AD/F50/14 Amdt 1 - Outer Wing End Rib Access Panel
1AD/F50/14 Amdt 1 - Outer Wing End Rib Access Panel
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.