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Standard

LIGHTING, INTEGRAL, FOR AIRCRAFT INSTRUMENTS: CRITERIA FOR DESIGN OF RED LIGHTED INSTRUMENTS

1991-04-01
HISTORICAL
ARP582A
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

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

2001-06-01
HISTORICAL
ARP582B
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

ELECTROLUMINESCENCE, DESIGN CRITERIA AND RECOMMENDATIONS FOR USE IN AEROSPACE VEHICLE CREW STATION AREAS

1991-04-01
HISTORICAL
ARP922
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.
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