Document ID: chunk:federal_register_of_legislation:F2006B09839:body:0
Version: federal_register_of_legislation:F2006B09839
Segment Type: other
Provision Reference: 
Character Range: 0–805

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

 Fokker F50 (F27 Mk 50) Series Aeroplanes

 AD/F50/14
 Amdt 1

 Outer Wing End Rib Access Panel 6/89

 Applicability: S/No. 20103 to 20108 and 20110 to 20145 inclusive. Requirement:  Action in accordance with Fokker SB F50-57-004. Rev. 1.
            Note: RLD AD 89-017 Issue 2 refers.

 Compliance: Prior to 31 May 1989.

            Background:  Deformation of the access panel increases the possibility of ice accretion and can cause heavy operation of the aileron during icing conditions. Amendment 1 references Revision 1 to the Requirement Document which lists additional aircraft affected, none of which are presently on the Australian Register.