CASA AD: AD/A320/166
Manufacturer: Airbus
Subject: Elevator and Aileron Computer
Applicability: A320 all certified models, all manufactured serial numbers, except aircraft that have incorporated Airbus modification 33317 during production or Airbus Service Bulletin A320-27-1149 whilst in service.

Requirement: Amend the Minimum Equipment List (MEL) by inserting Temporary Revision (TR) TR No 01-27/01H issue 01 of the Master Minimum Equipment List (MMEL) A318/A319/A320/A321 that introduces the operational limitation "Above FL 200, the use of speed brakes lever is limited to its half position" when the aircraft is under MMEL ELAC 1. Later revisions of the above document approved by the DGAC are acceptable for compliance with this Directive. Note: DGAC AD F-2005-013 (EASA Approval 2005-496) refers.
Summary: The Direction G�n�rale de l'Aviation Civile of France has advised that during investigations on an A320 airplane the following critical flight phase was evident: When the aircraft is under MMEL with ELAC 1 (Elevator and Aileron Computer) inoperative or ELAC 1 PITCH FAULT cautions displayed, the loss of SEC 1 (Spoiler and Elevator Computer) in descent when speed brakes are deflected will lead to: - the automatic retraction of speed brakes 3 and 4, - the loss of the double hydraulic pressurization on elevators. In manual mode and at high speed, the retraction of speed brakes 3 and 4 from their full extended position will induce a pitch down effect that cannot be counteracted by the elevator controlled by a single actuator causing the aircraft to pitch down and accelerate.

FMI: http://casa.gov.au/avreg/aircraft/ad/ADfiles/OVER/A320/A320-166.pdf