- 您的位置:
- 中国标准在线服务网 >>
- 全部标准分类 >>
- 国际标准 >>
- 49.060 >>
- ISO 8816:1993/Amd 1:2012 EN e0f4c1f9

【国际标准】 Aircraft — Solid-state remote power controllers — General requirements — Amendment 1
本网站 发布时间:
2024-05-11
- ISO 8816:1993/Amd 1:2012 EN
- 现行
选择类型:
电子版: 150元
/ 折扣价:
135 元
开通会员免费在线看70000余条国内标准,赠送文本下载次数,单本最低仅合13.3元!还可享标准出版进度查询、定制跟踪推送、标准查新等超多特权!  
查看详情>>

适用范围:
暂无
标准号:
ISO 8816:1993/Amd 1:2012 EN
标准名称:
Aircraft — Solid-state remote power controllers — General requirements — Amendment 1
英文名称:
Aircraft — Solid-state remote power controllers — General requirements — Amendment 1标准状态:
现行-
发布日期:
2012-09-14 -
实施日期:
出版语种:
EN
- 推荐标准
- 国家标准计划
- IEC 62668-1:2019/AMD1:2024 EN-FR fb430855 Amendment 1 - Process management for avionics - Counterfeit prevention - Part 1: Avoiding the use of counterfeit, fraudulent and recycled electronic components
- IEC TR 63238-1:2019 EN 3d99f7c2 Process management for avionics - Electronics design - Part 1: Electrical signal properties, naming conventions and interface control document (ICD)
- IEC TR 62396-6:2017 EN 153dfc1c Process management for avionics - Atmospheric radiation effects - Part 6: Extreme space weather - Potential impact on the avionics environment and electronics
- IEC TR 62396-7:2017 EN 5e548e9c Process management for avionics - Atmospheric radiation effects - Part 7: Management of single event effects (SEE) analysis process in avionics design
- ISO 2635:2003/Amd 1:2017 EN 27583fc5 Aircraft — Conductors for general purpose aircraft electrical cables and aerospace applications — Dimensions and characteristics — Amendment 1: Correction of table 1
- ISO 8056-2:1988/Amd 1:2016 EN 42ad14c4 Aircraft — Nickel-chromium and nickel-aluminium thermocouple extension cables — Part 2: Terminations — General requirements and tests — Amendment 1
- IEC TS 62564-1:2016 EN 6319989f Process management for avionics - Aerospace qualified electronic components (AQEC) - Part 1: Integrated circuits and discrete semiconductors
- IEC 62396-4:2013 EN 4e65a713 Process management for avionics - Atmospheric radiation effects - Part 4: Design of high voltage aircraft electronics managing potential single event effects
- IEC 60952-3:2013 EN-FR a7508d47 Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)
- ISO 8816:1993/Amd 1:2012 EN e0f4c1f9 Aircraft — Solid-state remote power controllers — General requirements — Amendment 1
- ISO 8843:2005/Amd 1:2012 EN ad5efdf8 Aircraft — Crimp-removable contacts for electrical connectors — Identification system — Amendment 1
- IEC TS 62564-1:2011 EN 2e79feab Process management for avionics - Aerospace qualified electronic components (AQEC) - Part 1: Integrated circuits and discrete semiconductors
- IEC TS 62396-5:2008 EN 7ca09d1c Process management for avionics - Atmospheric radiation effects - Part 5: Guidelines for assessing thermal neutron fluxes and effects in avionics systems
- ISO 5066-1:1986 EN 4d72dd66 Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 1: Operating characteristics and test conditions
- ISO 5066-2:1986 EN c747849c Aircraft — Hermetically sealed monostable electrical relays, 2A and 3A — Part 2: Type approval tests