Standard
AIRCRAFT POSITION LIGHTS
1964-12-10
CURRENT
AS271A
This specification covers three types of aircraft position lights.
Search Results
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
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
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
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
Wing Inspection Lights - Design Criteria
2006-09-12
HISTORICAL
ARP4087B
This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and nacelles and the upper surfaces of the wing. The addition of ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit.
Standard
WING INSPECTION LIGHTS - DESIGN CRITERIA
1996-04-01
HISTORICAL
ARP4087A
This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and nacelles and the upper surfaces of the wing.
Standard
Wing Inspection Lights - Design Criteria
2023-02-06
CURRENT
ARP4087D
This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and engine nacelles and the upper surfaces of the wing. The addition of an ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit. It is not intended that this recommended practice require the use of any particular light source such as halogen, LED, or other specific design of lamp.
Standard
Wing Inspection Lights – Design Criteria
2018-10-10
HISTORICAL
ARP4087C
This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and engine nacelles and the upper surfaces of the wing. The addition of an ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit. It is not intended that this Recommended Practice require the use of any particular light source such as Halogen, LED or other specific design of lamp.
Standard
SOME FACTORS AFFECTING VISIBILITY OF AIRCRAFT NAVIGATION LIGHTS
1970-06-15
HISTORICAL
AIR1106
Standard
Position and Anticollision Lights - Fixed-Wing Aircraft
2017-11-09
CURRENT
ARP991C
This document covers the recommended lighting performance and design criteria for: a Left Forward Navigation Position Lights (Red) b Right Forward Navigation Position Lights (Green) c Rear Navigation Position Lights (White) d Anticollision Lights (1) Red Flashing Lights Top and Bottom Fuselage (2) White Flashing Strobe Lights Wing Tips and/or Tail (3) Red Flashing Beacon Light on Top of Vertical Tail
Standard
POSITION AND ANTI-COLLISION LIGHTS-TRANSPORT CATEGORY AIRPLANES
1983-05-01
HISTORICAL
ARP991A
This ARP covers the recommended lighting performance and design criteria for: (a) Left Forward Navigation Position Lights (Red) (b) Right Forward Navigation Position Lights (Green) (c) Rear Navigation Position (White) (d) Anti-Collision Lights (Red and/or White Flashing)
Standard
POSITION AND ANTICOLLISION LIGHTS - TURBINE POWERED FIXED-WING AIRCRAFT
2007-03-09
HISTORICAL
ARP991B
This document covers the recommended lighting performance and design criteria for: a Left Forward Navigation Position Lights (Red) b Right Forward Navigation Position Lights (Green) c Rear Navigation Position Lights (White) d Anticollision Lights (1) Red Flashing Lights Top and Bottom Fuselage (2) White Flashing Lights Wing Tips and/or Tail
Standard
Minimum Performance Standard for Aircraft Position Lights
2011-03-17
HISTORICAL
AS8037B
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. 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. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.
Standard
Minimum Performance Standard for Aircraft Position Lights
2013-07-09
HISTORICAL
AS8037C
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. 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. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.
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 Aircraft Position Lights
2001-08-01
HISTORICAL
AS8037A
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights for nighttime operation. It is intended to describe suitable means for compliance with current Federal Aviation Regulations defining minimum position light requirements. 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. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.
Standard
Minimum Performance Standard for Aircraft Position Lights
2022-02-02
CURRENT
AS8037D
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment position lights. This SAE Aerospace Standard (AS) defines minimum and maximum 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. It is not intended that this standard require the use of any particular light source such as quartz-halogen, incandescent, or any other specific design of lamp.
