Document ID: chunk:federal_register_of_legislation:F2006L03612:body:0:p2
Version: federal_register_of_legislation:F2006L03612
Segment Type: other
Provision Reference: 
Character Range: 2752–4136

than 15716 or 26098.  Any T/R slider removed from service based on the requirements of this paragraph is not eligible for installation on any helicopter.

                    Terminating Action.

                Replacing the T/R slider with an FAA approved airworthy T/R slider without a CAGE code or with a legible CAGE code other than 15716 or 26098, constitutes terminating action for the requirements of this AD.

                Note 4:  FAA AD 2006-19-05 Amdt 39-14762 dated 5 September 2006 refers.
Compliance:        1. Within 25 hours after the effective date of this AD.

                     2. a. Before further flight, unless accomplished previously, and thereafter at intervals not to exceed 25 hours time in service (TIS).

                     2. b. Before further flight.

                   3. On or before accumulating 1000 hours TIS or on or before 12 months, whichever occurs first, after the effective date of this AD.
                This Airworthiness Directive becomes effective on 23 November 2006.
Background:     This AD is prompted by two accidents attributed to sub-standard T/R sliders that failed during flight.  The actions specified by this AD are intended to prevent failure of a T/R slider, loss of T/R control, and subsequent loss of control of the helicopter.

James Coyne
Delegate of the Civil Aviation Safety Authority

12 October 2006