ISO-16049-1-2001.pdf
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1、INTERNATIONAL STANDARD ISO 16049-1 First edition 2001-07-15 Reference number ISO 16049-1:2001(E) ISO 2001 Air cargo equipment Restraint straps Part 1: Design criteria and testing methods quipement pour le fret arien Sangles darrimage Partie 1: Critres de conception et mthodes dessai Copyright Intern
2、ational Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/19/2007 03:40:38 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 16049-1:2001(E) ii ISO 2001 All rights reserved PDF disclai
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5、file; the PDF-creation parameters were optimized for printing. Every care has been taken to ensure that the file is suitable for use by ISO member bodies. In the unlikely event that a problem relating to it is found, please inform the Central Secretariat at the address given below. ISO 2001 All righ
6、ts reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, elec- tronic or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address below or ISOs mem- ber body in the country of
7、 the requester. ISO copyright office Case postale 56 CH-1211 Geneva 20 Tel. + 41 22 749 01 11 Fax + 41 22 749 09 47 E-mail copyrightiso.ch Web www.iso.ch Printed in Switzerland Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Sta
8、ndards 1/9972545001 Not for Resale, 04/19/2007 03:40:38 MDTNo reproduction or networking permitted without license from IHS -,-,- ISO 16049-1:2001(E) ISO 2001 All rights reserved iii ContentsPage 1Scope .1 2Normative references .2 3Terms and definitions 2 4Design criteria 6 5Testing methods .10 6Qua
9、lity Control 13 7Markings .14 8Options .15 9Manufacturers instructions .15 10Operating instructions .16 Bibliography.17 Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/9972545001 Not for Resale, 04/19/2007 03:40:38 M
10、DTNo reproduction or networking permitted without license from IHS -,-,- ISO 16049-1:2001(E) iv ISO 2001 All rights reserved Foreword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing Internation
11、al 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, in liaison with ISO,
12、 also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 3. Draft International Standards a
13、dopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote. Attention is drawn to the possibility that some of the elements of this part of ISO 16049 may be the sub
14、ject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. International Standard ISO 16049-1 was prepared by Technical Committee ISO/TC 20,Aircraft and space vehicles, Subcommittee SC 9,Air cargo and ground equipment. ISO 16049 consists of the following
15、parts, under the general titleAir cargo equipment Restraint straps: Part 1: Design criteria and testing methods Part 2: Utilization guidelines and lashing calculations Copyright International Organization for Standardization Provided by IHS under license with ISO Licensee=NASA Technical Standards 1/
16、9972545001 Not for Resale, 04/19/2007 03:40:38 MDTNo reproduction or networking permitted without license from IHS -,-,- INTERNATIONAL STANDARDISO 16049-1:2001(E) ISO 2001 All rights reserved 1 Air cargo equipment Restraint straps Part 1: Design criteria and testing methods 1Scope 1.1This part of IS
17、O 16049 specifies the design criteria and testing methods applicable to air cargo restraint straps to be used for tie-down of unitized or non-unitized cargo on board civil transport aircraft. It aims at identifying the design criteria and testing methods adequate to guarantee the ultimate load and o
18、perational dependability of cargo restraint strap assemblies with a typical() rated ultimate tension load capability, as used by the airline industry in order to restrain, on board civil transport aircraft during flight: cargo loaded and tied down on to airworthiness certified air cargo pallets, the
19、mselves restrained into aircraft lower deck or main deck cargo systems meeting the requirements of ISO 8097 (NAS 3610), or non-unitized individual pieces of cargo, or pieces of cargo placed on to an unrestrained (“floating”) pallet into either lower deck or main deck containerized cargo compartments
20、 of an aircraft. 1.2The same restraint strap assemblies can also be used in other applications such as: non-containerized (bulk loaded) baggage and cargo compartments, to ensure cargo restraint inside an airworthiness certified air cargo container. NOTEThe ultimate loads permissible on the attachmen
21、t points available in most aircraft bulk compartments and inside most air cargo containers are significantly lower than(). This results in the restraint arrangements ultimate load capability being dictated by the weakest element, i.e. the attachment points. Typicalultimate load restraint straps will
22、 therefore be in excess of the requirements for such applications. 1.3This part of ISO 16049 describes the design criteria for individual restraint strap assemblies, but does not intend specifying in any manner the way they are to be used aboard aircraft to ensure proper restraint throughout the cer
23、tified flight envelope. It is important that tie-down arrangements meet all the applicable requirements of the Airworthiness Authorities approved Weight and Balance Manual for the aircraft type or sub-type concerned, particularly as regards, but not necessarily limited to, ultimate load factors to b
24、e taken into account to determine the number of straps to be used in each direction of restraint, maximum angles to be observed with the direction of restraint, minimum spacing of attachment points, etc. 1.4When restraint strap assemblies are attached to the edge rails of a certified air cargo palle
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