CTSO-C211 探测与避让（DAA）系统
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CTSO-C211
探测与避让（DAA）系统
CTSO
C211
探测
避让
DAA
系统
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CTSO-C211 探测与避让（DAA）系统,CTSO-C211,探测与避让（DAA）系统,CTSO,C211,探测,避让,DAA,系统
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编 号：CTSO-C211 日 期：2019 年 4 月 29 日 局长授权 批 准： 中国民用航空技术标准规定 - 1 - 本技术标准规定根据中国民用航空规章民用航空材料、零部件和机载设备技术标准规定 （CCAR37）颁发。中国民用航空技术标准规定是对用于民用航空器上的某些航空材料、零部件和机载设备接受适航审查时，必须遵守的准则。 探测与避让（DAA）系统 1. 目的 本技术标准规定（CTSO）适用于为探测与避让（DAA）系统申请技术标准规定项目批准书（CTSOA）的制造人。本 CTSO 规定了探测与避让（DAA）系统为获得批准和使用适用的 CTSO 标记进行标识所必须满足的最低性能标准。 2. 适用范围 本 CTSO 适用于自其生效之日起提交的申请。 按本 CTSO 批准的设备，其设计大改应按 CCAR-21-R4 第 21.353 条要求重新申请CTSOA。 3. 要求 在本CTSO生效之日或生效之后制造并欲使用本CTSO标记进行标识的探测与避让（DAA）系统，应满足 RTCA/DO-365探测及避让系统的最低性能标准 （2017.5.31） ，以适用于表 1 列出的功能设备CAAC CTSO-C211 - 2 - 类别及本 CTSO 第 3.h 节要求。本 CTSO 设备分类取决于系统提供的功能。1 类是基本的 DAA 系统，2 类是带有交通警戒及防撞系统（TCAS）II（7.1 版）功能，但不带有交通咨询的基本 DAA 系统。每种类型进一步细分为具有相应功能的独立部件。 表 1 提供了功能设备类别的详细信息。 表 1 DAA 设备类别及产品 类别 设备1 危险程度 DAA设备设计2&3 DAA 设备名称 功能 功能丧失 误导性信息1 基本型DAA 重大的 重大的 A 主动监视 空中交通控制雷达信标系统/S 模式入侵探测， TCAS II 模式数据，避撞协调数据 B 无人驾驶飞机(UA) DAA 处理器 轨迹处理，DAA 警戒2及导引2 C 控 制 站(CS) DAA处理器 DAA警戒2及导引2D CS DAA控制面板 DAA 模式控制 E CS DAA交通显示 交通、告警及导引信息显示 2 带有TCAS II 型DAA 重大的 危险的/非常重大的（见3.6.(2)(b)）A TCAS II, 7.1 版 ATCRBS/S 模式入侵探测， TCAS II 决断咨询状态及协调数据，避撞系统逻辑，混合监视 B UA DAA处理器 轨迹处理，DAA 警戒2及导引2 C CS DAA处理器 集成 TCAS II 的DAA警戒2及导引2D CS DAA控制面板 集成 TCAS II 的DAA 模式控制 CAAC CTSO-C211 - 3 - 类别 设备1 危险程度 DAA设备设计2&3 DAA 设备名称 功能 功能丧失 误导性信息E CS DAA交通显示 交通、警戒、导引及 RA 信息显示 注： 1.除了表 1 种列出的部件，为使 DAA 系统满足本 CTSO 功能要求，1 类及 2 类设备均需要集成于交通监视的空对空雷达（ATAR） ，以探测非协作飞机， 并集成于自动相关监视广播 （ADS-B） 接收系统，以接收 ADS-B 信息。CTSO-C212 提供了 ATAR 设备最低性能标准；CTSO-C166b 提供了 DAA 系统的 ADS-B 接收设备最低性能标准。DAA 系统使用的 CTSO-C166b 设备必须为 A 级设备，且具备接受1090MHz 的能力。除了 CTSO-C166b 的 A 级设备外，DAA 系统还可能采用 CTSO-C154c 设备。然而，由于 CTSO-C154c 设备本身不满足DAA 系统中 ADS-B 探测性能需求， 因此 CTSO-C154c 设备可能无法替代 CTSO-C166b 的 A 级设备。 2.设备既可以被定为类别 1 的设备， 也可以被定为类别 2 的设备。设备 A、B 均安装于飞机。如果设备 C、D 及 E 包含用于地面远程运行或 CS 的功能，或包含用于载人飞机的功能，则这些部件可安装于飞机上。设备 B 和 C 包含 DAA 警戒及导引功能，可在无人飞机系统平台上互换， 这些功能可能驻留于UA或CS中。 相应安装限制见5.a.(3)节。 3.对于单独设备的要求，详见 RTCA/DO-365 附录 O。 a功能 本 CTSO 的标准适用于采用仪表飞行规则（IFR）来提供交通警CAAC CTSO-C211 - 4 - 戒和导引功能以保持 DAA 足够清晰的 DAA 1 类及 2 类设备。此外，DAA系统2类设备包括集成于不带交通咨询功能的TCAS II系统 （7.1版）的 RA 能力。 注：DAA 足够清晰是指飞机周围的时间和/或空间边界清晰，以防止交通冲突（定量定义见 RTCA/DO-365 附录 C） 。 b. 失效状态类别 （1）本 CTSO 第 3.a 节定义的功能丧失会导致重大的失效状态。 （2）造成误导信息的功能失效包括如下： （i） 1 类及 2 类-功能异常导致的重大失效状态会造成 DAA 警戒和/或导引误导。 （ii） 2 类-未通告失效状态导致的危险的/特别重大的失效状态可能会导致 TCAS II 的 RA 功能错误或丧失。 （iii）设备的设计保证等级应至少与这种失效状态类别相对应。 c. 功能鉴定 应按 RTCA/DO-365 第 2.4 节中试验条件，证明设备性能满足要求。 d. 环境鉴定 应按 RTCA/DO-365 第 2.3 节中标准的环境条件及实验程序，证明机载及地面设备性能满足要求。申请人可采用除 RTCA/DO-365 第2.3 节、RTCA/DO-160G（机载及地面设备） 、MIL-STD-810G、MIL-STD-704 及 RTCA/DO-365 附录 J（地面设备）以外其它适用于机载或地面设备的标准环境条件和试验程序， 证明设备满足最低性能CAAC CTSO-C211 - 5 - 标准要求的性能。 注： 通常情况下，注： 通常情况下， RTCA/DO-160D （包括（包括 Change 1 和和 Change 2）或早期版本不再适用， 如果使用该版本则需按照本）或早期版本不再适用， 如果使用该版本则需按照本 CTSO 第第 3.g 节中的偏离要求进行证明。节中的偏离要求进行证明。 e. 软件鉴定 如果设备包含软件， 则软件应按照 RTCA/DO-178B 机载系统和设备合格审定中的软件考虑 （1992.12.1）或 RTCA/DO-178C机载系统和设备合格审定中的软件考虑 （2011.12.13）的要求进行研制。