AGL Component Library By Precision AGL Academy

Stop Bar Light

A critical runway safety system that provides visual indications to pilots at runway holding positions. Stop bar lights are a row of red unidirectional lights installed across the taxiway at the runway holding position, indicating that it is unsafe to proceed onto the runway.

Stop Bar Light

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Overview

What Is It?

A Stop Bar Light is a critical runway safety system that provides visual indications to pilots at runway holding positions. Stop bar lights are a row of red unidirectional lights installed across the taxiway at the runway holding position, indicating that it is unsafe to proceed onto the runway. These lights are typically installed at Runway Holding Position Markings and are controlled by the Air Traffic Controller or ALCMS. When illuminated, they provide a clear visual barrier that pilots must not cross without clearance, preventing runway incursions and ensuring safety during ground movement operations.

Purpose

Purpose & Function

A stop bar light's purpose is to give a runway holding position a hard, unmistakable visual barrier rather than a passive marking a pilot might inadvertently cross while distracted or in poor visibility. Because it is switched on and off under direct air traffic control — separate from the general AGL circuit — it functions as a live, moment-to-moment instruction: illuminated means clearance has not been given, and extinguished, together with a controller instruction, is what actually authorises the aircraft to proceed.

This makes the stop bar one of the primary defences against runway incursions, which remain among the most serious categories of ground safety event because they place an aircraft on the runway without clearance while another may be landing or departing. The unidirectional red beam, unmissable even in low visibility, is specifically designed so a pilot cannot cross the holding position without consciously registering that the light is still on.

Application

Where Is It Used?

Stop bar lights are installed at runway holding positions on taxiways at the runway threshold. They are used on:

  • Precision approach runways (CAT II and III) where enhanced safety is required
  • Busy airports with high traffic volumes where incursion risk is elevated
  • Runway holding positions at the intersection of taxiways and runways
  • Low visibility operations where clear visual cues are essential
  • Military airfields requiring positive runway control
Placement

Installation & Location

Stop bar fixtures are set out in a row across the full taxiway width at the runway holding position, using the standard load-rated inset base can recessed into the pavement, spaced tightly enough that the bar reads as a continuous red line rather than discrete points. Because the stop bar is switched independently of the taxiway centreline lighting, each fixture (or the bar as a group) is wired on its own control cable back to the runway/taxiway intersection controller in addition to the series-circuit power feed, with the associated elevated stop bar light (where fitted) mounted just clear of the pavement edge on its own frangible pole. Setting-out is tied to the holding-position marking survey so the bar sits exactly on the marked stop line.

Function

How Does It Work?

Stop bar lights operate as an integral part of the runway safety system:

  • Power: Powered from the constant current series circuit via an isolating transformer (typically 45W – 65W).
  • Light Source: Utilizes red LED arrays or red-filtered halogen lamps. The red colour provides a clear stop indication.
  • Configuration: Installed as a row of lights across the taxiway at the holding position.
  • Control: Controlled by the ATC or ALCMS, with illumination indicating that the runway is occupied and it is unsafe to proceed.
  • Deactivation: When the runway is clear and safe to cross, the lights are deactivated, allowing the pilot to proceed.
Architecture

System Architecture & Control Logic

Unlike runway edge or approach lights, stop bars are usually wired so each holding position can be commanded independently rather than as one uniform loop, because the whole safety function depends on switching a single bar without disturbing any other. Each stop bar's isolating transformer draws from a constant current series circuit dedicated to that position (or a selectively-switched tap on a shared regulator), so the ALCMS or ATC console can illuminate one stop bar while leaving adjacent taxiway lighting unaffected. Control logic is interlocked with runway occupancy: the ALCMS (increasingly integrated with A-SMGCS / runway incursion monitoring) drives the bar to red whenever the associated runway is occupied or otherwise unsafe to enter, and releases it — often together with the adjacent lead-on centreline lights — only once the runway is confirmed clear and a positive ATC clearance is given. This interlock, holding the stop bar illuminated whenever its paired lead-on lights are dark and vice versa, is what prevents a pilot from ever seeing a "go" indication on both at once. Circuit continuity is monitored at the regulator; an open circuit or failed transformer is reported to the ALCMS as a stop-bar fault requiring urgent attention, since an unlit stop bar cannot indicate "hold" at all.

