Document ID: chunk:federal_register_of_legislation:F2009L02804:body:0
Version: federal_register_of_legislation:F2009L02804
Segment Type: other
Provision Reference: 
Character Range: 0–1750

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Fuji FA-200 Series Aeroplanes
AD/FA-200/26  Nose and Main Landing     8/2009
              Gear Cylinder Assemblies

Applicability:  Model FA-200 aircraft.
Requirement:    Action in accordance with Fuji Heavy Industries Ltd Service Bulletin No. 200-013, dated 28 September 1999, or later JCAB approved revision.

                Note:  JCAB AD TCD-5230-2000 refers.
Compliance:     Unless the Detail Instructions of the Requirement document have already been accomplished, within 3 Months after 30 July 2009.  If the epoxy polyamide primer application required by paragraph 12-1(9) and 12-2(9) of the Requirement document has not been done, repeat the Detail Instructions of the Requirement document at intervals not to exceed 1,000 flight hours until the primer is applied.
                This Airworthiness Directive becomes effective on 30 July 2009.
Background:     The manufacturer received reports of corrosion on the inside surfaces of the nose and main landing gear cylinder assemblies.

David Villiers
Delegate of the Civil Aviation Safety Authority

18 June 2009