Your Selections

Aircraft instruments
Show Only

Collections

File Formats

Content Types

Dates

Sectors

Topics

Authors

Publishers

Affiliations

Committees

Events

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

TACHOMETER DRIVE - TYPE 1

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS54A
  • Current
Published 2019-02-18 by SAE International in United States
No Abstract Available.
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Aircraft On Board Weight and Balance System Requirements

AGE-2 Air Cargo
  • Aerospace Standard
  • ARP1409C
  • Current
Published 2018-10-18 by SAE International in United States
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.
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Operating Instructions for Aircraft Engines (Preparation of)

E-25 General Standards for Aerospace and Propulsion Systems
  • Aerospace Standard
  • AS177C
  • Current
Published 2018-09-11 by SAE International in United States
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Colors, Aeronautical Lights and Lighting Equipment, General Requirements For

A-20B Exterior Lighting Committee
  • Aerospace Standard
  • AS25050B
  • Current
Published 2017-03-07 by SAE International in United States
This specification covers the chromaticity and transmission requirements of aircraft lighting and light transmitting ware in descending order of transmission. It is intended for use in aviation lighting.
This content contains downloadable datasets
Annotation ability available

System and Method for Generating a Frequency-Modulated Linear Laser Waveform

  • Magazine Article
  • TBMG-26354
Published 2017-02-01 by Tech Briefs Media Group in United States

NASA's Langley Research Center has made a breakthrough improvement in laser frequency modulation. Frequency modulation technology has been used for surface mapping and measurement in sonar, radar, and time-of-flight laser technologies for decades. Although adequate, the accuracy of distance measurements made by these technologies can be improved by using a high-frequency triangular-waveform laser instead of a sine waveform or lower-frequency radio or microwaves. This new system generates a triangular modulation waveform with improved linearity that makes possible precision laser radar (light detection and ranging [lidar]) for a variety of applications.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Instrument and Cockpit Illumination for General Aviation Aircraft

A-20A Crew Station Lighting
  • Aerospace Standard
  • ARP1048B
  • Current
Published 2016-11-15 by SAE International in United States
This document establishes acceptable design criteria for instrument and cockpit illumination for general aviation aircraft.
This content contains downloadable datasets
Annotation ability available

System and Method for Generating a Frequency-Modulated Linear Laser Waveform

  • Magazine Article
  • TBMG-25725
Published 2016-11-01 by Tech Briefs Media Group in United States

NASA’s Langley Research Center has made a breakthrough improvement in laser frequency modulation. Frequency modulation technology has been used for surface mapping and measurement in sonar, radar, and time-of-flight laser technologies for decades. Although adequate, the accuracy of distance measurements made by these technologies can be improved by using a high-frequency triangular-waveform laser instead of a sine waveform or lower-frequency radio or microwaves. This new system generates a triangular modulation waveform with improved linearity that makes possible precision laser radar [light detection and ranging (lidar)] for a variety of applications.

   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Lights, Instrument, Individual, General Specification For

A-20A Crew Station Lighting
  • Aerospace Standard
  • AS50571B
  • Current
Published 2016-03-16 by SAE International in United States
This specification covers the general requirements for red and white individual instrument lights. This document has been streamlined. Appendix A to MIL-L-5057F lists those documents required for MIL-L-5057F acquisition and is a mandatory part of MIL-L-5057F. Those documents listed in Appendix A have the same status as those referenced directly in MIL-L-5057F (first tier documents). All other documents, referenced through tiering, may be used as guidance and information to supplement MIL-L-5057F. This document’s scope is limited to lamp source designs solely. Furthermore, the use of red lighting should not be considered for new design and included within this document to support requirements for existing military aircraft that still operate with this system of lighting.
This content contains downloadable datasets
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

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

A-4 Underwater Locator Device Working Group
  • Aerospace Standard
  • AS6254A
  • Current
Published 2015-12-06 by SAE International in United States
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. ARINC Standard 677 also provides installation guidance for Low Frequency ULDs.
Annotation ability available
   This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Minimum Performance Standard for Pitot and Pitot-Static Probes

A-4 Air Data Working Group
  • Aerospace Standard
  • AS8006A
  • Current
Published 2015-08-08 by SAE International in United States
This SAE Aerospace Standard (AS) covers the following basic types: Type I - Pitot pressure, straight and L-shaped, electrically heated. Type II - Pitot and static pressures, straight and L-shaped, electrically heated.
This content contains downloadable datasets
Annotation ability available