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AD/SA 315/10 - Main Rotor Blade Attachment Fittings
Eurocopter SA 315 (Lama) Series HelicoptEurocopter SA 315 (Lama) Series Helicopters
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Eurocopter SA 315 (Lama) Series Helicopters
| AD/SA 315/10 | Main Rotor Blade Attachment Fittings | 12/2006 |
|---|
| Applicability: | Model SA 315 B helicopters. |
|---|---|
| Requirement: | Perform a crack detection inspection on the attachment fitting in the area of the main rotor blade attachment bolts, in accordance with the procedure specified in Chapter 5 of the DGAC approved Maintenance Manual, Revision dated 03-96, or later approved revision.Note: DGAC AD 96-081-036(B) R1 refers. |
| Compliance: | At intervals not to exceed 400 flight hours. |
| This Airworthiness Directive becomes effective on 23 November 2006. | |
| Background: | The DGAC requires certain inspections in response to fatigue tests conducted on the main rotor blade spar/fitting. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
13 October 2006