BS ISO 6517-2013 en_1687 Air cargo Certified lower deck containers Design and testing《空运货物.被认证的下甲板集装箱.设计和测试》.pdf

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1、BSI Standards Publication BS ISO 6517:2013 Air cargo Certified lower deck containers Design and testingBS ISO 6517:2013 BRITISH STANDARD National foreword This British Standard is the UK implementation of ISO 6517:2013. It supersedes BS M 70:1993 which is withdrawn. The UK participation in its prepa

2、ration was entrusted to Technical Committee ACE/57, Air cargo and ground support equipment. A list of organizations represented on this committee can be obtained on request to its secretary. This publication does not purport to include all the necessary provisions of a contract. Users are responsibl

3、e for its correct application. The British Standards Institution 2013. Published by BSI Standards Limited 2013 ISBN 978 0 580 79162 8 ICS 49.120; 55.180.30 Compliance with a British Standard cannot confer immunity from legal obligations. This British Standard was published under the authority of the

4、 Standards Policy and Strategy Committee on 31 July 2013. Amendments issued since publication Date Text affectedBS ISO 6517:2013 ISO 2013 Air cargo Certified lower deck containers Design and testing Fret arien Conteneurs certifis de pont infrieur Conception et essais INTERNATIONAL STANDARD ISO 6517

5、Third edition 2013-07-01 Reference number ISO 6517:2013(E)BS ISO 6517:2013ISO 6517:2013(E)ii ISO 2013 All rights reserved COPYRIGHT PROTECTED DOCUMENT ISO 2013 All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized otherwise in any form or by any m

6、eans, electronic or mechanical, including photocopying, or posting on the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below or ISOs member body in the country of the requester. ISO copyright office Case postale 56 CH-1211 Gene

7、va 20 Tel. + 41 22 749 01 11 Fax + 41 22 749 09 47 E-mail copyrightiso.org Web www.iso.org Published in SwitzerlandBS ISO 6517:2013ISO 6517:2013(E) ISO 2013 All rights reserved iii Contents Page Foreword iv Introduction v 1 Scope . 1 2 Normative references 1 3 Container sizes and identification . 3

8、4 Requirements 3 4.1 General . 3 4.2 Airworthiness approval . 4 4.3 Materials . 4 4.4 Construction 4 4.5 Performance 7 4.6 Design loads 8 4.7 Environment . 8 5 Testing . 9 5.1 Ultimate load tests . 9 5.2 Operation tests 9 6 Markings 11 7 Customs/security sealing .12 8 Manufacturers instructions 13 9

9、 Quality control .13 9.1 Design and production 13 9.2 Operations 14 Bibliography .21BS ISO 6517:2013ISO 6517:2013(E) Foreword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Stand

10、ards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also ta

11、ke part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. The procedures used to develop this document and those intended for its further maintenance are described in the ISO/IEC Directives, Part 1. In p

12、articular the different approval criteria needed for the different types of ISO documents should be noted. This document was drafted in accordance with the editorial rules of the ISO/IEC Directives, Part 2. www.iso.org/directives Attention is drawn to the possibility that some of the elements of thi

13、s document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of any patent rights identified during the development of the document will be in the Introduction and/or on the ISO list of patent declarations received. www.iso.

14、org/patents Any trade name used in this document is information given for the convenience of users and does not constitute an endorsement. The committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 9, Air cargo and ground equipment. This third edition canc

15、els and replaces the second edition (ISO 6517:1992), which has been technically revised to take into account ISO 21100 and TSO/ETSO C90d.iv ISO 2013 All rights reservedBS ISO 6517:2013ISO 6517:2013(E) Introduction The basic functions of lower deck air cargo containers are: a) the unitization of bagg

16、age, cargo or mail during ground handling and transportation, and b) the restraint of their contents against accelerations encountered in flight. Throughout this International Standard, the minimum essential criteria are identified by use of the key word “sha ll”. Recommended c r iter ia a re ident

17、if ied by use of t he key word “shou ld” a nd, while not ma ndator y, are considered to be of primary importance in providing safe, economical and usable containers. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate

18、 methods to provide an equivalent level of quality and safety. The requirements of this International Standard are expressed in the applicable SI units, with approximate inch-pound units conversion between brackets for convenience in those countries using that system. Where it is deemed necessary to

