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Econolyst Ltd is a UK based consultancy firm dedicated to providing technology strategies, project
management, research and training in Additive Layer Manufacturing (ALM) technologies, and Rapid
Manufacturing (RM) applications. Econolyst work with both private sector businesses looking to
implement RM and public sector bodies responsible for assisting companies with technology change.
Econolyst uses a six step ‘RM implementation methodology’ to assist companies around the world to
fast track ALM processes into RM applications. we provide dedicated RM staff development through
Copyright - Econolyst 2008 www.econolyst.co.uk
9
Direct Rapid Manufacturing of Metallic Parts – A UK Industry overview 2008
our ‘RM-Master Classes’, a series of interactive 1 or 2-day training programs for engineers, designer
and business managers. Econolyst also provide support to Colleges, Universities and Research
Technology Organisations across Europe looking to develop Rapid Manufacturing programs of
education for both students and industrialists. Through our ‘RM-Media Service’, we can provide
bespoke packages of video footage, process animations and interviews with leading ALM process and
material vendors, and RM technology users. To maintain our unrivaled knowledge base, we are
engaged in a number of National and European research projects and initiatives focused wholly on
RM. We are always happy to assist clients from both the industrial and educational sectors with
research funding applications and project bid writing.
CONTACT DETAILS
Dr Phil Reeves - Managing Director
Econolyst Ltd
The Silversmiths
Crown Yard
Wirksworth
Derbyshire
DE4 4ET UK
Tel: +44 (0) 1629 824447
Fax: +44 (0) 870 1334869
Email: phil.reeves@econolyst.co.uk
Web: www.econolyst.co.uk
Copyright - Econolyst 2008 www.econolyst.co.uk
10
AIRWORTHINESS DIRECTIVE
No F-2005-013
Distribution:
B
Issue date:
January 19, 2005
Page :
1/2
This Airworthiness Directive is published by the DGAC on behalf of
EASA, Airworthiness Authority of the State of Design for the affected
product, part or appliance.
Translation of « Consigne de Navigabilité » of same
number.
In case of difficulty, reference should be made to
the French issue.
Direction
générale
de
l’aviation
civile
France
GSAC
publication
No person may operate an aircraft to which an Airworthiness Directive applies,
except in accordance with the requirements of that Airworthiness Directive,
unless otherwise agreed with the Authority of the State of Registry.
Corresponding foreign Airworthiness Directive(s):
Not applicable
Airworthiness Directive(s) replaced:
None
Person in charge of airworthiness:
AIRBUS SAS
Type certificate(s) No. 180
TCDS No 180
Type(s):
A320 aircraft
ATA chapter:
27
Subject:
Flight controls - ELAC 1 computer
1. EFFECTIVITY:
AIRBUS A320 all certified models, all manufactured serial numbers, except aircraft that have received
AIRBUS modification 33317 in production or AIRBUS Service Bulletin A320-27-1149 in service.
2. REASONS:
During investigations on A320, a critical flight phase has been evidenced.
In the case 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 pressurisation 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.
The aircraft pitches down and accelerates.
For this reason, this Airworthiness Directive (AD) renders mandatory an operational limitation.
3. MANDATORY ACTIONS AND COMPLIANCE TIMES:
From the effective date of this AD, apply the following:
Insert in the Minimum Equipment List (MEL) of the aircraft, the 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, and apply this procedure.
n/GH
AIRWORTHINESS DIRECTIVE
No F-2005-013
Distribution:
B
Issue date:
January 19, 2005
Page:
　
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