SAE AS 6163-2015 Temperature Controlled Container - Performance Requirements and Test Parameters.pdf

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1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref

2、rom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2015 SAE InternationalAll rights reserved. No part of this publi

3、cation may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE.TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada)Tel: +1 724-776-4970 (out

4、side USA)Fax: 724-776-0790Email: CustomerServicesae.orgSAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AS6163AEROSPACESTANDARDAS6163Issued 2015-12Temperature Controlled Container - Performance Req

5、uirements and Test ParametersRATIONALEWhile Temperature Controlled Containers (TCC) being transported as air cargo is not flight critical and the energy elements/systems are in compliance with Dangerous Goods Regulations (DGR), they nonetheless present the potential to interfere with the safe operat

6、ion of the aircraft systems and, therefore, need to have deterministic functions and failure modes.This SAE Aerospace Standard (AS) defines the minimum performance standard to demonstrate compliance with the regulatory design, test and operational requirements for a TCC. This compliance includes par

7、ameters such as design integrity, performance testing and operational airworthiness criteria that requires substantiation by the manufacturer when applying for aviation regulatory authority approvals.SAE INTERNATIONAL AS6163 Page 2 of 23TABLE OF CONTENTS 1. SCOPE 4 1.1 Purpose. 4 1.2 Field of Applic

8、ation 4 2. REFERENCES 4 2.1 Applicable Documents 4 2.1.1 SAE Publications. 4 2.1.2 Code of Federal Regulations (CFR) . 5 2.1.3 Federal Aviation Administration (FAA) National Policy Documents . 6 2.1.4 ISO Standards. 6 2.1.5 RTCA Publications 6 2.1.6 Airlines for America (A4A) Publications (Formerly

9、ATA) 6 2.1.7 IATA Publications 6 2.1.8 ICAO Publications . 7 2.2 European Publications 7 2.2.1 European Union Publications 7 2.2.2 EUROCAE Publications 7 2.3 Terms and Definitions . 8 2.4 Acronyms 9 3. CONTAINER CONFIGURATIONS . 10 3.1 Aircraft Container (Type - A) . 10 3.2 Non-Aircraft Container (T

10、ype - B) . 10 4. TEMPERATURE CONTROL SYSTEM CLASSIFICATIONS . 11 4.1 Aircraft Active System. 11 4.2 Stored Energy System 12 4.3 Passive and Ground Active System 12 4.4 Stored Energy and Ground Active System . 12 5. CLASSIFICATION. 13 5.1 Aircraft Container Classifications 14 5.2 Non-Aircraft Contain

11、ers. 14 6. COMPLIANCE OVERVIEW 15 7. COMPLIANCE MATRIX 15 8. DEFINITION OF REQUIREMENTS 16 8.1 Physical Test Requirements . 16 8.1.1 Flammability of Restraint Materials. 16 8.1.2 Flammability of Wiring. 16 8.1.3 Propagation Properties of Materials and Fluids 16 8.1.4 Battery Testing 16 8.1.5 Electro

12、magnetic Interference (EMI) 17 8.1.6 Magnetic Field. 17 8.1.7 Altitude 17 8.1.8 Emergency Rapid Decompression . 18 8.1.9 Load Restraint. 18 8.1.10 Fire Detection and Suppression 18 8.1.11 Shock 19 8.1.12 Vibration 19 8.2 Analysis Requirements . 19 8.2.1 System Safety Analysis. 19 8.2.2 Analysis of C

13、omponent Restraint 20 8.2.3 Software Consideration. 20 8.2.4 Hardware Qualification . 20 8.2.5 Analysis of Loading Scheme. 20 8.2.6 Deactivation of Active Ground System . 21 SAE INTERNATIONAL AS6163 Page 3 of 238.2.7 Dangerous Good Regulations. 21 8.3 Documentation Requirements 21 8.3.1 Continued Ai

14、rworthiness Instructions 21 8.4 TCC Marking . 22 8.4.1 Regulatory Approval Marking 22 8.4.2 System Marking 22 8.4.3 Type A Aircraft Container Marking 23 9. NOTES 23 9.1 Revision Indicator 23 Figure 1 Aircraft container configurations . 14 Figure 2 Non-aircraft container configurations 14 Figure 3 23

15、Table 1 13Table 2 15 SAE INTERNATIONAL AS6163 Page 4 of 231. SCOPEThis SAE Aerospace Standard (AS) defines the minimum performance standard to demonstrate compliance with the regulatory design, test and operational requirements for a Temperature Controlled Container (TCC).1.1 Purposex Establish the

16、minimum performance standard and test parameters that can be cited by global regulatory authorities within a Technical Standard Orders (TSO) for TCC.x Provide a means to verify that the design and operation of the TCC shall have no impact on the safe operation of the aircraft and the functionality o