Function

Control & State Overview

CONSTANT CURRENT REGULATOR Series Circuit — 5-Step (2.8A – 6.6A) ISOLATING TRANSFORMER 45W – 65W STOP BAR LIGHT FIXTURE Row Across Taxiway — Runway Holding Position ATC / ALCMS CONTROL Sets State by Runway Occupancy ILLUMINATED (RED) Runway Occupied — Unsafe to Proceed Pilot Must Hold Short DEACTIVATED Runway Clear — Safe to Cross Pilot May Proceed
The two states are mutually exclusive outcomes of the same control decision, not a sequence — deliberately left unmerged.
Construction

Physical Construction

Stop bar lights are built as flush (inset) fixtures — FAA Type L-852S — set into an L-868 base can recessed into the taxiway pavement, with a load-rated top surface designed to carry repeated aircraft wheel loading without cracking or settling. The lens is a red-filtered or intrinsically red-emitting hardened glass or polycarbonate unit, gasket-sealed to the low-profile housing to achieve an IP67/IP68 rating against fuel spillage, de-icing fluid, and standing water at the holding position. Because a row of stop bar lights must switch on and off together as a single ATC-controlled circuit, each fixture in the row wires back through sealed L-823 connectors to its own isolating transformer within the base can, with the row grouped on a common series circuit or CCR channel so all lights illuminate and extinguish in unison. The fixture body is kept low and chamfered to minimise tyre scrubbing and rolling impact as aircraft cross the holding position, and internal components are mounted to resist the vibration and thermal cycling of continuous surface traffic. Stainless-steel fasteners and corrosion-resistant wiring are standard given the fixture's direct exposure to aircraft traffic at this safety-critical location.

Specification

Technical Parameters

ParameterTypical Value
Light SourceRed LED array or 45W – 65W halogen with red filter
ColourRed (uni-directional, towards approaching aircraft)
Luminous Intensity200 – 2,000 candela (depending on setting)
Intensity Steps5-step (2.8A – 6.6A) CCR controlled
ConfigurationRow of lights across taxiway at holding position
Beam PatternUni-directional (towards approaching aircraft)
Mounting TypeFlush-mounted (inset) in pavement
Load CapacityRated for in-pavement aircraft wheel loading per FAA AC 150/5345-42; base-can bolts torqued per FAA Engineering Brief 83A
Isolating Transformer45W – 65W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
Operating Temperature-40°C to +55°C
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries circuit, constant current (CCR fed), individually switchable via stop bar control unit for runway incursion prevention
Rated Series Current6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A)
IsolationVia dedicated isolating transformer (45W–65W), not directly connected to series loop
Transformer SecondaryMatched to fixture wattage; sized to series circuit rating
Cable TypeL-824 single-conductor, direct-burial rated, plus control cable to the stop bar switching unit where individually selectable
ConnectorL-823 primary connector, submersible-rated splice
Insulation Resistance≥ 50 MΩ (megger test, cable-to-ground)
Earthing/GroundingFixture body and inset base can bonded to airfield earth grid
Fault ProtectionCCR-level ground fault/open-circuit detection plus stop bar control unit fault indication
Power SourceCCR output via ALCMS-controlled stop bar switching, regulated per ICAO/FAA intensity step schedule
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity≥ 300 cd (red) minimum average, per FAA AC 150/5345-46 Type L-852S / ICAO Annex 14 stop bar light limits
Intensity Steps (5-step)100% / 30% / 10% / 3% / 1% of rated peak intensity
Vertical Beam SpreadMain beam 1°–10° above horizontal; 10% curve extends to 0.5°–13°
Horizontal Beam SpreadMain beam ± 24° either side of the taxiway centreline; 10% curve extends to ± 30°, uni-directional
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 stop bar light figures
Chromaticity (Red)Traffic-signal red per the ITE Vehicle Traffic Control Signal Heads (VTCSH) standard, within ICAO Annex 14 red boundary (CIE coordinates)
DirectionalityVisible to approaching aircraft at the holding position only
Activation BehaviourIlluminated (red) when the stop bar is selected on; extinguished when ALCMS releases the bar for crossing
Maintenance Factor≥ 50% of new-fixture intensity before replacement/cleaning is due
Intensity Tolerance± 25% of rated value at each CCR step (field measurement)
Test MethodMobile photometric van/goniophotometer or fixed test bench per fixture
Compliance

