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Standard

Wing Inspection Lights – Design Criteria

2011-11-16
CURRENT
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

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

Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights

1991-02-27
HISTORICAL
AIR1106A
The scope of this Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a better technical understanding of such factors, and to aid in exercising appropriate judgement in the many possible flight eventualities.
Standard

Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights

2014-05-29
CURRENT
AIR1106B
The scope of this SAE Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a better technical understanding of such factors, and to aid in exercising appropriate judgment in the many possible flight eventualities.
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 ANTICOLLISION LIGHTS - TURBINE POWERED FIXED-WING AIRCRAFT

1996-04-01
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

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 ANTI-COLLISION LIGHTS - SST

1967-10-31
HISTORICAL
ARP991
This ARP covers the recommended lighting performance and design criteria for: (a) Left Forward Position Lights (Red) (b) Right Forward Position Lights (Green) (c) Rear Position Lights (White) (d) Anti-Collision Lights (Red or White Flashing)
Standard

Minimum Performance Standard for Anticollision Light Systems

2011-06-20
HISTORICAL
AS8017C
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment anticollision light systems. This Aerospace Standard defines 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. It is not intended that this standard require the use of any particular light source such as Xenon, LED or any other specific design of lamp.
Standard

Minimum Performance Standard for Anticollision Light Systems

2017-08-24
CURRENT
AS8017D
This SAE Aerospace Standard (AS) establishes minimum performance standards for new equipment anticollision light systems. This Aerospace Standard defines 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. It is not intended that this standard require the use of any particular light source such as Xenon, LED or any other specific design of lamp.
Standard

Minimum Performance Standard for Aircraft Position Lights

1986-01-01
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

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

2001-08-01
HISTORICAL
AS8037A
This Aerospace Standard (AS) establishes minimum performance standards for 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

2018-03-29
WIP
AS8037D
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

Measurement Procedures for Strobe Anticollision Lights

1998-12-01
HISTORICAL
ARP5029
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.
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.
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.
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