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Nya delar med FAA Form 8130-3 BASA USA - EG Presentatör Johan Brunnberg, Flygteknisk Inspektör & Del-M Koordinator Sjö- och luftfartsavdelningen Enheten för operatörer, fartyg och luftfartyg Sektionen för teknisk operation 1

Innehåll Grunder Nya delar Rebuilt PMA Kunskap Sammanfattning Extra 2

Grunder 3

Bilaterala avtal: En möjlighet som kräver kunskap BASA Bilateral Aviation Safety Agreement TIP Technical Implementation Procedures MAG Maintenance Annex Guidance 4

Del-M M.A.501 Installation (a) No component may be fitted unless it is in a satisfactory condition, has been appropriately released to service on an EASA Form 1 or equivalent and AMC M.A.501 (a) Installation 5. For the purpose of Part-M, a document equivalent to an EASA Form 1 may be: (a) a release document issued by an organisation under the terms of a bilateral agreement signed by the European Community; (Motsvarande i Del-145: 145.A.42 (a) 1 och AMC 145.A.42(a) 1. (a)) 5

FAA Form 8130-3 Tillverkningsintyg Underhållsintyg 6

Nya delar med 8130-3 Ska vara certifierade av tillverkaren 7

Att tänka på: 4-Namn på tillverkaren 4-Tillverkarens certifikatnummer 11- New 12- Statement (US krav enligt FAA Order 8130.21H) 13- Vid ny del 13c-Rätt funktion DMIR=Designated Manufacturing Inspection Representative 8

Ny del OBS: 13c-DART=Designated Airworthiness Representative maintenance 9

Ny del OBS: Under 2007 fanns avtal mellan Sverige och USA. Även då skulle nya delar vara certifierade av tillverkaren. 10 DART=DAR maintenance

Nya delar - MAG MAG sid 94, Section B, Appendices, Appendix 1, 10. RELEASE AND ACCEPTANCE OF COMPONENTS. k) Only the following new and used components may be fitted during maintenance. (1) New Components. i) New components should be traceable to the OEM as specified in the Type Certificate (TC) holder s Parts Catalogue and be in a satisfactory condition for installation. A release document issued by the OEM or Production Certificate (PC) holder should accompany the new component. The release document should clearly state that it is issued under the approval of the relevant AA under whose regulatory control the OEM or PC holder works. ii) For U.S. OEMs and PC holders, release should be on the FAA Form 8130-3 as a new part. 13

Rebuilt med 8130-3 Gäller endast för motorer som är certifierade av motortillverkaren 15

Rebuilt Engine Och följande: The [INSERT AIRCRAFT ENGINE MODEL] covered by this certificate conforms to the type design approved under EASA Type Certificate Number [INSERT TYPE CERTIFICATE NUMBER and REVISION LEVEL], is found to be in a condition for safe operation and has undergone a final operational check, 16

Rebuilt Förutsättningar Rebuilt Engines: En EASA Design Condition for Safe operation & AD Operational check Märkt Miljökraven Av motortillverkarken Rätt statement Se TIP 5.1.4 17

PMA med 8130-3 18

PMA Godkännande av delar Design godkännande av delar FAA PMA delar är godkända under följande förutsättningar: PMA delen är en icke kritisk komponent, eller PMA delen överensstämmer med konstruktionsdata framtaget under ett avtal med TCH/STCH enligt 14 CFR 21.303, eller PMA innehavaren har ett EASA STC För övriga PMA krävs ett EASA STC Ref: TIP 2.8.2 & 5.1.8 PMA = Parts Manufacturer Approval FAR 21 = Certification Procedures For Products And Parts 21.303 Application 19

PMA Att tänka på: 4-Namn på tillverkaren 4-Tillverkarens certifikatnummer 12- New 13- Statement 13-NOT Critical (3 st alternativ, se TIP 5.1.8 b) 14- Vid ny del 16-Rätt funktion 20

