EASA Presentation Pascal Medal Head Of Certification Experts - - PowerPoint PPT Presentation
EASA Presentation Pascal Medal Head Of Certification Experts - - PowerPoint PPT Presentation
13 th Military Airworthiness Conference 25 th September 2013 EASA Presentation Pascal Medal Head Of Certification Experts Department EASA Index Summary of European Civil Airworthiness Certification Civil aircraft certification: historical
25th September 2013 EASA Certification Experience 2
Index
Summary of European Civil Airworthiness Certification Civil aircraft certification: historical background From JAA to EASA System EASA Type Certification Process TC/STC procedures Certification Handbook/PID Certification Memos Level Of Involvement (LOI) Operational Suitability Data Items for cooperation RPAS MIDCAS Extended CAW e.g. A 400M
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Civil Type Certification: historical background
Historical Summary of European Civil Airworthiness Certification (1 / 2)
Convention on International Civil Aviation, Chicago in 1944: ICAO ICAO Civil Standards and recommended practices for airworthiness of aircraft adopted by ICAO Council on 01st March 1949 (pursuant to provisions of Article 37 Convention), and were designated as “Airworthiness of Aircraft” Annex 8 to the Convention On 06th June 2000, the Air Navigation Commission reviewed a recommendation of the Continuing Airworthiness Panel to formally introduce the “Type Certificate” concept in Annex 8, (already referred together with type certification process in Airworthiness Technical Manual Doc 9051) ICAO Annex 8 Type Certificate definition: “A document issued by a Contracting State to define the design of an aircraft type and to certify that this design meets the appropriate airworthiness requirements of that State” EASA Framework: Part 21.A.41 definition for Type Certificate 25th September 2013 EASA Certification Experience
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From JAA to EASA System
Historical Summary of European Civil Airworthiness Certification (2 / 2)
- Created on 1970, as an ECAC associated body
- Member States NAAs (44 ECAC members - 2012)
- Initial objective: to develop common airworthiness
certification specs for large transport aeroplanes (industry support – first Airbus programmes A300)
- 1987 extension of scope: common standards for
maintenance – ops – licensing - other aircraft types’ airworthiness specs
- Headquarter in Hoofdorp (NL) – Decisions with no
national legal value
- Aircraft Certification processes done by JAA- multi
NAAs teams - Recommendation for TC issued - To be legally adopted one by one by Member States - Subject to addition of National Differences.
- Standardisation a voluntary process to achieve
mutual recognition status.
- A JAA Member State may accept or not an initial
standardisation visit.
- EU Agency depending from DG-MOVE
- First discussions 1996 – Created by Basic
Regulation 1592/2002, currently EC 216/2008
- Created Sep 02 – Effective starting date 28 Sep 03
- Initial HQ Brussels – Moved to Cologne in 2003 –
Brussels Office opened in 2011
- At a first stage, focused on initial and continued
airworthiness
- Aircraft Certification processes by EASA teams –
TC’s issued and legally valid on all EASA member States with no further action – EASA adopts certification specifications and guidance material.
- Standardisation of Member States NAAs based on
EU Law.
- An EASA team standardisation visit can not be
refused.