软件的设计保证等级应与本 CTSO 第 3.b 节规定的失效状态类别一致。 f. 电子硬件鉴定 如果设备中包含复杂电子硬件，则应按照 RTCA/DO-254机载电子硬件设计保证指南 （2000.4.19）的要求进行研制。硬件的设计保证等级应与本 CTSO 第 3.b 节规定的失效状态类别一致。对于确定为简单的机载电子硬件， 可按 RTCA/DO-254 中第 1.6 节的要求处理。 g. 偏离 如果采用替代或等效的符合性方法来满足本 CTSO 规定的最低性能标准要求，则申请人必须表明设备保持了等效的安全水平。申请人应按照 CCAR-21-R4 第 21.368 条（一）要求申请偏离。 h. 机载数据记录能力 除了 RTCA/DO-365 第 .4 的性能要求，UA DDA 处理器应记录与入侵相关的目标源（如雷达、ADS-B 和/或主动监视） ，该入侵CAAC CTSO-C211 - 6 - 能够触发导引信息警戒，或导致 DAA 纠正警戒、DAA 告警或 TCAS II RA。 4. 标记 a. 至少应为一个主要部件设置永久清晰的标记，标记应包括CCAR-21-R4 第 21.423 条（二）规定的所有信息，并包括设备类型及部件名称，除非已在安装说明中标识或能够通过软件识别。 b. 如果设备中包含软件和/或机载电子硬件，则件号必须能够表明软件和硬件的构型。件号编排时，在件号中可为硬件、软件和机载电子硬件各划分一个单独区域。 d. 可以使用电子标记标识软件和机载电子硬件，此标记可通过软件写入硬件部件内部，而不用将其标识在设备铭牌中。如果使用电子标记，则其必须容易读取，无需使用特殊工具或设备。 5. 申请资料要求 申请人必须向负责该项目审查的人员提交相关技术资料以支持设计和生产批准。提交资料包括 CCAR-21-R4 第 21.353 条（一）1规定的符合性声明和以下资料副本。 a. 手册。包含以下内容： （1）运行说明和设备限制，该内容应对设备运行能力进行充分描述。 注：RTCA/DO-365 允许一些功能驻留于 CS（地面）或机载设备中。 因此， 必须能够清晰识别主要驻留功能的运行说明及部件限制，以保证 DAA 设备的能力满足本 CTSO 要求。 CAAC CTSO-C211 - 7 - （2）对所有偏离的详细描述。 （3）安装程序和限制。必须确保按照此安装程序安装设备后，设备仍符合本 CTSO 的要求。限制必须确定任何特殊的安装要求，包括但不限于：1）安装 1 类或 2 类，以及 UA 或地面 CS 应用；2）对于驻留在 UA 或 CS 中的 DAA 警戒和/或 DAA 导引功能（如表 1，注释 2 所示） ，识别部件是否提供了这些功能；3）可互换部件（UA 或CS）应具备安装兼容性要求，以确保能够提供表 1 中 DAA 系统 1 类或 2 类设备的功能；4）对于既可以定为 1 类又可以定为 2 类的设备，应识别给定安装批准的配置类型适用性。 安装限制还必须以注释的方式包含以下声明： “本设备满足技术标准规定中要求的最低性能标准。 如欲安装此设备，必须获得单独的安装批准。本设备满足技术标准规定中要求的最低性能标准。 如欲安装此设备，必须获得单独的安装批准。 ” （4）对于所有软件和机载电子硬件构型，包括如下内容： （i）软件件号，包括版本和设计保证等级； （ii）机载电子硬件件号，包括版本和设计保证等级； （iii）功能描述。 （5）设备中每个部件进行环境鉴定的试验条件总结。例如，可采用 RTCA/DO-160G机载设备环境条件和试验程序附录 A 的表格方式描述。 （6）原理图、布线图，以及设备安装所必需的其它文件。 （7）设备的可更换部件清单（注明件号） 。如适用，包括对供应商件号的交叉索引。 CAAC CTSO-C211 - 8 - b. 持续适航文件，包含设备周期性维护、校准及修理要求，以保证设备的持续适航性。 如适用， 应包括建议的检查间隔和使用寿命。 c. 如果设备包含软件， 则还应提供： 软件合格审定计划 （PSAC） 、软件构型索引和软件完结综述。 d. 如果设备包含简单的或复杂电子硬件，还应提供：硬件合格审定计划（PHAC） 、硬件验证计划、顶层图纸和硬件完结综述（或相似文件，如适用） 。 e. 铭牌图纸，规定设备如何标识本 CTSO 中第 4 节所要求的标记信息。 f. 确定设备中所包含而未按照本CTSO第3节进行评估的功能或性能（即：非 CTSO 功能） 。在获得 CTSOA 的同时非 CTSO 功能也一同被接受。接受这些非 CTSO 功能，申请人必须声明这些功能，并在 CTSO 申请时提供以下信息： （1）非 CTSO 功能的描述，如性能规范、失效状态类别、软件、硬件以及环境鉴定类别。还应包括一份确认非 CTSO 功能不会影响设备对本 CTSO 第 3 节要求符合性的声明。 （2）安装程序和限制，能够确保非 CTSO 功能满足第 5.f.(1)节所声明的功能和性能规范。 （3）第 5.f.(1)节所描述非 CTSO 功能的持续适航要求。 （4）接口要求和相关安装试验程序，以确保对第 5.f.(1)节性能资料要求的符合性。 （5） （如适用） 试验大纲、 试验分析和试验结果， 以验证 CTSOCAAC CTSO-C211 - 9 - 设备的性能不会受到非 CTSO 功能的影响。 （6） （如适用）试验大纲、试验分析和试验结果，以验证第5.f.(1)节描述的非 CTSO 功能的功能和性能。 g. 按 CCAR-21-R4 第 21.358 条要求提供质量系统方面的说明资料，包括功能试验规范。质量系统应确保检测到可能会对 CTSO 最低性能标准符合性有不利影响的任何更改，并相应地拒收该产品。 h. 按 CCAR-21-R4 第 21.355 条要求提供机构方面的说明文件。 i. 材料和工艺规范清单。 j. 定义设备设计的图纸和工艺清单（包括修订版次） 。 k. 制造人的 CTSO 鉴定报告， 表明按本 CTSO 第 3.c 节完成的试验结果。 6. 制造人资料要求 除直接提交给局方的资料外，还应准备如下技术资料供局方评审： a. 用来鉴定每件设备是否符合本 CTSO 要求的功能鉴定规范； b. 设备校准程序； c. 原理图； d. 布线图； e. 材料和工艺规范； f. 按本 CTSO 第 3.d 节要求进行的环境鉴定试验结果； g. 如果设备包含软件，提供 RTCA/DO-178B 或 RTCA/DO-178C中规定的相关文档， 包括所有支持RTCA/DO-178B或RTCA/DO-178CCAAC CTSO-C211 - 10 - 附件 A“软件等级的过程目标和输出”中适用目标的资料； h. 如果设备包含复杂电子硬件， 应提供 RTCA/DO-254 附录 A 表A-1 中定义的与设计保证等级和硬件生命周期相关的资料。对于简单电子硬件，应提供以下资料：测试用例或程序，测试结果，测试覆盖率分析，工具评估和鉴定资料，构型管理记录并包含问题报告。 i. 如果设备包含非 CTSO 功能，必须提供第 6.a 节至第 6.h 节与非 CTSO 功能相关的资料。 7. 随设备提交给用户的资料要求 a. 