Document ID: chunk:federal_register_of_legislation:F2007L02448:body:0:p2
Version: federal_register_of_legislation:F2007L02448
Segment Type: other
Provision Reference: 
Character Range: 2696–3697

support for any reason, verify the torque of the nuts in accordance with Requirement 1.

                Note:  Transport Canada ADCF-2000-29 and FAA AD 2001-01-51 refer.

Compliance:     1. Unless the initial inspection is already accomplished, within 25 hours time in service after 30 August 2007.  Thereafter at intervals not to exceed 600 hours time in service or 12 months, whichever occurs first.

                2. At not less than 20 hours time in service, nor more than 30 hours time in service.

             The compliance time for Requirement 2 remains unchanged by this issue of the Directive.
             This Amendment becomes effective on 30 August 2007.
Background:  The FAA received a report of the failure of a main rotor hydraulic actuator support, resulting in an accident of a Model 222U helicopter.

             Amendment 1 is issued to include the Model 230 helicopter in applicability.

David Villiers
Delegate of the Civil Aviation Safety Authority

11 July 2007