Document ID: chunk:federal_register_of_legislation:F2006B03466:body:0
Version: federal_register_of_legislation:F2006B03466
Segment Type: other
Provision Reference: 
Character Range: 0–786

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 British Aerospace BAe 146 Series Aeroplanes

 AD/BAe 146/12
 Amdt 1

 Elevator `G' Weight Damper 6/89

 Applicability: All models with S/Nos referenced in the Requirement document. Requirement: Action in accordance with BAe SB 27-77-00955 A & C Rev 2. Compliance:               Prior to 30 September 1989.
            Background: This AD contains two concurrent modifications. One to overcome control column oscillation at 2.5 Hz and the other to increase stick centring force following an autopilot cutout. Amendment 1 requires additional work, includes other series aircraft and includes variations dependent on modification state.