19、 use exact values, the SI unit ones are to be used. Per exception, the exact figures are those in inches for container base overall outside dimensions. ISO 2013 All rights reserved vBS ISO 6517:2013BS ISO 6517:2013Air cargo Certified lower deck containers Design and testing 1 Scope 1.1 This Internat

20、ional Standard covers the minimum design and operational testing requirements for general purpose base-restrained containers exclusively intended for the lower deck compartments of main line civil transport aircraft, capable of being used by either airlines or shippers and requiring airworthiness au

21、thority approval (certification). NOTE 1 The metric equivalents for dimensions have been rounded up or down to the nearest millimetre, except in critical dimensions. Masses have been rounded up to the nearest kilogram and forces have been rounded up to the nearest 10 N. NOTE 2 Containers with other

22、base sizes than those specified by this International Standard can also be built to a lower deck contour, but they need not be carried exclusively on the lower deck. See ISO 10327. 1.2 This International Standard does not cover the performance requirements and ultimate load testing parameters for ap

23、proval by airworthiness authorities (certification), which are covered in ISO 21100 or, for units approved prior to 2012, ISO 8097:2001. The design and operational testing requirements of this International Standard are additional to those of these standards. 2 Normative references The following doc

24、uments, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. ISO 4116:1986, Air cargo

25、 equipment Ground equipment requirements for compatibility with aircraft unit load devices ISO 7166:1985, Aircraft Rail and stud configuration for passenger equipment and cargo restraint ISO 8097:2001, Aircraft Minimum airworthiness requirements and test conditions for certified air cargo unit load

26、devices (Endorsement of NAS 3610 10th edition) ISO/TR 8647:1990, Environmental degradation of textiles used in air cargo restraint equipment ISO 10046:1996, Aircraft Methodology of calculating cargo compartment volumes ISO 10327:1995, Aircraft Certified aircraft container for air cargo Specification

27、 and testing ISO 11242:1996, Aircraft Pressure equalization requirements for cargo containers ISO 21100: 1) , Air cargo unit load devices Performance requirements and test parameters CAAC CCAR-21, Certification Procedures for Products and Parts 2) CAAC CCAR-25, Airworthiness Standards Transport Cate

28、gory Airplanes, paragraph 25.855, Cargo or baggage compartments, and Appendix F 2) CAAC CCAR-121, Air Carriers Certification and Operations system 2) 1) To be published. (Technical revision of ISO/PAS 21100:2011.) 2) The Civil Aviation Administration of China (CAAC) listed documents constitute the C

29、hinese government transport aircraft airworthiness approval Regulations. INTERNATIONAL ST ANDARD ISO 6517:2013(E) ISO 2013 All rights reserved 1BS ISO 6517:2013ISO 6517:2013(E) CAAC Chinese Technical Standard Order CTSO C90d Cargo pallets, nets and containers 2) EASA Part 21 Certification of aircraf

30、t and related products, parts and appliances, and of design and production organisations (Commission Regulation (EU) No 748/2012) 3) EASA CS-25 Certification Specifications for Large Aeroplanes, paragraph 25.855, Cargo or baggage compartments, and Appendix F 3) EASA (European Aviation Safety Agency)

31、 EU-OPS 1.035 Quality system 3) EASA European Technical Standard Order ETSO C90d Cargo pallets, nets and containers (Unit Load Devices) 3) Japanese Airworthiness Standard Part 3 (Civil Aeronautics Law Article 10 4) 4) U.S. Code of Federal Regulations Title 14 CFR Part 21 Certification Procedures for

32、 Products and Parts 5) U.S. Code of Federal Regulations Title 14 Part 25 Airworthiness Standards: Transport Category Airplanes (“14 CFR Part 25”), paragraph 25.855, Cargo or baggage compartments, and Appendix F 5) U.S. Code of Federal Regulations Title 14 CFR Part 121 Air carriers certification and

33、operation 5) U.S. Federal Aviation Administration Advisory Circular AC 120-59 Air carriers internal evaluation programs 5) U.S. Federal Aviation Administration Technical Standard Order TSO C90d Cargo Pallets, Nets and Containers 5) EUROCAE ED-14G, Environmental conditions and test procedures for air

34、borne equipment 6) NOTE 3 Also see informative references in Bibliography. 3) The listed EASA documents constitute the European governments transport aircraft airworthiness approval Regulations, and can be obtained from the European Aviation Safety Agency (EASA), Otto Platz 1, Postfach 101253, D-504

