AGL Component Library By Precision AGL Academy

Take-Off Hold Light (THL)

A critical runway safety lighting system that provides visual indications to pilots awaiting take-off clearance. THL systems are an integral component of the Runway Status Light (RWSL) system, displaying red lights on the runway to indicate when it is unsafe to begin a take-off roll.

Take-Off Hold Light (THL)

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Overview

What Is It?

A Take-Off Hold Light (THL) is a runway safety lighting system that provides visual indications to pilots at the runway holding position. The THL system consists of a double row of red lights embedded in the runway surface at the take-off/"line up and wait" position, beginning approximately 114 m (375 ft) beyond the runway threshold and extending roughly 457 m (1,500 ft) down the runway. When illuminated, these lights indicate to the pilot that it is unsafe to commence the take-off roll due to runway occupancy by another aircraft or vehicle. The THL system is part of the Runway Status Light (RWSL) system and is designed to prevent runway incursions and collisions during take-off operations.

Purpose

Purpose & Function

The THL exists to give a pilot lined up for takeoff a direct, independent confirmation that the runway ahead is actually clear, rather than relying solely on an air traffic control clearance that could be based on incomplete information or delivered just before a conflicting aircraft or vehicle enters the runway. Because the lights are embedded in the pavement directly in the pilot's line of sight at the takeoff position, illuminated red lights communicate "do not begin the roll" in a way that requires no radio call and no interpretation, closing the reaction-time gap between a developing runway conflict and the pilot's decision to hold. This makes the THL a direct layer of incursion protection specifically at the highest-consequence moment of ground operations: the instant before a departing aircraft commits to its takeoff roll.

Application

Where Is It Used?

THL systems are deployed as part of the FAA's Runway Status Light (RWSL) program at a defined set of high-traffic, towered airports selected on the basis of operations volume and runway incursion history, rather than any single runway's instrument approach category. They are used in conjunction with runway entrance lights, runway intersection lights, and runway guard lights to provide comprehensive runway safety. THL systems are typically installed at:

  • Runway take-off ("line up and wait") positions, beginning approximately 114 m (375 ft) beyond the runway threshold and extending about 457 m (1,500 ft)
  • Intersecting runways where conflicts may occur during take-off
  • Runways with high traffic volume where incursion risk is significant
  • Major international airports implementing advanced surface movement control
Placement

Installation & Location

Fixtures are installed in two rows flanking the runway centreline at the take-off position, beginning approximately 114 m (375 ft) beyond the runway threshold and extending about 457 m (1,500 ft) down the runway, with each row set a fixed offset from the centreline so the red lights are visible to a pilot lined up for departure without being mistaken for centreline lighting. Each unit mounts on an L-868 base can recessed flush with the runway pavement, rated for the full wheel-load and jet-blast environment of the take-off roll, with cabling run in pavement ducting back to the THL control cabinet. The control cabinet houses the interface to the Runway Status Light surveillance feed, which illuminates the row only when the runway is occupied or a conflict is detected, and is typically co-located with or networked to the adjacent runway guard light controllers so the two subsystems act in a coordinated sequence. Setting-out is tied to the runway centreline survey so the light rows remain parallel and symmetrical about the centreline for the full length of the take-off hold zone.

Function

How Does It Work?

The THL system operates as part of the Runway Status Light (RWSL) system:

  • Surveillance: Radar, ADS-B, and surface movement radar data track all aircraft and vehicles on the airfield.
  • Detection: The RWSL processing system detects when a runway is occupied by an aircraft or vehicle.
  • Activation: When the runway is occupied, the THL system illuminates red lights on the runway at the take-off position, indicating to the pilot that it is unsafe to start the take-off roll.
  • Deactivation: When the runway is clear, the THL system deactivates, allowing the pilot to proceed with take-off.
Architecture

System Architecture & Control Logic

THL is not a standalone system — it is one output function of the wider Runway Status Light (RWSL) architecture, sharing its surveillance and processing layer with the Runway Entrance and Runway Intersection Light functions. Surface surveillance data (ASDE-X/ASSC radar, multilateration, and ADS-B) is fused continuously in the RWSL processing system, which runs a dedicated THL algorithm evaluating the runway ahead of each departure position for occupancy by a landing, departing, or crossing aircraft or vehicle. When a hazard is predicted, the algorithm issues an illuminate command to the light control and monitoring subsystem, which energises the in-pavement THL fixture array at the take-off position; when the runway clears, the same path issues the extinguish command. Because the decision is made entirely within the processing system, illumination happens in well under a second and does not wait on, or route through, air traffic control — the pilot sees the red lights as a direct, independent cue rather than a controller instruction. The light control and monitoring subsystem still reports THL circuit and fixture health back to the tower's ATC display and to maintenance, so status is visible even though command authority isn't.

