49.090 机上设备和仪器 标准查询与下载

SAE AS264E-2002 商用运输机仪表和驾驶舱照明

Instrument and Cockpit Lighting for Commercial Transport Aircraft

SAE ARP493A-2002 旋钮，控制飞机，推荐设计

Knobs, Control Aircraft, Recommended Design

CEA-709.1-B-2002 控制网络协议规范

This specification applies to a communication protocol for networked control systems. The protocol provides peer-to-peer communication for networked control and is suitable for implementing both peer-to-peer and master-slave control strategies. This specification describes services in layers 2-7. In the layer 2 (data link layer) specification, it also describes the MAC sub-layer interface to the physical layer. The physical layer provides a choice of transmission media.

Control Network Protocol Specification

SAE ARP4102/11C-2002 (R)机载风的切变系统[代替:SAE ARP4109]

This document recommends criteria for Airborne Windshear Systems, including operational objectives, characteristics and functional requirements. The recommendations in this document apply to transport aircraft, and describe the operational objectives of windshear alerting systems, situational displays, guidance systems and avoidance/detection systems.

(R) Airborne Windshear Systems [Superseded: SAE ARP 4109]

CEA-897-2002 家庭电视系统F-连接器彩色编码

This specification contains all the information necessary to facilitate the exchange of data and control information over twisted pair media within a home.

F-Connectors Color Coding for Home Television Systems

ARINC 610B ITEM 4.0-2001 功能需求

Function Requirements

Function Requirements

DLA MS25331 REV C VALID NOTICE 2-2001 打样试验指示器的灯装置

MS25331C, dated 14 September 2001, has been reviewed and determined to be valid for use in acquistion

LIGHT ASSEMBLY, PRESS TO TEST INDICATOR

DLA MS25331 REV C VALID NOTICE 1-2001 打样试验指示器的灯装置

MIL-DTL-11589/55E, dated 21 January 1999, is hereby reactivated and may be used for either new or existing design acquisition.

LIGHT ASSEMBLY, PRESS TO TEST INDICATOR

AIR FORCE DI-QCIC-81611-2001 精密测量仪器实验室(PMEL)质量指南

This Data Item Description (DID) contains the format and content preparation instructions for the data product generated by the specific and discrete task requirement as delineated in the contract.

PRECISION MEASUREMENT EQUIPMENT LABORATORY (PMEL) QUALITY MANUAL

SAE ARP427A-2001 压力比仪器

To recommend requirements for electrical Pressure Ratio Indicating Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Para. 3.3. This recommended practice is to be considered as being currently applicable and necessarily subject to revision from time to time due to rapid development in the aircraft industry. This Aeronautical Recommended Practice covers two types of two unit Pressure Ratio Instruments each of which consist of a Transducer and an Indicator. The Transducer computes the ratio of two pressures and converts this ratio to a synchro electrical signal which is transmitted to the Indicator. TYPE I - All material in this document applies to this classification only. TYPE II - Additional material for this classification will be added to superseding issues as the state of the art permits.

Pressure Ratio Instruments

SAE AIR818D-2001 飞机仪表和仪表系统标准:措辞术语,表达方式,环境设计标准

This Aerospace Information Report, (AIR) is intended to provide the sponsors of Aerospace Standards, (AS), with standard wording, formatting, and minimum environment and design requirements for use in the preparation of their document. The individual shall use only those parts of this AIR which apply to their particular document. The individual sponsor may expand the standard wording, especially under Sections 4, 5, and 6 as required. The paragraphs of this AIR shall be used verbatim wherever possible. Unless otherwise directed by SAE, cross referenced documents shall be called out by specific revision letter, e.g. shall be in accordance with AS XXXXB. In addition, all non-SAE documents called out shall include the document title when initially identified. However, every effort shall be made to keep cross-referencing to an absolute minimum.

Aircraft Instrument and Instrument System Standards: Wording Terminology, Phraseology, Environment and Design Standards For

SAE AS412B-2001 一氧化碳检测仪器

To specify minimum requirements for carbon monoxide detector instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This standard is not intended to cover fire detectors. This Aeronautical Standard covers the basic type of carbon monoxide detector instrument used to determine toxic concentrations of carbon monoxide by the measurement of heat changes through catalytic oxidation.

Carbon Monoxide Detector Instruments

SAE AS408C-2001 测压仪表.燃料,油和液压(装有活塞式发动机的飞机)

This Aerospace Standard establishes the essential minimum safe performance standards for fuel, oil and hydraulic pressure instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aerospace Standard covers two basic types of fuel, oil and hydraulic pressure instruments as follows: Type I - Direct Indicating, Type II - Remote Indicating. This Aerospace Standard does not apply to engine mounted torque meter systems.

Pressure Instruments - Fuel, Oil and Hydraulic (Reciprocating Engine Powered Aircraft)

SAE AS405C-2001 燃料和油量装置

This Aeronautical Standard covers two basic types of instruments as follows: Type I - Float Instruments, Type II - Capacitance Instruments. To specify minimum requirements for Fuel and Oil Quantity Instruments for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3.

Fuel and Oil Quantity Instruments

SAE AS404C-2001 电动转速针:磁阻力(指示器&发生器)

To specify minimum requirements for Electric Tachometers primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers magnetic drag tachometers with or without built-in synchroscopes.

Electric Tachometer: Magnetic Drag (Indicator& Generator)

SAE AS402B-2001 自动驾驶仪

To specify minimum requirements for Automatic Pilots primarily for use in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers Automatic Pilots intended for use on aircraft to automatically operate the aerodynamic controls to maintain flight and/or to provide maneuvering about the three axes through servo control.

Automatic Pilots

SAE AS398B-2001 非稳定型磁性方向仪(磁罗盘)

To specify minimum requirements for non-stabilized magnetic direction instruments for use in aircraft, the operation of which may subject the instrument to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types of instruments as follows: Type I - Direct Reading, Type II - Remote Indicating.

Direction Instrument, Magnetic, Non-Stabilized Type (Magnetic Compass)

SAE ARP794A-2001 气流偏差指示仪(ADI)

This Aerospace Recommended Practice recommends the industry standards for an Airstream Deviation Instrument primarily for use with turbine-powered, subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.4. This recommended practice covers an instrument which measures and displays angle of deviation of the airstream dependent on mounting location on the aircraft.

Airstream Deviation Instrument (ADI)

SAE ARP5288-2001 运输类飞机平视显示器(HUD)系统

The material provided in this document consists of recommendations related to the design, analysis, testing, and intended functions of head up displays (HUDs) for transport category airplanes. The content of the document is limited to statements of general design and installation considerations, including display function criticality and compliance considerations; symbology, coding, clutter, dimensionality, and attention getting requirements; equipment installation display visual characteristics; failure modes; information display and formatting; specific integrated display and mode; and system verification.

Transport Category Airplane Head Up Display (HUD) Systems

NAVY QPL-22075-17 NOTICE 1-2001 ID-663D/U型方位一距离一航向指示器

Qualified Products List QPL-22075-16, dated 22 May 2000, is hereby inactive for new design.Military Specification MIL-I-22075C(AS), which covered the products listed thereon was inactivated on 17 September 1997.

INDICATOR, BEARING-DISTANCE-HEADING ID-663D/U