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AD/SA 315/11 - Main Rotor Hub
Eurocopter SA 315 (Lama) Series HelicoptEurocopter SA 315 (Lama) Series Helicopters
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Eurocopter SA 315 (Lama) Series Helicopters
| AD/SA 315/11 | Main Rotor Hub | 12/2006 |
|---|
| Applicability: | Model SA 315 B helicopters equipped with main rotor hub body part number 3160.12.10020 and 3160.12.10020.1. |
|---|---|
| Requirement: | Inspect the visible internal and external areas of the rotor hub yoke lugs in accordance with the Maintenance Manual Work Card 5720.601 (issued 12.83).Note: DGAC AD 84-134-29(B) and LAMA Telex Service No. 65.34 refer. |
| Compliance: | At intervals not to exceed 400 flight hours, until the accumulation of 3,000 flight hours.Upon the accumulation of 3,000 flight hours, inspect at intervals not to exceed 50 flight hours. |
| This Airworthiness Directive becomes effective on 23 November 2006. | |
| Background: | The DGAC requires inspection for cracks in the lugs of the rotor hub yokes. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
13 October 2006