Applicable Standards

ICAO Annex 14

Stop bar light requirements and installation standards

FAA AC 150/5345-46

Specification for stop bar lights

IEC TS 61827

Electrical and photometric performance for AGL luminaires

FAA AC 150/5345-53

Airport Lighting Equipment Certification Program

Prerequisites

Installation Requirements

Recess Coring & Base Can Setting
Civil

Core or cast the recess and set each L-868 base can to the holding-position marking survey so the bar sits exactly on the marked stop line, with the top flush and load-rated for repeated wheel loading.

Full-Width Spacing
Civil

Space fixtures tightly enough across the full taxiway width that the bar reads as a continuous red line rather than discrete points when illuminated.

Independent Control Cable Run
Electrical

Lay a dedicated control cable back to the runway/taxiway intersection controller in addition to the series-circuit power feed, since the stop bar must switch independently of the adjacent taxiway centreline lighting.

L-823 Connector Termination
Electrical

Terminate and seal each fixture's connector to a submersible rating before backfill, given continuous exposure to fuel spillage, de-icing fluid, and standing water at the holding position.

Isolating Transformer Matching
Electrical

Confirm each fixture's isolating transformer matches the series circuit's rated current step, and that the full row is grouped on a common circuit or CCR channel so all lights illuminate and extinguish in unison.

Interlock Wiring Check
Electrical

Confirm the stop bar's control wiring is correctly interlocked with the associated lead-on centreline lights before energisation, so the two can never both show a "go" indication at once.

Wheel Load Rating Confirmation
Mechanical

Confirm the base can and fixture top surface are rated for the heaviest aircraft wheel loading expected, with the profile kept low and chamfered to minimise tyre scrubbing and rolling impact.

Pre-Energisation Sign-off
Documentation

Record base can position, cable route, connector seal, and interlock wiring as-built before backfill, since these are not inspectable once the pavement is reinstated.

Verification

Testing & Commissioning

Insulation Resistance Test
Pre-Energisation

Megger-test the isolating transformer and series loop before the circuit is energised, confirming insulation resistance clears the acceptable minimum.

Loop Continuity & Resistance Test
Pre-Energisation

Verify series loop continuity end to end and record total loop resistance, ruling out open circuits or high-resistance splices before first energisation.

Primary/Secondary Voltage Verification
Energisation

With the CCR energised, confirm secondary voltage at the L-823 connector matches the transformer's rated ratio at the commissioned current step.

Control System Communication Test
Energisation

Confirm the stop bar responds correctly to ATC/ALCMS on/off commands and reports its status back to the control system.

Photometric Intensity Test (Red)
Final Acceptance

Measure red beam intensity and colour with a calibrated photometer against ICAO/FAA thresholds before handover.

Flush-Fit & Load Ring Verification
Final Acceptance

Confirm the load ring is correctly seated and the fixture sits flush with the surrounding pavement before trafficking.

Pavement Surround & Sealant Check
Pre-Energisation

Confirm the pavement cutout and sealant application meet spec before the fixture is finally set.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, activation, and photometric readings in the commissioning dossier for handover.

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify red beam intensity and chromaticity against ICAO / FAA thresholds using a calibrated photometer; colour shift usually points to filter fade or LED aging.

