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AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE
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 39.1 (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/A320/154 Integrated Drive Generator C AD/A320/154 Integrated Drive Generator Connector 8/2004
AD/A320/154 Integrated Drive Generator Connector 8/2004
TX
Applicability: Airbus Industrie model aeroplanes, all serial numbers with IAE V2500 engines, as follows:
A319-131, -132 and -133
A320-231, -232 and -233
A321-131, -231 and -232
Requirement: Ensure the following operational procedures are incorporated in the Aircraft Flight Manual (AFM) either by inserting AFM Temporary Revision 4.02.00/20 or a copy of the following into the AFM:
INTERMITTENT ELECTRICAL POWER SUPPLY INTERMITTENT ELECTRICAL POWER SUPPLY
INTERMITTENT ELECTRICAL POWER SUPPLY
If Sustained flickering of PFD, ND ECAM, MCDU and/or
If Warnings and/or Flags affecting ADR, AP, ELEC data are observed:
IDG Feeder pin/socket arcing can be suspected and then, the following procedures have to be applied:
If occurrences involve one, or a combination, of the following equipment: DMC1,
ECAM upper DU, PFD1,
ND1, MCDU1, ADR1
GEN1...............................................OFF