AGL Component Library By Precision AGL Academy

Runway Guard Light

A critical safety lighting system that provides visual warning to pilots and vehicle operators approaching an active runway. Runway guard lights are a standalone ICAO Annex 14 / FAA-mandated fixture, flashing continuously whenever the associated lighting circuit is energised, and are independent of the Runway Status Light (RWSL) system — helping to prevent runway incursions and enhance airfield safety.

Runway Guard Light

Image disclaimer: For identification and illustration only. It may show a product by another manufacturer and may not depict the exact item described; it is not a statement of any product’s quality, approval or performance. Third-party image and trademark rights belong to their owners. See full notice.

Overview

What Is It?

A Runway Guard Light (RGL), commonly called a "wig-wag," is a visual warning system installed at runway holding positions to alert pilots and vehicle operators that they are approaching an active runway. Unlike the automated, occupancy-driven Runway Status Light (RWSL) system, an RGL is a standalone fixture that flashes continuously — typically alternating amber/yellow, either as a pair of elevated units either side of the taxiway (Configuration A) or a row of in-pavement units across the taxiway (Configuration B) — for as long as the associated circuit is switched on, independent of whether the runway is actually occupied. It serves as a constant, unmissable reminder of the holding position, not a dynamic go/no-go signal.

Purpose

Purpose & Function

The runway guard light exists as the last visual checkpoint before a pilot or vehicle operator physically crosses onto an active runway, placed precisely at the holding position where a moment's inattention has the most serious consequence. Its flashing amber pattern is deliberately distinct from steady-burning taxiway and runway lighting, drawing attention specifically because a flashing signal is harder to overlook than a static one, especially in a high-workload taxi phase where attention may be divided. Because the fixture flashes continuously rather than only in response to a detected conflict, its purpose is best understood as a constant, unambiguous marker of where the runway environment begins, reinforcing — rather than replacing — a pilot's own judgement and any ATC clearance to enter or cross. At airports where RWSL is also installed, RGL is a complementary but functionally separate layer, not a component driven by the same occupancy logic.

Application

Where Is It Used?

Installed at runway holding positions on taxiways, typically at the intersection where a taxiway meets the runway. Runway guard lights are used on:

  • Precision approach runways (CAT II and III) where enhanced safety is required
  • Busy airports with high traffic volumes where runway incursion risk is elevated
  • Runway crossings where taxiways intersect active runways
  • Intersecting runways where crossing traffic needs to be managed
Placement

Installation & Location

A pair of Runway Guard Light fixtures (the elevated "wig-wag" configuration) is installed on either side of the taxiway at the runway holding position, mounted on frangible stems set back from the pavement edge so the alternating flashing beams are visible to a pilot or vehicle operator approaching the holding point; where an in-pavement configuration is used instead, a row of flush units is set across the taxiway following the same layout as Runway Entrance Lights. Each fixture is fed by cable run in a trench or duct back to a control/flasher unit that drives the alternating flash pattern, typically switched on with the taxiway edge lighting circuit (for night or low-visibility operation, or continuously per local operating policy) rather than by any occupancy sensor. The control unit and any associated transformer are housed in an enclosure clear of the taxiway shoulder, with setting-out tied to the holding position marking so the fixtures sit at the same reference line as the hold line.

Function

How Does It Work?

Runway guard lights are typically powered from the series circuit via isolating transformers, with a dedicated flasher interface producing the alternating amber/yellow wig-wag pattern. Unlike RWSL fixtures, RGL activation is not driven by surveillance data or runway occupancy: the lights flash continuously at a fixed rate whenever the circuit is energised, on a schedule set by airport operating procedure (commonly linked to darkness/low-visibility operation, or run 24/7 at busier fields). This constant flashing is what makes the fixture effective as an always-present reminder of the holding position, rather than a conditional warning.

