1、BS ISO 4118:2016Air cargo Non-certifiedlower deck containers Design and testingBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS ISO 4118:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of ISO 4118:2016.It supersedes BS ISO 4118:
2、2000 which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/57, Air cargo and ground support equipment.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the nec
3、essaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2016.Published by BSI Standards Limited 2016ISBN 978 0 580 81689 5ICS 49.120; 55.180.30Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Stan
4、dard was published under the authority of theStandards Policy and Strategy Committee on 31 July 2016.Amendments/corrigenda issued since publicationDate T e x t a f f e c t e dBS ISO 4118:2016 ISO 2016Air cargo Non-certified lower deck containers Design and testingFret arien Conteneurs non-certifis d
5、e pont infrieur Conception et essaisINTERNATIONAL STANDARDISO4118Fourth edition 2016-07-01Reference numberISO 4118:2016(E)BS ISO 4118:2016ISO 4118:2016(E)ii ISO 2016 All rights reservedCOPYRIGHT PROTECTED DOCUMENT ISO 2016, Published in SwitzerlandAll rights reserved. Unless otherwise specified, no
6、part of this publication may be reproduced or utilized otherwise in any form or by any means, 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
7、 body in the country of the requester.ISO copyright officeCh. de Blandonnet 8 CP 401CH-1214 Vernier, Geneva, SwitzerlandTel. +41 22 749 01 11Fax +41 22 749 09 47copyrightiso.orgwww.iso.orgBS ISO 4118:2016ISO 4118:2016(E)Foreword vIntroduction vi1 Scope . 12 Normative references 13 Terms and definiti
8、ons . 24 Dimensions and ratings 25 Design requirements 45.1 General . 45.2 Base . 55.3 Body 55.4 Doors . 65.5 Internal tie-down 75.6 Placard holders . 75.7 Design options . 76 Flight conditions performance and testing 76.1 Pressure equalization and rapid decompression 76.2 Flight loads . 77 Ground c
9、onditions performance and testing 97.1 General . 97.2 Bridging and cresting 97.3 Impact test 97.4 Rain test 97.5 Racking test . 108 Markings 109 Customs/security sealing (optional) 1110 Manufacturers instructions 1111 Quality control .1211.1 Design and production 1211.2 Operations 12Annex A (normati
10、ve) Code DKC half-width contoured containers dimensions and design requirements .16Annex B (normative) Code DKE/DKN half-width contoured containers dimensions and design requirements .18Annex C (normative) Code DKP half-width rectangular containers dimensions and design requirements .20Annex D (norm
11、ative) Code DLF full-width contoured containers dimensions and design requirements .22Annex E (normative) Code DLP full-width rectangular containers dimensions and design requirements .24Annex F (normative) Code DPE/DPN half-width contoured containers dimensions and design requirements .26Annex G (n
12、ormative) Code DQF full-width contoured containers dimensions and design requirements .28Annex H (normative) Code DQP full-width rectangular containers dimensions and design requirements .30 ISO 2016 All rights reserved iiiContents PageBS ISO 4118:2016ISO 4118:2016(E)Annex I (normative) Code DAF ful
13、l-width contoured containers dimensions and design requirements .32Annex J (normative) Code DMF full-width contoured containers dimensions and design requirements .33Annex K (normative) Code DKH low height full-width containers dimensions and design requirements .34Annex L (normative) Code DKG low h
14、eight half-width containers dimensions and design requirements .35Bibliography .37iv ISO 2016 All rights reservedBS ISO 4118:2016ISO 4118:2016(E)ForewordISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of pr
15、eparing International Standards 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, i
16、n liaison with ISO, also take 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/IE
17、C Directives, Part 1. In particular 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 (see www.iso.org/directives).Attention is drawn to the possibility t
18、hat some of the elements of this 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
