标准摘要
[中文适用范围]: 涉及各类需要高精度高度信息的航空器设备,为相关工程实践提供了重要的技术支撑,促进了航空安全体系的完善与发展。通过统一技术指标,该规范有助于提升整个行业在高度测量领域的技术水平与安全性。 [外文原描述]: The instrument system specified shall accept an input of static pressure and in some equipment other inputs that contribute altitude information to provide a visual indication of pressure altitude. If equipped with an automatic correction mechanism, it shall indicate by a positive means when the automatic correction mechanism is not in use. If the static source pressure error compensating mechanism is operational it shall be functional throughout the required operating envelope of the particular aircraft. Each aircraft type has its own static source error data which shall be obtained from the airframe manufacturer’s certified data. When a Central Air Data Computer is used in the altimeter system, the CADC shall be certified to its own governing document and the altimeter system (CADC and display) shall comply with the requirements of this document.NOTE: The instrument system specified herein does not include the aircraft pressure lines and pressure sources.Cross Reference: NASATN-D822,RTCADO-138
英文名称PRESSURE ALTIMETER SYSTEM MINIMUM SAFE PERFORMANCE STANDARD