2. THE PF PRESSES THE PEDAL DISC PUSHBUTTON ON THE NOSEWHEEL TILLER, AND SILENTLY APPLIES FULL LEFT RUDDER, FULL RIGHT RUDDER, AND NEUTRAL. THE PNF CALLS OUT "FULL LEFT", "FULL RIGHT", "NEUTRAL", AS EACH FULL TRAVEL/NEUTRAL POSITION IS REACHED. 3. THE PNF APPLIES FULL LONGITUDINAL 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. |