如欲向一个机构（例如运营人或修理站）提交一件或多件按本 CTSO 制造的设备，则应随设备提供本 CTSO 第 5.a 节和 5.b 节的资料副本， 以及设备正确安装、 审定、 使用和持续适航所必需的资料。 b. 如果设备包含已声明的非 CTSO 功能，则还应包括第 5.f.(1)节至第 5.f.(4)节所规定资料的副本。 c. 如果设备包含软件，为型号审定，补充型号审定或申请人提供开口问题报告总结，以支持本 CTSO 的安装批准。 8. 引用文件 aRTCA 文件可从以下地址订购： Radio Technical Commission for Aeronautics, Inc. 1150 18th Street NW, Suite 910, Washington D.C. 20036 也可通过网站 订购副本。 bMIL-STD 文件可从以下地址订购： DLA Document Services, Building 4/D CAAC CTSO-C211 - 11 - 700 Robbins Avenue, Philadelphia, PA 19111-5094 也可通过网站 订购副本。 English Translation Version for Reference Only Number：CTSO-C211 Date of approval：Apr 29, 2019 Approved by：Xu Chaoqun China Civil Aviation Technical Standard Order - 1 - This China Civil Aviation Technical Standard Order (CTSO) is issued according to Part 37 of the China Civil Aviation Regulations (CCAR-37). Each CTSO is a criterion which the concerned aeronautical materials, parts or appliances used on civil aircraft must comply with when it is presented for airworthiness certification. Detect and Avoid (DAA) Systems 1. Purpose. This China Civil Aviation Technical Standard Order (CTSO) is for manufacturers applying for a Detect and Avoid (DAA) Systems CTSO authorization (CTSOA). This CTSO prescribes the minimum performance standards (MPS) that Detect and Avoid (DAA) Systems must first meet for approval and identification with the applicable CTSO marking. 2. Applicability. This CTSO affects new application submitted after its effective date. Major design changes to article approved under this CTSO will require a new authorization in accordance with section 21.353 of CCAR-21-R4. 3. Requirements New models of DAA equipment identified and manufactured on or English Translation Version for Reference Only CAAC CTSO-C211 - 2 - after the effective date of this CTSO must meet the MPS qualification and documentation requirements in Section 2 of RTCA Document No. RTCA DO-365, Minimum Operational Performance Standards for Detect and Avoid Systems, dated May 31, 2017, as appropriate to the functional equipment classes listed in Table 1, and paragraph 3.h. The different classes for this CTSO are defined by the different functionalities the system provides. Class 1 is the basic DAA system and Class 2 is the basic DAA system with Traffic Alert and Collision Avoidance System (TCAS) II (Version 7.1) functions except for traffic advisories. Each class is further subdivided into several individual articles with corresponding functionalities. Table 1 provides details of the functional equipment classes and articles. Table 1 DAA Classes and Articles class Equipment1 criticality DAA Article Designation 2&3 DAA Equipment Article Name Function Loss of Function MisleadingInformation1 DAA-Basic major major A Active Surveillance Air Traffic ControlRadar Beacon System (ATCRBS)/ModeS Intruder Detection,TCAS II Mode data, Collision Avoidance coordination data B Unmanned Aircraft (UA) DAA Processor Track Processing, DAA Alerting2 and Guidance2 English Translation Version for Reference Only CAAC CTSO-C211 - 3 - class Equipment1 criticality DAA Article Designation 2&3 DAA Equipment Article Name Function Loss of Function MisleadingInformationC Control Station (CS) DAA Processor DAA Alerting2 and Guidance2 D CS DAA Control Panel DAA Mode Control E CS DAA Traffic Display Display of Traffic, Alerting, and Guidance Information 2 DAA with TCAS II Major Hazardous/Severe Major (See 3.b.