Document ID: chunk:federal_register_of_legislation:F2006B09787:body:0
Version: federal_register_of_legislation:F2006B09787
Segment Type: other
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Character Range: 0–852

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

 Fokker F28 Series Aeroplanes

 AD/F28/52
 Amdt 1

 Rudder Pedal Adjustment Mechanism Stops 7/88

 Applicability: All model F28 with S/Nos 11003 to 11224 inclusive, 11226, 11991 and 11992. Requirement:               Action in accordance with Fokker SB F28/27-158 Revision 1.
            Note: RLD AD 85-78 refers.

 Compliance: Prior to 1 September 1986.

            Background: The possibility exists of insufficient rudder deflection when the rudder pedals are adjusted to the maximum forward position. This Directive requires the installation of stops in the adjustment mechanism. Amdt 1 reflects Revision 1 to the SB which removes S/Nos 11225, 11227 through 11231 from the Applicability listing.