49.090 机上设备和仪器 标准查询与下载



共找到 1494 条与 机上设备和仪器 相关的标准,共 100

本标准规定了民用航空器机载飞行数据记录器主要参数记录要求和译码技术规范。 本标准适用于民用航空器飞行数据记录器参数的译码及其应用。

Flight data recorder parameret decoding specification

ICS
49.090
CCS
V45
发布
2004-01-09
实施
2004-05-01

This report identifies the reasons for, and results associated with, the conduct of a flight simulation research project evaluating the effect of low powered laser beam illumination of pilot crewmembers operating in the navigable airspace. This evaluation was primarily concerned with the possible degradation of pilot performance when illuminated by a laser while operating in an airport terminal area where pilot workloads are normally at their maximum. The purpose of the reported simulation evaluation was to validate guidelines established by the FAA for allowable laser exposures in navigable airspace.

Evaluation of Human Factor Considerations for Outdoor Laser Operations in the Navigable Airspace

ICS
49.090
CCS
V04
发布
2004-01-01
实施

The objective of this ARP is to provide a set of user-centered design guidelines for the implementation of data driven electronic aeronautical charts, which dynamically create charts from a database of individual elements. The data driven chart is intended to provide information required to navigate, but it is not intended to supplant the aircraft?s primary navigation display. These guidelines seek to provide a balance between standardization of equipment with similar intended functions and individual manufacturer innovation. This ARP provides guidelines for the display of an electronic chart that can replace existing paper. This document addresses what information is required, when it is required, and how it should be displayed and controlled. This document does not include all the detailed specifications required to generate an electronic aeronautical chart. This document primarily addresses the human factors aspects of electronic chart display, and does not address the software, hardware or system integrity/availability issues associated with certification of an electronic chart system. During the transition to data driven charts, the guidelines of this document should be applied to interim electronic chart products that may be pre-composed, such as vector or raster based electronic charts. This document is designed primarily for IFR Aeronautical Charts. There is a limited discussion of its applicability to VFR charts.

Electronic Display of Aeronautical Information (Charts)

ICS
49.090
CCS
V41
发布
2004
实施

Specification and test requirements for a single-axis Coriolis vibratory gyro (CVG) for use as a sensor in attitude control systems, angular displacement measuring systems, and angular rate measuring systems are defined. A standard specification format guide for the preparation of a single-axis CVG is provided.

Standard Specification Format Guide and Test Procedure for Coriolis Vibratory Gyros

ICS
49.090
CCS
V45
发布
2004
实施

This list has been prepared for use by or for the Government in the acquisition of products covered by Specification MIL-PRF-83287. Listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense

INDICATORS, FAULT LOCATING, GENERAL SPECIFICATION FOR

ICS
49.090
CCS
V45
发布
2004
实施

CEA-2006-A defines characteristics that, considered collectively, describe the performance of power amplifiers designed for use in mobile applications. Power amplifiers designed for use in mobile applications include, but are not limited to; separate single and multi-channel amplifiers, integrated amplifiers and bandwidth-limited amplifiers that are connected to and rely solely on the vehicle’s primary electrical system for power input and have output power ratings of greater than 5 watts when measured in accordance with CEA-2006-A.

Testing& Measurement Methods for Mobile Audio Amplifiers

ICS
49.090
CCS
L64
发布
2004
实施

This standard defines electrical and mechanical properties for a connector that will pass audio, video and associated metadata signals, control signals, and power between portable electronic devices and in-home and in-vehicle audio/video systems.

DTV 1394 Interface Specification

ICS
49.090
CCS
L65
发布
2004
实施

CEA-544-B defines the measurement procedures for the low frequency (5-54 MHz) immunity of tuners in a cable system, based on requirements in FCC regulations that define the assumed levels of the desired signal, low frequency interference and the required receiver immunity. These procedures define the specific tests needed to determine compliance with the requirements.

Low Frequency Immunity of Tuners in a Cable System

ICS
49.090
CCS
L65
发布
2004
实施

This standard was developed under the auspices of the Consumer Electronics Association (CEA) R4 Video Systems Committee.

Consumer Camcorder or Video Camera Low Light Performance

ICS
49.090
CCS
L64
发布
2003-09-01
实施

This standard was developed under the auspices of the Consumer Electronics Association (CEA, formerly CEMA) Technology & Standards R7.6 Digital Home Network Subcommittee.

Digital Entertainment Network

ICS
49.090
CCS
L64
发布
2003-07-01
实施

Aircraft-Magnetic indicators-Part 1:Characteristics

ICS
49.090
CCS
发布
2003-06-30
实施

Aircraft-Magnetic indicators-Part 2:Tests

ICS
49.090
CCS
发布
2003-06-30
实施

이 규격은 KS W ISO 5065-1(항공기-자기 지시기-제1부:특성)에 대한 시험

Aircraft-Magnetic indicators-Part 2:Tests

ICS
49.090
CCS
V20
发布
2003-06-30
实施
2003-06-30

Aircraft-Magnetic indicators-Part 2:Tests

ICS
49.090
CCS
发布
2003-06-30
实施

1.1 이 규격은 항공기에 사용되는 자기 지시기의 일반적인 작동 특성과 표준화 원리에

Aircraft-Magnetic indicators-Part 1:Characteristics

ICS
49.090
CCS
V20
发布
2003-06-30
实施
2003-06-30

Aircraft-Magnetic indicators-Part 1:Characteristics

ICS
49.090
CCS
发布
2003-06-30
实施

This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. This document is not intended to specify design methods, mechanisms or material to accomplish the requirements set forth.

(R) Aircraft On Board Weight and Balance System Requirements

ICS
49.090
CCS
V36
发布
2003-03-01
实施

The function of a multifunctional display (MFD) system is to provide the crew access to a variety of data, or combinations of data, used to fly the aircraft, to navigate, to communicate, and to manage aircraft systems. MFDs may also display primary flight information (PFI) as needed to insure continuity of operations. This document sets forth design and operational recommendations concerning the human factors considerations for MFD systems. The MFD system may contain one or more electronic display devices capable of presenting data in several possible formats. MFDs are designed to depict PFI, navigation, communication, aircraft state, aircraft system management, weather, traffic, and/or other information used by the flight crew for command and control of the aircraft. The information displayed may be combined to make an integrated display or one set of data may simply replace another. The information contained in this document can be applied to the design of all MFDs, including electronic flight bags (EFB), regardless of aircraft type. This document makes extensive use of lessons learned and information developed and currently in use by systems and airframe manufacturers through the evolutionary development of todays advanced systems. Some assumptions used in developing this document include: MFDs will incorporate a human-centered design using knowledge gained from previous work and research; This document is intended to apply to new systems or modifications to existing systems; Each function of a MFD is capable of providing accurate and timely information appropriate to the tasks of the flight crew for certain aircraft operations throughout all phases of flight; MFD systems will be based on the aeronautical English language, but other languages may have to be considered; MFD systems will meet international harmonized certification requirements; Use of the information in this document is subject to the certification requirements for a given airplane; The design process should include operator training considerations throughout its development; PFI will be available on the flight deck at all times.

Human Factor Considerations in the Design of Multifunction Display Systems for Civil Aircraft

ICS
49.090
CCS
V40
发布
2003-03-01
实施

Metal plain bush used for instrument (8281)

ICS
49.090
CCS
V35
发布
2003-02-24
实施
2003-02-24

Metal plain bush used for instrument (8280)

ICS
49.090
CCS
V35
发布
2003-02-24
实施
2003-02-24



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