Lens Cleaning
Quarterly

Clean rubber deposits, dust, and de-icing fluid residue from the lens so the stop bar's red cue stays clearly visible to flight crews and vehicle operators.

Control System Communication Test
Semi-annual

Verify communication between the stop bar and ATC / ALCMS, and confirm activation and deactivation timing, since a comms failure can leave the bar in the wrong state.

Seal & Load Ring Inspection
Annual

Check the inset fixture's seal and load-bearing ring for cracking or wear, since these units carry full aircraft wheel loads and must stay watertight.

Insulation Resistance Test
Annual

Megger-test the isolation transformer and series circuit to confirm insulation resistance stays above the minimum, flagging moisture ingress before it causes a series-circuit fault.

Cable & Connector Inspection
Annual

Examine primary and secondary cable connections for corrosion or loose crimps, a common source of intermittent series-circuit faults.

Pavement Surround Inspection
Annual

Check the pavement immediately around each fixture for spalling, cracking, or settlement that could affect drainage or create FOD risk on the holding point.

Field Notes

Common Field Issues

Red Filter/LED Degradation

Red light sources and filters are susceptible to UV degradation and thermal stress. Over time, output can decrease or colour can shift. Regular photometric testing and replacement is essential.

Lens Contamination

Stop bar lights are exposed to rubber deposits, dust, and de-icing fluids. Regular cleaning with approved solvents and soft brushes is required to maintain light output.

Control System Communication Failure

Stop bar lights rely on communication with the ATC or ALCMS. Network failures can cause the lights to fail to activate or deactivate at the correct time. Redundant communication paths are essential.

Diagnostics

Troubleshooting Guide

Single Fixture Dark, Rest of Bar Normal
Likely Cause
Failed LED module, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding) in the in-pavement fixture.
Diagnostic Steps
Confirm series loop continuity through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised.
Corrective Action
Replace the LED module if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before reinstating the can.
Entire Stop Bar Fails to Illuminate on Command
Likely Cause
Open-circuit fault in the series loop, or the ATC/ALCMS command signal is not reaching the CCR due to a communication or control-cable fault.
Diagnostic Steps
Check the CCR fault/open-circuit indication and its command-signal status first; loop-resistance test from the CCR output; verify the ATC/ALCMS control link and redundant path.
Corrective Action
Restore or repair the control communication link, or excavate and repair the faulted cable section; re-test before reinstating the circuit.
Stop Bar Fails to Extinguish or Remains Lit
Likely Cause
Command signal from ATC/ALCMS is not being received or acknowledged by the CCR, or a stuck contactor/relay in the control circuit.
Diagnostic Steps
Check the CCR's command status against the ATC/ALCMS log; test the extinguish command signal path; inspect control relays and contactors for sticking.
Corrective Action
Repair or replace the faulted relay/contactor, or restore the communication path, then confirm the bar responds correctly to both commands.
CCR Trips on Overcurrent or Ground Fault
Likely Cause
Moisture ingress at a fixture base can or connector has degraded insulation resistance, creating a short or partial ground fault on the series loop.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect fixtures for cracked lenses, condensation, or damaged secondary cable jackets.
Corrective Action
Dry out or replace the affected fixture/connector, renew O-rings and gaskets, and confirm insulation resistance is back above the acceptable minimum before re-energising.
Reduced or Discoloured Red Output
Likely Cause
Contaminated or eroded lens, or a red LED array/filter degraded by UV exposure and thermal stress.
Diagnostic Steps
Run a photometric and chromaticity check against ICAO/FAA thresholds; inspect and clean the lens of rubber deposits or de-icing fluid residue.
Corrective Action
Clean or replace the lens, replace a degraded LED module or filter, and re-verify with a follow-up photometric reading.
Fixture Cracked, Loose, or Sitting Proud of Pavement
Likely Cause
Repeated tyre loading has fatigued the housing or its retaining ring, or the surrounding pavement/subgrade has settled or heaved around the can.
Diagnostic Steps
Visually and physically check the fixture body, lens, and retaining ring for cracking or play; measure fixture height against the surrounding pavement surface.
Corrective Action
Replace the cracked housing or lens, re-seat and re-seal the fixture flush with the pavement, and address any base can or subgrade settlement to prevent recurrence.
Reliability