Architecture

System Architecture & Control Logic

Runway guard lights are wired onto the airfield's constant-current series circuit like other elevated and in-pavement AGL fixtures, each fed through its own isolating transformer, but their flash behaviour is not set by the CCR's brightness steps alone. A dedicated flasher/switching interface taps the same loop current and converts it into a rapid alternating (A/B) flash pattern between the two lamps of a Configuration A pair, or in sequence across the fixtures of a Configuration B row. The command to energise that interface comes from the ALCMS on a schedule tied to airport operating procedure — commonly switched with the taxiway lighting circuit for darkness or low-visibility operation, or left continuously on — and is entirely independent of any runway-occupancy surveillance system such as RWSL; on fields where RWSL is also present, the two operate side by side with no shared activation logic. Once energised, the fixture flashes continuously until the ALCMS commands it off. Fault supervision therefore centres on the flasher interface and the series circuit itself: a flasher stuck in one state, a lamp that fails to alternate in step, or a loss of series current is reported as an RGL fault requiring field follow-up.

ALCMS (On/Off Schedule) → Flasher / Switching Interface → Series Circuit → Isolating Transformer → Fixture Pair (alternating A/B)

ALCMS ON/OFF SCHEDULE Darkness / low-vis / continuous, per operating policy FLASHER / SWITCHING INTERFACE Converts ON command to continuous alternating flash SERIES CIRCUIT (LOOP) Same loop as other AGL fixtures; flasher overrides step ISOLATING TRANSFORMER (PER FIXTURE) Taps loop current to fixture secondary RGL FIXTURE PAIR Lamps A and B alternate out of phase, continuously ALCMS-SCHEDULED, NOT SURVEILLANCE-DRIVEN Flashes continuously for as long as ALCMS keeps it on Independent of RWSL or runway occupancy status CIRCUIT/FLASHER HEALTH Interface monitors series current and lamp alternation Loss of current or stuck flasher flags a fault for follow-up
System Logic

How the Continuous Flash Schedule Works

Schedule
ALCMS On/Off Command
Darkness, low-visibility ops, or continuous per airport policy
Decision
Is the RGL Circuit Commanded On?
Not linked to runway occupancy or RWSL
Circuit Energised
Flash
Guard Lights Flash Continuously
Amber/yellow, 45–50 fpm per lamp, alternating
Reminder
Marks the Holding Position
Pilot/vehicle operator still requires a clearance to proceed
Duration
Continues Until Scheduled Off
Not affected by aircraft or vehicle movements
Circuit De-Energised
Standby
Lights Remain Off
Per ALCMS schedule (e.g. daylight VMC at some fields)
Result
No Flash Warning Present
Other holding-position markings and ATC clearance still apply
Runway guard lights operate on a fixed schedule set by the ALCMS, not on a real-time read of runway occupancy — that distinction is precisely what separates them from RWSL. Once energised, the fixture simply flashes continuously until commanded off, which is why the series circuit and flasher interface (see Field Notes below) are the components that most affect whether the light does its job.
Construction

Physical Construction

The fixture is typically an inset (flush) unit seating into an L-868 base can recessed into the taxiway pavement at the runway-holding position, with the top surface load-rated for aircraft wheel loading; elevated (wig-wag) configurations instead mount two paired units on frangible fittings either side of the taxiway. The housing is a die-cast aluminium alloy body, anodised or powder-coated for corrosion resistance against de-icing fluid, fuel spillage, and UV exposure. The amber LED array sits under a high-strength polycarbonate or borosilicate glass lens, gasket-sealed to the housing with an O-ring to achieve an IP67/IP68 rating against water and dust ingress. Internal wiring terminates at L-823 primary connectors, which mate to the secondary leads of the isolating transformer housed in an adjacent base can, with a separate control link carrying the ALCMS on/off command to the flasher interface. Stainless-steel fasteners are used throughout, and the base can assembly includes a drainage provision to prevent water pooling around the transformer and cable entry points.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array (amber/yellow)
ColourAmber / Yellow (flashing)
Flash PatternFlashing, 45–50 flashes per minute per lamp (alternating)
IntensityControlled by CCR (typically 5-step)
Beam PatternOmnidirectional or uni-directional towards approaching traffic
Mounting TypeFlush-mounted (inset) in taxiway pavement
Load Capacity≈27,000 kg (59,400 lbs) wheel load — governing case: fully loaded A380-800 tyre, per FAA Engineering Brief 83A
Isolating Transformer45W / 65W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
IntegrationALCMS on/off scheduling; independent of RWSL
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries circuit, constant current (CCR fed)
Rated Series Current6.6A (5-step)
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, 5kV or 600V per circuit design
ConnectorL-823 primary connector, submersible-rated splice
Control LinkSeparate ALCMS on/off command cabling to the flasher interface, independent of the power series circuit
Insulation Resistance≥ 50 MΩ (megger test, cable-to-ground)
Earthing/GroundingFixture body and base can bonded to airfield earth grid
Fault ProtectionCCR-level ground fault and open-circuit detection, plus flasher stuck-state / lamp-alternation fault detection
Power SourceCCR output, regulated per ICAO/FAA intensity step schedule; flasher on/off state governed by ALCMS schedule, independent of RWSL
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity (100%)≥ 3,000 cd average (amber/yellow) per ICAO Annex 14 §5.3.23 / FAA AC 150/5345-46 (Type L-804)
Intensity Steps (5-step)100% / 30% / 10% / 3% / 1% of rated peak intensity
Flash Rate45–50 flashes per minute per lamp, alternating pair pattern
Vertical Beam SpreadMain beam 2°–15° above horizontal (peak ~3°–4°)
Horizontal Beam SpreadOmnidirectional (elevated type) or ± 5° to ± 7.5° uni-directional (inset type)
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures
Chromaticity (Amber/Yellow)Within ICAO/FAA amber-yellow boundary (CIE coordinates)
DirectionalityToward approaching/taxiing traffic at the hold point
Maintenance Factor≥ 50% of new-fixture intensity before replacement/cleaning is due
Test MethodMobile photometric van/goniophotometer or fixed test bench per fixture
Compliance