(2)(b) A TCAS II, Version 7.1 ATCRBS/Mode S Intruder Detection,TCAS II Resolution Advisories (RA)Status and coordination data, Collision Avoidance System Logic, Hybrid Surveillance B UA DAA Processor Track Processing, DAA Alerting2 and Guidance2 C CS DAA Processor DAA Alerting2 and Guidance2 with TCAS II Integration D CS DAA Control Panel DAA Mode Control with TCAS II Integration E CS DAA Traffic Display Display of Traffic, Alerting, Guidance, and RA Information Notes: English Translation Version for Reference Only CAAC CTSO-C211 - 4 - 1. In addition to the articles listed in Table 1, in order for the DAA system to function according to this CTSO, both Class 1 and Class 2 Equipment will require the integration of an Air-to-Air Radar for Traffic Surveillance (ATAR) to detect non-cooperative aircraft and an Automatic Dependent Surveillance-Broadcast (ADS-B) In system to receive ADS-B messages. CTSO-C212 provides the MPS for ATAR equipment. CTSO-C166b provides MPS for ADS-B In equipment for DAA systems. CTSO-C166b equipment used with DAA systems must be Class A, 1090 MHz with receive capability. CTSO-C154c equipment may also be used in addition to CTSO-C166b Class A equipment. However, CTSO-C154c equipment may not be used in place of CTSO-C166b Class A equipment because CTSO-C154c equipment by itself does not meet the ADS-B detection performance requirements for a DAA system. 2. Articles can be designated both Class 1 and 2 equipment. Articles A and B are installed on aircraft. Articles C, D, and E contain functions that operate remotely on the ground or in a CS, or, for manned aircraft, may be located in the aircraft. Articles B and C contain DAA alerting and guidance functions that are interchangeable on an unmanned aircraft system platform. They may reside either in the UA or in the CS. See Section 5.a.(3) for installation limitations associated with interchangeability and class designations. 3. The requirements for the individual articles are identified in English Translation Version for Reference Only CAAC CTSO-C211 - 5 - RTCA DO-365, Appendix O. a. Functionality. This CTSOs standard applies to DAA Class 1 and 2 equipment intended to be used in aircraft operating under Instrument Flight Rules (IFR) to provide alerting and guidance against traffic to remain DAA Well-Clear. In addition, the Class 2 DAA system includes RA capability by integrating a TCAS II System (Version 7.1) without traffic advisories. Note: DAA Well-Clear is a temporal and/or spatial boundary around the aircraft intended to be an electronic means of avoiding conflicting traffic (see Appendix C in RTCA DO-365 for the quantitative definition). b. Failure Condition Classifications. (1) Loss of the function defined in paragraph 3.a is a major failure