1、AECMA STANDARD NORME AECMA AECMA NORM prEN 9102 Edition P 1 January 2001 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES STANDARDIZATION Gulledelle 96 - B-1200 BRUXELLES - Tel. (+32) 2 775 8123 - Fax. (+32) 2 763 3565 ICs: Descriptors: Srie arospatiale Systmes qualit Revue premier arti
2、cle ENGLISH VERSION Aerospace series Quality Systems First article inspection Luft- und Raumfahrt Qualittsmanagement Erstmusterprfung This Herospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green pa
3、per for the needs of AECMA- Members. It has been technically approved by the experts of the concerned Technical Cornmittee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is
4、affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Offcial Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committ
5、ee for Standardization) for formal vote. NOTE This standard is technically equivalent to SAE AS91 02 Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX Edition approved for publication 2001-01-31 Comments should be sent
6、 within six months after the date of publication to Gulledelle 96 AECMA-STAN 8-1200 BRUXELLES Procedure and Process Domain Mr Zagonel aecma 200 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networkin
7、g permitted without license from IHS-,-,-Page 2 prEN 9102: 2001 Foreword In December 1998, the Aerospace Industry has established the International Aerospace Quality Group (IAQG) with the purpose of achieving significant improvements in quality and reductions in cost throughout the value stream. Thi
8、s organization, with representation from Aerospace companies in Americas, Asia and Europe and sponsored by SAE, SJAC and AECMA has agreed to take responsibility for the technical contents of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS unde
9、r license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 9102: 2001 Contents 1 1 . 1 1.2 1.3 2 3 4 5 6 6.1 6.2 6.3 6.4 6.5 6.6 6.7 Introduction . . . Convention References Definitions . . Applicability . . Requirements . Forms Form 1 : Part N
10、umber Accountability Form 2: Product Accountability - Raw Material, Special process(s), Instructions to complete Form 2: Product Accountability - Raw Material, Special Process(s), Functional Testing . Form 3: Characteristic Accountability, Verification and Compatibility Evaluation Form 3 -Continuati
11、on Sheet: Characteristic Accountability, Verification and Compatibility Evaluation Instructions to Complete Form 3 and Form 3 -Continuation Sheet: Characteristic Accountability, Verification and Compatibility Evaluation Instructions to Complete Form 1 : Part Number Accountability Functional testing
12、. . . 4 4 4 4 4 5 6 6 9 10 11 13 14 16 17 18 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 9102: 2001 1 Introduction 1 .I Scope This aero
13、space standard establishes documentation requirements for the First Article Inspection (FAI). 1.2 Purpose The purpose of the First Article Inspection is to provide objective evidence that all engineering design and specification requirements are properly understood, accounted for, verified, and docu
14、mented. The purpose of this standard is to provide a consistent documentation requirement for Aerospace Components First Article Inspection. It is intended that the documentation generated will be a quality record of the Supplier and Customer for review of accountability and planning, for performing
15、 periodic surveillance and audits to verify conformance, for evaluating root cause and corrective action for any non-conformances, and for problem investigations. 1.3 Convent i on The following convention is used in this Standard. 0 The words “shall” and “must” indicate mandatory requirements. 0 The
16、 word “should” indicates mandatory requirements with some flexibility allowed in, be able to show that their approach meets the intent of the requirement and this standard. Words “typical”, “Example” or “e.g.” indicate suggestions given for guidance only. “Notes” are used for additional clarificatio
17、ns. 2 References EN 9100 “Quality Systems- Aerospace - Model for Quality Assurance in Design, Development, Production, Installation and Servicing”, Published by AECMA, Brussels, BELGIUM, January 2000. AS91 O0 “Quality Systems - Aerospace- Model for Quality Assurance in Design, Development, Productio
18、n, Installation and Servicing”, Published by SAE, Warrendale, PA, USA, Nov. 1, 1999. I SJAC91 O0 “Quality Systems-Aerospace-Model for Quality Assurance in Design, Development, Production, Installation and Serving”, Published by JSA, Tokyo, Japan, Dec. 20, 1999 Copyright Association Europeene des Con
19、structeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 9102: 2001 3 Definitions 3.1 attribute a characteristic or property that is appraised in terms of whether it does or does not conf
20、orm (for example, go or no-go), with respect to a given requirement. 3.2 balloon drawing balloon drawing is drawing with each characteristic or requirement clearly marked with unique identifier number. The number may be circled or boxed for easy visual identification. 3.3 design characteristics thos
21、e dimensional, visual, functional, mechanical, and material features or properties, which describe and constitute the design of the article and can be measured, inspected, tested, or verified to determine conformance to the design requirements. Dimensional features include in-process locating featur
22、es such as target-machined (or forgedkast) dimensions on forgings, castings, and weld/braze joint preparation necessary for acceptance of finished joint. Material features or properties may include processing variables and sequences which are specified by the drawing (e.g., heat treat temperature, f
23、luorescent penetrant class, ultrasonic scans, sequence of welding and heat treat) - these provide assurance of intended characteristics that could not be otherwise defined. 3.4 drawing requirements requirements of the drawing (including Parts Lists), specification, or purchasing document to which th
24、e article is to be made, including notes, specifications, and lower-level drawings thereby invoked. 3.5 evaluation measurement, inspection, or testing to determine conformance of a characteristic to drawing requirements. 3.6 first article inspection (FAI) a complete, independent, and documented phys
25、ical and functional inspection process to verify that prescribed production methods have produced an acceptable item as specified by engineering drawings, planning, purchase order, engineering specifications, and/or other applicable design documents. 3.7 first article inspection report (FAIR) the fo
26、rms and package of documentation for a part number or assembly, including FA1 results, as described per this Standard. 3.8 first production run the first group of one or more parts that are the result of a planned process designed to be used for future production of these same parts. Prototype parts
