AD/A320/136 Amdt 3 - Digital Distance and Radio Magnetic Indicators

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B01882 In force Legislative Instrument

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AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/A320/136 Amdt 2 and issues the following AD under subregulation 39.1 (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/A320/136

Amdt 3


Digital Distance and Radio Magnetic Indicators 2/2004

 

 

Applicability: Airbus A319 series aeroplanes, all serial numbers (MSM) after 0909, fitted with a Thales Avionics (formerly Sextant or Sextant Avionique) Digital Distance and Radio Magnetic Indicator (DDRMI) with a part number (P/N) listed below.

 

Airbus A320 series aeroplanes, all MSN after 0843, fitted with a Thales Avionics DDRMI with a P/N listed below.

 

Airbus A321 series aeroplanes, all MSN after 1011, fitted with a Thales Avionics DDRMI with a P/N listed below.

 

All other Airbus A319/A320/A321 series aeroplanes fitted with a Thales Avionics DDRMI with a P/N listed below and having a serial number (S/N) different from the S/N recorded in the Aircraft Inspection Report (AIR) delivered from the production line, or with a Thales Avionics DDRMI that has been repaired after May 1999.

 

DDRMI Part Numbers

 

63543-150-3

63543-250-1

63543-253-2

63543-150-2

63543-250-2

63540-041-2

63543-150-1

 

 

 

This Directive is not applicable to aeroplanes with Airbus modification 32414 or 32415 or 32416 or 32417 embodied during production or whilst in service in accordance with Airbus Industrie Service Bulletin (SB) A320-34-1264 Revision 1.

 

Requirement: 1. Unless previously accomplished in accordance with the original issue of this Directive, deactivate the DDRMI in accordance with paragraph 4 of Airbus Industrie All Operator Telex (AOT) A320-34A1262 Revision 01 dated 21 August 2002.

 

2. Dispatch with an inoperative standby compass (Master Minimum Equipment List [MMEL] reference 34-22-02 a) is limited to a ‘B’ rectification interval.

Airbus Industrie A319, A320 and A321 Series Aeroplanes

 

AD/A320/136 Amdt 2 (continued)

 

Note 1: This Airworthiness Directive supersedes the MMEL for the inoperative DDRMI despatch condition (reference 34-57-01). Therefore this Airworthiness Directive may supersede any Minimum Equipment List (MEL) limitation concerning the DDRMI in accordance with AOT A320-34A1262 Revision 01 paragraph 3.5.

 

Note 2: DGAC Telegraphic AD 2002-458(B) R2 refers.

 

Compliance: For Requirement 1 - Remains unchanged as ‘Before 2 October 2002’.

 

For Requirement 2 - As of the effective date of this Amendment. This Amendment becomes effective on 19 February 2004.

Background: Airbus received reports from two operators advising of DDRMI circuit breakers tripping, followed by loss of VOR and DME sources for navigation and displays. Investigations showed the DDRMI power transformer had short circuited, leading to leakage of 115 VAC to systems connected to the DDRMI ARINC 429 busses.

 

The original issue of this Directive required temporary deactivation of the DDRMI to prevent possible loss of essential equipment due to an in-flight failure of the DDRMI.

 

Amendment 1 extended the range of affected aircraft to aircraft that may have DDRMI version B power transformers.

 

Amendment 2 introduces a reference to SB A320-34-1264 Revision 1 as an alternate method of incorporating modification 32414 or 32415 or 32416 or 32417.

 

This Amendment corrects the issue date of AOT 34A1262 Revision 01.

 

The original issue of this Airworthiness Directive became effective on 29 March 2002.

 

Amendment 1 of this Airworthiness Directive became effective on 25 September 2002.

 

Amendment 2 of this Airworthiness Directive became effective on 22 January 2004.


David Villiers

Delegate of the Civil Aviation Safety Authority 8 January 2004


The above AD is notified in the Commonwealth of Australia Gazette on 28 January 2004.

Overview

The Civil Aviation Safety Authority (CASA) introduced Airworthiness Directive (AD) AD/A320/136 Amdt 3 in 2004 to address safety issues related to the Digital Distance and Radio Magnetic Indicators (DDRMI) in Airbus A319, A320, and A321 series aeroplanes. This AD was enacted under the Civil Aviation Safety Regulations 1998, with the primary objective of ensuring the safe operation of these aircraft by rectifying the unsafe condition identified with the DDRMI systems. The directive mandates the deactivation of the DDRMI unless previously accomplished as per the original directive, and specifies limitations on the dispatch of aeroplanes with an inoperative standby compass. This directive is a response to reports of circuit breaker tripping in the DDRMI, which led to the loss of VOR and DME sources for navigation and displays, due to a short circuit in the DDRMI power transformer. The AD is applicable to specific serial numbers and part numbers of the Thales Avionics DDRMI, and it supersedes previous directives and MEL limitations concerning the DDRMI.

Scope and Application

The Airworthiness Directive AD/A320/136 Amdt 3 applies specifically to Airbus A319, A320, and A321 series aeroplanes that are equipped with a Thales Avionics Digital Distance and Radio Magnetic Indicator (DDRMI) with certain part numbers, and manufactured after specific serial numbers. The directive mandates actions to be taken to address an identified unsafe condition related to the potential short-circuiting of the DDRMI power transformer, which can cause significant navigation and display issues. The requirement to deactivate the DDRMI applies to aircraft that have not previously complied with the original issue of this directive, and additionally, it specifies that the dispatch of an aeroplane with an inoperative standby compass is limited to a 'B' rectification interval. Notably, this directive does not apply to aeroplanes that have incorporated specified Airbus modifications during production or in service as per Airbus Industrie Service Bulletin A320-34-1264 Revision 1. The directive is applicable throughout the Commonwealth of Australia and aligns with the overarching regulatory framework of the Civil Aviation Safety Authority (CASA), extending its jurisdictional reach to ensure compliance with safety standards across all relevant aircraft within the specified parameters.

Key Provisions

The Airworthiness Directive (AD) AD/A320/136 Amdt 3, issued under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998 (CASR 1998), applies to specific Airbus A319, A320, and A321 series aeroplanes equipped with a Thales Avionics Digital Distance and Radio Magnetic Indicator (DDRMI) of certain part numbers. The AD mandates deactivation of the DDRMI unless it has already been done in accordance with the original AD issue, and limits the dispatch of these aircraft with an inoperative standby compass to a 'B' rectification interval. The directive is effective for aeroplanes with specified serial numbers (MSN) and does not apply to those with certain Airbus modifications or those repaired after May 1999. This amendment also references an alternate method of incorporating specific modifications through Airbus Industrie Service Bulletin (SB) A320-34-1264 Revision 1. Entities governed by this AD must ensure compliance with the specified requirements. This includes deactivating the DDRMI in line with Airbus Industrie All Operator Telex (AOT) A320-34A1262 Revision 01 dated 21 August 2002, and adhering to the dispatch limitations for aeroplanes with an inoperative standby compass. Additionally, operators must ensure that the compliance deadlines are met for the deactivation of the DDRMI and the dispatch restrictions. Failure to comply with the AD may result in civil or criminal penalties. The AD does not specify exact penalties, but non-compliance with CASR 1998 generally may lead to enforcement actions by the Civil Aviation Safety Authority (CASA), including fines and potential grounding of the aircraft. The severity of the penalties may depend on the extent of the non-compliance and the risk posed to aviation safety.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.