Applicable Standards

ICAO Annex 14

Runway guard light requirements and installation standards

FAA AC 150/5345-46

Specification for runway guard lights

IEC 61827

Electrical and photometric performance for AGL luminaires

FAA AC 150/5345-53

Airport Lighting Equipment Certification Program

Prerequisites

Installation Requirements

Base Can Excavation & Grade
Civil

Excavate and compact the sub-grade to design depth before setting the flush-mounted base can(s), holding the can top level and flush with the taxiway pavement surface to bear the rated wheel load.

Drainage Provision
Civil

Provide a weep hole or drainage path at the base can to prevent water pooling around the transformer and cable entry, consistent with the fixture's submersible IP rating.

Duct & Cable Route
Electrical

Lay the series circuit duct/cable route to design depth and separation from other services, routing feeds for both fixture heads together and avoiding sharp bends that could stress the L-823 connector.

L-823 Connector Termination
Electrical

Terminate and seal the primary connector per manufacturer procedure, keeping the splice fully submersible-rated before backfill or reinstatement of the base can.

Isolating Transformer Matching
Electrical

Confirm the isolating transformer wattage (45W/65W) and ratio match the fixture and the series circuit's rated current step before connection.

Dual-Head Spacing & Orientation
Mechanical

Set the paired wig-wag heads at the design spacing and orientation facing approaching traffic on the taxiway centreline, per the aiming diagram for the hold-short position.

ALCMS Interface Wiring
Electrical

Terminate the flasher/switching interface's ALCMS control cabling per the system architecture before commissioning tests begin.

Pre-Energisation Sign-off
Documentation

Record base can position, cable route, connector seal, and head spacing as-built before backfill, since these are not inspectable once the site is closed.

Verification

Testing & Commissioning

Insulation Resistance Test
Pre-Energisation

Megger-test the circuit before energisation, confirming insulation resistance clears the acceptable minimum ahead of backfill.

Loop Continuity & Resistance Test
Pre-Energisation

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

Wig-Wag Flash Pattern Verification
Energisation

Confirm the alternating flash sequence and rate between the two fixture heads matches spec once the unit is energised.

Photometric Intensity Test
Final Acceptance

Measure yellow beam intensity with a calibrated photometer against applicable thresholds before handover.

ALCMS Interface Verification
Energisation

Confirm the fixture correctly follows on/off commands from the ALCMS and begins/stops its continuous alternating flash pattern accordingly.

Fixture Alignment & Aim Verification
Final Acceptance

Confirm elevation and azimuth of both heads match the design aiming diagram so the hold-short cue is visible to approaching traffic.

Seal & Gasket Integrity Check
Pre-Energisation

Check gaskets and enclosure seals before the unit is trafficked and exposed to weather.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, flash-pattern, and photometric readings alongside as-built position in the commissioning dossier.

