Document ID: chunk:federal_register_of_legislation:F2006B02708:body:0:p2
Version: federal_register_of_legislation:F2006B02708
Segment Type: other
Provision Reference: 
Character Range: 2980–4009

Note 2: FAA AD 2003-11-19 Amdt 39-13178 refers.

           Compliance: For Requirement 1 - Within 6 months after the effective date of this Directive. For Requirement 2 - Within 18 months after the effective date of this Directive.
           For Requirement 3 - Before reinstallation of the autopilot unit after the modification required by Requirement 2.

           For Requirement 4 - After 7 February 2004.

           This Airworthiness Directive becomes effective on 7 August 2003.

           Background: This Directive requires, under certain conditions, replacement of the autopilot pitch control computer with a modified computer, testing of the modified system and revision of the AFM. These actions are intended to prevent undesirable and potentially dangerous pitch oscillations during coupled instrument landing system (ILS) approaches.

 Jim Coyne
 Delegate of the Civil Aviation Safety Authority 26 June 2003

 The above AD is notified in the Commonwealth of Australia Gazette on 16 July 2003.