Surveillance Sensors → RWSL Processing System (THL Algorithm) → Light Control & Monitoring → THL Fixture Array (with health feedback to ATC display)

SURVEILLANCE SENSORS ASDE-X / ASSC radar, multilateration, ADS-B Shared with REL / RIL functions RWSL PROCESSING SYSTEM Dedicated THL algorithm evaluates departure runway Sub-second hazard prediction, fully automated LIGHT CONTROL & MONITORING SUBSYSTEM Drives THL field circuit, reports fixture status THL FIXTURE ARRAY (IN-PAVEMENT) Red, in-line at the take-off position Illuminate or extinguish per algorithm command DIRECT PILOT CUE — NOT AN ATC INSTRUCTION Algorithm alone issues the illuminate command Tower cannot switch the THL fixture directly HEALTH FEEDBACK THL circuit and fixture status reported to the tower ATC display and to maintenance for fault dispatch
Logic Flow

Runway Occupancy Decision Flow

Surveillance DataRadar · ADS-B · Surface Movement Radar
Runway Occupancy Check
Runway Occupied
THL IlluminatesRed lights energised at take-off position
Pilot HoldsTake-off roll withheld
Runway Clear
THL DeactivatedLights extinguished
Pilot ClearedTake-off roll authorised
Construction

Physical Construction

The fixture housing is a heavy-duty die-cast aluminium or ductile-iron body machined to seat directly into an L-868 base can and finished to resist the fuel, hydraulic fluid, and de-icing chemical exposure typical of the take-off position. Because the unit lies flush with the pavement directly in the path of the main gear, the top plate is engineered to the full ≈27,000 kg (59,400 lb) wheel-load rating — governing case: fully loaded A380-800 tyre, per FAA Engineering Brief 83A and set with a slight crown to shed water and limit standing-fluid film over the lens. The red uni-directional beam is formed by an LED array or halogen lamp behind a toughened glass or polycarbonate lens, gasket-sealed to the housing with an O-ring or silicone seal to achieve an IP67/IP68 rating so the unit remains watertight under standing water and de-icing fluid immersion. Internal wiring terminates at L-823 primary connectors potted for direct burial, which mate to the secondary leads of the isolating transformer housed in an adjacent base can, keeping the series-circuit splice out of the wheel-load path and clear of surface water. Stainless-steel fasteners and a torque-rated top-cap seal are used throughout, and a dedicated interface cable runs from the fixture circuit back to the THL control cabinet that carries the RWSL activation command.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array (red)
ColourRed (uni-directional, towards approaching aircraft)
IntensityControlled by CCR (typically 5-step)
Beam PatternUni-directional (3° vertical x 6° horizontal)
PositionBeginning ≈114 m (375 ft) beyond runway threshold, extending ≈457 m (1,500 ft)
Mounting TypeFlush-mounted (inset) in runway 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)
IntegrationRWSL system interface
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries circuit, constant current (CCR fed)
Rated Series Current6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A)
IsolationVia dedicated isolating transformer (45W/65W), sited clear of the wheel-load path
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
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
Control InterfaceDedicated command link from THL control cabinet, driven by RWSL runway-occupancy logic
Power SourceCCR output, regulated per ICAO/FAA intensity step schedule
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity (100%)≥ 2,000 cd (red) per ICAO Annex 14 / IEC 61827
Intensity StepsTypically 5-step, but commanded on/off (steady or flashing) by RWSL logic rather than pilot-selected step
Vertical Beam SpreadMain beam 2°–15° above horizontal (peak ~3°–4°), uni-directional
Horizontal Beam Spread± 5° to ± 7.5° either side of runway centreline plane
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures
Chromaticity (Red)Within ICAO Annex 14 red boundary (CIE coordinates)
DirectionalityVisible to approaching/departing aircraft only; opaque/baffled to the opposite direction
Activation BehaviourSteady-burning red when illuminated; extinguished (not dimmed) when hold clears, per RWSL logic
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

THL system requirements and installation standards

FAA AC 150/5345-46

Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures

IEC 61827

Electrical and photometric performance for AGL luminaires

FAA AC 150/5345-53

Airport Lighting Equipment Certification Program

Prerequisites

Installation Requirements

Pavement Cut-Out & Base Can Setting
Civil

Core or saw-cut the pavement to the design cut-out, setting the base can flush and level so the finished fixture holds the required ≈27,000 kg (FAA EB 83A governing case) wheel-load tolerance.

