Document ID: chunk:federal_register_of_legislation:F2006B02381:body:0
Version: federal_register_of_legislation:F2006B02381
Segment Type: other
Provision Reference: 
Character Range: 0–2423

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

    AMD Falcon 50 and 900 Series Aeroplanes

    AD/AMD 50/14
    Amdt 1

    Horizontal Stabiliser Hinge 9/99

               Applicability: Mystere Falcon 50 aircraft with serial numbers 242 through 262, Mystere Falcon 900 aircraft with serial numbers 139 through 169, and Falcon 900 EX aircraft with serial numbers 1 through 21.

                 Requirement: 1. Incorporate the following temporary changes and revisions, as applicable: For the MF 50:
                      Aircraft Flight Manual, TC 46 (TC 12 for S/N 251, 253 on).

                      Maintenance Manual Chapter 5-40, Revision 10.

                 For the MF 900:

                      Aircraft Flight Manual, TC 69.

                      Maintenance Manual Chapter 5-40, Revision 9.

                 For the F 900 EX:

                      Aircraft Flight Manual, TC 14.

                      Maintenance Manual Chapter 5-40, Revision 2.

2.    Perform the check specified in Chapter 5 of the Maintenance Manual at the revision status referenced in Requirement 1 of this Directive, as applicable.

3.    Action in accordance with Dassault Aviation Service Bulletin F 50-274, F 900- 203, or F 900 EX-37, as applicable.

               Note: DGAC AD 1997-370-020 (B) R2 refers.

    Compliance: 1. Unless already accomplished, before 23 May 1998.

2.    Before 27 February 2004 or supplementary 3750 flight cycles, whichever occurs first.

3.    Before 6 years and 2 Months or 3750 flight cycles since new, whichever occurs first.

               The compliance remains unchanged for Requirement 1 of this Directive. This Amendment becomes effective on 9 September 1999.
               Background: A check performed on a test aircraft revealed deformation of the horizontal stabiliser attachment and hinge outer rings which may create excessive play in the hinge.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

           Amendment 1 is issued in response to a new DGAC AD which deletes the mandatory inspection to be performed after a stall as required in Maintenance Manual Chapter 5.50

           The original issue of this Airworthiness Directive became effective on 23 April 1998.