Document ID: chunk:federal_register_of_legislation:F2006B08693:reg:785759
Version: federal_register_of_legislation:F2006B08693
Segment Type: reg
Provision Reference: reg 785759
Character Range: 2909–4215

785759

           Note 3: FAA Emergency AD 2003-08-52 refers.
           Compliance: 1. Within 30 flight hours or 3 days from the effective date of this directive. 2a. Within 30 flight hours or 3 days from the effective date of this directive,
              whichever is the later.

              2b. Within 100 flight hours or 10 days from the effective date of this directive, whichever occurs first.

3.        Within 100 flight hours or 10 days from the effective date of this directive, whichever occurs first.

4.        From the effective date of this directive.

           This Airworthiness Directive becomes effective on 17 April 2003.

           Background: This directive is in response to 12 stall events that occurred over a 6- month period. It has been determined that in the majority of the stall events the VG was rigged to the N1 schedule. Re-rigging the VG to the N schedule will give a highe r stall margin. If the VG schedule is not adjusted to the N schedule the aircraft could suffer a dual inflight shutdown or power loss during deceleration from take off power to climb power.

 David Villiers
 Delegate of the Civil Aviation Safety Authority 16 April 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 17 April 2003.