17、f the on board systems.x Provide a means to verify that the design and operation of the TCC shall create no additional burden to the flight crew of the aircraft.1.2 Field of ApplicationThis Aerospace Standard applies to all airworthiness approved Temperature Controlled Container (TCC) intended for c

18、arriage on board civil transport category aircraft.It is intended to provide the TCC manufacturers, airworthiness certification authorities and air cargo carriers/operators withthe means to define and execute a unified program of airworthiness design approval, irrespective of the Aircraft Certificat

19、ion Office (ACO) or global regulatory authority via a TSO approval (or ETSO equivalent).In addition to the design approval requirements defined within this document, the TCC manufacturer shall also have to demonstrate an appropriate Design Organization Approval (DOA) and/or Production Organization A

20、pproval (POA) status for the article with their regional aviation regulatory authority.2. REFERENCES2.1 Applicable DocumentsThe following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publicat

21、ions shall be the issue in effect on the date of the purchase order. In theevent of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exem

22、ption has been obtained.2.1.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or +1 724-776-4970 (outside USA), www.sae.org.AS8036 Cargo Compartment Fire Detection InstrumentsARP4761 Guidelines and Methods

23、 for Conducting the Safety Assessment Process on Civil Airborne Systems and EquipmentARP4754 Guidelines for Development of Civil Aircraft and SystemsAS36100 Air Cargo Unit Load Devices - Performance Requirements and Test ParametersAS36102 Air Cargo Unit Load Devices - Testing DevicesSAE INTERNATIONA

24、L AS6163 Page 5 of 232.1.2 Code of Federal Regulations (CFR)Available from the United States Government Printing Office, 732 North Capitol Street, NW, Washington, DC 20401, Tel: 202-512-1800, www.gpo.gov.2.1.2.1 Title 14 CFR, Part 21 - Certification Procedures for Products and PartsApplicable parts

25、within Title 14 CFR Part 21, Subpart O Technical Standard Order Approval, sections 21.601 to 21.6212.1.2.2 Title 14 CFR, Part 25 - Airworthiness Standards: Transport Category AirplanesApplicable parts within Title 14 CFR Part 25, sections 25.1 to 25.1733Sections referenced within this document:25.3

26、Special Provisions for ETOPS Type Design Approvals25.561 General25.853(a) Compartment Interiors25.851(b) Built-in Fire Extinguishers25.855 Cargo or Baggage Compartment25.857 Cargo Compartment Classification25.858 Cargo or Baggage Compartment Smoke or Fire Detection Systems25.869 Fire Protection: Sys

27、tems25.1301 Function and Installation25.1309 Equipment, Systems, and Installation25.1353 Electrical Equipment and Installations25.1529 Instructions for Continued Airworthiness25.1713 Fire Protection: EWIS2.1.2.3 Title 49 CFR - Code of Federal RegulationsApplicable Parts within Title 49 CFR Parts 100

28、 to 185 Hazardous Materials Transportation (HMR).Parts referenced within this document:49 CFR 173.159 Batteries, wet49 CFR 173.159(a) Exception for non-spillable batteriesSAE INTERNATIONAL AS6163 Page 6 of 232.1.3 Federal Aviation Administration (FAA) National Policy DocumentsAvailable from Federal

29、Aviation Administration, 800 Independence Avenue, SW, Washington, DC 20591, Tel: 866-835-5322, www.faa.gov.TSO C90 Cargo Pallets, Nets and ContainersTSO C173 Nickel-Cadmium, Nickel Metal-Hydride, and Lead Acid BatteriesAC 20-152 Design Assurance Guidance for Airborne Electronic HardwareAC 25-9 Smoke

30、 Detection, Penetration, and Evacuation Tests and Related ANM Flight Manual Emergency ProceduresAC 25.1309-1 System Design and Analysis2.1.4 ISO StandardsAvailable at http:/webstore.ansi.org/ISO 7137 Environmental Conditions and Test Procedures for Airborne EquipmentISO 21100 Air Cargo Unit Load Dev

31、ices Performance Requirements and Testing ParametersISO 11242 Aircraft - Pressure Equalization Requirements for Cargo Containers2.1.5 RTCA PublicationsAvailable from RTCA, Inc., 1150 18th Street, NW, Suite 910, Washington, DC 20036, Tel: 202-833-9339, www.rtca.org.DO-160 Environmental Conditions and

32、 Test Procedures for Airborne EquipmentDO-178 Software Considerations in Airborne Systems and Equipment CertificationDO-254 Design Assurance Guidance for Airborne Electronic HardwareDO-293 Minimum Operational Performance Standards for Nickel-Cadmium and Lead Acid Batteries2.1.6 Airlines for America