Drainage & Sealant Provision
Civil

Provide a drainage path at the base can and seal the pavement-to-housing interface with an approved sealant rated for aircraft fuel and de-icing fluid exposure.

Duct & Cable Route
Electrical

Lay the series circuit duct/cable route at the design position (beginning ≈114 m / 375 ft beyond the threshold, extending ≈457 m / 1,500 ft), keeping bend radii within tolerance for the L-823 connector.

L-823 Connector Termination
Electrical

Terminate and seal the primary connector to IP67/IP68 submersible rating per manufacturer procedure before backfill or reinstatement of the base can.

Isolating Transformer Matching
Electrical

Confirm the isolating transformer rating (45W/65W) matches the fixture and the series circuit's 6.6A rated current step before connection.

RWSL Interface Wiring
Electrical

Route and terminate the RWSL control/interface link to the fixture's CCR channel, keeping the activation circuit isolated from unrelated series loops.

Flush Alignment & Centreline Setting
Mechanical

Set the in-pavement fixture flush and level against the centreline and design position, confirming no protrusion above the surrounding pavement surface.

Pre-Energisation Sign-off
Documentation

Record base can position, cable route, connector seal, and RWSL wiring as-built before backfill or pavement reinstatement, since these are not inspectable once the site is closed.

Verification

Testing & Commissioning

Insulation Resistance Test
Pre-Energisation

Megger-test the circuit and LED driver primary wiring before energisation, confirming insulation resistance clears the acceptable minimum.

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.

RWSL Activation & Response Time Test
Energisation

Confirm the fixture illuminates within the mandated response time of an RWSL activation command, and extinguishes cleanly on clear.

Photometric Intensity Test (Red)
Final Acceptance

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

LED Driver Output Verification
Energisation

Confirm the LED driver delivers rated output current and voltage to the array under commissioned load.

Fixture Alignment & Flush-Fit Verification
Final Acceptance

Confirm the in-pavement fixture sits flush and level within the centreline, within the design aiming tolerance.

Housing & Pavement Seal Check
Pre-Energisation

Inspect housing and pavement interface seals before the fixture is trafficked.

Documentation & As-Built Sign-off
Final Acceptance

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

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify red 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 tyre rubber deposits picked up at the take-off position so light output and visibility to the pilot stay within spec.

RWSL Activation Test
Semi-annual

Verify the fixture activates and clears correctly on RWSL commands, since a communication fault here can leave the light failing to switch at the correct time.

LED Driver Inspection
Annual

Check the LED driver for signs of thermal stress or degradation and replace on schedule, since driver failure is a common cause of THL outages.

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.

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 runway pavement for settlement, cracking, or debris that could affect drainage or wheel-load rating.

Field Notes

Common Field Issues

Lens Contamination from Rubber Deposits

THL lights are exposed to tyre rubber deposits from aircraft at the take-off position. Regular cleaning with approved solvents and soft brushes is required to maintain light output and visibility.

RWSL Communication Failure

THL lights rely on communication with the RWSL system. Network failures can cause the lights to fail to activate or deactivate at the correct time. Redundant communication paths and regular system checks are essential.

