ASTM名称
数字
FAA要求的ASTM文件标题变更
接受1,2
补充资料3
通过小型飞机战略政策
部分
F3234/F3234M–17标准规范
小型外部照明
飞机
删除：
表1
飞机型号代码合规矩阵
在F3234/F3234M-17中找到的表不是
认可的。将确定适用性
通过小型飞机战略政策
部分
F3235–17a标准规范
飞机蓄电池
删除：
第4.2节
删除：
表1
如果申请飞机认证
已安装锂电池的申请人
可以使用RTCA提供的指导
DO-311A，或可获得FAA认可
在
根据§23.2010。
飞机型号代码合规矩阵
不接受F3235-17a中的表格。
适用性将由
小型飞机战略政策部分。
F3236–17标准规范
高强度辐射
现场（HIRF）保护
小型飞机
删除：
表1
修订：
表2 400至700 Mhz频率范围
场强平均值：
替换为：“100伏/米”
带有：“50伏/米”
替换：第4.2.3.3节
与：联邦航空局第4.2.3.3节“从40到
400 MHz，使用传导磁化率
测试，在40℃下至少30 mA开始
飞机型号代码合规矩阵
不接受F3236-17中的表格。
适用性将由
小型飞机战略政策部分。
第23部分：基于ASTM共识标准的认可合规手段
2022年3月11日生效
1参考通知编号NOA-23-22-01，于2022年3月11日在《联邦公报》[87 FR 13911]2中发布。合规手段适用于传统的第23部分飞机，而非新颖设计。新设计需要评估和可能的修改
合规手段。
3您可以在FAA小型飞机问题列表（SAIL）中找到更多信息：
https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/第8页
ASTM名称
数字
FAA要求的ASTM文件标题变更
接受1,2
补充资料3
MHz，每频率降低20 dB
在400下，十年至最小3 mA
兆赫。”
F3239–19标准规范
飞机电气
推进系统
联邦航空局并不普遍接受F3239–
19由于对标准缺乏经验。
鼓励申请人考虑：
建议F3239-19开发
他们的电气顺应性方法
逐项推进系统
原因任何合规方法
建议必须建立安全等级
等同于认证往复式和
涡轮机推进系统和接收
FAA根据
§23.2010.
F3254–19标准规范
飞机相互作用
系统和结构
图2、3和4
替换为：“远程”
与：“10-5”
替换为：“极不可能”
1级、2级和3级飞机的“10-8”
4级飞机的“10-9”
其他建议的概率为：
由联邦航空局逐案考虑
原因
F3309/F3309–21标准操作规程
简化安全
系统评估
和小型设备
飞机
没有一个
F3316/F3316M–19标准规范
电气系统
带电动或
混合电力推进
联邦航空局并不普遍接受
F3316/F3316M–19由于缺乏经验
与标准。
删除：
表1
鼓励申请人考虑：
建议F3316/F3316M–19用于
他们方法的发展
电气系统安装的合规性ASTM Designation Number ASTM Document Title Changes Required for FAA Acceptance1,2 Additional Information3 by the Small Airplane Strategic Policy Section. F3234/F3234M – 17 Standard Specification for Exterior Lighting in Small Aircraft Remove: Table 1 Aircraft Type Code compliance matrix table found in F3234/F3234M-17 are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section. F3235 – 17a Standard Specification for Aircraft Storage Batteries Remove: Section 4.2 Remove: Table 1 If applying for certification of an airplane with installed lithium batteries, applicants may use the guidance provided by RTCA DO-311A, or may obtain FAA acceptance of a different method of compliance in accordance with §23.2010. Aircraft Type Code compliance matrix table found in F3235-17a are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section. F3236 – 17 Standard Specification for High Intensity Radiated Field (HIRF) Protection in Small Aircraft Remove: Table 1 Revise: Table 2 400 to 700 Mhz frequency range field strength average value: Replace: “100 volts/meter” With: “50 volts/meter” Replace: Section 4.2.3.3 With: FAA Section 4.2.3.3 “From 40 to 400 MHz, use conducted susceptibility tests, starting at a minimum of 30 mA at 40 Aircraft Type Code compliance matrix table found in F3236-17 are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section. Part 23 Accepted Means of Compliance Based on ASTM Consensus Standards Effective March 11, 2022 1 Reference Notice No. NOA-23-22-01, published in the Federal Register on March 11, 2022 [87 FR 13911] 2 The means of compliance are intended for traditional part 23 airplanes, not for novel designs. Novel designs require evaluation and possible modification of the means of compliance. 3 You may find additional information on the FAA Small Airplane Issues List (SAIL) here: https://www.faa.gov/aircraft/air_cert/design_approvals/small_airplanes/small_airplanes_regs/ Page 8 ASTM Designation Number ASTM Document Title Changes Required for FAA Acceptance1,2 Additional Information3 MHz, decreasing 20 dB per frequency decade to a minimum of 3 mA at 400 MHz.” F3239 – 19 Standard Specification for Aircraft Electric Propulsion Systems FAA does not universally accept F3239 – 19 due to inexperience with the standard. Applicants are encouraged to consider proposing F3239 – 19 for development of their method of compliance for electric propulsion systems on a project-by-project basis. Any method of compliance proposed must establish a level of safety equivalent to certified reciprocating and turbine propulsion systems and receive acceptance by FAA in accordance with §23.2010. F3254 – 19 Standard Specification for Aircraft Interaction of Systems and Structures Figures 2, 3 and 4 Replace: “Remote” With: “10-5” Replace: “Extremely Improbable” With: “10-8” for Level 1, 2 and 3 airplanes and with “10-9” for Level 4 airplanes” Other proposed probabilities will be considered by the FAA on a case by case basis. F3309/F3309M – 21 Standard Practice for Simplified Safety Assessment of Systems and Equipment in Small Aircraft None F3316/F3316M – 19 Standard Specification for Electrical Systems for Aircraft with Electric or Hybrid-Electric Propulsion FAA does not universally accept F3316/F3316M – 19 due to inexperience with the standard. Remove: Table 1 Applicants are encouraged to consider proposing F3316/F3316M – 19 for development of their method of compliance for electrical systems instal
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