condition. (2) Failure of the function that causes misleading information is as follows: (a) For Class 1 and Class 2 - Major failure condition for malfunctions causing misleading DAA alerting and/or guidance. (b) For Class 2 Only - Hazardous/severe-major for un-annunciated failures condition that could generate an incorrect or false TCAS II RA, or result in a missing TCAS II RA. (c) Develop the system to, at least, the design assurance level applicable to these failure condition classifications. English Translation Version for Reference Only CAAC CTSO-C211 - 6 - c. Functional Qualification. Demonstrate the required functional performance under the test conditions specified in RTCA DO-365, Section 2.4. d. Environmental Qualification. Demonstrate the required performance under the test conditions specified in RTCA DO-365, Section 2.3 using standard environmental conditions and test procedures appropriate for airborne and ground equipment. Applicant may use a different standard environmental condition and test procedure than those specified in RTCA DO-365, section 2.3, which includes use of RTCA/DO-160G (for both airborne and ground equipment) and MIL-STD-810G, MIL-STD-704, and RTCA/DO-365, Appendix J (for ground equipment), provided the standard selected is appropriate for the airborne or ground equipment. Note: The use of RTCA/DO-160D (with Changes 1 and 2 only, without Change 3 incorporated) or earlier versions is generally not considered appropriate and will require substantiation via the deviation process as discussed in paragraph 3.g of this CTSO. e. Software Qualification. If the article includes software, develop the software according to RTCA, Inc. document RTCA/DO-178B, Software Considerations in Airborne Systems and Equipment Certification, dated December 1, 1992, or RTCA, Inc. document RTCA/DO-178C, Software Considerations in English Translation Version for Reference Only CAAC CTSO-C211 - 7 - Airborne Systems and Equipment Certification, dated December 13, 2011, including referenced supplements as applicable, to at least the software level consistent with the failure condition classification defined in paragraph 3.b of this CTSO. f. Electronic Hardware Qualification. If the article includes complex custom airborne electronic hardware, then develop the component according to RTCA, Inc. Document RTCA/DO-254, Design Assurance Guidance for Airborne Electronic Hardware, dated April 19, 2000, to at least the design assurance level consistent with the failure condition classification defined in paragraph 3.b of this CTSO. For custom airborne electronic hardware determined to be simple, RTCA/DO-254, paragraph 1.6 applies. g. Deviations. For using alternative or equivalent means of compliance to the criteria in the MPS of this CTSO, the applicant must show that the equipment maintains an equivalent level of safety. Apply for a deviation under the provision of 21.368(a) in CCAR-21-R4. 