LED Driver Failure

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

Diagnostics

Troubleshooting Guide

THL Row Fails to Illuminate When Runway Is Occupied
Likely Cause
Loss of the illuminate command from the RWSL processing system's THL algorithm, or a fault in the light control and monitoring subsystem between the processing layer and the fixture array.
Diagnostic Steps
Check the RWSL processing system's THL algorithm status and command log for this position; confirm the light control and monitoring subsystem is receiving and relaying the illuminate command; force a manual test activation to isolate processing-side vs fixture-side faults.
Corrective Action
Restore the processing-to-control-subsystem link if the command is not reaching the array, or repair/replace the control and monitoring subsystem interface; escalate a persistent algorithm-side fault to RWSL system maintenance.
Single Fixture Dark Within the THL Row
Likely Cause
Failed LED module or isolating transformer on that unit, or an open series-loop connection isolating just that fixture from the rest of the row.
Diagnostic Steps
Confirm the rest of the row illuminates correctly on a test activation; check series loop continuity through the affected fixture's transformer; inspect L-823 connectors at that unit for corrosion or an open crimp.
Corrective Action
Replace the failed LED module or transformer, or re-terminate the faulted connector; re-verify with a follow-up test activation before returning the row to service.
Lights Remain Illuminated After Runway Is Clear
Likely Cause
The extinguish command from the RWSL processing system is not reaching the fixture array, or surveillance data is still reporting a stale occupancy condition for that runway.
Diagnostic Steps
Compare the RWSL processing system's current occupancy determination against actual runway status; issue a manual extinguish command through the light control and monitoring subsystem and observe response; check for a latched fault in that subsystem.
Corrective Action
Reset or replace the latched control and monitoring subsystem interface; if the surveillance feed itself is stale, escalate to RWSL system maintenance to clear or restart the affected sensor/processing path.
Health Status Not Reporting to ATC Display
Likely Cause
Broken or misconfigured feedback link between the light control and monitoring subsystem and the tower's ATC display, independent of whether the THL fixtures themselves are functioning.
Diagnostic Steps
Confirm THL fixture operation is unaffected by activating the row manually; check the monitoring subsystem's reporting link and configuration to the ATC display; test with a known fixture-health event to see if it registers at the tower.
Corrective Action
Restore or reconfigure the reporting link between the monitoring subsystem and the ATC display; treat this as a monitoring-only fault and continue operating the THL row while the reporting path is repaired, per RWSL fault procedure.
Reduced Light Output / Rubber-Contaminated Lens
Likely Cause
Tyre rubber deposits from repeated take-off rolls building up on the lens, or a hazed/eroded lens from prolonged jet-blast and wheel-load exposure at the flush-mounted position.
Diagnostic Steps
Visually inspect the lens for rubber film or surface degradation; run a photometric intensity check against ICAO/FAA thresholds if contamination alone doesn't explain the reduced output.
Corrective Action
Clean the lens with approved solvents and a soft brush; replace the lens or fixture if photometric output remains below threshold after cleaning.
Series Circuit Fault or Insulation Resistance Drop at THL Position
Likely Cause
Moisture ingress at the base can, gaskets, or connectors under the runway pavement, or wheel-load/jet-blast stress on the ducted cable run to the fixture.
Diagnostic Steps
Megger the isolation transformer and series circuit for the affected segment; inspect base can seals, top-cap O-rings, and connector torque; check the pavement and duct run for settlement or damage.
Corrective Action
Dry out or replace the affected transformer/connector, renew gaskets and O-rings, and confirm insulation resistance is restored above the acceptable minimum before re-energising the circuit.
Reliability

Failure Modes & Root Causes

Loss of RWSL Illuminate/Extinguish Command
High Severity
Root Cause
Failure or degradation of the communication path between the RWSL processing system's THL algorithm and the light control and monitoring subsystem, or a fault within the algorithm's occupancy determination itself.
Effect
THL row fails to illuminate for an occupied runway (loss of a safety-critical warning) or fails to extinguish once clear, either of which undermines pilot confidence in the system.
Detection Method
RWSL processing system command/status log review, periodic manual test activation of the row, and monitoring of the communication link's health indicators.
LED Module / Isolating Transformer Failure
High Severity
Root Cause
Thermal stress or power-surge damage to the LED driver/module, or moisture-driven insulation breakdown in the isolating transformer winding.
Effect
Single fixture goes dark within the THL row, reducing the row's warning conspicuity even while the RWSL command chain is functioning correctly.
Detection Method
Test activation to confirm which unit fails to light, series loop continuity check through the fixture's transformer, and megger testing of the winding.
Health/Status Monitoring Link Failure
Medium Severity
Root Cause
Broken or misconfigured reporting link between the light control and monitoring subsystem and the tower's ATC display, independent of fixture health.
Effect
Loss of fixture-health visibility at the tower even though the THL row itself continues to operate correctly, delaying awareness of a genuine fixture fault.
Detection Method
Manual row activation to confirm fixture operation is unaffected, followed by a known fixture-health test event to verify it registers correctly at the ATC display.
Lens Contamination or Erosion
Low Severity
Root Cause
Accumulated tyre rubber deposits from repeated take-off rolls, or a hazed/eroded lens from prolonged jet-blast and wheel-load exposure at the flush-mounted position.
Effect
Reduced or uneven light output that can fall below ICAO/FAA photometric thresholds, weakening the row's visual warning at the take-off position.
Detection Method
Scheduled visual inspection for rubber film or lens degradation, backed by photometric intensity testing when contamination alone doesn't explain the shortfall.
L-823 Connector / Series Circuit Insulation Breakdown
Medium Severity
Root Cause
Moisture ingress at the base can, gaskets, or connectors under the runway pavement, compounded by wheel-load and jet-blast stress on the ducted cable run to the fixture.
Effect
Intermittent operation or a partial ground fault that degrades insulation resistance on the series circuit serving the THL position.
Detection Method
Megger testing of the isolation transformer and series circuit segment, and visual inspection of base can seals, top-cap O-rings, and connector torque.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