19、declarations received (see www.iso.org/patents).Any trade name used in this document is information given for the convenience of users and does not constitute an endorsement.For an explanation on the meaning of ISO specific terms and expressions related to conformity assessment, as well as informati
20、on about ISOs adherence to the World Trade Organization (WTO) principles in the Technical Barriers to Trade (TBT) see the following URL: www.iso.org/iso/foreword.html.The committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 9, Air cargo and ground equipm
21、ent.This fourth edition cancels and replaces the third edition (ISO 4118:2005), of which it constitutes a complete technical revision. ISO 2016 All rights reserved vBS ISO 4118:2016ISO 4118:2016(E)IntroductionThe basic functions of air cargo containers area) the unitization of baggage, cargo or mail
22、 during ground handling and transportation, andb) the restraint in accordance with aircraft Weight and Balance Manual requirements of their contents against accelerations encountered in flight.This revision introduces containers flight conditions testing in order to provide means to substantiate the
23、ir ability to withstand maximum flight loads so that neither the container nor its contents can become a hazard or damage the aircraft structure.Throughout this International Standard, the minimum essential criteria are identified by use of the key word “shall.” Recommended criteria are identified b
24、y use of the key word “should” and, while not mandatory, are considered to be of primary importance in providing safe, economical and practical air transport containers. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alter
25、nate methods to provide an equivalent level of 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 use exac
26、t values, the SI unit ones are to be used, except for container base plan-view dimensions, whose exact values are those expressed in inches.vi ISO 2016 All rights reservedBS ISO 4118:2016Air cargo Non-certified lower deck containers Design and testing1 ScopeThis International Standard covers the des
27、ign, performance and testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness approval/certification when loaded under the conditions of compartment restraint and/or where applicable according to the aircraft types approved Weight and Balance Ma
28、nual, ISO 8097 or ISO 21100 equivalent base plate restraint for these containers.Aircraft Weight and Balance Manuals require non-certified containers be constructed then loaded in such a manner that neither the container nor its contents can become a hazard or damage the aircraft structure under fli
29、ght conditions. Compliance with the present International Standard is one means of demonstrating compliance with these requirements.Most sizes of containers covered by this International Standard (base sizes K, L, P and Q) cannot physically be loaded and latched on aircraft main deck cargo systems.
30、Base size A and M containers can, but are not allowed on aircraft main decks, which in general do not accept non-certified units. Accordingly, all containers covered by this International Standard are intended to be used/installed exclusively in aircraft lower deck compartmentsNOTE The metric equiva
31、lents 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. See introduction where it is deemed necessary to use exact values.2 Normative reference
32、sThe following documents, 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 411
33、6, Air cargo equipment Ground equipment requirements for compatibility with aircraft unit load devicesISO 7166, Aircraft Rail and stud configuration for passenger equipment and cargo restraintISO 10046, Aircraft Methodology of calculating cargo compartment volumesISO 10254, Air cargo and ground equi
34、pment VocabularyISO 11242, Aircraft Pressure equalization requirements for cargo containersISO 21100, Air cargo unit load devices Performance requirements and test parametersCAAC CCAR-25, Airworthiness Standards Transport Category Airplanes, paragraph 25.855, Cargo or baggage compartments1)U.S. Code
35、 of Federal Regulations 14 CFR Part 25, Airworthiness Standards: Transport category airplanes, paragraph 25.855, Cargo or baggage compartments2)1) The Civil Aviation Administration of China (CAAC) CCAR-25 constitutes the Chinese government transport aircraft airworthiness Regulations.2) 14 CFR Part