4. Marking. a. Mark at least one major component permanently and legibly with all the information in 21.423(b) of CCAR-21-R4. b. If the article includes software and/or airborne electronic English Translation Version for Reference Only CAAC CTSO-C211 - 8 - hardware, then the article part numbering scheme must identify the software and airborne electronic hardware configuration. The part numbering scheme can use separate, unique part numbers for software, hardware, and airborne electronic hardware. c. The applicant may use electronic part marking to identify software or airborne electronic hardware components by embedding the identification within the hardware component itself (using software) rather than marking it on the equipment nameplate. If electronic marking is used, it must be readily accessible without the use of special tools or equipment. 5. Application Data Requirements. The applicant must furnish the responsible certification personnel with the related data to support design and production approval. The application data include a statement of conformance as specified in section 21.353(a)(1) in CCAR-21-R4 and one copy each of the following technical data: a. A Manual(s) containing the following: (1) Operating instructions and equipment limitations sufficient to describe the equipments operational capability. (2) Describe in detail all deviations. (3) Installation procedures and limitations sufficient to ensure that English Translation Version for Reference Only CAAC CTSO-C211 - 9 - the HUD, when installed according to the installation or operational procedures, still meets this CTSOs requirements. Installation procedures must address the installation specific functional performance requirements of paragraph 3.c of this CTSO. Limitations must identify any unique aspects of the installation. The limitations must include a note with the following statement: “This article meets the minimum performance and quality control standards required by a CTSO. Installation of this article requires separate approval.” (4) For each unique configuration of software and airborne electronic hardware, reference the following: (a) Software part number, including revision and design assurance level; (b) Airborne electronic hardware part number, including revision and design assurance level; (c) Functional description. (5) A summary of the test conditions used for environmental qualifications for each component of the article. For example, a form as described in RTCA/DO-160G, Environmental Conditions and Test Procedures for Airborne Equipment, Appendix A. (6) Schematic drawings, wiring diagrams, and any other documentation necessary for installation of the HUD. English Translation Version for Reference Only CAAC CTSO-C211 - 10 - (7) List of replaceable components, by part number, that makes up the Class 1 DAA or Class 2 DAA equipment. Include vendor part number cross-references, when applicable. b. Instructions covering periodic maintenance, calibration, and repair, to ensure that the DAA continues to meet the CTSO approved design. Include recommended inspection intervals and service life, as appropriate. c. If the article includes