SAE規格 AIR6808, Revision A, 2024: Aerospace Vehicle Wiring, Lessons Learned

SAE規格 AIR6808, Revision A, 2024: Aerospace Vehicle Wiring, Lessons Learned

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SAE規格 AIR6808, Revision A, 2024: Aerospace Vehicle Wiring, Lessons Learned

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SAE AIR6808, Revision A, 2024: Aerospace Vehicle Wiring, Lessons Learned
SAE規格 AIR6808, Revision A, 2024: 航空宇宙車両の配線、得られた教訓
発行元 SAE International
発行年/月 2024年3月
装丁 ペーパー
ページ数 83 ページ
発送予定 海外倉庫よりお取り寄せ 1-2週間以内に発送します
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Description

This AIR is limited to the requirements of AS50881 and examines these requirements, providing rationale behind them. AS50881 is only applicable to the aircraft EWIS. Pods and other devices that can be attached to an aircraft are considered as part of the aircraft equipment design. Its scope does not include wiring inside of airborne electronic equipment but does apply to wiring externally attached to such equipment. The AS50881 scope does not include attached devices but does include the interface between the pod/equipment and aircraft wiring. Section 3.3.5 addresses components such as antennas and other similar equipment that were once supplied as Government Furnished Aeronautical/Aerospace Equipment (GFAE).

Purpose
The purpose of this document is to provide information about how each of the requirements of AS50881 can affect performance, safety, reliability, and maintainability attributes and the potential consequences of their omission.

Paragraph Organization
The paragraphs listed in Section 3 are the same titles used in AS50881 Revision G Section 3. Section 3 lists the individual EWIS system, process, or performance requirements. Each requirement paragraph from AS50881 is show in green font. Following each AS50881 green requirement paragraph (green font), when applicable, there is a “rationale” paragraph in black font. The rationale following each requirement paragraph in this AIR provides information regarding the EWIS safety, reliability, historical context, and performance implications.