1. U.S./Europe International Aviation Safety Conference By: Frédéric Copigneaux, EASA and Mary Cheston, FAA Date: 7 June 2006 “Global Aviation Safety Processes: Refining, Reinforcing, and Streamlining” IP Made Simple… (sort of…) Understanding the US/EC Airworthiness Agreement (Part 2 - The Implementation Procedures) U.S-EU Feedback Forum

2. IP Made Simple 2 7 June 2006 2 Overview The New U.S./EC picture Structure of the Implementation Procedures Content –General, but important… –What's new…

3. IP Made Simple 3 7 June 2006 3 Technical Implementation Procedures The Technical Implementation Procedures for Airworthiness and Environmental Certification (IP) are the third level of the agreement between the European Community and the United States 1.Executive Agreement 2.Annex 3.Technical implementation procedures  These IP are binding for: –The FAA and EASA, –The NAA where referenced in the Agreement and Airworthiness Annex.

4. IP Made Simple 4 7 June 2006 4 Scope Asymetrical Arrangement (1) Only one set of rules and procedures govern products from the US to all 25 EU Member States and EASA. FAA EU MS 1 EU MS 2 EU MS 4 EU MS 5 EU MS 3 EASA

5. IP Made Simple 5 7 June 2006 5 Scope Asymetrical Arrangement (2) Same rules and procedures apply for EASA and qualified Member States (within the scope of EASA design accreditation and per the Annex 1 Appendix.) i.e. FAA’s prior bilateral partners may have different design privileges than in the past. FAA EU MS 1 EU MS 2 EU MS 4 EU MS… EU MS 3 EASA EU MS 25

6. IP Made Simple 6 7 June 2006 6 Approach Build on the experience acquired with current BASA IPAs Improve practical aspects based on experience Increase recognition and privileges in a pragmatic "step-by-step" approach: "Existing reciprocal acceptance plus"

7. IP Made Simple 7 7 June 2006 7 Structure of the IP Sections 1.General 2.Design approval procedures 3.Post design approval procedures 4.Administration of design approvals 5.Export airworthiness procedures 6.Technical assistance 7.Further working arrangements

8. IP Made Simple 8 7 June 2006 8 Appendices A.List of addresses for EASA and FAA B.Coverage of certain prior bilateral agreements (pre-2007) between the US and EU Member States C.FAA and EASA recognised standards D.FAA/EASA Type Validation and Post Type Validation Procedures E.List of Acronyms

9. IP Made Simple 9 7 June 2006 9 1. General… but important ! 1.1Communication Clearly identified mechanisms for communication 1.1.1 Changes in systems 1.1.2Communication (language) 1.1.3Technical consultations 1.1.4 Interpretation and resolution of conflicts 1.1.5Communications involving Designees 1.1.6Split State of Design/State of Manufacture projects through working arrangements

10. IP Made Simple 10 7 June 2006 10 Confidence Building… 1.2Type Certification Standardization Confidence Building Process –To address the (few) TC projects which are still allocated to NAAs 1.3Confidence Building Process for Environmental Certification –Opening the path to some future reciprocal acceptance of findings in the field of environmental certification.

11. IP Made Simple 11 7 June 2006 11 Certification Oversight Board 1.4Certification Oversight Board The body (replacing the CMT) in charge of managing and expanding the IP. –Regular sessions including "industry sessions" –Cooperation in quality assurance and standardisation –Management of US recognition of EU Member States

12. IP Made Simple 12 7 June 2006 12 General… continued 1.5Applicable Requirements, Procedures, and Guidance Material –Lists applicable FARs and certification specifications 1.6Definitions –One set of definitions specific to all activities covered under this IP.

13. IP Made Simple 13 7 June 2006 13 2. Design Approval Procedures General application processes for all design approvals (para. 2.0.9) Other requirements specific to a particular design approval (e.g. TC, STC data package) –Principle is that all applications are transmitted through FAA or EASA first as applicable

14. IP Made Simple 14 7 June 2006 14 Type Validation Principles (TVP) updated to reflect new concept of Joint Certification. New concept, based on validation and technical assistance, to suit the needs of the industry when involved in a cooperative project where industrial partners are responsible for design and production of significant components of a product. VA acts on behalf of the CA for these components. 2. Design Approval Procedures

15. IP Made Simple 15 7 June 2006 15 STCs Where the scope of acceptance is the most asymetrical –EU accepts all US STCs irrespective of State of Design (SoD) of product, –US accepts: EU STC on EU SoD products, EU STC on foreign SoD products after confidence building exercises –Continuation of those accepted today (Germany) –Basic STCs accepted with some exceptions –Commitment to extend the confidence building as more complex projects arrive for EASA approval Fast track process for Basic STCs according to TVP (Appendix D § 6).

16. IP Made Simple 16 7 June 2006 16 AFM and Operational Suitability Approvals AFM signature delegations are more clearly identified –Revisions are removed from PTVP design change classifications. Cooperation on operational evaluation and maintenance review boards.