36、25 constitutes the U.S.A. Government transport aircraft airworthiness Regulations, and can be obtained from: US Government Printing Office, Mail Stop SSOP, Washington DC 20402-9328, U.S.A. or its web site at www.gpoaccess.gov.from: US Government Printing Office, Mail Stop SSOP, Washington DC 20402-9
37、328, U.S.A. or its INTERNATIONAL STANDARD ISO 4118:2016(E) ISO 2016 All rights reserved 1BS ISO 4118:2016ISO 4118:2016(E)European Aviation Safety Agency CS-25, Certification Specifications for Large Aeroplanes, paragraph 25.855, Cargo or baggage compartments3)Japanese Airworthiness Standard Part 3 (
38、Civil Aeronautics Law Article 10, paragraph 4)4)3 Terms and definitionsFor the purposes of this document, the definitions in ISO 10254 and the following apply.3.1aircraft containercompletely enclosed unit load device which interfaces directly with the aircraft cargo handling and restraint system and
39、 alone performs all the functions of a unit load device3.2certificationapprovalapproval by an airworthiness authority that a component or item of equipment meets the required performance for aircraft installation3.3non-certified containercontainer exclusively for the lower deck of wide-body aircraft
40、, which is not subject to airworthiness approval (certification), but may be carried under conditions specified by the aircrafts Weight and Balance Manual3.4Weight and Balance ManualWb) the second letter A, K, L, M, P or Q denoting the base size as defined in ISO 21100;c) the third letter denoting t
41、he contour determined in accordance with ISO 10046 (see NOTE).website at www.gpoaccess.gov.3) EASA CS-25 constitutes the European Governments transport aircraft airworthiness Regulations and can be obtained from: European Aviation Safety Agency (EASA), Postfach 101253, D-50452 Cologne, Germany, or i
42、ts web site at www.easa.europa.eu.4) Japanese Airworthiness Standard Part 3 (ISBN 4-89279-661-1) constitutes the Japanese government transport aircraft airworthiness Regulations, and can be obtained from the Civil Aviation Bureau (CAB) of the Ministry of Land, Infrastructure, Transportation and Tour
43、ism, Tokyo, Japan, or its website at www.mlit.go.jp/en.5) 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 113, Montral, Qubec H4Z 1M1, Canada, web site at www.iata.org.2 ISO 2016
44、 All rights reservedBS ISO 4118:2016ISO 4118:2016(E)The identification code shall be prominently marked on two opposite sides of the container (see Clause 8).EXAMPLEA non-certified aircraft container (D) of base size 3 175 mm x 1 534 mm (125 in x 60,4 in) (size L) and of nominal overall width 3 175
45、mm (125 in) (rectangular contour P) shall be designated as DLP.NOTE The containers 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 (Refe
46、rences 5 and 6) for any code changes.4.2 External contours, dimensions, and ratings of applicable containers are shown in Table 1.Table 1 Ratings and contour dimensions of non-certified containersName of containers and nominal dimensions in mm (in)Rating (Maxi-mum operation-al gross mass) kg (lb)aCo
47、ntour and external dimensionsIATA Identifica-tion Code (IATA 40/1)bHalf-width contoured container, 2 337 mm (92 in) wide, with base dimensions 1 534 mm 1 562 mm (60,4 in 61,5 in)1 588 kg (3 500 lb)Annex A DKCHalf-width contoured container, 2 007 mm (79 in) wide, with base dimensions 1 534 mm 1 562 m
48、m (60,4 in 61,5 in)1 588 kg (3 500 lb)Annex B DKE/DKNHalf-width rectangular container, 1 562 mm (61,5 in) wide, with base dimensions 1 534 mm 1 562 mm (60,4 in 61,5 in)1 588 kg (3 500 lb)Annex C DKPFull-width contoured container, 4 064 mm (160 in) wide, with base dimensions 1 534 mm 3 175 mm (60,4 i
49、n 125 in)3 175 kg (7 000 lb)Annex D DLFFull-width rectangular container, 3 175 mm (125 in) wide, with base dimensions 1 534 mm 3 175 mm (60,4 in 125 in)3 175 kg (7 000 lb)Annex E DLPHalf-width contoured container, 1 562 mm (61,5 in) wide, with base dimensions 1 534 mm 1 194 mm (60,4 in 47 in)1 225 kg (2 700 lb)Annex F DPE/DPNFull-width contoured container, 3 175 mm (125 in) wide, with base dimensions 1 534 mm 2 438 mm (60,4 in 96 in)2 449 kg (5 400 lb)Annex G DQFFull-width rectangular cont
