1、BRITISH STANDARD AEROSPACE SERIES BS EN 9102:2006 Quality systems First article inspection The European Standard EN 9102:2006 has the status of a British Standard ICS 03.120.10; 49.020 BS EN 9102:2006 This British Standard was published under the authority of the Standards Policy and Strategy Commit
2、tee on 31 May 2006 BSI 2006 ISBN 0 580 48399 1 National foreword This British Standard is the official English language version of EN 9102:2006. The UK participation in its preparation was entrusted to Technical Committee ACE/1, International and European aerospace policy and processes, which has th
3、e responsibility to: aid enquirers to understand the text; present to the responsible international/European committee any UK interests informed; monitor related international and European developments and promulgate them in the UK. A list of organizations represented on this committee can be obtain
4、ed on request to its secretary. Cross-references The British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of
5、 the BSI Electronic Catalogue or of British Standards Online. This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summ
6、ary of pages This document comprises a front cover, an inside front cover, the EN title page, pages 2 to 16, an inside back cover and a back cover. The BSI copyright notice displayed in this document indicates when the document was last issued. Amendments issued since publication Amd. No. Date Comme
7、nts enquiries on the interpretation, or proposals for change, and keep EUROPEANSTANDARD NORMEEUROPENNE EUROPISCHENORM EN9102 April2006 ICS03.120.10;49.020 EnglishVersion AerospaceseriesQualitysystemsFirstarticleinspection SriearospatialeSystmesqualitRevuepremier article LuftundRaumfahrtQualittsmanag
8、ement Erstmusterprfung ThisEuropeanStandardwasapprovedbyCENon28October2005. CENmembersareboundtocomplywiththeCEN/CENELECInternalRegulationswhichstipulatetheconditionsforgivingthisEurope an Standardthestatusofanationalstandardwithoutanyalteration.Uptodatelistsandbibliographicalreferencesconcernings u
9、chnational standardsmaybeobtainedonapplicationtotheCentralSecretariatortoanyCENmember. ThisEuropeanStandardexistsinthreeofficialversions(English,French,German).Aversioninanyotherlanguagemadebytra nslation undertheresponsibilityofaCENmemberintoitsownlanguageandnotifiedtotheCentralSecretariathasthesam
10、estatusast heofficial versions. CENmembersarethenationalstandardsbodiesofAustria,Belgium,Cyprus,CzechRepublic,Denmark,Estonia,Finland,France, Germany,Greece,Hungary,Iceland,Ireland,Italy,Latvia,Lithuania,Luxembourg,Malta,Netherlands,Norway,Poland,Portugal, Romania, Slovakia,Slovenia,Spain,Sweden,Swi
11、tzerlandandUnitedKingdom. EUROPEANCOMMITTEEFORSTANDARDIZATION COMITEUROPENDENORMALISATION EUROPISCHESKOMITEEFRNORMUNG ManagementCentre:ruedeStassart,36B1050Brussels 2006CEN Allrightsofexploitationinanyformandbyanymeansreserved worldwideforCENnationalMembers. Ref.No.EN9102:2006:EEN 9102:2006 2 Conten
12、ts Page Foreword 3 1 Scope .4 2 Normative references .4 3 Terms and definitions.4 4 Applicability .6 5 Requirements 6 Annex A (normative) Forms and guidelines to complete the forms.9 Bibliography.16 EN 9102:2006 3 Foreword This European Standard (EN 9102:2006) has been prepared by the European Assoc
13、iation of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of AECMA, prior to its pres
14、entation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by October 2006, and conflicting national standards shall be withdrawn at the latest by October 2006. Attention is drawn to the possib
15、ility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. In December 1998, the Aerospace Industry has established the International Aerospace Quality Group (IAQG) with the pur
16、pose of achieving significant improvements in quality and reductions in cost throughout the value stream. This 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
17、this standard. This standard was reviewed by the Domain Technical Coordinator of AECMA-STANs Quality Domain. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Cze
18、ch Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. 4 1 Scope 1.1 General This standard establis
19、hes requirements for performing and documenting the First Article Inspection (FAI). 1.2 Purpose The purpose of the First Article Inspection is to give objective evidence that all engineering, design and specification requirements are correctly understood, accounted for, verified, and recorded. The p
20、urpose of this standard is to provide a consistent documentation requirement for aerospace components FAI. 1.3 Convention The following convention is used in this standard. The words “shall” and “must” indicate mandatory requirements. The word “should” indicates mandatory requirements with some flex
21、ibility allowed in compliance methodology. An organization is permitted to show that its approach meets the intent of the requirement and this standard. Words “typical”, “example” or “e.g.” show suggestions given for guidance only. “Notes” are used for additional clarification. 2 Normative reference
22、s The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 9103, Aerospace series Quality management sy
23、stems Variation management of key characteristics. EN 9131, Aerospace series Quality management systems Nonconformance documentation.1)3 Terms and definitions For the purposes of this standard, the following terms and definitions apply. 3.1 attribute data result from a characteristic or property tha
24、t is appraised only as to whether it does or does not conform to a given requirement (for example, go/no-go, accept/reject, pass/fail, etc.) 3.2 deliverable software embedded or loadable airborne, space borne or ground support software components that are part of an aircraft type design, weapon syst
25、em, missile or spacecraft 1) Published as AECMA Prestandard at the date of publication of this standard. EN 9102:20065 3.3 design characteristics those dimensional, visual, functional, mechanical, and material features or properties, which describe and constitute the design of the article as specifi
26、ed by drawing requirements These characteristics can be measured, inspected, tested, or verified to determine conformance to the design requirements. Dimensional features include in-process locating features such as target-machined (or forged/cast) dimensions on forgings and castings, and, weld/braz