27、, or parts built using methods different from that intended for the normal production process, shall not be considered as part of the first production run. 3.9 inaccessible characteristic a characteristic that cannot be evaluated at any time after it is generated without destroying the part. Inacces
28、sible dimensions may include internal dimensions of castings, internal dimensions of a welded or brazed assembly which are Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without l
29、icense from IHS-,-,-Page 6 prEN 9102: 2001 called out for the assembly. Inaccessible non-dimensional characteristics include material strength, certain metallurgical features and manufacturing processes including non destructive testing. 3.1 O interchangeable and replaceable (I but “First Article In
30、spection” is used for all of these.) 3.12 multiple characteristics identical characteristics which occur at more than one location (e.g., “4 Places”) but are established by a single set of drawing requirements. Examples: bolt hole circles, dovetail slots, corner radii, cooling holes. 3.13 source sub
31、stantiation also referred to as “Engineering Source Approval”. Engineering approval of product and/or part specific process after satisfactory substantiation testing. 3.14 standard catalogue hardware standard parts having all characteristics identified by text description, National/Military Standard
32、 Drawing, or catalogue item. 4 Applicability This Aerospace Standard applies to assemblies and all levels of parts within an assembly, including castings and forgings, and to organizations that are responsible for producing the design characteristics of the product. Suppliers and their Subcontractor
33、s shall be responsible for flow down of the requirements of the applicable revision of this Standard to Subcontractors who produce design characteristics, and for ensuring that Characteristics conform to Customer requirements. NOTE Procured Standard catalog hardware (standard parts) is excluded. 5 R
34、equirements 5.1 First Article Inspection (FAI) shall be performed for a new pari representative of the first production run. This includes all details and sub-assemblies which constitute the end item ordered. The First Article Inspection Record shall not be considered complete until all non-conformi
35、ties are resolved. Prototype parts, or parts built using methods different from that intended for the normal production process, shall not be considered as part of the first Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Resa
36、leNo reproduction or networking permitted without license from IHS-,-,-Page 7 prEN 9102: 2001 production run. 5.2 complete re-accomplishment of the FA1 for affected characteristics is required for the following events: The FA1 requirement once invoked shall continue to apply even after initial compl
37、iance. Partial or 1. 2. 3. 4. 5. 6. A change in the design affecting form, fit or function of the part. A change in manufacturing source (s), processes, inspection method(s), location, tooling or materials with the potential of affecting fit, form or function. When required as part of corrective act
38、ion for a part number with repetitive rejection history (typically, a part with three repeated rejections or as required by customer). A change in numerical control program or translation to another media. A natural or man-made occurrence which may adversely affect the manufacturing process. A lapse
39、 in production for two years or as specified by Customer 5.3 and prior approved configurations. The FA1 requirements may be satisfied by addressing differences between current configuration 5.4 Forms: Forms given in Section 6 of this Standard shall be used to document the results of the First Articl
40、e Inspection. These forms may be generated by any media (e.g. electronic media); however, they must contain all the information required on the forms shown in this Standard (.e. each item listed on form must appear with the same reference number). SAE allows free reproduction of the Forms of this St
41、andard for FAI. An electronic version of the form will also be made available through the Internet along with this standard. All forms shall be completed in English or in a language specified by Customer. 5.5 Quality Records: All First Article Inspection documentation required by this standard shall
42、 be considered Quality/Acceptance Records and shall be retained in accordance with specified Customer requirements. 5.6 Evaluation: The following elements shall be reviewed by the Supplier in support of First Article Inspection validation. Documented evidence of this evaluation shall be made availab
43、le upon Customer request: 1. Manufacturing Routing Sheets. 2. 3. Complete FA1 forms (all pages and continuation sheets as required). Referenced exhibits supporting the FA1 (e.g. CMM data printouts, test data, Acceptance Test Procedures, process certifications, etc.). Copyright Association Europeene
44、des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 8 prEN 9102: 2001 4. Copy of any non-conformance document(s), processed through appropriate Material Review process and associated
45、 corrective action(s). 5. Material certifications, as applicable. 6. 7. Inspection plans. 8. Process capability studies, as applicable. 9. Gauge correlation, as applicable. IO. Marked up drawing (or “ballooned” drawing) that correlates characteristic number from FA1 to the drawing. 11. Part Marking
46、replication Special Process Certifications, as applicable (and operator certification (e.g. NDT, welding), if required). 5.7 Completion of FA1 Forms: The FA1 Forms shall be completed in accordance with form instructions provided within this standard. The following represents the minimum information
47、that shall be recorded on, or attached to, the FA1 Form. 1. Part Number. 2. Serial Number, if applicable. 3. 4. Company Name. 5. 6. 7. Name of Preparer, Title. 8. Date of FAI. 9. Dimensional Characteristics. 1 O. Material and Process Specification(s) and Revision Level. 11. List of processes verifie
48、d, including certification and Supplier name for all customers specified processes. 12. Applicable Drawing Notes. 13. Drawing Zone Locations (including drawing zone numbers). 14. Results of actual measurements and tests for each characteristic and applicable drawing note. 15. Suppliers Review/Approv
49、al Signature. 16. Manufacturing andlor Quality Planning PaperlRouter Number Including RevisionlEdition. 17. Purchase Order/Contract Number including Revision/Edition, if applicable. 18. Non-conformance Document Number(s), if applicable 19. Verification that all Supplier Engineering has been Approved by the Customer when applicable, including Acceptance Test Procedures (ATPs), Quality Test Reports, and Application Software Data. 20. Indicatio