Failure Modes & Root Causes

LED Module Failure
High Severity
Root Cause
Solder-joint fatigue from thermal cycling, moisture ingress through a compromised board seal, or ordinary end-of-life lumen depreciation in the in-pavement fixture.
Effect
Single fixture goes dark or drops below minimum intensity while the rest of the bar continues to operate normally, weakening the red stop cue at that point.
Detection Method
Nighttime visual patrol, periodic photometric intensity survey, and continuity/secondary-voltage checks at the fixture connector.
Isolating Transformer Winding Failure
High Severity
Root Cause
Moisture ingress leading to insulation breakdown, a manufacturing defect in the winding, or a blown primary fuse-wire link from a transient surge.
Effect
Open-circuit point in the series loop; can darken the single fixture or, if the open extends to the loop itself, take down the entire stop bar.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
L-823 Connector / Splice Degradation
Medium Severity
Root Cause
Improper seating or crimping during installation, gasket failure allowing groundwater ingress, or corrosion building up on the pins over time.
Effect
Intermittent operation, flickering, or a partial ground fault that degrades circuit insulation resistance.
Detection Method
Insulation resistance (megger) testing of the circuit and visual inspection of connectors at the fixture base can during maintenance.
Series Cable Insulation Breakdown
High Severity
Root Cause
Cable jacket damage from nearby excavation or rodent activity, age-related insulation degradation, or prolonged standing water in the duct run.
Effect
Ground fault or short circuit that trips the CCR or darkens the entire series loop.
Detection Method
Full-circuit megger test to flag the low-resistance segment, followed by sectionalised testing or time-domain reflectometry to pinpoint the fault location.
ATC / ALCMS Command Link Fault
High Severity
Root Cause
Communication or control-cable fault between ATC/ALCMS and the CCR, or a lost or corrupted command signal.
Effect
The stop bar fails to illuminate on command or fails to extinguish when cleared, directly undermining a runway-incursion safeguard.
Detection Method
CCR command-status check against the ATC/ALCMS log, and verification of the control communication link and its redundant path.
Control Relay / Contactor Sticking
Medium Severity
Root Cause
Contact wear, contamination, or mechanical fatigue in the control relay or contactor that switches the stop bar on ATC command.
Effect
The bar remains lit after the extinguish command, or fails to respond to the illuminate command, creating a conflicting signal to flight crews.
Detection Method
Testing of the extinguish and illuminate command signal paths, and inspection of control relays and contactors for sticking.
Red Lens / Filter Degradation
Low Severity
Root Cause
Contaminated or eroded lens, or a red LED array/filter degraded by UV exposure and thermal stress.
Effect
Reduced or discoloured red output that can fall below ICAO/FAA chromaticity thresholds.
Detection Method
Photometric and chromaticity check against ICAO/FAA thresholds, and visual inspection and cleaning of the lens.
Flush Housing / Pavement Settlement
Medium Severity
Root Cause
Repeated tyre loading fatiguing the housing or retaining ring, or surrounding pavement/subgrade settling or heaving around the base can.
Effect
Fixture cracks, loosens, or sits proud of or below the pavement surface, creating an FOD and wheel-loading hazard at a safety-critical location.
Detection Method
Physical and visual check of the fixture body, lens, and retaining ring for cracking or play, and measurement of fixture height against the surrounding pavement.
Precautions

Safety & Operational Notes

Series & Control Circuit Isolation
Electrical Safety

Stop bar lights are switched independently of the taxiway centreline lighting; confirm both the series-circuit power feed and the separate control cable back to the intersection controller are isolated before opening a base can or handling connectors.

