42/15 - Wing Inner Skin Surface at Rear Spar Junction
Avions de Transport Regional ATR 42 SeriAvions de Transport Regional ATR 42 Series Aeroplanes
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Avions de Transport Regional ATR 42 Series Aeroplanes
| AD/ATR 42/15 | Wing Inner Skin Surface at Rear Spar Junction | 9/2007 |
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| Applicability: | Model ATR 42-300 and -320 aircraft, serial numbers 3 through 59. |
|---|---|
| Requirement: | Action in accordance with the requirements of DGAC AD 98-147-075(B). |
| Compliance: | Before the accumulation of 33,000 flights. |
| This Airworthiness Directive becomes effective on 30 August 2007. | |
| Background: | This Directive requires fastener hole cold-working in order to prevent the initiation and development of fatigue damage. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
10 July 2007