Document ID: chunk:federal_register_of_legislation:F2006L03811:body:0:p3
Version: federal_register_of_legislation:F2006L03811
Segment Type: other
Provision Reference: 
Character Range: 5779–7569

spares must be modified before installation on an aircraft, by the embodiment of modifications 07.2214 and 07.2215; and the inside of the tube visually inspected in accordance with paragraph 2.B.(1) of SB No. 55.01 Revision 4.

             Note:  DGAC AD 96-277-037(A) R2 refers.
Compliance:     1.a. Inspect thereafter at intervals not to exceed 6 years.

                1.b. As specified in Requirement 1.b.

                  1.c. (i) After the last flight of the day.

                  1.c. (ii) At intervals not to exceed 400 flight hours or 4 months, whichever occurs first.

                1.d. Unless already accomplished, within 50 flight hours after 21 December 2006, and thereafter at intervals not to exceed 400 flight hours; or whenever the stabiliser is removed.

                1.e. Unless already accomplished, before 21 January 2007.

                2.a. Inspect thereafter at intervals not to exceed 6 years.

                2.b. As specified in Requirement 2.b.

                 2.c. (i) After the last flight of the day.

                2.c. (ii) At intervals not to exceed 400 flight hours or 4 months, whichever occurs first.

                2.d. As specified in Requirement 2.d.

                2.e. Unless already accomplished, within 50 flight hours after 21 December 2006, and thereafter at intervals not to exceed 400 flight hours; or whenever the stabiliser is removed.

                3. Unless already accomplished, within 30 days after 21 December 2006.
             This Airworthiness Directive becomes effective on 21 December 2006.
Background:  This Directive requires certain actions in order to improve the horizontal stabiliser fatigue strength.

David Villiers
Delegate of the Civil Aviation Safety Authority

7 November 2006