Aircraft Modification Project under EASA DOA System

EXPLOITATION AÉRIENNE
Navigabilité des Aéronefs
réf. MODADV
Code OACI 133
ENAC - TA
Aircraft Modification Project under EASA
DOA System - Advanced
FORMATION EN ANGLAIS
DURÉE
2.5 jours
PLACES OFFERTES
20
Objectifs
To know what to do, technically and administratively, under Part 21 regulation, to get an STC
approval, and to understand the global regulatory environment for designing an STC.
DATES ET LIEUX
ENAC Toulouse :
7 avril 2015 au 9 avril 2015
ENAC Toulouse :
4 avril 2016 au 6 avril 2016
Participants concernés
Engineers and executive involved in aircraft airworthiness.
CONDITIONS DE
PARTICIPATION
Frais pédagogiques :
Catégorie B
2016 : 945 €
Informations pratiques :
voir en fin de catalogue
CONTACT ADMINISTRATIF
ENAC
Eric PFEIFFER
Tél. : +33 (0)5 62 17 43 43
Bulletin d'inscription obligatoire :
voir en fin de catalogue
Contenu
Numerous actors (such as air carriers, MRO or specialised companies) design their own major
modifications to be installed onto aircraft. These major modifications, which are not designed
by the type certificate holder of the concerned aircraft, are called STC (supplemental type
certificate).
This module intends to provide a wide knowledge about the STC, and to describe the
interactions between STC and existing organisations approvals (especially DOA, but also
POA, CAMO and approval of maintenance organisations).
Introduction to applicable international airworthiness regulations and STC key
notions
ICAO requirements for changed products
Reminder on EASA regulations and delegation system
EASA Part 21 subpart E
Regulatory environment of the production
Presentation of the different actors involved during a change project (DOA,
POA, MOA, CAMO and authorities) and of their interactions
General responsibility for control of aircraft configuration
Interactions between approved organisations during change project
STC project development and coordination with EASA
STC validation by foreign authorities
Reminder of the principles for design and certification, using DOA
documentary system
Demonstration of capability – DOA
Design and certification procedures principles
Establishment of a certification plan
Procedures for coordination with production
Presentation of the key notions for conducting flight tests during an STC
development program
Notion of permit to fly
Flight conditions and permit to fly
Specific requirements and complex modifications
Issues related to human factors in design organisations
Notion of human factor
The “dirty dozen” of deign organisations
Legal responsibility of DOA authorised signatories and related actors
RESPONSABLE(S) DU STAGE
Method
Muriel GIZARDIN [Aéroport Sûreté
Météo]
Lectures
For information only : 18 hours
www.enac.fr
ENAC : [email protected]
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