Search Results

Standard

Design Criteria for White Incandescent Lighted Aerospace Instruments

2012-06-29

HISTORICAL

ARP798A

This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.

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Design, Layout, Criteria - Plastic Integrally Lighted Panels

2007-09-27

HISTORICAL

ARP498B

This document is intended to cover the design of plastic lighted panels, mounting plates, and their installation.

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Design, Layout, Criteria - Plastic Integrally Lighted Panels

2012-04-04

CURRENT

ARP498C

This document is intended to cover the design of plastic lighted panels, mounting plates, and their installation.

Standard

Color-Coded Incandescent Flange Base T-1 and T-1 3/4 Lamps for Voltage Identification

2020-03-12

CURRENT

AS4156C

This document specifies that black is the only color that can be used for the insulator at the bottom of the base of T-1 and T-1 ¾ Flanged Base lamps.

Standard

Design Criteria for White Incandescent Lighted Aerospace Instruments

2017-07-19

CURRENT

ARP798B

This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures recommended for use with white incandescent integrally lighted instruments. Its use should provide uniformity of illumination from instrument to instrument and legibility under daylight operation. An appendix is provided to familiarize the designer with some of the techniques used to obtain uniformity of color and illumination in various types of instruments.

Standard

Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays

2012-09-12

CURRENT

ARP1782B

This ARP describes methods for measuring the visual performance of direct view cathode ray tube displays used in aircraft flight decks and cockpits. Procedures may vary depending upon the type of display (for example, monochrome, color shadowmask, beam index, etc.), but all types are considered.

Standard

Photometric and Colorimetric Measurement Procedures for Airborne Direct View CRT Displays

2008-05-01

HISTORICAL

ARP1782A

This ARP describes methods for measuring the visual performance of direct view cathode ray tube displays used in aircraft flight decks and cockpits. Procedures may vary depending upon the type of display (for example, monochrome, color shadowmask, beam index, etc.), but all types are considered.

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LIGHT ASSEMBLY, COCKPIT, FIXED

2006-02-02

HISTORICAL

AS25027

Standard

LIGHT ASSEMBLY, COCKPIT, FIXED

2013-03-05

HISTORICAL

AS25027A

Standard

LIGHT ASSEMBLY, COCKPIT, FIXED

2018-06-29

CURRENT

AS25027B

Standard

Night Vision Goggle (NVG) Filters

2006-02-28

HISTORICAL

ARP4169A

This SAE Aerospace Recommended Practice (ARP) discusses the desired characteristics of night vision goggle (NVG) filters that can be used with incandescent, electroluminescent (EL) and light emitting diode (LED) light sources to achieve NVG compatible lighting of aerospace crew stations. This document also discusses the parameters that need to be considered when selecting a night vision goggle/daylight viewing (NVG/DV) filter for proper contrast enhancement to achieve readability in daylight. The recommendations set forth in this document are to aid in the design of NVG compatible lighting that will meet the requirements of MIL-L-85762A.

Standard

Night Vision Goggle (NVG) Filters

2014-02-27

CURRENT

ARP4169B

This SAE Aerospace Recommended Practice (ARP) discusses the desired characteristics of night vision goggle (NVG) filters that can be used with incandescent, electroluminescent (EL) and light emitting diode (LED) light sources to achieve NVG compatible lighting of aerospace crew stations. This document also discusses the parameters that need to be considered when selecting a night vision goggle/daylight viewing (NVG/DV) filter for proper contrast enhancement to achieve readability in daylight. The recommendations set forth in this document are to aid in the design of NVG compatible lighting that will meet the requirements of MIL-L-85762A and MIL-STD-3009.

Standard

Night Vision Goggle (NVG) Filters

2021-03-18

WIP

ARP4169C

This SAE Aerospace Recommended Practice (ARP) discusses the desired characteristics of night vision goggle (NVG) filters that can be used with incandescent, electroluminescent (EL) and light emitting diode (LED) light sources to achieve NVG compatible lighting of aerospace crew stations. This document also discusses the parameters that need to be considered when selecting a night vision goggle/daylight viewing (NVG/DV) filter for proper contrast enhancement to achieve readability in daylight. The recommendations set forth in this document are to aid in the design of NVG compatible lighting that will meet the requirements of MIL-L-85762A and MIL-STD-3009.

Standard

Lights, Instrument, Individual, General Specification For

2010-01-08

HISTORICAL

AS50571A

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.

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Lights, Instrument, Individual, General Specification For

2016-03-16

CURRENT

AS50571B

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.

Standard

Lighting, Integral, For Aircraft Instruments: Criteria for Design of Red Incandescent Lighted Instruments

2006-08-23

HISTORICAL

ARP582C

This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures for illuminating systems for integrally lighted aircraft instruments in order to provide (a) uniformity of illumination within each instrument, (b) legibility of instrument presentation under daylight or integral light, and (c) uniformity of illumination between instrument displays.

Standard

Lighting, Integral, For Aircraft Instruments: Criteria for Design of Red Incandescent Lighted Instruments

2012-04-04

CURRENT

ARP582D

This SAE Aerospace Recommended Practice (ARP) covers the general requirements and test procedures for illuminating systems for integrally lighted aircraft instruments in order to provide (a) uniformity of illumination within each instrument, (b) legibility of instrument presentation under daylight or integral light, and (c) uniformity of illumination between instrument displays.

Standard

Lighting, Integral, for Aircraft Instruments; Criteria for Design

1961-08-15

HISTORICAL

ARP582

This ARP covers the general requirements and test procedures for illuminating systems for integrally lighted aircraft instruments in order to provide (a) uniformity of illumination within each instrument, (b) legibility of instrument presentation under daylight or integral light, and (c) uniformity of illumination between instrument displays.

Standard

Electroluminescence, Design Criteria and Recommendations for Use in Aerospace Vehicle Crew Station Areas

2006-10-26

HISTORICAL

ARP922A

The scope of this ARP is to provide general requirements for application of electroluminescence to Aerospace Vehicle Crew Station Area instruments and control panels. The design brightness and color recommendations stated in this ARP are intended to apply where a crew station has multiple usage of electroluminescence in both instruments and control panels and when different manufacturers may be involved. These recommendations may also be helpful for the design of individually used displays incorporating electroluminescence, however, this light source has extensive design versatility through variance of manufacturing and operating parameters and the numerous acceptable design recommendations will not be stated herein. Electroluminescence will herein be referred to as EL.

Standard

Electroluminescence, Design Criteria and Recommendations for Use in Aerospace Vehicle Crew Station Areas

2012-02-09

CURRENT

ARP922B

The scope of this ARP is to provide general requirements for application of electroluminescence to Aerospace Vehicle Crew Station Area instruments and control panels. The design brightness and color recommendations stated in this ARP are intended to apply where a crew station has multiple usage of electroluminescence in both instruments and control panels and when different manufacturers may be involved. These recommendations may also be helpful for the design of individually used displays incorporating electroluminescence, however, this light source has extensive design versatility through variance of manufacturing and operating parameters and the numerous acceptable design recommendations will not be stated herein. Electroluminescence will herein be referred to as EL.