Air cargo unit load devices — Load distribution model

This document defines the industry agreed model for load distribution on air cargo unit load devices (ULD) bases to apply the maximum allowable centre of gravity (C.G.) eccentricity. Its purpose is to establish a common reference load distribution algorithm for: a) comparable and repeatable ULD testing methods, or equivalent numeric simulations; b) aircraft structure and cargo systems design assumptions, consistent with existing airframers practices; and c) definition of operators unit load devices utilization rules and cargo build-up training programs. It applies to all types of unit load devices intended for use on board civil transport aircraft and airworthiness approved in accordance with the performance requirements and testing parameters of either ISO 21100 or, as applicable, ISO 8097. It also applies to non-airworthiness approved (non-certified) containers as defined in ISO 4118, the utilisation of which is controlled by the provisions of the aircraft type's Weight and Balance Manual and other airframe manufacturer's documents.

Unités de charge de fret aérien — Modèle de répartition des charges

General Information

Status
Published
Publication Date
25-Feb-2020
Current Stage
6060 - International Standard published
Start Date
26-Feb-2020
Due Date
19-Oct-2019
Completion Date
26-Feb-2020
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INTERNATIONAL ISO
STANDARD 21785
First edition
2020-02
Air cargo unit load devices — Load
distribution model
Unités de charge de fret aérien — Modèle de répartition des charges
Reference number
ISO 21785:2020(E)
©
ISO 2020

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ISO 21785:2020(E)

COPYRIGHT PROTECTED DOCUMENT
© ISO 2020
All rights reserved. Unless otherwise specified, or required in the context of its implementation, no part of this publication may
be reproduced or utilized otherwise in any form or by any means, electronic or mechanical, including photocopying, or posting
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Published in Switzerland
ii © ISO 2020 – All rights reserved

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ISO 21785:2020(E)

Contents Page
Foreword .iv
Introduction .v
1 Scope . 1
2 Normative references . 1
3 Terms and definitions . 1
4 Load distribution model . 2
4.1 Principle . 2
4.2 Application . 4
5 Operational C.G. trade-off . 4
5.1 General . 4
5.2 One direction trade-off . 4
5.3 Two directions trade-off . 5
5.4 Required precautions . 5
Bibliography . 7
© ISO 2020 – All rights reserved iii

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ISO 21785:2020(E)

Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards
bodies (ISO member bodies). The work of preparing 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, in 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/IEC 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 that 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 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 of the voluntary nature of standards, the meaning of ISO specific terms and
expressions related to conformity assessment, as well as information about ISO's adherence to the
World Trade Organization (WTO) principles in the Technical Barriers to Trade (TBT) see www .iso .org/
iso/ foreword .html.
This document was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles,
Subcommittee SC 9, Air cargo and ground equipment.
Any feedback or questions on this document should be directed to the user’s national standards body. A
complete listing of these bodies can be found at www .iso .org/ members .html.
iv © ISO 2020 – All rights reserved

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ISO 21785:2020(E)

Introduction
This document specifies a reference model for load distribution on air cargo unit load device (ULD)
bases, to reflect in a standardized manner maximum allowable centre of gravity (C.G.) eccentricity
limitations.
The civil aviation requirements referred to in this document are those concerning certification
of transport aircraft and appliances to be installed aboard them, and constitute the set of design
and operation requirements internationally agreed in application of International Civil Aviation
Organization (ICAO) Annex 8, Airworthiness of aircraft, to the Convention on International Civil
Aviation.
Throughout this document, the minimum essential criteria are identified by use of the key word "shall".
Recommended criteria are identified by use of the key word “should” and, while not mandatory, are
considered to be of primary importance in providing safe air cargo unit load devices. Deviation from
recommended criteria should only occur after careful consideration and thorough service evaluation
have shown alternate methods to provide an equivalent level of safety.
© ISO 2020 – All rights reserved v

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INTERNATIONAL STANDARD ISO 21785:2020(E)
Air cargo unit load devices — Load distribution model
1 Scope
This document defines the industry agreed model for load distribution on air cargo unit load devices
(ULD) bases to apply the maximum allowable centre of gravity (C.G.) eccentricity.
Its purpose is to establish a common reference load distribution algorithm for:
a) comparable and repeatable ULD testing methods, or equivalent numeric simulations;
b) aircraft structure and cargo systems design assumptions, consistent with existing airframers
practices; and
c) definition of operators unit load devices utilization rules and cargo build-up training programs.
It applies to all types of unit load devices intended for use on board civil transport aircraft and
airworthiness approved in accordance with the performance requirements and testing parameters of
either ISO 21100 or, as applicable, ISO 8097.
It also applies to non-airworthiness approved (non-certified) containers as defined in ISO 4118,
the utilisation of which is controlled by the provisions of the aircraft type's Weight and Balance Manual
and other airframe manufacturer's documents.
2 Normative references
The following documents are referred to in the text in such a way that some or all of their content
constitutes requirements 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.
ISO 8097, Aircraft — Minimum airworthiness requirements and test conditions for certified air cargo unit
load devices
ISO 10254, Air cargo and ground equipment — Vocabulary
ISO 21100, Air cargo unit load devices — Performance requirements and test parameters
3 Terms and definitions
For the purposes of this document, the terms and definitions of ISO 10254 and the following apply:
ISO and IEC maintain terminological databases for use in standardization at the following addresses:
— ISO Online browsing platform: available at https:// www .iso .org/ obp
— IEC Electropedia: available at http:// www .electropedia .org/
3.1
eccentricity
offset
plan view distance between the overall centre of gravity (C.G.) of the unit load
device and its contents and the geometric centre of its base, expressed in percentage of the base length
and width
© ISO 2020 – All rights reserved 1

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ISO 21785:2020(E)

3.2
homogeneous cargo
cargo of homogeneous density and of such a nature that the whole weight of each piece is evenly
distributed over the whole of that piece's footprint area
4 Load distribution model
4.1 Principle
4.1.1 Airworthiness approval of each type and size of unit load device includes maximum load centre
of gravity (C.G.) eccentricity (offset) allowances at unit maximum gross mass, that are part of its testing
and approval (see ISO 21100 or ISO 8097, as applicable, for unit load device configurations and ultimate
load criteri
...

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