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AD/SA 315/2 - Free-Wheel Inspections following Main Rotor Impact
Eurocopter SA 315 (Lama) Series HelicoptEurocopter SA 315 (Lama) Series Helicopters
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Eurocopter SA 315 (Lama) Series Helicopters
| AD/SA 315/2 | Free-Wheel Inspections followingMain Rotor Impact | 12/2006 |
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| Applicability: | EUROCOPTER SA 315 B (LAMA) helicopters on which the main rotor has hit an obstacle while rotating. |
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| Requirement: | Carry out the actions detailed in EUROCOPTER Telex Service N° 01.27 dated22 April 1992 or later DGAC approved revision.Note: DGAC AD 92-130-033(B) dated 10 June 1992 refers. |
| Compliance: | Before further flight after any time the main rotor hits an obstacle. |
| This Airworthiness Directive becomes effective on 23 November 2006. | |
| Background: | The actions detailed in this AD are intended to prevent failure of the freewheel following the main rotor hitting an obstacle. |
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James Coyne
Delegate of the Civil Aviation Safety Authority
29 September 2006