Document ID: chunk:federal_register_of_legislation:F2020L01118:body:0
Version: federal_register_of_legislation:F2020L01118
Segment Type: other
Provision Reference: 
Character Range: 0–7466

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and 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. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct an 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.

Swift Museum Foundation GC-1A and GC-1B Series Aeroplanes
AD/GC-1/1  State of Design Airworthiness Directives  18/2020

Applicability:  Swift Museum Foundation Inc. GC-1A and GC-1B.
Requirement:       1. Determine the applicability of the United States of America Federal Aviation Administration (FAA) Airworthiness Directives (AD) listed in Table 1.
                   2. If it is determined that an FAA AD listed in Table 1, as in force from time to time, is applicable and has not been previously accomplished, perform the actions required by that AD.
                   Table 1
   FAA AD          Issue Date                                                                                                                                                                                   Title
   56-16-04                                                                                                                                                                                                   Landing Gear Torque Knees
   51-10-05                                                                                                                                                                                                   Fuselage Reinforcement Rework
   51-02-02                                                                                                                                                                                                   Asbestos Cloth Removal
   48-28-01                                                                                                                                                                                                   Fuselage Bulkhead Rework
   47-25-07                                                                                                                                                                                                   Oil Radiator Outlet Sleeve
   47-25-06                                                                                                                                                                                                   Carburettor Flexible Air Duct
   47-06-06                                                                                                                                                                                                   Engine Breather Line
   47-06-05                                                                                                                                                                                                   Battery Vent Plugs
   47-06-04                                                                                                                                                                                                   Landing Gear Washers
   47-06-03                                                                                                                                                                                                   Elevator Cable Collars
   47-06-02                                                                                                                                                                                                   Landing Gear Retraction Placard
   46-42-01                                                                                                                                                                                                   Cabin Heater Valve Replacement

                                                                                                                                   FAA AD                                                                                                                                                                                                                                                                                                  Issue Date                            Title
   46-33-02                                                                                                                                                                                                                                                                                                                                                                                                                                 Fuselage Bulkhead Flange Stiffener
   46-23-04                                                                                                                                                                                                                                                                                                                                                                                                                                 Addition of Rivets in Wing Skin
Note 1:  FAAs ADs may be accessed via the internet at the following URL:
      http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/Frameset?OpenPage
Note 2:  The words "as in force from time to time" require compliance with the most recent version of the referenced document.
Compliance:                                                                                                                     If a certificate of airworthiness has not been issued for the aircraft - before issue of the certificate of airworthiness.
                                                                                                                                If a certificate of airworthiness has been issued for the aircraft - within 6 months after the commencement date of this Directive.
                                                                                                                                This AD commences on 17 September 2020.
Background:                                                                                                                     The FAA ADs listed in Table 1 of this Directive require once-only actions for which the compliance date and/or period has passed.  CASA has determined that these ADs may be applicable to Australian registered aircraft.  This Directive is issued to ensure all State of Design ADs are complied with.
                                                                                                                                CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, some of the ADs listed in Table 1 will not be applicable to some aeroplanes.

Pieter van Dijk
Delegate of the Civil Aviation Safety Authority
25 August 2020