Document ID: chunk:federal_register_of_legislation:F2005L02066:body:0:p2
Version: federal_register_of_legislation:F2005L02066
Segment Type: other
Provision Reference: 
Character Range: 4657–5783

the applicable TR(s) listed in the above Table has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of the applicable TR may be removed from the AFM.
                Note 2:  FAA AD 2005-13-21 Amdt 39-14158 refers.
Compliance:     For Requirements 1 and 2 - Within 12 months after the effective date of this Directive.
                For Requirement 3 - Within 1 month after the effective date of this Directive or concurrently with the replacement required by Requirement 2, whichever occurs first.
                This Airworthiness Directive becomes effective on 1 September 2005.
Background:     This Directive requires the inspection of the ACU to determine the part number and, if necessary, the replacement of the ACU with a new, improved ACU.  The Directive also requires the revision of the AFM Limitations Section.  These actions are intended to prevent uncommanded movement of the horizontal stabilizer, which could result in reduced controllability of the aeroplane.

David Villiers
Delegate of the Civil Aviation Safety Authority

21 July 2005