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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

LANDING AND TAXIING LIGHTS - DESIGN CRITERIA FOR INSTALLATION
1991-01-30
HISTORICAL
ARP693B
This SAE Recommended Practice includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a Single engine personal and/or liaison type b Light twin engine c Large multiengine propeller d Large multiengine turbojet e Military high performance fighter and attack f Helicopter
Standard

LANDING AND TAXIING LIGHTS- DESIGN CRITERIA FOR INSTALLATION
1961-06-01
HISTORICAL
ARP693
This ARP includes requirements for installations of adequate landing and taxiing lighting systems of aircraft of the following categories: 1 Single engine personal and/or liaison type. 2 Light twin engine. 3 Large multi-engine propeller. 4 Large multi-engine turbo-jet. 5 Military high performance fighter and attack. 6 Helicopter.
Standard

Landing and Taxiing Lights - Design Criteria for Installation
2006-06-28
HISTORICAL
ARP693C
This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a Single engine personal and/or liaison type b Light twin engine c Large multiengine propeller d Large multiengine turbojet e Military high performance fighter and attack f Helicopter
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 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

LED Landing, Taxiing, Runway Turnoff, and Recognition Lights
2022-09-23
HISTORICAL
ARP6402A
This document includes recommendations of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a Single engine personal and/or liaison type b Light twin engine c Large multiengine propeller d Large multiengine turbojet e Military high performance fighter and attack f Helicopter which are subject to the following CFR Parts certification: Part 23 – Airworthiness Standards: Normal, Utility, Acrobatic and Commuter Aircrafts Part 25 – Airworthiness Standards: Transport Category Aircrafts Part 27 – Airworthiness Standards: Normal Category Rotorcraft Part 29 – Airworthiness Standards: Transport Category Rotorcraft
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
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.
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