Incursion-Prevention Control — Do Not Bypass
Compliance

The stop bar is a primary runway-incursion barrier that pilots and vehicle operators must not cross while illuminated; never bypass, force to extinguished, or leave the bar in an ambiguous state during maintenance without ATC's explicit knowledge and sign-off.

Holding Position Work Coordination
Operational

Work at the runway holding position requires ATC coordination and a NOTAM where the bar will be dark or out of service, with the holding position clearly marked by other means in the interim.

Frangibility of the Elevated Unit
Mechanical

Where an elevated stop bar light is fitted alongside the inset bar, never substitute the frangible pole mounting with a rigid fitting or over-torque it; it must still shear cleanly if struck.

Insulation Test Before Re-Energisation
Electrical Safety

After any cable, connector, or transformer work, megger test the affected loop before restoring power, since a residual fault at re-energisation can trip the circuit or leave a gap in the bar.

Restore to Compliant State
Compliance

Do not return the bar to service with an unverified control response; confirm it illuminates and extinguishes correctly on command, reads as a continuous red line, and is photometrically conformant before closing out and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Circuit Priority Should Match Its Safety Role
Electrical

Stop bar lights sit on a life-safety circuit that prevents runway incursions; confirm they're on a protected, monitored circuit tier with priority equal to or higher than the runway lighting they protect, not a standard taxiway branch that could fail without immediate alerting.

Verify Interlock With ATC Selective Switching
Configuration

Where stop bars are selectively switched by ATC to control runway access, confirm the fixture-to-switch mapping after any taxiway renumbering or control system change; a stop bar wired to the wrong control point can extinguish when a controller believes a different one has been cleared.

A 'Stuck On' Fault Is as Serious as a Dark Fixture
Troubleshooting

A stop bar that fails to extinguish when ATC clears it for crossing is at least as operationally serious as one that fails to illuminate, since it can prompt pilots to disregard the indication entirely if it persists; treat stuck-on faults with the same urgency as a failed-dark report, not as a lower-priority nuisance.

Insulation Test Before Re-Energising
Electrical Safety

After any cable, connector, or transformer work on a stop bar circuit, megger test the affected loop before restoring power; a residual fault at re-energisation risks tripping the regulator and darkening the stop bar at the exact location where that failure matters most.

Frangibility Where Elevated Stop Bars Are Used
Mechanical

Where elevated stop bar fixtures are used instead of inset units, the frangible mount needs to shear cleanly under aircraft or vehicle impact just as with other elevated AGL fixtures; never substitute a rigid fitting or over-torque the mount even though the fixture sits at a taxiway holding position rather than the runway itself.

Confirm Unidirectional Aim Toward Approaching Traffic Only
Installation

Stop bar lights are unidirectional and must present red only to traffic approaching the holding position, not to traffic already on the runway or crossing from the other direction; verify aim and shielding after installation or realignment, since a light visible from the wrong direction can create confusing or contradictory indications.

Quick Answers

Frequently Asked Questions

Short answers about the Stop Bar Light: what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is a Stop Bar Light?

A Stop Bar Light is a critical runway safety system that provides visual indications to pilots at runway holding positions. Stop bar lights are a row of red unidirectional lights installed across the taxiway at the runway holding position, indicating that it is unsafe to proceed onto the runway. These lights are typically installed at Runway Holding Position Markings and are controlled by the Air Traffic Controller or ALCMS. When illuminated, they provide a clear visual barrier that pilots must not cross without clearance, preventing runway incursions and ensuring safety during ground movement operations.

Q2What is the purpose of a Stop Bar Light?

A stop bar light's purpose is to give a runway holding position a hard, unmistakable visual barrier rather than a passive marking a pilot might inadvertently cross while distracted or in poor visibility. Because it is switched on and off under direct air traffic control — separate from the general AGL circuit — it functions as a live, moment-to-moment instruction: illuminated means clearance has not been given, and extinguished, together with a controller instruction, is what actually authorises the aircraft to proceed.

Q3Where is a Stop Bar Light used and installed?