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify amber beam intensity against ICAO / FAA thresholds using a calibrated photometer; degraded output usually points to lens contamination or an aging LED array.

Lens Cleaning
Quarterly

Clear the lens of rubber deposits and surface film picked up from taxiing traffic so beam visibility to approaching aircraft and vehicles stays within spec.

Flash Pattern Verification
Semi-annual

Confirm the flash rate falls within the specified range and that both lens units flash in sync; an erratic pattern is often the first sign of a failing driver.

Seal & Gasket Inspection
Annual

Check top-cap O-rings and gaskets for cracking or compression set, and re-torque fasteners to spec to keep the flush-mounted fixture watertight under wheel loading.

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.

ALCMS Interface Check
Semi-annual

Verify the fixture switches on and off correctly on ALCMS schedule commands, since the flasher/switching interface is the single point that most affects whether the light does its job.

Cable & Connector Inspection
Annual

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

Housing & Pavement Inspection
Annual

Check the base can and surrounding pavement for settlement, cracking, or debris that could affect drainage or wheel-load rating.

Field Notes

Common Field Issues

Lens Contamination

Runway guard lights are exposed to rubber deposits, tyre debris, and de-icing fluids. Regular cleaning with approved solvents and soft brushes is required to maintain light output and visibility.

LED Driver Failure

LED drivers in runway guard lights can fail due to thermal stress or power surges. Regular inspection and replacement of faulty drivers is essential to maintain system reliability.

ALCMS Interface Fault

Runway guard lights rely on the ALCMS on/off command reaching the flasher interface. A wiring fault or interface failure can leave the lights stuck off when they are scheduled to be on, or stuck on when they should be off. Regular interface checks and prompt fault reporting are recommended.

Diagnostics

Troubleshooting Guide

Lights Fail to Flash When Runway Is Occupied
Likely Cause
Loss of the ALCMS on/off command reaching the flasher interface, or a flasher unit stuck in the off state despite a valid ON command.
Diagnostic Steps
Check the ALCMS interface status for this fixture group; verify the flasher/switching interface is receiving the ON command; confirm loop voltage is present at the transformer secondary with a manual test activation.
Corrective Action
Restore or re-route the ALCMS control cabling, or replace the flasher interface if it fails to respond to a manual activation test; log the fault to maintenance for follow-up.
One Lamp of a Wig-Wag Pair Dark or Out of Step
Likely Cause
Failed LED module or isolating transformer on the affected unit, or a flasher interface no longer alternating the A/B pattern correctly between the two fixtures.
Diagnostic Steps
Observe the pair through a full flash cycle to confirm which side is dark or mistimed; check series loop continuity through the affected fixture's transformer; verify the flasher output alternates cleanly between the A and B legs.
Corrective Action
Replace the failed LED module or transformer on the affected fixture; if both units are healthy but out of step, replace the flasher/switching interface.
Lights Remain Flashing After Runway Is Clear
Likely Cause
Flasher interface stuck in the on state, or the ALCMS command not being cleared/updated when the schedule calls for the circuit to be off.
Diagnostic Steps
Cross-check the ALCMS's current commanded state for this fixture group against the actual scheduled state; issue a manual extinguish command to the flasher interface and observe response; inspect the flasher for a hardware latch fault.
Corrective Action
Reset or replace the stuck flasher interface; if the ALCMS command itself is stale, escalate to ALCMS maintenance to clear or restart the affected control channel.
Erratic or Irregular Flash Rate
Likely Cause
Ageing or thermally stressed LED driver, or a marginal flasher interface no longer holding the specified 45–50 flashes-per-minute-per-lamp rate under load.
Diagnostic Steps
Time the flash rate against the specified range during an activation; check driver output and case temperature for signs of thermal stress; substitute a known-good flasher interface to isolate the fault.
Corrective Action
Replace the degraded LED driver or flasher interface, then re-verify the flash rate falls within the specified range before returning the fixture to service.
Reduced Conspicuity / Hazy Lens
Likely Cause
Rubber deposits, de-icing fluid residue, or fuel-spill film built up on the lens, or a hazed/eroded lens on an inset unit exposed to constant wheel traffic.
Diagnostic Steps
Visually inspect the lens for contamination or surface degradation during a scheduled activation check; run a photometric check if haze is suspected beyond surface contamination.
Corrective Action
Clean the lens with approved solvents and a soft brush; replace the lens or fixture if erosion or haze persists after cleaning and photometric output remains below threshold.
Series Circuit Fault Traced to Guard Light Position
Likely Cause
Moisture ingress at the base can or L-823 connectors has degraded insulation resistance, or pavement/subgrade settlement around an inset unit has damaged cabling.
Diagnostic Steps
Megger the circuit segment covering the guard light position; inspect the base can, gaskets, and connector seals for water ingress; check surrounding pavement for settlement or cracking that may have stressed the cable run.
Corrective Action
Dry out or replace the affected connector/transformer, renew seals, and confirm insulation resistance is restored; address pavement settlement to prevent recurrence before re-energising the circuit.
Reliability