PMA 13- Export statement saknas. (US krav enligt FAA Order 8130.21H) 21

PMA FAQ på EASA hemsida EASA FAQ: EASA acceptance of US Parts Manufacturers approvals (PMAs) (23/07/2007) Which statements on the FAA Form 8130-3 are acceptable for the import of US PMA parts by a European Maintenance, Repair and Overhaul company (MRO)? Use of EASA Form 1 as an export certification document (03/12/2012) http://easa.europa.eu/the-agency/faqs/international-co-operation 22

PMA Statements The technical implementation procedures (TIP) allow three statements on the FORM 8130-3 in the case of exported PMA parts: For a PMA part which is not a critical component, the following statement should be written in the remarks block of the FAA Form 8130-3: This PMA part is not a critical component. For a PMA part conforming to design data obtained under a licensing agreement from the TC or STC holder according to 14 CFR Part 21, the following statement should be written in the remarks block of the FAA Form 8130-3: Produced under licensing agreement from the holder of [INSERT TC or STC NUMBER]. If the PMA holder is also the holder of the EASA STC design approval which incorporates the PMA part into an EASA certified or validated product, the following statement should be written in the remarks block of the FAA Form 8130-3: Produced by the holder of the EASA STC number XXXXX. Multiple statements were not envisaged, but are acceptable if they provide at least one of the required information and do not contradict each other. Inacceptable Forms 8130-3, e.g. when none of the required statements is present, should be refused and the parts rejected. 23

Kunskap 24

Har alla funktioner tillräckliga kunskaper? Delar från EASA Del-M Del-21 145/MF CAMO (Luftvärdighetsansvarig) Delar från USA Delar från Canada Bilaterala avtal Ankomst -kontroll Auditör Ankomst -kontroll Auditör ARS Delar från Brasilien 25

Exempel på avtal, dokument som behövs för att få kunskap för bedömning av delar från USA: BASA (Bilateral Aviation Safety Agreement) MAG (Maintenance Annex Guidance) TIP (Technical Implementation Procedures) http://easa.europa.eu/document-library/bilateral-agreements FAA Order 8130.21H (Procedures for Completion and Use of the Authorized Release Certificate, FAA Form 8130-3, Airworthiness Approval Tag) (FAA Order 8110.37E (DER Handbook)) 26

Sammanfattning Grunder Nya delar (Certifierade av tillverkaren) Rebuilt Engines (Certifierade av motortillverkaren) PMA (Under rätt förutsättningar) Kunskap 27

Extra: Nya delar. Svar från EASA. Om DMIR, DAR, DER. Exempel på 8130-3 från FAA Order 8130.21H, Appendix A. 28

Nya delar Svar från EASA 29

In accordance with the BASA, EASA M.S. should accept a new part coming from USA if it meets cumulatively the following conditions: 1. It was manufactured under an U.S. production approval; 2. Conforms to an EASA approved design; 3. Is eligible for installation in a product or appliance which has been granted an EASA design approval; 4. It is accompanied by an FAA form 8130-3 authorized release certificate. All these conditions are reflected in MAG. In particular in the supplement example contained in the MAG, item 10 it is stated: New Components. i. New components should be traceable to the OEM as specified in the Type Certificate (TC) holder s Parts Catalogue and be in a satisfactory condition for installation. A release document issued by the OEM or Production Certificate (PC) holder should accompany the new component. ii. For U.S. OEMs and PC holders, release should be on the FAA Form 8130-3 as a new part. 30

This means that only FAA Form 8130-3 issued by U.S OEM s and PC holders are acceptable. There are two possibilities in relation to signature of those forms: 1. Designated Manufacturing Inspection Representative (DMIR) 2. Under the ODA System 31

1-Designated Manufacturing Inspection Representative (DMIR) A DMIR may, among others, do the following: Issue Export certificates of airworthiness and airworthiness approval tags in accordance with subpart L of FAR part 21; A DMIR must possess aeronautical knowledge and experience, be employed by a Production Approval Holder (PAH), or a PAH's approved supplier, and meet the qualification requirements of Order 8100.8. 32

2-Under the ODA System Organisation Designation Authorisation (ODA) is an authorisation by the FAA for an organisation, comprised of an ODA unit(s) using approved procedures, to make approvals on behalf of the FAA. An ODA unit is an identifiable unit of two or more individuals within an organisation that performs the delegated functions on behalf of the FAA. 33

