CTHIn ForceLegislation
AD/BELL 222/30 - Swashplate Drive Link P/N222-010-460-101
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AD/BELL 222/30 - Swashplate Drive Link P/N222-010-460-101
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| AD/BELL 222/30 | Swashplate Drive Link P/N222-010-460-101 | 8/2005 |
|---|
| Applicability: | All Bell 222 series helicopters. |
|---|---|
| Requirement: | Remove and do not install swashplate drive links P/N 222-010-460-101.Note: FAA AD 82-09-53 Amdt 39-4434 refers. |
| Compliance: | Before further flight, after the effective date of this AD |
| This Airworthiness Directive becomes effective on 4 August 2005. | |
| Background: | This directive is issued to prevent possible main rotor swashplate drive link failure due to excessive bearing wear and possible link cracks. Failure of a swashplate drive link could result in loss of control of the helicopter. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
21 June 2005