Search Results

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

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

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

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 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 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

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

Minimum Performance Standard for Anticollision Light Systems

2004-01-30

HISTORICAL

AS8017B

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

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

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

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.

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 Strobe Anticollision Lights

2007-07-09

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 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

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

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.