33、(A4A) Publications (Formerly ATA)Available from Airlines for America (A4A), 1301 Pennsylvania Avenue, NW, Suite 1100, Washington, DC 20004, Tel: 202-626-4000, www.airlines.org.ATA Spec 100 Manufacturers Technical DataATA iSpec 2200 Information Standards for Aviation Maintenance2.1.7 IATA Publication

34、sAvailable from International Air Transport Association, Publications Assistant, 800 Place Victoria, P.O. Box 113, Montreal, Quebec H4Z 1M1, Canada, Tel: 1-514-874-0202, www.iata.org.IATA ULD Regulations (ULDR)IATA Dangerous Goods Regulations (DGR)SAE INTERNATIONAL AS6163 Page 7 of 232.1.8 ICAO Publ

35、icationsAvailable from International Civil Aviation Organization, 999 University Street, Montreal, Quebec H3C 5H7, Canada, Tel: +1 514-954-8219, http:/www.icao.int/.Technical Instructions for the Safe Transport of Dangerous Goods by Air (Doc. 9284-AN/905)2.2 European PublicationsThe following Europe

36、an publications are included as reference documents and may be substituted by European manufacturers to form part of this document to the extent specified herein. The latest issue of all publications shall apply unless stated otherwise. The applicable issue of publications shall be the latest issue

37、in effect on the date of use. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, shall supersede applicable laws and regulations unless a specific exemption has been obtained.2.2.1 Eur

38、opean Union PublicationsAvailable from European Aviation Safety Agency, Postfach 10 12 53, D-50452 Cologne, Germany, Tel: +49-221-8999-000, www.easa.eu.int.European Aviation Safety Agency (EASA) CS-25, Certification Specifications for Large AeroplanesEuropean Aviation Safety Agency (EASA) CS-ETSO, C

39、ertification Specifications for European Technical Standard OrdersEuropean Technical Standard Order (ETSO) C90 - Cargo Pallets, Nets and ContainersEuropean Technical Standard Order (ETSO) C173 - Nickel-Cadmium and Lead Acid BatteriesEuropean Aviation Safety Agency (EASA) I.A.W EU965/2012 - Technical

40、 requirements and administrative procedures related to air operationsEuropean Aviation Safety Agency (EASA) GM1 CAT.GEN.MPA.200 Transport of dangerous goods2.2.2 EUROCAE PublicationsAvailable from EUROCAE Secretariat, 102 rue Etienne Dolet, 92240 Malakoff, France, Tel: +33 1 40 92 79 30, .ED-12 Soft

41、ware Considerations in Airborne Systems and Equipment CertificationED-14 Environmental Conditions and Test Procedures for Airborne EquipmentSAE INTERNATIONAL AS6163 Page 8 of 232.3 Terms and DefinitionsFor the purposes of this Aviation Standard and listed documents, the following terms and definitio

42、ns apply unless otherwise defined in the document:ACTIVE SYSTEM: A system that monitors and automatically controls and activates autonomous systems or functions within the TCC during the whole shipment cycle including in-flight.BATTERY: Stored energy device that consists of multiple cells permanentl

43、y interconnected within a single case.CHECK: An examination (e.g., An inspection or test) to determine the physical integrity and/or functional capability of an item.COMPLEX: A system is complex when its operation, failure modes, or failure effects are difficult to comprehend without the aid of anal

44、ytical methods.DESIGN APPROVAL: A means by which the regulatory authority can issue a letter giving a manufacturer a formal approval of a design that has been shown compliant with all the necessary regulatory requirements, i.e., a TSO authorization letter of TSO design approval. Note: Other means of

45、 approval may be acceptable.FAILURE: An occurrence, which affects the operation of a component, part, or element such that it can no longer function as intended, (this includes both loss of function and malfunction). Note: Errors may cause Failures, but are not considered to be Failures.FAILURE COND

46、ITION: A condition having an effect on the aircraft and/or its occupants, either direct or consequential, which is caused or contributed to by one or more failures or errors, considering flight phase and relevant adverse operational or environmental conditions, or external events. Failure Conditions

47、 may be classified according to their severities.FLIGHT SAFE MODE: A condition that prevents a non-aircraft device, system or function from operating when transported onboard an aircraft.GROUND ACTIVE SYSTEM: A system that monitors and automatically controls and activates autonomous systems or funct

48、ions within the TCC during the ground portion of the shipment cycle only.PASSIVE: A container that contains no system active during flight, is inert and has no external influence or moving parts.PRODUCTION APPROVAL: A means by which the regulatory authority can issue a letter giving a manufacturer a

49、 formal product approval that allows the production of an article in accordance with its approved design and quality system for a specific manufacturing site, i.e., a TSO authorization letter.STORED ENERGY SYSTEM: A system that monitors and automatically controls the release of stored energy within the TCC during the whole shipment cycle.TEMPERATURE CONTROLLED CONTAINER (TCC): Device for grouping, t