The relevant types of ODA system could be but not limited to: Production Certification ODA (PC ODA). A production certificate (PC) ODA holder may issue airworthiness certificates and approvals, determine conformity, perform evaluation leading to amendment of its production limitation record, and approve minor changes to its quality control manual. To qualify for a PC ODA, an applicant must be an existing PC holder, or have applied for a TC and PC. Technical Standard Order Authorization Holder ODA (TSOA ODA). Holders of a technical standard order authorisation (TSOA) ODA may issue airworthiness approvals and determine conformity of articles, test articles and test set-ups in support of FAA managed TC or STC projects. Only existing technical standard order (TSO) authorization holders qualify for a TSOA ODA. 34

Om DMIR, DAR, DER från FAA hemsida 35

http://www.faa.gov/other_visit/aviation_industry/designees_delegations/designee_types/dmir/ Designated Manufacturing Inspection Representative (DMIR) A DMIR is an individual appointed in accordance with 14 CFR 183.31. A DMIR may, within limits prescribed by, and under the general supervision of, the Administrator, do the following: Issue Original airworthiness certificates for aircraft and airworthiness approvals for engines, propellers, and product parts that conform to the approved design requirements and are in a condition for safe operation; Export certificates of airworthiness and airworthiness approval tags in accordance with subpart L of part 21 of this chapter; Experimental certificates for aircraft for which the manufacturer holds the type certificate and which have undergone changes to the type design requiring a flight test; and Special flight permits to export aircraft. Conduct any inspections that may be necessary to determine that Prototype products and related parts conform to design specifications; and Production products and related parts conform to the approved type design and are in condition for safe operation. Perform functions authorized by this section for the manufacturer, or the manufacturer's supplier, at any location authorized by the FAA. A DMIR must possess aeronautical knowledge and experience, be employed by a Production Approval Holder (PAH), or a PAH's approved supplier, and meet the qualification requirements of Order 8100.8. 36

http://www.faa.gov/other_visit/aviation_industry/designees_delegations/designee_types/dar/ Designated Airworthiness Representative (DAR) A DAR is an individual appointed in accordance with 14 CFR 183.33 who may perform examination, inspection, and testing services necessary to the issuance of certificates. There are two types of DARs, manufacturing and maintenance. Manufacturing DARs must possess aeronautical knowledge, experience, and meet the qualification requirements of Order 8100.8. Maintenance DARs must hold: a mechanic's certificate with an airframe and powerplant rating under 14 CFR part 65, Certification: Airmen Other Than Flight Crewmembers, or a repairman certificate and be employed at a repair station certificated under 14 CFR part 145, or an air carrier operating certificate holder with an FAA-approved continuous airworthiness program, and must meet the qualification requirements of Order 8100.8, Chapter 14. Specialized Experience Amateur-Built and Light-Sport Aircraft DARs Both Manufacturing DARs and Maintenance DARs may be authorized to perform airworthiness certification of light-sport aircraft. DAR qualification criteria and selection procedures for amateur-built and light-sport aircraft airworthiness functions are provided in Order 8100.8. The DAR Directory (PDF)provides a list of DARs, by state and technical discipline 37

Eget tillägg: NOTE on Designated Airworthiness Representative (DAR) A DAR is an individual appointed in accordance with 14 CFR 183.33 who may perform examination, inspection, and testing services necessary to the issuance of certificates. There are two types of DARs, manufacturing (DAR-F) and maintenance (DAR-T). Manufacturing DARs (DAR-F) must possess aeronautical knowledge, experience, and meet the qualification requirements of Order 8100.8. The main difference between DMIR and DAR-F is that: DAR-F can issue 8130-3 only for domestic use. Eget tillägg: Domestic use = Endast för USA 38

DER (Designated Engineering Representative) Se FAA Order 8110.37E DER Handbook http://www.faa.gov/regulations_policies/orders_notices/ index.cfm/go/document.information/documentid/10185 33 39