V41 导航通讯系统与设备 标准查询与下载

SAE ARP5119-1999 用于大角度接近IMC(集成市场通讯)的下视电子飞行显示器的位置和显示器符号要求

The recommendations of this document apply to such aircraft as are able to perform both normal angle and steep IMC approaches, the latter being defined as those approaches having a final approach segment angle greater than 4? Such aircraft can include both conventional and STOL fixed-wing aircraft, commercial air transport and/or utility and normal category helicopters, compound helicopters and powered lift vehicles (tiltrotors, tiltfans, tiltwings, etc.). The purpose of this document is to set forth the recommendations of SAE Committee G-10 Vertical Flight Subcommittee relative to the location, control, and implementation of electronic flight information systems, primary flight displays, secondary (standby flight) displays, engine and instruments displays, crew alert displays and associated required flight deck/cockpit displays. These recommendations are intended to derive intuitive and easily interpretable displays and display locations to minimize confusion, distraction and fatigue, thereby reducing crew workload and increasing crew performance, efficiency, safety and reducing factors detrimental to flight safety. In arriving at these recommendations the committee carefully reviewed the layouts of modern commercial and military aircraft, developmental tiltrotor flight deck/cockpit layouts, the recommendations and requirements of the Federal Aviation Administration Aircraft Certification branch and the requirements of commercial operators and aircraft manufacturers. In cases where conflicting opinions existed, suitable compromises were made. This document applies to all electronic flight instrument display systems, including but not limited to liquid crystal displays (LCD), field emitting diodes (FED), light emitting diodes (LED) or cathode ray tube (CRT) technology.

Location of and Display Symbology Requirements for Head-Down Electronic Flight Displays for Steep IMC Approaches

SAE AS5604-1999 领航员备用磁罗盘

This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilots standby compasses as specified herein.

Compass; Magnetic, Pilot磗 Standby FSC 6605; Should Be Used Instead of MIL-C-5604B, Which Was Cancelled on 31 August 1999

SAE ARP5287-1999 机载平视显示器(HUD)的光学测量规程

This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne binocular Head-Up Displays (HUDs). This document covers methods for conformal and non-conformal HUD systems that are intended for use in the cockpit by the pilot or copilot. The focus of this document is on displays that generate the HUD information using a cathode ray tube (CRT), however, the majority of the methods can be applied to other display technologies. These measurement methods are provided for testing to the requirements of AS8055. This document does not address measurement methods for sensor-imaging systems, or displays worn by the pilot (goggles, helmet-mounted displays).

Optical Measurement Procedures for Airborne Head Up Display (HUD)

QJ 3081-1999 仪器仪表管理检查考核评定标准

Instrumentation management inspection and assessment standards

SAE ARP5365-1999 交通信息座舱显示器的人性化界面标准

This SAE Aerospace Recommended Practice (ARP) sets forth design and operational recommendations concerning the human factors issues and criteia for cockpit display of traffic information systems. The visual and aural characteristics are covered for both the alerting components and traffic depiction/situation components. The display system may contain any one or a combination of these components. Although the system functionality assumed for this document exemplifies fixed- wing aircraft implementation, the recommendations do not preclude other aircraft types. The recommendations contained in this document address both near and far term technology directed toward providing in flight traffic awareness, although the present version remains primarily focused on near term applications. Since this document provides recommendations, the guidance is provided in the form of should statements as opposed to the shall statements that appear in standards and requirements.

Human Interface Criteria for Cockpit Display of Traffic Information

SAE ARP4714-1999 电子发动机控制器的外部软件装载

This paper presents guidelines for development of a procedure for external software loading of an electronic engine control(EEC)for a commercial application, on-wing or in a qualified service shop. This paper makes the following assumptions: a. The EEC is designed to accept external software loading. b. The EEC is certified as part of an engine. c. The support equipment is qualified in accordance with procedures set forth by the engine (and aircraft, if necessary) certifying authority if the EEC cannot detect an integrity violation of the loaded program. The software to be loaded has been approved by the engine and aircraft certifying authorities. One or more configurations of EEC hardware has been identified for each version of software which is to be loaded in the EEC. It is appropriate to use these guidelines in the initial development phase, although the certification issues would not be applicable. Approval as used herein means approval by the engine (and aircraft, if necessary) certifying authority. There are cases where the engine may commence certification activities and no specific aircraft application has been identified. In these cases, the aircraft certification authority should be notified of the EECs external software loading capability when the engines application is identified. The appropriate documentation can be delivered to the aircraft certifying authority at that time.