Failure Modes & Root Causes

LED Driver Failure
High Severity
Root Cause
Thermal cycling stress inside the driver housing from repeated activation, a power surge transient, or an aging driver drifting off its regulated output as it nears end-of-life.
Effect
One or both lamps of the wig-wag pair go dark or flash at reduced intensity, weakening the fixture's conspicuity to approaching flight crews.
Detection Method
Scheduled activation check with a visual or photometric intensity comparison between the paired lamps, and driver case-temperature inspection during maintenance.
Flasher / Switching Interface Failure
High Severity
Root Cause
Relay or solid-state switching component wear from continuous duty cycling, a firmware fault, or a failed activation-command interpreter in the interface.
Effect
Fixture fails to flash on a valid ALCMS ON command, remains flashing after being commanded off, or the A/B wig-wag pattern loses its alternating sequence.
Detection Method
Manual activation test against the ALCMS command, flash-rate timing check, and inspection of the interface's fault/status indicators.
ALCMS Control Link Loss
High Severity
Root Cause
Control cable damage, a failed interface card, or an interrupted command feed between the ALCMS and the local flasher interface.
Effect
Guard light fails to switch on when scheduled, or continues flashing on a stale command after being scheduled off, reducing confidence in the fixture's state.
Detection Method
ALCMS interface status monitoring at the control system, and correlation of local fixture behaviour against the commanded schedule during a test activation.
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 that darkens the affected wig-wag unit or, if the open extends to the loop itself, takes down the entire circuit.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
Wig-Wag Synchronisation Drift
Medium Severity
Root Cause
Mismatched timing settings between the paired flasher outputs, or one unit's LED driver responding more slowly than its pair after partial degradation.
Effect
The two lamps of the pair flash out of the required alternating sequence, weakening the attention-getting wig-wag effect.
Detection Method
Visual timing observation through several flash cycles during an activation check, or channel comparison of the two flasher outputs for phase drift.
Lens Contamination / Optical Degradation
Low Severity
Root Cause
Rubber deposits, de-icing fluid residue, and fuel-spill film accumulating on the lens, compounded by UV exposure and abrasive erosion on inset units exposed to wheel traffic.
Effect
Reduced conspicuity and light output that can fall below the level needed for the fixture to be reliably seen from the cockpit.
Detection Method
Visual inspection during scheduled cleaning cycles, and a photometric intensity check where haze or erosion is suspected beyond surface contamination.
L-823 Connector / Base Can Moisture Ingress
Medium Severity
Root Cause
Improper seating or crimping during installation, gasket failure allowing groundwater ingress, or pavement/subgrade settlement around an inset unit stressing the cable run.
Effect
Intermittent operation, flickering, or a partial ground fault that degrades circuit insulation resistance across the guard light's series segment.
Detection Method
Insulation resistance (megger) testing of the circuit segment, and visual inspection of connectors and base can seals during maintenance.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

Runway guard lights sit on a constant-current series circuit that can carry several kV across the loop. De-energise and lock out the CCR, then verify zero energy at the fixture before opening a base can or handling connectors.

Surveillance Interlock Dependency
Operational

The alternating flash is switched by the ALCMS on a fixed operating schedule, not by any surveillance feed; any work on the fixture or control unit must be followed by a check confirming the flasher still correctly responds to the ALCMS on/off command before returning the system to service.

