AD/F50/38 - Auto Flight Idle Stop Mechanism Modification
1AD/F50/38 - Auto Flight Idle Stop Mechanism Modification
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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/F50/38 Auto Flight Idle Stop Mechanism Modification 10/90
Applicability: Model F50 series with serial numbers 20103 through 20108, 20110 through 20159,
20161 through 20173 and 20176 through 20178.
Requirement: Action in accordance with Fokker Service Bulletin F50-76-008 Revision 1.
Note: RLD AD 90-043 refers.
Compliance: Prior to 1 January 1991.
Background: Reports have been received of incidents where the power levers could not be retarded below flight idle during landing. This Directive requires a modification of the mechanism adjustment of the auto flight idle stop located on the engine