External Software Loading of Electronic Engine Controls

MH/T 4006.1-1998 航空无线电导航设备.第1部分：仪表着陆系统(ILS)技术要求

本标准规定了民用航空仪表着陆系统设备的通用技术要求，它是民用航空仪表着陆系统设备制定规划和更新、设计、制造、检验以及运行的依据。 本标准适用于民用航空行业各类仪表着陆系统设备。

Aeronautical radio navigation aids.Part 1:Technical requirements for instrument landing system(ILS)

MH/T 4006.3-1998 航空无线电导航设备.第3部分：测距仪(DME)技术要求

本标准规定了民用航空测距仪设备的通用技术要求，它是民用航空测距仪设备制定规划和更新、设计、制造、检验以及运行的依据。 本标准适用于民用航空行业各种地面测距仪(DME)设备。

Aeronautical radio navigation aids.Part 3:Technical requirements for distance measuring equipment(DME)

MH/T 4006.4-1998 航空无线电导航设备.第4部分：无方向性信标(NDB)技术要求

本标准规定了民用航空无方向性信标(NDB)设备的通用技术要求，它是民用航空无方向性信标设备制定规划和更新、设计、制造、检验及运行的依据。 本标准适用于民用航空行业各类地面无方向性信标设备。

Aeronautical radio navigation aids.Part 4:Technical requirements for non-directional radio beacon(NDB)

MH/T 4006.2-1998 航空无线电导航设备.第2部分：甚高频全向信标(VOR)技术要求

本标准规定了民用航空甚高频全向信标设备的通用技术要求，它是民用航空甚高频全向信标制定规划和更新、设计、制造、检验以及运行的依据。 本标准适用于民用航空行业各类甚高频全向信标设备。

Aeronautical radio navigation aids.Part 2:Technical requirements for very high frequency omnidirectional range(VOR)

SAE ARP4032A-1998 对于飞机电子显示器色彩应用中人的因素的考虑

Although this document is specifically intended for the application of color to cathode-ray-tube (CRT) instrumentation, most portions are also compatible with other emerging electronic display technologies, whether they are self-luminous or light modulating devices, such as liquid crystal displays. However, it is not intended to address the concerns brought about by the use of specialized equipment such as head-up displays and night vision goggles. Identifiable incompatibilities or special considerations for color display technologies other than the CRT have been noted in the recommendations. This document makes recommendations concerning human factors issues in the application of color to self-luminous display instrument systems.

Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays

SJ 20697-1998 敌我识别和空中交通管制(IFF/ATC)机载询问应答机通用规范

本规范规定了敌我识别《IFF》(含询问应答)和空中交通管制《ATC》(仅含应答)机载询问应答机的要求、质量保证规定，交货准备等。 本规范适用于询问应答机的设计，生产和验收，是制定产品规范的基本依据。

General specification for IFF/ATC airborne interrogator-transponders

SJ 20698-1998 敌我识别和空中交通管制(IFF/ATC)地面询问应答机通用规范

本规范规定了敌我识别《IFF》(含询问应答)和空中交通管制《ATC》(仅含询问)地面询问应答机的要求、质量保证规定，交货准备等。 本规范适用于询问应答机的设计、生产、检验、包装、运输和贮存。是制订产品规范的基本依据。

General specification for IFF/ATC ground interrogator-transponders

SAE AIR4742-1998 FDI平视显示器显示导航系统(经核准用于B-727飞机)的显示特性

The scope of this document is limited to descriptions of the display characteristics of the Flight Dynamics, Inc. (FDI) Model 1000WS Head up Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category III landing operations. The symbology depicted in this document is referenced to the particular pilot task(s) for which it was designed. Also included are descriptions of operational features of the particular symbol along with any associated criteria regarding symbology constraints, source data, or position error.

