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Airworthiness Directives (ADs)

CAA-2004-07-015B

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
2007/01/22
Applicability
AIRBUS aircraft A330-200, A330-300, A340-200 and A340-300 series, all certified models and all serial numbers. The requirements of paragraphs 1, 2 and 4 of this Airworthiness Directive (AD) are not applicable to Airbus A330-200 aircraft on which AIRBUS modification 53969 or 54833 has been embodied in production or AIRBUS Service Bulletin (SB) A330-27-3134 or SB A330-27-3136 has been embodied in service. Reminder: It is the responsibility of the operator to ensure that any spare part that has been or could be installed on the aircraft does not invalidate the compliance of the aircraft with the requirements of this AD.
Model Number
A330 and A340-200 and -300 series
CAA AD Number
CAA-2004-07-015B
Aeronautics Authority of Original AD
EASA
Original AD Number
2007-0009
Effective Date
2007/01/23
Subject
Flight Controls - Elevator Servo Controls Solenoid Valve O-ring Seals - Replacement & Airplane Flight Manual / Master MEL - Temporary Revision & Flight Controls – Elevator Servo Controls – Modification
Reference Publications (Revision/ATA/SB)
ATA 27 Supersedure:DGAC AD F-2004-158(CAA-2004-07-015A) Ref. AOT A330-27A3129 dated June 24, 2004 AOT A330-27A3129 Revision 01 dated July 16, 2004 AIRBUS SB A330-27A3131 AIRBUS SB A340-27A4130 A330 AFM TR 4.02.00/25 issue 02 A340 AFM TR 4.02.00/40 issue 02 A330 MMEL TR N° 01-27/01K issue 01 A330 MMEL TR N° 01-27/02K issue 01 A340 MMEL TR N° 01-27/01M issue 01 A340 MMEL TR N° 01-27/02M issue 01 AIRBUS Service Bulletin A330-27-3134 or later approved revision thereof.
Remarks
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