V45 航空仪表 标准查询与下载

DIN EN 303213-2:2013 高级地面移动导航和控制系统(A-SMGCS).第2部分:A-SMGCS等级2包括外部接口用欧洲单一空中互操作性规则EC 552/2004下应用的共同体规范(英文版本EN 303 213-2 V1.3.1(2012-12)的核准本作为德国标准)

Advanced Surface Movement Guidance and Control System (A-SMGCS) - Part 2: Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004 for A-SMGCS Level 2 including external interfaces (Endorsement of the E

SAE ARP5602/14-2013 航空航天平台纤维光学培训和航空航天纤维光学工程师知识能力认知教育用指南的重新认证

This document established re-certification guidelines applicable to fiber optic fabricator technical training for individuals involved in the manufacturing, installation, support, integration and testing of fiber optic systems. Applicable personnel include: Managers, Engineers, Technicians, Trainers/Instructors, Third Party Maintenance Agencies, Quality Assurance, Production

A Re-Certification Guideline for Aerospace Platform Fiber Optic Training and Awareness Education Aerospace Fiber Optics Fabricator Hands-on Competencies

IEEE 292/COR-2013 单一自由度弹簧受限比率陀螺仪用IEEE规范格式勘误表

Errata to Specification Format for Single-Degree-of-Freedom Spring-Restrained Rate Gyros

SAE ARP4032B-2013 飞机电子显示器色彩应用中的人体工程学考虑

This document is intended for the application of color to cathode-ray-tube (CRT) displays, liquid crystal displays (LCD) and other types of display technologies such as projection displays. Emerging color display technologies other than those noted above, may not be adequately covered by these recommendations. Color recommendations will not address Night Vision Devices (NVD), Head-Up Displays (HUD) or Head or Helmet Mounted Displays (HMD). This document is applicabel to aircraft as understood in 14 CFR Parts 23, Part 27 and Part 29, and EASA CS-23, CS-25, CS-27 and CS-29 certification standards.

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

SAE ARP5677-2012 改进的合成视觉系统机载实施的人体工程学注意事项

The scope of this document is limited to Enhanced Synthetic Vision Systems ESVS human factors considerations and requirements in comprehension, interpretation and application of imagery and integrated symbology in Enhanced (sensor) and Synthetic (database) Vision Systems in aircraft. Any overlap into logic problems or hardware/software design should be considered to be incidental to the human factors issues. Where the performance characteristics of specific technologies are relevant they will be identified, and where performance criteria are relevant to specific intended functions/use they will be identified. From a regulatory view, intended function (Guida

Human Engineering Considerations for Airborne Implementation of Enhanced Synthetic Vision Systems

DIN EN 303214:2012 数据链接服务(DLS)系统.统一的欧洲天空互用性规则EC 552/2004下应用的团体规范,地面组件和系统试验要求(英文版本EN 303214V1.2.1 (2012-04)的核准本作为德国标准)

Data Link Services (DLS) System - Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004, Requirements for ground constituents and system testing (Endorsement of the English version EN 303214 V1.2.1 (

IEC TS 62647-2:2012 航空电子设备过程管理.含无铅锡焊的航空和防御电子系统.第2部分:锡毒害作用的缓解

Process management for avionics - Aerospace and defence electronic systems containing lead-free solder - Part 2: Mitigation of the deleterious effects of tin

SAE AS397B-2012 稳定型非磁性方向仪(航向陀螺仪)

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This document has been declared "NONCURRENT". It is recommended, therefore, that this document not be specified for new designs. "NONCURRENT" refers to those documents which have previously been widely referenced and may continue to be required on some existing designs. To specify minimum requirements for non-magnetic gyroscopically stabilized direction indicators for use in aircraft, the operation of which may subject the instruments to the environmental conditions specified in Paragraph 3.3. This Aeronautical Standard covers two basic types as follows: Type I - Air Operated, Type II - Electrically Operated.

Direction Instrument, Non-Magnetic, Stabilized Type (Directional Gyro)

SAE AS405D-2012 燃料和石油量仪器

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. 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 AS5604A-2012 导航备用磁性指南针

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers the design requirements and all performance requirements for procurement of 1 7/8 inch dial pilot's standby compasses as specified herein.