17. IP Made Simple 17 7 June 2006 17 TSO and ETSO Appliances Simple validation process--building on successful experience. Expanded to include acceptance of findings of compliance for non-(E)TSO functions when included in a TSO appliance. Detailed guidance for ETSOA on APU.

18. IP Made Simple 18 7 June 2006 18 Aeronautical Databases Acceptance of FAA/EASA Letters of Acceptance for data suppliers. IP also lists those communications, navigation, and surveillance standards that are considered equivalent by both authorities (Appendix C).

19. IP Made Simple 19 7 June 2006 19 PMA Parts Building on past acceptance FAA PMA parts automatically accepted, except PMA on critical components, outside of a licensing agreement with the OEM. –Such critical component PMA parts will continue to require EASA STC approval. –FAA and EASA continue to discuss the policy required to strengthen FAA’s technical investigation of critical PMA components so that in the future EASA would be able to accept critical PMA.

20. IP Made Simple 20 7 June 2006 20 Procedures for Environmental Testing IP provides that environmental "test witnessing and other functions" may be delegated to the other authority. Confidence building process is planned to broaden acceptance to environmental findings in the future.

21. IP Made Simple 21 7 June 2006 21 3. Post Design Approval Procedures 3.1Continued Airworthiness 3.2Design Changes 3.3Repair Data 3.4Design Support for Production Based on a Licensing Agreement

22. IP Made Simple 22 7 June 2006 22 Continued Airworthiness (Post TC) Routine sharing of data and structured processes for feedback. –Consultation in cases where the importing authority would unilaterally publish an AD Sharing manual changes that affect airworthiness or operating limitations, life limits, etc. Addresses Alternative Means of Compliance (AMOCs) of general applicability to streamline their recognition, e.g. automatic EASA recognition of FAA AMOC.

23. IP Made Simple 23 7 June 2006 23 Design Changes (Post TC) SYSTEMS are being accepted—applicable classifications are those of the exporting authority. All minor design changes are automatically accepted from each other’s systems. Major design changes by TC /STC holder are accepted according to Post TVP. –Level 1 Major, Level 2, etc. Major design changes by another person than the TC/STC holder should be handled as STCs.

24. IP Made Simple 24 7 June 2006 24 Design Changes (Post TC) FAA alterations are accepted for used aircraft imported in EU (except for alterations on critical components).

25. IP Made Simple 25 7 June 2006 25 Repair Data (Post TC) Streamlining of Reciprocal Acceptance Automatic acceptance of all repair data (minor/major) regardless of the State of Design of the product from: –TC/STC holder, or –third party except repair data on critical components. Fast track process for EASA validation of critical component major repair data when the FAA can confirm that the third party has entered into an arrangement with the TC /STC holder for this data.

26. IP Made Simple 26 7 June 2006 26 Post-Design Approval Airworthiness Acceptance FAA and EASA Acceptance of Post-Design Approvals without additional review FAA review of Major Level 1 changes, critical component repairs EASA review of Major Level 1 changes, critical component PMA, repair data, and alterations

27. IP Made Simple 27 7 June 2006 27 4. Administration of Design Approvals This section contains procedural guidance for: –Transfer of certificates and approvals –Surrenders or withdrawals of certificates and approvals Expectation is early notice/communication from holder and authority.

28. IP Made Simple 28 7 June 2006 28 5. Export Airworthiness Certification Introduces requirement for an EASA Export Certificate of Airworthiness Certifying statements for export –New products and parts and used aircraft –Subject to a prototype demonstration with individual Member States, EASA Form 1 for new parts will be recognized in the US system. Information on aircraft noise and engine emission levels Coordination of exceptions when issuing either: 1)an Export Certificate of Airworthiness OR 2)Authorized Release Cert. (Form 1 or 8130-3)

29. IP Made Simple 29 7 June 2006 29 Used Aircraft All scenarios addressed in the text, e.g. EU aircraft, US aircraft, third country aircraft. –Consultation if the used aircraft had military service history. –Acceptance without further review of: 1)All repair data (including on critical components) on used aircraft imported from the other’s system. 2)FAA alterations (except those on critical components) on used aircraft imported from the United States. FAA is willing to streamline further the issuance of U.S. standard certificate of airworthiness, based on EASA Export Certificate. –Grandfathered such acceptance from Germany and UK

30. IP Made Simple 30 7 June 2006 30 Technical Assistance Complete provisions for technical assistance to be provided to each other: –In support of certification (test witnessing, compliance findings, etc.), –Conformity and surveillance support, –Airworthiness certification support. Requests for release of proprietary data and public access to information

31. IP Made Simple 31 7 June 2006 31 Further Working Arrangements Similar to current bilaterals, additional working arrangements may be developed for specific cases. –e.g. joint certification projects, extensive technical assistance, split SoD/SoM products, etc.

32. IP Made Simple 32 7 June 2006 32 All things have an end… Thanks for listening Any questions ?