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
F2490–20标准指南
飞机电气负荷
和电源
容量分析
没有一个
F3061/F3061M–20标准规范
系统和设备
小型飞机
删除：
表1、3、4、5、13和14
将17.3.1替换为以下内容：
（a） 每个电气或电子系统：
执行一个功能，该功能失败
将阻止继续安全飞行，以及
必须设计飞机着陆
并安装为：-
（1） 飞机层面的功能不是：
在以下期间和之后受到不利影响：
飞机暴露于雷电的时间；
和
（2） 系统恢复正常运行
在以下情况下及时执行该职能：
飞机暴露在雷电中，除非：
系统的恢复与其他冲突
操作或功能要求
系统。
将17.3.2替换为以下内容：
（b） 每个电气和电子系统
执行功能的
这将***降低
飞机型号代码合规矩阵
F3061/F3061M–20中的表格如下：
不接受。适用性将是
由小型飞机战略决定
政策部分。
F3061/F3061M-20不包含手段
显示符合§23.2310的要求
水上飞机和两栖动物的浮力。如果
申请水上飞机认证，或
两栖动物，申请人可使用
§23.751、23.755和
23.757在修正案23-63中，作为
符合§23.2310，或可获得
联邦航空局接受不同的方法
符合§23.2010的要求。
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2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
飞机的能力或
机组人员应对不利情况
操作条件，必须设计和
已安装，以便系统恢复
该功能在
飞机暴露后及时
闪电。
删除17.3.3
F3062/F3062M–20标准规范
飞机动力装置
安装
没有一个
F3063/F3063M–20标准规范
飞机燃料和能源
储存和交付
没有一个
F3064/F3064M–21标准规范
飞机动力装置
控制、操作和
指示
没有一个
F3065/F3065M–21a标准规范
飞机螺旋桨系统
安装
没有一个
F3066/F3066M–18标准规范
飞机动力装置
安装危险
缓解
没有一个
F3082/F3082M–17标准规范
重量和中心
飞机重力
没有一个
F3083/F3083M–20a标准规范
紧急情况，
不vASTM Designation Number ASTM Document Title Changes Required for FAA Acceptance1,2 Additional Information3 F2490 – 20 Standard Guide for Aircraft Electrical Load and Power Source Capacity Analysis None F3061/F3061M – 20 Standard Specification for Systems and Equipment in Small Aircraft Remove: Tables 1, 3, 4, 5, 13 and 14 Replace 17.3.1 with the following: (a) Each electrical or electronic system that performs a function, the failure of which would prevent the continued safe flight and landing of the airplane, must be designed and installed such that - (1) The function at the airplane level is not adversely affected during and after the time the airplane is exposed to lightning; and (2) The system recovers normal operation of that function in a timely manner after the airplane is exposed to lightning unless the system&＃39;s recovery conflicts with other operational or functional requirements of the system. Replace 17.3.2 with the following: (b) Each electrical and electronic system that performs a function, the failure of which would significantly reduce the Aircraft Type Code compliance matrix tables found in F3061/F3061M – 20 are not accepted. Applicability will be determined by the Small Airplane Strategic Policy Section. F3061/F3061M-20 does not contain means for showing compliance to §23.2310 Buoyancy for seaplanes and amphibians. If applying for certification of a seaplane or amphibian, applicants may use the provisions of §§23.751, 23.755, and 23.757 at amendment 23-63 as a means of complying with §23.2310, or may obtain FAA acceptance of a different method of compliance in accordance with §23.2010. 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 2 ASTM Designation Number ASTM Document Title Changes Required for FAA Acceptance1,2 Additional Information3 capability of the airplane or the ability of the flight crew to respond to an adverse operating condition, must be designed and installed such that the system recovers normal operation of that function in a timely manner after the airplane is exposed to lightning. Remove 17.3.3 F3062/F3062M – 20 Standard Specification for Aircraft Powerplant Installation None F3063/F3063M – 20 Standard Specification for Aircraft Fuel and Energy Storage and Delivery None F3064/F3064M – 21 Standard Specification for Aircraft Powerplant Control, Operation, and Indication None F3065/F3065M – 21a Standard Specification for Aircraft Propeller System Installation None F3066/F3066M – 18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation None F3082/F3082M – 17 Standard Specification for Weights and Centers of Gravity of Aircraft None F3083/F3083M – 20a Standard Specification for Emergency Conditions, Non
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