Holding Position Work Coordination
Operational

These fixtures act as the final visual barrier before entering the runway environment; work here requires ATC coordination and a NOTAM where lights will be dark, with the holding position clearly marked by other means in the interim.

Frangibility Where Elevated
Mechanical

Where the elevated "wig-wag" configuration is used, never substitute the frangible stem with a rigid fitting or over-torque it; it must still shear cleanly if struck by an aircraft or ground vehicle.

Insulation Test Before Re-Energisation
Electrical Safety

After any cable, connector, or transformer work, megger test the affected series loop before restoring power, since a residual fault at re-energisation can trip the CCR or darken the pair.

Restore to Compliant State
Compliance

Do not return the fixture to service with an unverified surveillance interlock; confirm the alternating flash pattern, activation logic, and photometric conformance before closing out and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Verify Command Timing, Not Just State
ALCMS Integration

A guard light that correctly alternates when commanded can still create confusion if the ALCMS-command-to-activation latency has drifted; benchmark end-to-end activation timing after any controller firmware update, not just a pass/fail flash check.

LED Alternation Can Outrun the Spec Envelope
Retrofit

LED drivers can switch faster than the incandescent lamps the alternating flash rate was originally tuned for, so a retrofit that hits the numeric flash-rate spec can still read as a distracting strobe to pilots; validate the retrofit against observed visual character, not the datasheet number alone.

Frangible Stem Fatigue in the Wig-Wag Configuration
Mechanical

The elevated wig-wag mounting puts continuous wind and jet-blast loading on the frangible stem that a flush-mounted fixture never sees. Treat these stems as a wear item on the overhaul cycle, since cumulative fatigue can lower the shear point well before any visible damage appears.

Nuisance Dark Pairs Often Trace to the Loop, Not the Fixture
Troubleshooting

When a guard light pair goes dark intermittently, the fixture itself is rarely the first thing to check; a slow-drifting series loop connection or an isolating transformer nearing end of life produces the same symptom and is far more common at holding-position locations with heavy vehicle traffic nearby.

Keep Pair Brightness Matched Across the Loop
Design

Where several guard light pairs share one CCR loop, uneven cable runs or a mix of lamp ages between pairs can make one holding position visibly dimmer than another even though each fixture individually tests in tolerance; balance loop impedance and lamp condition at the design and overhaul stage, not after a pilot report.

Base Can Seals Take the Brunt at Holding Positions
Durability

Holding positions collect standing water and de-icing fluid runoff more than most other AGL locations on the field. Specify base can and connector seals rated for that exposure and check gasket condition every overhaul rather than only when a fault is already reported.

Quick Answers

Frequently Asked Questions

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

Q1What is a Runway Guard Light?

A Runway Guard Light (RGL) , commonly called a "wig-wag," is a visual warning system installed at runway holding positions to alert pilots and vehicle operators that they are approaching an active runway.

Q2What is the purpose of a Runway Guard Light?

The runway guard light exists as the last visual checkpoint before a pilot or vehicle operator physically crosses onto an active runway, placed precisely at the holding position where a moment's inattention has the most serious consequence. Its flashing amber pattern is deliberately distinct from steady-burning taxiway and runway lighting, drawing attention specifically because a flashing signal is harder to overlook than a static one, especially in a high-workload taxi phase where attention may be divided.

Q3Where is a Runway Guard Light used and installed?

Installed at runway holding positions on taxiways, typically at the intersection where a taxiway meets the runway. Runway guard lights are used on: Precision approach runways (CAT II and III) where enhanced safety is required Busy airports with high traffic volumes where runway incursion risk is elevated Runway crossings where taxiways intersect active runways Intersecting runways where crossing traffic needs to be managed.

Q4How does a Runway Guard Light work?

Runway guard lights are typically powered from the series circuit via isolating transformers, with a dedicated flasher interface producing the alternating amber/yellow wig-wag pattern. Unlike RWSL fixtures, RGL activation is not driven by surveillance data or runway occupancy: the lights flash continuously at a fixed rate whenever the circuit is energised, on a schedule set by airport operating procedure (commonly linked to darkness/low-visibility operation, or run 24/7 at busier fields). This constant flashing is what makes the fixture effective as an always-present reminder of the holding position, rather than a conditional warning.