software: a plan for software aspects of certification (PSAC), software configuration index, and software accomplishment summary. d. If the article includes simple or complex custom airborne electronic hardware: a plan for hardware aspects of certification (PHAC), hardware verification plan, top-level drawing, and hardware accomplishment summary (or similar document, as applicable). e. A drawing depicting how the article will be marked with the information required by paragraph 4 of this CTSO. f. Identify functionality contained in the article not evaluated under paragraph 3 of this CTSO (that is, non-CTSO functions). Non-CTSO functions are accepted in parallel with the CTSO authorization. For those non-CTSO functions to be accepted, the applicant must declare these functions and include the following information with the CTSO application: English Translation Version for Reference Only CAAC CTSO-C211 - 11 - (1) Description of the non-CTSO function(s), such as performance specifications, failure condition classifications, software, hardware, and environmental qualification levels. Include a statement confirming that the non-CTSO function(s) do not interfere with the articles compliance with the requirements of paragraph 3. (2) Installation procedures and limitations sufficient to ensure that the non-CTSO function(s) meets the declared functions and performance specification(s) described in paragraph 5.f.(1). (3) Instructions for continued performance applicable to the non-CTSO function(s) described in paragraph 5.f.(1). (4) Interface requirements and applicable installation test procedures to ensure compliance with the performance data defined in paragraph 5.f.(1). (5) Test plans and analysis, as appropriate, to verify that performance of the hosting CTSO article is not affected by the non-CTSO function(s). (6) Test plans and analysis, as appropriate, to verify the function and performance of the non-CTSO function(s) as described in paragraph 5.f.(1). g. The quality manual required by section 21.358 of CCAR-21-R4 including functional test specifications. The quality system must ensure that you will detect any change to the approved design that could English Translation Version for Reference Only CAAC CTSO-C211 - 12 - adversely affect compliance with the CTSO MPS and reject the article accordingly. Applicants who currently hold CTSOAs must submit revisions to the existing quality manual as necessary. h. A description of your organization as required by section 21.355 of CCAR-21-R4. i. Material and process specifications list. j. A list of all drawings and processes (including revision level) that define the articles design. k. Manufacturers CTSO qualification report showing results of testing accomplished according to paragraph 3.c of this CTSO. 6. Manufacturer Data Requirements. Besides the data given directly to the authorities, have the following technical data available for review by the authorities: a. Functional qualification specifications for
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