AD/A320/199 A319 State of Design Airworthiness Directives (Cth)
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.
Airbus Industrie A319, A320 and A321 Series Aeroplanes
| AD/A320/199 | A319 - State of Design Airworthiness Directives | 3/2007 |
Applicability: | A319 series aeroplanes. | ||
Requirement: | 1. Determine the applicability of the Direction Générale de l’Aviation Civile of France (DGAC) Airworthiness Directives (AD) listed in Table 1. | ||
| 2. If it is determined that a DGAC AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD. | |||
| Table 1 | |||
| DGAC AD Number | Effective Date | Title | |
1996-293(B)R1 | 28 December 1996 | Auxiliary Power Unit APIC APS 3200 | |
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 Center Tank (ATA 28) | |
| 2001-363(B) | 18 August 2001 | Oxygen Systems - Inspection of Oxygen Passenger Containers - (Dräeger Type I and II) (ATA 35) | |
| Note 1: DGAC ADs may be accessed via the internet at the following URL:
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Compliance: | For Requirements 1 and 2 - Within 30 days after the effective date of this Directive. |
| This Airworthiness Directive becomes effective on 15 March 2007. | |
Background: | The DGAC ADs listed in Table 1 of this Directive require one time actions for which the compliance date and/or period has passed. CASA has determined that these ADs may be applicable to recently registered Australian 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, not all the ADs listed in Table 1 will be applicable to all A319 series aeroplanes. |
James Coyne
Delegate of the Civil Aviation Safety Authority
17 January 2007
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