Document ID: chunk:federal_register_of_legislation:F2021L00316:body:0:p1
Version: federal_register_of_legislation:F2021L00316
Segment Type: other
Provision Reference: 
Character Range: 0–3556

AIRWORTHINESS DIRECTIVE
On the commencement date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below repeals Airworthiness Directive AD/A320/199 Amdt 1 and issues the following AD under subregulation 39.001 (1) of CASR and subsection 33 (3) of the Acts Interpretation Act 1901. 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.

Airbus A319, A320 and A321 Series Aeroplanes
AD/A320/199 Amdt 2  State of Design Airworthiness Directives  6/2021

Applicability:  A319, A320 and A321 series aeroplanes manufactured prior to 1 January 2002.
Requirement:         1. Determine the applicability of the French Directorate General for Civil Aviation (DGAC) and United States of America Federal Aviation Administration (FAA) Airworthiness Directives (AD) listed in Table 1, as in force from time to time.
                Note 1:  The words "as in force from time to time" require compliance with the most recent version of the referenced document.
                    2.              If it is determined that an AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD.
                Table 1
                AD Number           Effective Date     Title
                1992-164-026(B)     29 August 1992     Reinforcement of nose landing gear wheels
                1992-211-036(B) R1  9 May 1993         Trimmable horizontal stabilizer
                1992-271-039(B) R3  23 March 1996      Electric terminal blocks
                1994-030-050(B)     12 February1994    Junction box and electrical harness on CFM 56-5A

                1994-058-053(B) R1  16 July 1994       IAE V2500-A1 engine fire extinguisher distribution pipe
                1994-167-057(B)     30 July 1994       IAE V2500-A1 sealing of fire wall
                1995-016-063(B)     28 January 1995    Main landing gear shock absorber upper bearing dowel retention
                1996-170-082(B)     7 September 1996   Fuel pump strainer
                FAA AD 97-03-06     6 March 1997       Auxiliary Power International Corporation (APIC) Model APS3200 Auxiliary Power Units
                1997-203-102(B)R1   18 April 1998      Probe Heater Computer

                1998-152-114(B)     18 April 1998      Probe Heater Computer (ATA 30)
                                                       Test Procedures
                1998-451-121(B)     28 November 1998   ILS Receiver (ATA 34)
                1999-361-138(B)     18 September 1999  Litton GPSSU (ATA 34)
                2000-004-142(B)     22 January 2000    Rockwell Collins Radio Altimeter Software Anomalies (ATA 34)
                2001-271(B)         7 July 2001        Loss of Fuel Quantity Indication on Centre Tank (ATA 28)
                2001-363(B)         18 August 2001     Oxygen Systems - Inspection of Oxygen Passenger Containers -(Dräeger Type I and II) (ATA 35)

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