27、e 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, fluorescent penetrant class, ultrasonic scans, sequence of welding and heat treat). These
28、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 the article is to be made These include any notes, specifications, and lower-level drawings
29、invoked. 3.5 first article inspection (FAI) complete, independent, and documented physical 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/o
30、r other applicable design documents 3.6 first article inspection report (FAIR) forms and package of documentation for a part number or assembly, including FAI results, as per this standard 3.7 first production run parts first group of one or more parts that are the result of a planned process design
31、ed to be used for future production of these same parts Prototype parts, or parts built using methods different from those intended for the normal production process, shall not be considered as part of the first production run. 3.8 multiple characteristics identical characteristics that occur at mor
32、e than one location (e.g. “4 places”) but are established by a single set of drawing requirements. (e.g., rivet hole size, dovetail slots, corner radii, chemical milling pocket thickness) 3.9 product result of a process, which in the context of this standard includes finished detailed parts and asse
33、mblies. It also includes forgings and castings 3.10 reference characteristics characteristics that are used for “information only” or to show relationship These are dimensions without tolerances and refer to other dimensions on the drawing. 3.11 standard catalogue hardware part or material that conf
34、orms to an established industry or national authority published specification, having all characteristics identified by text description, national/military standard drawing, or catalogue item EN 9102:20066 3.12 variables data quantitative measurements taken on a continuous scale For example, the dia
35、meter of a cylinder or the gap between mating parts. 4 Applicability This standard applies to assemblies sub- assemblies, and detail parts including castings and forgings. This standard applies to organizations that are responsible for producing the design characteristics of the product. The organiz
36、ation shall flow down the requirements of this standard to suppliers who produce design characteristics. This standard does not apply to procured Standard catalogue hardware or Deliverable software. 5 Requirements 5.1 Part requirements The organization shall perform FAI on new product representative
37、 of the First Production Run. NOTE 1 For assemblies, the assembly level FAI shall be performed on those characteristics specified on the assembly drawing. NOTE 2 The organization shall not use prototype parts, or parts manufactured using methods different from those intended for the normal productio
38、n process, for the FAI. This standard may be used to verify conformance of a prototype part to design requirements. 5.2 Evaluation activities The organization should conduct the following activities in support of FAI. 1) Review documentation for the manufacturing process (e.g., routing sheets, manuf
39、acturing/quality plans, manufacturing work instructions, etc.) to make sure all operations are complete as planned. 2) Review referenced exhibits supporting the FAI (e.g., inspection data, test data, Acceptance Test Procedures, etc.) for completeness. 3) Review nonconformance documentation (if any),
40、 for completeness. NOTE EN 9131 may be used as a guidance 4) Review material certifications for compliance, as applicable. 5) Verify that approved Special Process sources are used (as applicable), and that the manufacturing planning/routing document calls out the correct specification. 6) Verify tha
41、t Key Characteristic requirements have been met, as applicable (see EN 9103 for guidance). 7) Verify part specific gages and/or tooling are qualified and traceable, as applicable. 8) Verify that every design characteristic requirement is accounted for, uniquely identified and has inspection results
42、traceable to each unique identifier. EN 9102:20067 5.3 Partial or re-accomplishment of First Article Inspection The FAI requirement, once invoked, shall continue to apply even after initial compliance. The FAI requirements may be satisfied by a partial FAI that addresses differences between the curr
43、ent configuration and prior approved configurations. When a partial FAI is performed, the Organization shall complete only the affected fields in the FAI forms. FAI requirements may also be satisfied by previously approved FAI performed on identical characteristics of similar parts produced by ident
44、ical means. When FAI requirements (partial or complete) are satisfied in this manner, identify the approved configuration in the index of part numbers on Form 1. The organization shall perform a full FAI, or a partial FAI for affected characteristics, when any of the following events occurs: 1) A ch
45、ange in the design affecting fit, form or function of the part. 2) A change in manufacturing source(s), process(es), inspection method(s), location of manufacture, tooling or materials, that can potentially affect fit, form or function. 3) A change in numerical control program or translation to anot
46、her media that can potentially affect fit, form or function. 4) A natural or man-made event, which may adversely affect the manufacturing process. 5) A lapse in production for two years or as specified by the customer. 5.4 Nonconformance handling The FAI is not complete until the organization closes
47、 all nonconformances affecting the part and implements corrective actions. The organization shall re-do an FAI for those affected characteristics and shall record the results. 5.5 Documentation 5.5.1 Forms The Annex A of this standard contains forms that comply with the documentation requirements of
48、 this standard. Each field in the forms is designated with a unique reference number. Each field is also identified as: (R) Required: This is mandatory information. (CR) Conditionally Required: This field must be completed when applicable. (i.e. when there exists a Customer requirement, then this field must be filled in) (O) Optional: This field is provided for convenience. Forms contained in the Annex A should be used to document the results of the FAI. NOTE 1 The fields in the forms are colour-coded for convenience. Use of bla