Display Characteristics of FDI Head-Up Guidance System as Approved for the B-727 Airplane

NAVY MIL-STD-291 C-1998 标准战术空中导航TACAN信号

This standard defines the Standard TACAN Signal. The characteristics and tolerances specified will ensure compatibility of all airborne and ground equipment.

STANDARD TACTICAL AIR NAVIGATION (TACAN) SIGNAL

AIAA G-034-1998 参考和标准电离层模型的指南

Guide to Reference and Standard Ionosphere Models

Guide to Reference and Standard Ionosphere Models

SAE ARP4102/8A-1998 驾驶舱平视显示器[代替:SAE ARP 1068B]

This SAE Aerospace Recommended Practice (ARP) recommends criteria for the design and installation of Head-Up Display (HUD) systems. The recommendations are applicable to HUD systems for transport category aircraft, which display flight information (focused at infinity) in the forward field of view. The HUD total system requirement recommendations shall primarily lead to certifiable fail-passive CAT III characteristics and performance. This document forms a part of these recommendations. This document does not address devices for peripheral vision of displays worn by the pilot, nor the presentation of enhanced vision system (EVS) information.

Flight Deck Head-Up Displays [Superseded: SAE ARP 1068B]

SAE AS4111-1998 数字式时分制指令/响应型多路传输数据总线远程终端的确认试验计划

This SAE Aerospace Standard (AS) contains a sample test plan for AS 15531 or MIL-STD-1553B Remote Terminals (RT) that may serve several different purposes. This document is intended to be contractually binding when specifically called out in a specification, Statement of Work (SOW), or when required by a Data Item Description (DID). Any and all contractor changes, alterations, or testing deviations to this section shall be separately listed for easy review. The purpose of these tests is to verify that the Unit Under Test (UUT) responds properly in accordance with the requirements of the governing standard. The tests are not intended to verify the mission aspects stated in the equipment specification. The pass criteria is defined in each test paragraph. If any test fails, record the UUT response to that test. This general test plan is intended for design verification of remote terminals designed to meet the requirements of AS 15531 and MIL-STD-1553B with Notice 2. Appendix A, B, and C provide cross references among this test plan, AS 15531, and MIL-STD-1553B. For those remote terminals not required to meet Notice 2, Appendix D and E list the changes in this test plan for MIL-STD-1553B only and MIL-STD-1553B, Notice 1. The test plan requirements apply to the terminal under test, when invoked in a specification or statement of work. When invoked in a specification or statement of work, these requirements apply to the remote terminal and associated equipment which is developed either alone or as a portion of a system or subsystem development. The contractor is responsible for invoking all the applicable requirements of this document on any and all subcontractors he/she may employ.

Validation Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Remote Terminals

SAE ARP5108-1997 地形分离保证显示技术的人性化界面标准

This document sets forth design and operational recommendations concerning the human factors issues and criteria for airborne terrain separation assurance systems. The visual and aural chracteristics are covered for both the alerting components and terrain depiction/situation components. The display system may contain any one or a combination of these components. Although the system functionality assumed for this document exemplifies commercial aircraft implementation, the recommendations do not exclude other fixed wing aircraft types. Because of their unique operations with respect to terrain, rotorcraft will be addressed in a separate document. The assumptions about the system that guided and bounded the recommendations include: the system will have a human centered design based on the lessons learned from past systems; the system is an on-board system that is not dependent on ground systems (except possibly navigation sensors) for operation; the system is intended to be used for terrain separation rather than navigation; there will be pilot in the loop/manual involvement in any flight path changes; information will be accessible by all flight crew members; the system will be based on the English language, but other languages may have to be considered; the system will address all fixed wing airplane types; the system will be operational full time in all flight phases; and the system will meet harmonized certification requirements.

Human Interface Criteria for Terrain Separation Assurance Display Technology

HB 7280-1996 机载多普勒雷达导航设备最低性能要求

本标准规定了机载多普勒雷达导航设备必须满足的最低性能要求。 　　本标准适用于民用飞机上所用的多普勒雷达导航设备。

Minimum performance requirements for airborne doppler radar navigation equipment