Document ID: chunk:federal_register_of_legislation:F2007L01362:body:0:p2
Version: federal_register_of_legislation:F2007L01362
Segment Type: other
Provision Reference: 
Character Range: 3003–6059

AND LATERAL
   SIDESTICK DEFLECTION, AND SILENTLY CHECKS FULL TRAVEL
   AND CORRECT SENSE OF ALL ELEVATORS AND ALL
   AILERONS, AND CORRECT DEFLECTION AND RETRACTION OF
   ALL SPOILERS, ON THE ECAM F/CTL PAGE."

   Note 1:  The task sharing between the PF and the PNF for the above flight control checks can be amended by each operator depending on its operational policy and local airworthiness requirements.

   Note 2:  The above listed procedure is included in A330 FCOM Vol.3 Rev.19 / Standard Operating Procedures 3.03.10 p3 can be used to amend the flight control check procedure:

      2. Inspection of each elevator servo control in damping position 3CS1 and 3CS2

        a. Perform a dye penetrant inspection of the mode selector valve position transducer attachment lugs in accordance with the instructions of Airbus Service Bulletin (SB) A330-27A3115 Rev 02.

        b. Repeat the inspection in Requirement 2a. of this AD.

   Note 3:  Requirement 1 of this AD is no longer required once both damping servo controls are repetitively inspected as required by Requirement 2b.  However, it is recommended to follow flight control check as procedure given in § 1. which has been introduced in FCOM documentation.

      3. In case of any crack finding, replace the transducer by a spare one or replace the elevator servo control in accordance with the instructions of Airbus SB
      A330-27A3115 Rev 02.

      4. Inspection of spare transducer or elevator servo control

      Do not install a spare transducer or a transducer fitted on a spare elevator servo control as replacement part on an aircraft, unless it has been inspected in accordance with the instructions of Airbus SB A330 27A3115 Rev 02.

                5. Elevator servo-controls PN SC4800-7A and PN SC4800-9

                Modify the four elevator servo-controls in accordance with instructions defined in Airbus SB A330-27-3128.  Mode valve transducer MVT100 removed from servo-controls as required by this Requirement must be discarded.

                6. Elevator servo-controls PN SC4800-10 and PN SC4800-11

                Identify the serial number (SN) of elevator servo controls Part Number (PN) SC4800-10 and SC4800-11.

                If SN is 2324 or below, modify the elevator servo controls (active and damping) of both elevators (LH and RH) in accordance with instructions of Goodrich VSB 4800-27-16 Rev.03. Mode valve transducer MVT100 removed from servo-controls as required by this Requirement must be discarded.

             The installation of the new reinforced mode valve transducer (MVT200) in the elevator servo controls as listed in Requirements 5 and/or 6 cancels the repetitive inspections required by this AD.

             Later approved revisions of the referenced documents may be used in lieu of those listed in this AD.

             Note 4:  EASA AD 2007-0011 dated 9 January 2007 refers.  This AD supersedes DGAC AD F-2003-460.
Compliance:     1. Remains unchanged as 18 March 2004 (the effective date of Amendment 1