THL fixtures 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 base can before opening it or handling connectors.

Take-Off Roll Zone Coordination
Operational

These fixtures sit directly in the take-off roll path; work here requires full runway closure with ATC coordination and a NOTAM, not a live-traffic gap, since the location offers no separation margin from a departing aircraft.

Surveillance Interlock Dependency
Operational

The red hold indication is driven entirely by the RWSL surveillance feed; any work on the fixture or control cabinet must be followed by an integration check confirming the interlock still correctly activates before returning the system to service.

Wheel-Load & Jet-Blast Rating
Mechanical

The inset fixture must sit precisely flush with the pavement and be rated for the full wheel-load and jet-blast environment of the take-off roll; a proud edge or depression here is a high-speed FOD and wheel-impact risk.

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 leave a gap in the hold-light row.

Restore to Compliant State
Compliance

Do not return the fixture to service with an unverified surveillance interlock; confirm activation timing, coordination with the adjacent runway guard lights, and photometric conformance before closing out and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Sub-Second Timing Is a Health Metric in Its Own Right
Verification

Because illumination has to happen in well under a second directly from the surveillance/processing chain, response latency is worth trending after any processing system update, not just occupancy accuracy. A system that eventually reaches the right answer but too slowly has failed its purpose just as surely as one that gets the wrong answer.

Shared Sensor Layer Means Shared Failure Modes
Surveillance

THL shares its surveillance and processing layer with the REL and RIL functions, so a coverage gap or calibration drift in the radar/ADS-B/multilateration feed can degrade all three simultaneously even though only THL is being watched during a routine check. Treat a THL anomaly as a prompt to verify REL/RIL behaviour too.

Diagnose Faults With a Fail-Safe Mindset
Failure Mode

The system's entire safety case rests on illuminating when a hazard is present, so any reported fault should be characterised by which way it fails — a fixture stuck lit is an operational nuisance, one that can't illuminate on command is a runway-incursion risk requiring immediate action, and the two shouldn't be triaged the same way.

Wheel-Load Rating at Rotation Speed, Not Taxi Speed
Mechanical

The THL fixture sits in the same in-pavement environment as any inset fixture, but sees rotation and rejected-takeoff speeds rather than taxi speeds. A seating tolerance that would be a minor issue on a taxiway centreline light is a higher-consequence FOD and wheel-impact risk here.

Functional Tests Need Their Own Safety Coordination
Operational

A test illumination of the THL fixture or algorithm can be mistaken for a genuine hold indication by a crew monitoring the frequency or a controller glancing at the runway if it isn't clearly flagged in advance. Build test coordination into the work plan as its own safety item, not an afterthought to the electrical work.

Health Feedback and Command Are Separate Paths
Architecture

Fixture health is reported to the tower display over a separate path from the illuminate/extinguish command itself, so a healthy status readout doesn't guarantee the command path is functioning, and vice versa. Verify both paths independently after any processing system or cabinet work, not just the one you touched.

Quick Answers

Frequently Asked Questions

Short answers about the Take-Off Hold Light (THL): what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is a Take-Off Hold Light (THL)?

A Take-Off Hold Light (THL) is a runway safety lighting system that provides visual indications to pilots at the runway holding position. The THL system consists of a double row of red lights embedded in the runway surface at the take-off/"line up and wait" position, beginning approximately 114 m (375 ft) beyond the runway threshold and extending roughly 457 m (1,500 ft) down the runway.

