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Tests and Testing Manufacturing Nanotechnology Research and development A-20B Exterior Lighting Committee

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Standard

Design Requirements and Test Procedures for Dual Mode Exterior Lights
2023-02-20
CURRENT
ARP5825B
This SAE Aerospace Recommended Practice (ARP) contains the general requirements and test procedures for Dual Mode (NVIS Friendly visible and Covert) exterior lighting for most rotorcraft and fixed wing aircraft and could be applicable to ground vehicles that desire a Dual Mode lighting system.
Standard

Design Requirements and Test Procedures for Dual Mode Exterior Lights
2005-07-13
HISTORICAL
ARP5825
This SAE Aerospace Recommended Practice (ARP) contains the general requirements and test procedures for Dual Mode (NVIS Friendly visible and Covert) exterior lighting for most rotorcraft and fixed wing aircraft and could be applicable to ground vehicles that desire a Dual Mode lighting system.
Standard

Design Requirements and Test Procedures for Dual Mode Exterior Lights
2016-05-06
HISTORICAL
ARP5825A
This SAE Aerospace Recommended Practice (ARP) contains the general requirements and test procedures for Dual Mode (NVIS Friendly visible and Covert) exterior lighting for most rotorcraft and fixed wing aircraft and could be applicable to ground vehicles that desire a Dual Mode lighting system.
Standard

Design and Maintenance Considerations For Aircraft Exterior Lighting Plastic Lenses
2005-03-08
HISTORICAL
ARP5637
The information in this document is intented to apply to commercial jet transport category airplanes that incorporate plastic (polycarbonate or acrylic) lenses on exterior light assemblies, or are being considered for such an application. Exterior lighting applications include position light assemblies, anticollision light asemblies, and landing light assemblies. However, much of the material provided herein is general in nature and is directly applicable to many aircraft categories including, but not limited to, helicopters, general aviation aircraft, and military aircraft.
Standard

Design and Maintenance Considerations for Aircraft Exterior Lighting Plastic Lenses
2017-09-13
CURRENT
ARP5637A
The information in this document is intended to apply to commercial jet transport category airplanes that incorporate plastic (polycarbonate or acrylic) lenses on exterior light assemblies, or are being considered for such an application as opposed to glass lens designs. Exterior lighting applications include position light assemblies, anticollision light asemblies, and landing light assemblies. However, much of the material provided herein is general in nature and is directly applicable to many aircraft categories including, but not limited to, helicopters, general aviation aircraft, and military aircraft.
Standard

High Intensity Discharge Light Sources
2006-02-17
HISTORICAL
ARP5647
This SAE Aerospace Recommend Practice (ARP) is intended to recommend safety related best practices when using metal halides high intensity discharge (HID) lamps and power supplies in aircraft applications.
Standard

High Intensity Discharge Light Sources
2020-08-10
CURRENT
ARP5647B
This SAE Aerospace Recommend Practice (ARP) is intended to identify both safety related best practices and unique design considerations of metal halides High Intensity Discharge (HID) lamps and power supplies in aircraft applications.
Standard

High Intensity Discharge Light Sources
2014-04-03
HISTORICAL
ARP5647A
This SAE Aerospace Recommend Practice (ARP) is intended to identify both safety related best practices and unique design considerations of metal halides High Intensity Discharge (HID) lamps and power supplies in aircraft applications.
Standard

Lighting Applications for Unmanned Aircraft Systems (UAS)
2019-12-05
CURRENT
ARP6336
This SAE Aerospace Recommended Practice (ARP) provides technical recommendations for the lighting applications for Unmanned Aircraft Systems (UAS). The technical content of this ARP discusses the unique trade-offs that are necessary to maintain commonality to the U.S. Federal Aviation Regulations (FARs)1 for aerospace lighting. The recommendations set forth in this document are to aid in the design of Unmanned Aircraft (UA) lighting for the size of aircraft and operation for which the aircraft is intended. In addition, certain concepts of operation for which UASs are suited will require unique lighting solutions.
Standard

MINIMUM PERFORMANCE STANDARD FOR AIRCRAFT POSITION LIGHTS
1991-04-01
HISTORICAL
AS8037
This Aerospace Standard defines minimum light intensity in terms of candelas in vertical and horizontal-directions about the longitudinal, vertical and lateral axes of the aircraft. It also defines color tolerances in terms of limiting chromaticities for the light emitted from the position lights.
Standard

MINIMUM PERFORMANCE STANDARD FOR ANTICOLLISION LIGHT SYSTEMS
1991-04-20
HISTORICAL
AS8017A
This Aerospace Standard will define minimum light intensity in terms of "effective intensity" as defined in paragraph 3.5 of this standard and specified vertical and horizontal directions about the longitudinal and vertical axis of the airplane. It will also define flash rate and color for the anticollision light system.
Standard

Measurement Procedures for Short Pulse Width Strobe Anticollision Lights
2019-07-30
CURRENT
ARP5029B
This SAE Aerospace Recommended Practice (ARP) provides the user with standardized guidelines for the measurement of effective intensity of short pulse width strobe anticollision lights for aircraft in the laboratory, in maintenance facilities, and in the field. A common source of traceability for calibration of the measurement systems, compensation for known causes of variation in light output such as the use of colored lenses, and recommendations which minimize sources of errors and uncertainties are included in this document. Estimates of uncertainty and error sources for each class of measurement are discussed.
Standard

Measurement Procedures for Strobe Anticollision Lights
2014-01-07
HISTORICAL
ARP5029A
This SAE Aerospace Recommended Practice (ARP) provides the user with standardized guidelines for the measurement of effective intensity of strobe anticollision lights for aircraft in the laboratory, in maintenance facilities, and in the field. A common source of traceability for calibration of the measurement systems, compensation for known causes of variation in light output, and recommendations which minimize sources of errors and uncertainties are included in this document. Estimates of uncertainty and error sources for each class of measurement are discussed.
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