35、52 Cologne, Germany, or its website at www.easa.europa.eu.int. 4) Japanese Airworthiness Standard Part 3 (ISBN 4-89279-661-1) constitutes the Japanese government transport aircraft airworthiness approval Regulations, and can be obtained from the Civil Aviation Bureau (CAB) of the Ministry of Land, I

36、nfrastructure and Transport, Tokyo, Japan, or its website at www.mlit.go.jp/en. 5) The listed FAA documents constitute the U.S.A. government transport aircraft airworthiness approval Regulations, and can be obtained from the U.S. Government Printing Office, Mail Stop SSOP , Washington DC 20402- 9328

37、, or its website at www.gpoaccess.gov. 6) EUROCAE ED-14G can be obtained from the European Organisation for Civil Aviation Equipment, 102 rue Etienne Dolet, 92240 Malakoff, France, or its website at www.eurocae.eu.2 ISO 2013 All rights reservedBS ISO 6517:2013ISO 6517:2013(E) 3 Container sizes and i

38、dentification 3.1 The overall maximum dimensions of the containers are shown in Figures 2 to 6. They embrace two base sizes: Size K: 1 562 mm 1 534 mm (61,5 in 60,4 in), Size L: 3 175 mm 1 534 mm (125 in 60,4 in). and seven contours (see 3.2 NOTE): Contour C: nominal overall width 2 337 mm (92 in) (

39、see Figure 3), Contour E: nominal overall width 2 007 mm (79 in) (see Figure 2), Contour F: nominal overall width 4 064 mm (160 in) (see Figure 4), Contour G: nominal overall width 2 007 mm (79 in) (see Figure 6), Contour H: nominal overall width 2 438 mm (96 in) (see Figure 6), Contour P: nominal o

40、verall width 3 175 mm (125 in) (see Figure 4), Contour U: nominal overall width 4 724 mm (186 in) (see Figure 5). 3.2 Container types complying with this International Standard are identified according to their ISO 21100 configuration by a type code composed of three letters 7) : a) the first letter

41、 A denoting a certified aircraft container complying with the performance requirements of ISO 21100 type 2 or, for units approved prior to 2012, ISO 8097 type II; b) the second letter denoting the base size in accordance with ISO 21100; c) the third letter denoting the contour determined in accordan

42、ce with ISO 10046 (see NOTE 3). The identification code shall be prominently marked on two opposite sides of the container (see 6.3). EXAMPLE A certified aircraft container (A) of base size 3 175 mm 1 534 mm (125 in 60,4 in) (size L) and of nominal overall width 3 175 mm (125 in) (contour P) shall b

43、e designated as follows: ALP. NOTE The container type codes third (contour) digit is subject to change to accommodate evolving airline needs. Check the latest yearly edition of IATA Unit Load Devices Regulations Standard Specifications 40/1 and 50/0 Appendix E (references 6and 7in Bibliography) for

44、any code changes. 4 Requirements 4.1 General 4.1.1 The container shall consist of a complete structural enclosure meeting ISO 21100 type 2 or ISO 8097 type II performance requirements, and all the requirements of the present clause. 4.1.2 The container manufacturer shall provide the user instruction

45、s for the maintenance and repair of the container necessary to maintain its continuing airworthiness qualification (see 9.1). 7) The type code is, by industry consensus, under custody of and assigned by the International Air Transport Association (IATA), ULD Registrar, 800 Place Victoria, P .O. Box

46、113, Montral, Qubec H4Z 1M1, Canada, website www.iata.org. ISO 2013 All rights reserved 3BS ISO 6517:2013ISO 6517:2013(E) 4.1.3 The manufacturer shall provide the user instructions for installation, operation and servicing of the container (see 8.2), which shall comply with load distribution and cen

47、tre of gravity conditions of ISO 21100 and refer to methods to achieve the centre of gravity location control requirements. 4.1.4 The design, materials and construction of the container shall be of aircraft quality. Maintainability and reparability shall be a factor in the design to ensure the minim

48、um need for maintenance, and shall ensure that such maintenance and repair can be accomplished with ease and at minimum cost. 4.1.5 The structure shall be designed to make the maximum internal cross-section available for loading cargo, within the limits of structural design and the space required fo

49、r latching. 4.1.6 The materials and design shall be selected to provide for an empty (tare) weight as low as possible, consistent with maintainability objectives (see 4.1.4). NOTE A direct environmental impact of container use is that their weight results in additional fuel burn by aircraft. Therefore, apart from economic advantages, reducing container weight as much as possible to still meet performance objectives is a highly effective environmental contribution