AD/A330/57 Amdt 2 - Engine - Icing Conditions During Descent - Operational Procedure (Cth)

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 revokes Airworthiness Directive (AD) AD/A330/57 Amdt 1 and issues the following 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 A330 Series Aeroplanes AD/A330/57 Amdt 2 Engine - Icing Conditions During 10/2007 Descent - Operational Procedure

Applicability: Airbus A330-201, -202, -203, -301, -302 and -303 series aeroplanes, all serial numbers except those on which Airbus modification 56554 has been embodied during production or Airbus SB A330-73-3048 dated 6 June 2007 has been embodied whilst in service. Requirement: 1. If not previously accomplished in accordance with either AD/A330/57 (EASA AD 2006-0212-E) or AD/A330/57 Amdt 1 (EASA AD 2006-0259-E), incorporate the following amendment into the Aircraft Flight Manual (AFM): "ICING CONDITIONS EXPECTED DURING DESCENT

• If icing conditions (including ice crystals) are expected during descent:

• At top of descent, or at the latest before entering the expected icing conditions:

Select ENG ANTI ICE and WING ANTI ICE to ON.

Select PACK FLOW at HI.

• Below 10 000 ft: