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

1988-10-01

HISTORICAL

ARP4087

This ARP is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and nacelles so that they may be visually inspected by the crew of the aircraft at night.

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

2004-02-05

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

2018-08-13

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

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

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

MINIMUM PERFORMANCE STANDARD FOR ANTICOLLISION LIGHT SYSTEMS

1978-01-01

HISTORICAL

AS8017

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

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

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

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

Aircraft Flashtube Anticollision Lighting Systems

2018-08-28

CURRENT

AIR1276B

This document covers red and white anticollision lights using flashtubes as the light source.

Standard

Aerial Refueling Lights - Design Criteria

2021-12-01

CURRENT

ARP694D

This SAE Aerospace Recommended Practice (ARP) is intended to cover all external lights on the tanker and fixed wing receiver airplanes used to accomplish aerial refueling. This ARP describes lights used for two basic types of aerial refueling: the probe and drogue, and the boom/receptacle method.