ISO INTERNATIONAL STANDARD 8668-4 First edition 1993-10-15 Aircraft --- Terminal junction systems Part 4: Detail specification for type 2 system Aéronefs -- Systemes de raccordement a modules amovibles Partie 4 Spécification détaillée pour le systeme du type 2 SO Reference number ISO 8668-4:1993(E) CyemainalganizatnfSandadization No reproduction or networking permitted without license from IHS Not for Resale ISO8668-4:1993(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 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. 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. International Standard ISO 8668-4 was prepared by Technical Committee ISO/Tc 20, Aircraft and space vehicles, Sub-Committee SC 1, Aerospace electricalrequirements. IsO 8668 consists of the following parts, under the general title Aircraft - Terminal junction systems: Part 1:Characteristics —Part 2:Tests Part 3. Detail specification for type 1 system Part 4: Detail specification for type 2 system Part5:Detailspecificationfortype3system -Part6.Detail specification for type 4 system @ISO1993 All rights reserved No part of this publication may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without per- mission in writing from the publisher. International Organization for Standardization Case Postale 56 . CH-1211 Geneve 20 · Switzerland Printed in Switzerland Standardizatior ded by IHS t Not for Resale ISO8668-4:1993(E) INTERNATIONAL STANDARD Aircraft - Terminal iunction systems - Part 4: Detail specification for type 2 system 1 Scope 1.1 This part of ISO 8668 specifies the particular characteristics of a terminal junction system (TJS), designated as type 2, and intended for use at temperatures from - 55 C to + 155 °C. 1.2 The junction system covered by this part of ISO 8668 comprises: a) feedback modules in four sizes; b) feedthrough modules in four sizes; c) frames adapted to these modules: monolithic frame and double frame for feedback modules, and double frame for feedthrough modules; d) spacers; e) removable male crimp contacts of sizes 22, 20, 16 and 12; f) sealing plugs. 2 Normative references The following standards contain provisions which, through reference in this text, constitute provisions of this part of IsO 8668 At the time of publication, the editions indicated were valid. All standards are subject to revision, and most recent editions of the standards indicated below. Members of IEC and ISO maintain registers of currently valid International Standards. ISO 8668-2:1986, Aircraft -- Terminal junction systems - Part 2: Tests. MiL-1-81969:1982, Connector and electrical contact -- General specification for installing and removal tools. 3 Definitions For the purposes of this part of 1O 8668, the definitions given in IsO 8668-1 and the following definition apply [See also IEC 50(581):1978, International Electrotechnical Vocabulary - Chapter 581. Electromechanical com- ponents for electronic equipment.j Not for Resale
ISO 8668-4 1993 Aircraft — Terminal junction systems — Part 4 Detail specification for t
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