Q5What are the typical technical parameters of a Runway Guard Light?

Typical values are — Light Source: LED array (amber/yellow); Colour: Amber / Yellow (flashing); Flash Pattern: Flashing, 45–50 flashes per minute per lamp (alternating); Intensity: Controlled by CCR (typically 5-step); Beam Pattern: Omnidirectional or uni-directional towards approaching traffic; Mounting Type: Flush-mounted (inset) in taxiway pavement; Load Capacity: ≈27,000 kg (59,400 lbs) wheel load — governing case: fully loaded A380-800 tyre, per FAA Engineering Brief 83A; Isolating Transformer: 45W / 65W (6.6A series circuit); Protection Class: IP67 / IP68 (submersible); Integration: ALCMS on/off scheduling; independent of RWSL.

Q6What are the electrical requirements for a Runway Guard Light?

Typical requirements are — Circuit Type: Series circuit, constant current (CCR fed); Rated Series Current: 6.6A (5-step); 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, 5kV or 600V per circuit design; Connector: L-823 primary connector, submersible-rated splice; Control Link: Separate ALCMS on/off command cabling to the flasher interface, independent of the power series circuit; Insulation Resistance: ≥ 50 MΩ (megger test, cable-to-ground).

Q7What photometric requirements apply to a Runway Guard Light?

Typical requirements are — Main Beam Intensity (100%): ≥ 3,000 cd average (amber/yellow) per ICAO Annex 14 §5.3.23 / FAA AC 150/5345-46 (Type L-804); Intensity Steps (5-step): 100% / 30% / 10% / 3% / 1% of rated peak intensity; Flash Rate: 45–50 flashes per minute per lamp, alternating pair pattern; Vertical Beam Spread: Main beam 2°–15° above horizontal (peak ~3°–4°); Horizontal Beam Spread: Omnidirectional (elevated type) or ± 5° to ± 7.5° uni-directional (inset type); Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures; Chromaticity (Amber/Yellow): Within ICAO/FAA amber-yellow boundary (CIE coordinates).

Q8Which standards apply to a Runway Guard Light?

The main references are ICAO Annex 14 — Runway guard light requirements and installation standards; FAA AC 150/5345-46 — Specification for runway guard lights; IEC 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 Runway Guard Light be inspected and maintained?

Typical maintenance tasks and intervals are: Photometric Intensity Check (annual); Lens Cleaning (quarterly); Flash Pattern Verification (semi-annual); Seal & Gasket Inspection (annual); Insulation Resistance Test (annual); ALCMS Interface Check (semi-annual); Cable & Connector Inspection (annual); Housing & Pavement Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Runway Guard Light faults?

Common symptoms covered are: Lights Fail to Flash When Runway Is Occupied; One Lamp of a Wig-Wag Pair Dark or Out of Step; Lights Remain Flashing After Runway Is Clear; Erratic or Irregular Flash Rate; Reduced Conspicuity / Hazy Lens; Series Circuit Fault Traced to Guard Light Position. For example, for "Lights Fail to Flash When Runway Is Occupied": Likely Cause: Loss of the ALCMS on/off command reaching the flasher interface, or a flasher unit stuck in the off state despite a valid ON command. Diagnostic Steps: Check the ALCMS interface status for this fixture group; verify the flasher/switching interface is receiving the ON command; confirm loop voltage is present at the transformer secondary with a manual test activation. Corrective Action: Restore or re-route the ALCMS control cabling, or replace the flasher interface if it fails to respond to a manual activation test; log the fault to maintenance for follow-up.

Go Further

Go Beyond the Component. Understand the Complete AGL System.

You have explored the component. Now understand how it works within the complete Airfield Ground Lighting system.

Learn AGL from fundamentals to design, installation, testing, photometry, commissioning, maintenance and troubleshooting through structured technical training at Precision AGL Academy.

Build practical knowledge. Understand the circuit. Read the standards. Troubleshoot with confidence.

Your next step in AGL starts here.

The Learning Pathway
Learn Understand Design Test Maintain Document Apply Certify

Need expert guidance on runway guard light selection or installation?

Precision AGL Academy provides advice on ALCMS integration, placement, and field testing of runway guard light systems.