Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft

This document specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft. This document is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication. It does not apply to previously in-service regional aircraft models, which present a considerable variety of tow bar attachment fittings. However, a simple retrofit modification is described that can make certain in-service fittings compatible with a tow bar head in conformity with this document, where deemed appropriate in order to facilitate operation of such aircraft types at airports. This document is applicable to regional commercial transport aircraft airworthiness certified with a maximum ramp mass of ≤ 50 000 kg (110 000 lb). It does not apply to: — aircraft airworthiness certified as commuter category aeroplanes; — aircraft airworthiness certified as main line aircraft with a maximum ramp mass of > 50 000 kg (110 000 lb), which are covered by ISO 8267-1.

Aéronefs — Exigences d'interface des ferrures d'attache de barre de tractage — Partie 2: Aéronefs régionaux

General Information

Status
Published
Publication Date
05-Dec-2023
Current Stage
6060 - International Standard published
Start Date
06-Dec-2023
Due Date
14-Oct-2023
Completion Date
06-Dec-2023
Ref Project

Relations

Standard
ISO 8267-2:2023 - Aircraft — Tow bar attachment fittings interface requirements — Part 2: Regional aircraft Released:6. 12. 2023
English language
5 pages
sale 15% off
Preview
sale 15% off
Preview

Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 8267-2
Fourth edition
2023-12
Aircraft — Tow bar attachment fittings
interface requirements —
Part 2:
Regional aircraft
Aéronefs — Exigences d'interface des ferrures d'attache de barre de
tractage —
Partie 2: Aéronefs régionaux
Reference number
© ISO 2023
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 on
the internet or an intranet, without prior written permission. Permission can be requested from either ISO at the address below
or ISO’s member body in the country of the requester.
ISO copyright office
CP 401 • Ch. de Blandonnet 8
CH-1214 Vernier, Geneva
Phone: +41 22 749 01 11
Email: copyright@iso.org
Website: www.iso.org
Published in Switzerland
ii
Contents  Page
Foreword .iv
Introduction .v
1 Scope . 1
2  Normative references . 1
3  Terms and definitions . 1
4  Requirements . 2
4.1 Fitting location . 2
4.2 Towing loads . 2
4.3 Aircraft mass categories . 2
4.4 Fitting configuration, dimensions and clearances . 2
4.5 Tow bar fit . 3
5  Retrofit option . 3
Bibliography . 5
iii
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 document 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).
ISO draws attention to the possibility that the implementation of this document may involve the use
of (a) patent(s). ISO takes no position concerning the evidence, validity or applicability of any claimed
patent rights in respect thereof. As of the date of publication of this document, ISO had not received
notice of (a) patent(s) which may be required to implement this document. However, implementers are
cautioned that this may not represent the latest information, which may be obtained from the patent
database available at www.iso.org/patents. ISO shall not be held responsible for identifying any or all
such patent rights.
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 ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 9, Air cargo
and ground equipment.
This fourth edition cancels and replaces the third edition (ISO 8267-2:2019), which has been technically
revised.
The main changes are as follows:
— the normative and aircraft airworthiness references have been updated.
A list of all parts in the ISO 8267 series can be found on the ISO website.
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
Introduction
The purpose of this document is to achieve tow bar attachment fittings interface standardization by
aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow
bar with a standard connection can be used for all aircraft types within or near that mass category,
so as to assist operators and airport handling companies in reducing the number of different tow bar
types used.
In this document, the following verbal forms are used:
— “shall” indicates a requirement;
— “should” indicates a recommendation;
— “may” indicates a permission;
— “can” indicates a possibility or a capability.
Recommended criteria are, while not mandatory, considered to be of primary importance in providing
safe aircraft towing arrangements. Deviation from recommended criteria should only occur after
careful consideration, extensive testing, and tho
...

Questions, Comments and Discussion

Ask us and Technical Secretary will try to provide an answer. You can facilitate discussion about the standard in here.