Search Results

Standard

Landing and Taxiing Lights - Design Criteria for Installation

2012-03-01

HISTORICAL

ARP693D

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

LED Landing, Taxiing, Runway Turnoff, and Recognition Lights

2011-06-21

HISTORICAL

ARP6402

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

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

Colors, Aeronautical Lights and Lighting Equipment, General Requirements For

2010-01-06

HISTORICAL

AS25050A

This specification covers the chromaticity and transmission requirements of equipment light transmitting ware in the descending order of transmission. It is intended for use in military aircraft lighting.

Standard

AIRCRAFT FLASHTUBE ANTICOLLISION LIGHTING SYSTEMS

2007-07-09

HISTORICAL

AIR1276A

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

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

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

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

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

High Intensity Discharge Light Sources

2006-02-17

HISTORICAL

ARP5647

This SAE Aerospace Recommend Practice (ARP) is intended to recommend safety related best practices when using metal halides high intensity discharge (HID) lamps and power supplies in aircraft applications.

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 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

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

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

Position Light Flashers: Single-Circuit (Personal Aircraft Types)

2002-12-16

CURRENT

AS273

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

Aircraft Anti-Collision Lights

1998-08-01

CURRENT

AS827

The purpose of this standard is to specify minimum requirements for aircraft anti-collision lights. This standard covers two types of aircraft anti-collision lights.

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

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

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