Compass; Magnetic, Pilots Standby

SAE AS17983A-2012 飞行员备用磁性指南针

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

Compass, Magnetic, Pilots Standby

IEC TS 62647-1:2012 航空电子设备过程管理.含无铅锡焊的航空和防御电子系统.第1部分:无铅无操纵稳定性建议

Process management for avionics - Aerospace and defence electronic systems containing lead-free solder - Part 1: Preparation for a lead-free control plan

DIN EN 3706:2012 航空航天系列. 铝合金5086十字槽无头螺纹塞; 德文和英文版本EN 3706-2012

Aerospace series - Headless threaded plugs, cross recess, in aluminium alloy 5086; German and English version EN 3706:2012

IEC TS 62668-1:2012 过程管理 防伪 第1部分 避免使用假冒、欺诈和回收的电子元件

Process management - Counterfeit prevention - Part 1: Avoiding the use of counterfeit, fraudulent and recycled electronic components

SAE AS6254-2012 低频率水下定位装置最低性能标准(声音)(自供电)

This SAE Aerospace Standard (AS) covers ULDs utilized in finding submerged aircraft. Such ULDs are installed within the aircraft in a manner that they are unlikely to become separated during crash conditions. The low frequency ULD should be attached to the airframe in accordance with the manufacturer's recommendations in order to maximize the underwater detection range.

Minimum Performance Standard for Low Frequency Underwater Locating Devices (Acoustic) (Self-Powered)

SAE AS5659-2012 WDM LAN标准

This standard, consisting of five document, applies to designers, suppliers, and users of optical network services, systems, and components within mobile military and commercial aerospace platforms. The standard applies to any optical network which uses Wavelength Division Multiplexing in any optical media.

WDM LAN Standard

SAE AIR5026A-2011 试验室仪器

This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document; they will use many more channels of instrumentation, and in most cases will have requirements for measurements that are never made in post-overhaul testing, such as fan airflow measurements, or strain measurements on compressor blades. The specifications for each parameter to be measured, in terms of measurement range and measurement accuracy, are established by the engine manufacturers. Each test cell instrument system should meet or exceed those requirements. Furthermore, each instrument system should be recalibrated regularly, to ensure that it is still performing correctly.

Test Cell Instrumentation

SAE AIR1168/5A-2011 气动热力学试验仪器和测量

Like the technologies to which it contributes, the science of instrumentation seems to be expanding to unlimited proportions. In considering instrumentation techniques, primary emphasis was given in this section to the fundamentals of pressure, temperature, and flow measurement. Accent was placed on common measurement methods, such as manometers, thermocouples, and head meters, rather than on difficult and specialized techniques. Icing, humidity, velocity, and other special measurements were touched on briefly. Many of the references cited were survey articles or texts containing excellent bibliographies to assist a more detailed study where required.

Aerothermodynamic Test Instrumentation and Measurement

DIN EN 303214:2011 数据链接服务系统.统一的欧洲天空互用性规则EC 552/2004下应用的团体规范,地面组件和系统试验要求(英文版本EN 303214 V1.1.1的核准本

Data Link Services (DLS) System - Community Specification for application under the Single European Sky Interoperability Regulation EC 552/2004, Requirements for ground constituents and system testing (Endorsement of the English version EN 303214 V1.1.1 (

SAE AS8034B-2011 机载多用途电子显示屏的最低性能标准

This SAE Aerospace Standard (AS) specifies minimum performance standards for all types of Electronic Displays and Electronic Display Systems that are intended for use in the flight deck by the flightcrew in all 14 CFR Part 23, 25, 27, and 29 aircraft. The requirements and recommendations in this document are intended to apply to all installed electronic displays and electronic display systems within the flight deck, regardless of intended function, criticality, or location within the flight deck, but may also be used for non-installed electronic displays. This document provides baseline requirements and recommendations (see section 2.3 for definitions of "shall" and "should"). This document primarily addresses hardware requirements, such as electrical, mechanical, optical, and environmental. It does not address system specific functions. It does not contain an exhaustive or comprehensive list of requirements for specific systems or functions, such as TCAS, ADS-B, GPS, weather, or shared display considerations (e.g., when should alerts be inhibited on a display system that simultaneously depicts navigation data integrated with terrain data or traffic alerting). This document is intended to be used in combination with other guidance material contained in current system specific, TSOs, Advisory Circulars (ACs), and other Federal Aviation Administration (FAA)-approved guidance material.

Minimum Performance Standard for Airborne Multipurpose Electronic Displays