49.090 机上设备和仪器 标准查询与下载

NAVY MIL-I-22126 B (3)-2001 螺旋桨发动机扭矩指示器

This amendment forms a part of MIL-I-22126B(AS), dated 17 August 1972, and has been approved by the Naval Air Systems Command, Department of the Navy. It is available for use by all Departments and Agencies of the Department of Defense.

INDICATOR, TORQUEMETER, ENGINE, TURBOPROP

NAVY MIL-I-81454 (3)-2001 ID-1481(*)/A型垂直陀螺仪指示器

This amendment forms a part of MIL-I-81454(AS), dated 15 January 1967, and is approved for use by the Naval Air Systems Command, Department of the Navy and is available for use by all Departments and Agencies of the Department of Defense.

INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A

NAVY MIL-I-8974 A (2)-2001 事件指示器一般规范

This amendment forms a part of MIL-I-8974A, dated 15 July 1981, and is approved for use by all Departments and Agencies of the Department of Defense.

INDICATOR, EVENT COUNTING, GENERAL SPECIFICATION FOR

SAE AMS2521C-2001 反射减少用于减少反射涂料的仪器玻璃

This specification covers optical-quality coatings applied to instrument glasses. This coating has been used typically to reduce the intensity of reflection from the surfaces of instrument glasses and to increase light transmission through the glasses, but usage is not limited to such applications.

Coating, Reflection-Reducing for Instrument Glasses

SAE AMS3151C-2001 流体，飞机罗盘

This specification covers one grade of hydrocarbon compass fluid. This product has been used typically for use as a filling medium for magnetic compasses.

Fluid, Aircraft Compass

ISO/TR 10201:2001 航空航天 电子仪表和系统的标准

This Technical Report gives a list of standards related to electronic instruments and systems for aerospace.

Aerospace - Standards for electronic instruments and systems

ARINC 753-3 ITEM 6.0-2001 数据链接控制功能

Data Link Control Functions

Data Link Control Functions

NAVY MIL-I-81388 A (2)-2001 液态氧质量指示器中继器

The margins of this amendment are marked with asterisks to indicate where changes from the previous amendment were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous amendment.

INDICATOR REPEATERS, LIQUID OXYGEN QUANTITY

NAVY MIL-I-81387 A (3)-2001 液态氧质量指示器

The margins of this amendment are marked with asterisks to indicate where changes from the previous amendment were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous amendment.

INDICATOR, LIQUID OXYGEN QUANTITY

SAE ARP5366-2001 自动驾驶仪,飞行指挥和自动推力系统

This document recommends criteria for the design and installation of autopilot, flight director and autothrust systems. These three systems are highly interrelated and will be referred to generically as an integrated flight guidance system (IFGS).

Autopilot, Flight Director, and Autothrust Systems

NAVY MIL-I-20037 B NOTICE 3-2001 液体水准的直接和间接管状的玻璃或塑料指示器

MIL-I-20037B, dated 1 June 1984, with Amendment 2, dated 8 Dec 2000, is inactive for new design and is no longer used, except for replacement purposes. Future acquisition for this material should refer to ASTM F2045, "Standard Specification for Indicators, Sight, Liquid Level, Direct and Indirect Reading, Tubular Glass/Plastic."

INDICATORS, SIGHT, LIQUID LEVEL, DIRECT/INDIRECT READING, TUBULAR GLASS/PLASTIC

SAE ARP4102/9A-2001 飞行管理系统(FMS)

This document recommends criteria and requirements for a Flight Management System (FMS) for transport aircraft.

Flight Management System (FMS)

GOST R 51747-2001 航空器用微波无线电航标仪表进场着陆系统.主要参数与测量方法

Настоящий стандарт распространяется на радиомаячную систему инструментального захода летательных аппаратов на посадку сантиметрового

Microwave radio beacon instrument approach landing system for air vehicles. Main parameters and methods of measuring

IEEE 836-2001 线性加速度测量仪精密离心试验推荐规程

Describes the conduct and analysis of precision tests that are to be performed on linear accelerometers using centrifuge techniques

Recommended practice for precision centrifuge testing of linear accelerometers

SAE AIR5273-2001 致动系统故障探测方法

This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation, but also includes one augmented-control system. The purpose of this document is to aid the designers of the systems of the future by showing what succeeded in the past.

Actuation System Failure Detection Methods

ANSI/IEEE 528:2001 惯量传感器术语标准

This standard provides a listing of terms and definitions related to inertial sensors. The criterion for inclusion of terms and definitions in this standard is their general usefulness as related to inertial sensor technology.

Standard for Inertial Sensor Terminology

SAE AS5498-2001 飞行中冰检测系统的最低操作性能规范

The objective of this Minimum Operational Performance Specification is to specify the minimum performance of onboard inflight icing detection systems. Throughout the document, these devices are referred to as Flight Icing Detection Systems (FIDS). These systems are intended to either provide information which indicates the presence of ice accreted in flight on monitored surfaces or indicate the presence of icing conditions in the atmosphere. They may operate the airplane anti-ice/deice systems. Detection of ice accreted on the ground is not considered in this document but can be found in ED-104. This MOPS was written for the use of FIDS on airplanes only, as defined in paragraph 1.5. Use on other aircraft may require additional considerations.

Minimum Operational Performance Specification for Inflight Icing Detection Systems

SAE AS5134A-2001 航空求救信号

This SAE Aerospace Standard (AS) provides minimum performance and design standards to be applied to an Aviation Distress Signal, a handheld, high- intensity, stroboscopic light source designed to facilitate location and rescue of aviation accident/ditching survivors by ground, sea or airborne search and rescue resources. The purpose of this document is to define a device that can be used in lieu of pyrotechnic devices in aviation survival kits - while meeting two primary objectives: (1) provide an equivalent level of safety to pyrotechnics with respect to utility as an aid to search and rescue, and (2) eliminate significant potential equipment and personnel hazards posed by the use of pyrotechnics by untrained personnel in inflatable life rafts.

Aviation Distress Signal

CEA-775.2-2000 数字存储媒体互操作性选择信息服务

Users of this standard should be aware that ongoing standardization work in the 1394 Trade Association may have a future impact on this standard.

Service selection information for digital storage media interoperability

AIR FORCE MS28025 REV D VALID NOTICE 2-2000 航空器加速器

MS28025D remains inactive for new design, however the document is valid for acquisition when needed.

ACCELEROMETER-AIRCRAFT