Stop bar lights are installed at runway holding positions on taxiways at the runway threshold. They are used on: Precision approach runways (CAT II and III) where enhanced safety is required Busy airports with high traffic volumes where incursion risk is elevated Runway holding positions at the intersection of taxiways and runways Low visibility operations where clear visual cues are essential Military airfields requiring positive runway control.

Q4How does a Stop Bar Light work?

Stop bar lights operate as an integral part of the runway safety system: Power: Powered from the constant current series circuit via an isolating transformer (typically 45W – 65W). Light Source: Utilizes red LED arrays or red-filtered halogen lamps. The red colour provides a clear stop indication. Configuration: Installed as a row of lights across the taxiway at the holding position. Control: Controlled by the ATC or ALCMS, with illumination indicating that the runway is occupied and it is unsafe to proceed.

Q5What are the typical technical parameters of a Stop Bar Light?

Typical values are — Light Source: Red LED array or 45W – 65W halogen with red filter; Colour: Red (uni-directional, towards approaching aircraft); Luminous Intensity: 200 – 2,000 candela (depending on setting); Intensity Steps: 5-step (2.8A – 6.6A) CCR controlled; Configuration: Row of lights across taxiway at holding position; Beam Pattern: Uni-directional (towards approaching aircraft); Mounting Type: Flush-mounted (inset) in pavement; Load Capacity: Rated for in-pavement aircraft wheel loading per FAA AC 150/5345-42; base-can bolts torqued per FAA Engineering Brief 83A; Isolating Transformer: 45W – 65W (6.6A series circuit).

Q6What are the electrical requirements for a Stop Bar Light?

Typical requirements are — Circuit Type: Series circuit, constant current (CCR fed), individually switchable via stop bar control unit for runway incursion prevention; Rated Series Current: 6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A); Isolation: Via dedicated isolating transformer (45W–65W), not directly connected to series loop; Transformer Secondary: Matched to fixture wattage; sized to series circuit rating; Cable Type: L-824 single-conductor, direct-burial rated, plus control cable to the stop bar switching unit where individually selectable; Connector: L-823 primary connector, submersible-rated splice.

Q7What photometric requirements apply to a Stop Bar Light?

Typical requirements are — Main Beam Intensity: ≥ 300 cd (red) minimum average, per FAA AC 150/5345-46 Type L-852S / ICAO Annex 14 stop bar light limits; Intensity Steps (5-step): 100% / 30% / 10% / 3% / 1% of rated peak intensity; Vertical Beam Spread: Main beam 1°–10° above horizontal; 10% curve extends to 0.5°–13°; Horizontal Beam Spread: Main beam ± 24° either side of the taxiway centreline; 10% curve extends to ± 30°, uni-directional; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 stop bar light figures.

Q8Which standards apply to a Stop Bar Light?

The main references are ICAO Annex 14 — Stop bar light requirements and installation standards; FAA AC 150/5345-46 — Specification for stop bar lights; IEC TS 61827 — Electrical and photometric performance for AGL luminaires; FAA AC 150/5345-53 — Airport Lighting Equipment Certification Program. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should a Stop Bar Light be inspected and maintained?

Typical maintenance tasks and intervals are: Photometric Intensity Check (annual); Lens Cleaning (quarterly); Control System Communication Test (semi-annual); Seal & Load Ring Inspection (annual); Insulation Resistance Test (annual); Cable & Connector Inspection (annual); Pavement Surround Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Stop Bar Light faults?

Common symptoms covered are: Single Fixture Dark, Rest of Bar Normal; Entire Stop Bar Fails to Illuminate on Command; Stop Bar Fails to Extinguish or Remains Lit; CCR Trips on Overcurrent or Ground Fault; Reduced or Discoloured Red Output; Fixture Cracked, Loose, or Sitting Proud of Pavement. For example, for "Single Fixture Dark, Rest of Bar Normal": Likely Cause: Failed LED module, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding) in the in-pavement fixture. Diagnostic Steps: Confirm series loop continuity through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised. Corrective Action: Replace the LED module if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before reinstating the can.

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