- 1st Remit extension 2008: Ops – Licensing –
Aeromedical - Third Country Operators – Training Orgs
- 2nd Remit extension 2009: Aerodromes - ATM
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EASA Type Certification Process
Type Certificate “Basic Regulation” 216/2008
- Article 3.c): “Product” shall mean an
aircraft, engine, propeller
- Article 5.2.a): Products shall have a type
certificate
Objectives for a Certification System:
- Safe
- Common regulatory and certification standards
- Effective
- User friendly and time - cost efficient (single TC
valid in all Member States)
- Meet both Public and Industry expectations
Principles for a Certification System (EU products):
- Rely on three related and required approvals
- Product Type Certification approval – TC
- Design Organisation Approval - DOA
- Production Organisation Approval – POA
- Continued Airworthiness process allow to
legally enforce necessary corrective actions based on in service experience
Advantages:
- Every organisation (EASA, DOA, POA) having their own
roles and responsibilities
- Industry has detailed product knowledge, expertise and
I+D capabilities
- Type Investigation and compliance demonstration by DOAs
approved and audited by EASA
- Independent Checking function inside DOA
- Monitoring and verification by EASA on both organisation
and at product level
- It allows EASA to decide and agree with DOA which
aspects of compliance verification can be delegated to DOA and which ones retained by Agency, allowing to focus on more critical aspects of compliance verification (level of involvement definition)
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EASA Type Certification Process
Advantages:
It allows EASA to decide and agree with DOA which aspects of compliance verification can be delegated to DOA and which ones retained by Agency, allowing to focus on more critical aspects of compliance verification (level of involvement definition)
25th September 2013 EASA Certification Experience
TC Process: Phases
Phase I Technical Familiarization Establishment Type Certif. Basis Phase II: Certification Programme Agreement Phase III: Compliance Determination Phase IV: Final EASA report – TC Issuance TODAY Certification Programme defines on Applicant side
- Programme Milestones
- Responsibles (names,
tasks, competences)
- Working methods
- Applicable requirments
- Proposed testing
- Substantiation
documents, analysis, reports and evidences to be generated Today’s EASA practice with “big” DOA players about compliance docs:
- CAT 1 to be EASA
accepted
- CAT 2: 6 weeks for
EASA comments, after that considered accepted
- CAT 3: DOA approved,
available to EASA on demand TOMORROW
Level of Involvement
Concept (LoI)
- For each means of
compliance demonstration, Agency shall determine LoI
- Objective criteria to
define Agency LoI
- Potential unsafe
conditions, past accidents, etc
- Based on level of
performance showed in the past by Applicant
- Dynamically adapted
as level of performance showed during particular process
- Applicant shall record
justification of compliance
- Subject to
revision/update / change as cert. process progress: LoI may decrease or increase
- Degree of Technology
novelty for both the Agency and applicant
EASA Certification Procedures
TC/STC procedures
EASA - Internal working procedures
Certification Handbook (User Guide)
Certification Memos
EASA - Certification Memoranda
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Level Of Involvement Proposal 1/2
Formally introduce a risk based approach both in product certification and design organisation approvals, Enable the Agency to determine its level of involvement in product certification on the basis of consistently tangible criteria, based on safety risk, Introduce the possibility to approve major changes, major repairs and STC under a DOA privilege, under certain conditions, Establish product certification and design organisation approvals as two separate processes sharing the same common risk based elements, Improve the clarity of part 21 text, by separating the requirements applicable to product certification and design organization approvals
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Level Of Involvement 2/2
Enablers in Part 21, but needs amendments to AMC material to specify the conditions, On going initiatives with Industry participation, pilot projects, Assess & Rely on DOA (rating table), Linked to Safety Management System, Aim is to better tackle the important aspects, focusing resources where really needed,
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Operational Suitability Data
Referenced in Regulation 216/2008, article 5, 7 , 8, 21, annex 4, etc… Amendment to REG 748/2012 part 21 “OSD” (opinion agreed in July 2013)
Paragraph 21-A-15 is laying down the OSD items:
Minimum Syllabus of Pilot Type Rating (+ CS-FC) Minimum Syllabus of Maintenance Certifying Staff (+ CS-MCS) Determination of type or variant for Cabin Crew (+ CS-CCM) MMEL (+ CS-MMEL) Definition of scope of aircraft validation source data to support
- bjective qualification of simulators (+ CS-SIM)
Other Type related Operational Suitability elements
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Cooperation EASA / EDA
Arrangement EASA/EDA signed on 18th June 2013 Support needs to be considered (several options), but EASA certification is funded through a F&C scheme, resources can
- nly be deployed if income is set adequately
Cooperation already in force: Flight Test Center(s): CEV France, Italy, Germany, to be pursued and amplified,
EASA Focal point for Military coordination: Jose Penedo is acting
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Items for Cooperation 1/2
Remotely Piloted Aircraft Systems
MIDCAS, EASA involvement has started
EASA - Policy statements On going projects:
A 400M post TC and CAW-MoU Arrangement(s) for surveillance (organisations) Certification of configurations for Civil /Military use, simplifying the processes,
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Items for Cooperation 2/2
Training activities
EASA workshops & internal training may be opened to military entities, Agreement to use Military facilities for e.g. training of EASA Flight personnel, Temporary staff assignments, TBD
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