AD/AMD 50/15 - Take-Off Configuration Warning
1AD/AMD 50/15 - Take-Off Configuration Warning
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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 AMD Falcon 50 and 900 Series Aeroplanes
AD/AMD 50/15 Take-Off Configuration Warning 12/98
Applicability: Mystère Falcon 50 aeroplanes with serial numbers 252, 250 and below, without Modification No F50 M1850 or Dassault Aviation Service Bulletin F50-240 incorporated.
Requirement: Modify the take-off warning system in accordance with Dassault Aviation Service Bulletin F50-240 dated 5 April 1995.
Note: DGAC AD 98-300-022(B).
Compliance: Prior to 8 May 1999.
This Airworthiness Directive becomes effective on 5 November 1998.
Background: This directive introduces a modification whereby the ‘T/O CONFIG’ light on the warning panel illuminates when the park brake is not released and the aircraft is on the ground with at least one of the power levers set at full power.