Q2What is the purpose of a Take-Off Hold Light (THL)?

The THL exists to give a pilot lined up for takeoff a direct, independent confirmation that the runway ahead is actually clear, rather than relying solely on an air traffic control clearance that could be based on incomplete information or delivered just before a conflicting aircraft or vehicle enters the runway.

Q3Where is a Take-Off Hold Light (THL) used and installed?

THL systems are deployed as part of the FAA's Runway Status Light (RWSL) program at a defined set of high-traffic, towered airports selected on the basis of operations volume and runway incursion history, rather than any single runway's instrument approach category. They are used in conjunction with runway entrance lights, runway intersection lights, and runway guard lights to provide comprehensive runway safety.

Q4How does a Take-Off Hold Light (THL) work?

The THL system operates as part of the Runway Status Light (RWSL) system: Surveillance: Radar, ADS-B, and surface movement radar data track all aircraft and vehicles on the airfield. Detection: The RWSL processing system detects when a runway is occupied by an aircraft or vehicle. Activation: When the runway is occupied, the THL system illuminates red lights on the runway at the take-off position, indicating to the pilot that it is unsafe to start the take-off roll. Deactivation: When the runway is clear, the THL system deactivates, allowing the pilot to proceed with take-off.

Q5What are the typical technical parameters of a Take-Off Hold Light (THL)?

Typical values are — Light Source: LED array (red); Colour: Red (uni-directional, towards approaching aircraft); Intensity: Controlled by CCR (typically 5-step); Beam Pattern: Uni-directional (3° vertical x 6° horizontal); Position: Beginning ≈114 m (375 ft) beyond runway threshold, extending ≈457 m (1,500 ft); Mounting Type: Flush-mounted (inset) in runway 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: RWSL system interface.

Q6What are the electrical requirements for a Take-Off Hold Light (THL)?

Typical requirements are — Circuit Type: Series circuit, constant current (CCR fed); Rated Series Current: 6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A); Isolation: Via dedicated isolating transformer (45W/65W), sited clear of the wheel-load path; 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; Insulation Resistance: ≥ 50 MΩ (megger test, cable-to-ground); Earthing/Grounding: Fixture body and base can bonded to airfield earth grid.

Q7What photometric requirements apply to a Take-Off Hold Light (THL)?

Typical requirements are — Main Beam Intensity (100%): ≥ 2,000 cd (red) per ICAO Annex 14 / IEC 61827; Intensity Steps: Typically 5-step, but commanded on/off (steady or flashing) by RWSL logic rather than pilot-selected step; Vertical Beam Spread: Main beam 2°–15° above horizontal (peak ~3°–4°), uni-directional; Horizontal Beam Spread: ± 5° to ± 7.5° either side of runway centreline plane; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures; Chromaticity (Red): Within ICAO Annex 14 red boundary (CIE coordinates); Directionality: Visible to approaching/departing aircraft only; opaque/baffled to the opposite direction.

Q8Which standards apply to a Take-Off Hold Light (THL)?

The main references are ICAO Annex 14 — THL system requirements and installation standards; FAA AC 150/5345-46 — Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures; 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 Take-Off Hold Light (THL) be inspected and maintained?

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

Q10How do I troubleshoot common Take-Off Hold Light (THL) faults?

Common symptoms covered are: THL Row Fails to Illuminate When Runway Is Occupied; Single Fixture Dark Within the THL Row; Lights Remain Illuminated After Runway Is Clear; Health Status Not Reporting to ATC Display; Reduced Light Output / Rubber-Contaminated Lens; Series Circuit Fault or Insulation Resistance Drop at THL Position. For example, for "THL Row Fails to Illuminate When Runway Is Occupied": Likely Cause: Loss of the illuminate command from the RWSL processing system's THL algorithm, or a fault in the light control and monitoring subsystem between the processing layer and the fixture array. Diagnostic Steps: Check the RWSL processing system's THL algorithm status and command log for this position; confirm the light control and monitoring subsystem is receiving and relaying the illuminate command; force a manual test activation to isolate processing-side vs fixture-side faults. Corrective Action: Restore the processing-to-control-subsystem link if the command is not reaching the array, or repair/replace the control and monitoring subsystem interface; escalate a persistent algorithm-side fault to RWSL system maintenance.

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 THL system selection or installation?

Precision AGL Academy provides advice on RWSL integration, positioning, and field testing of Take-Off Hold Light systems.