AGL Component Library By Precision AGL Academy

Runway Centreline Light

A precision visual guidance aid installed along the runway centreline, providing pilots with continuous reference during takeoff, landing, and roll-out. Features unique colour coding (white, red, and alternating red/white) to indicate remaining runway distance.

Runway Centreline Light

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Overview

What Is It?

A Runway Centreline Light is a series of flush-mounted inset lights installed along the exact centre of the runway. These lights provide critical longitudinal guidance to pilots, particularly during low-visibility operations. The colour coding is standardized: white lights from the threshold to 900 metres from the runway end, alternating red and white from 900 to 300 metres from the runway end, and all red from 300 metres to the runway end. This colour transition gives pilots a visual cue of the remaining runway length.

Purpose

Purpose & Function

Centreline lights exist to keep an aircraft tracking the exact longitudinal axis of the runway when the pilot's outside visual references are degraded, most critically during CAT II/III landings and low-visibility takeoffs where edge lights alone cannot provide fine enough lateral guidance. Because the fixture sits directly on the line the aircraft's nose and main gear must follow, it lets the pilot correct drift immediately rather than relying on peripheral edge references, which is essential for staying within the narrow safety margins of a precision approach. The colour transition from white, to alternating red/white, to solid red is itself a purpose-built distance cue: it tells the pilot how much runway remains without requiring them to consult instruments, supporting the decision to continue, brake, or abort during the high-workload final stage of landing or takeoff roll.

Application

Where Is It Used?

Installed on precision approach runways (CAT I, II, and III) and many non-precision runways where centreline guidance is required. Per ICAO Annex 14, the standard longitudinal spacing is 15 metres; a wider 30-metre spacing may only be used where the centreline lighting's serviceability meets the specified maintenance objectives and the runway is intended for use in RVR conditions of 350 m or greater (i.e., less demanding, non-CAT II/III operations). CAT II/III precision approach and low-visibility runways are therefore kept at the 15-metre spacing. They are used in conjunction with runway edge lights and touchdown zone lights to provide comprehensive visual guidance during all phases of the approach and landing.

Placement

Installation & Location

Fixtures are set into the runway pavement along the physical centreline, tied to the runway centreline survey so the line of lights remains true along the full runway length. Inset (flush) L-850-series fittings are used almost exclusively on the centreline, since an elevated fixture on the landing surface itself would present a strike hazard, and each unit is seated into a base can recessed into the pavement and sealed against surface water and jet-blast erosion. Standard spacing is 15 m, with a wider 30 m spacing permitted only where centreline light serviceability meets the maintenance objectives and the runway supports RVR ≥ 350 m; CAT II/III and other low-visibility runways are kept at 15 m throughout. Colour transitions are built into the setting-out: white along the body of the runway, alternating red/white through the last 900 m, and solid red for the final 300 m. Each fixture is fed by cable run in pavement ducting back to its isolating transformer, with transformers housed clear of the light base to keep the series-circuit joint out of standing water, and installation must maintain the pavement grade and load-bearing strength around each cut-in.

Function

How Does It Work?

Each centreline light is powered from the constant current series circuit via an isolating transformer. The lights use a bi-directional optical system to project a narrow beam (typically 4° vertical x 6° horizontal) both ahead and behind the fixture, ensuring visibility to pilots on approach and during roll-out. The colour transition is achieved using coloured filters or dichroic lenses. The intensity is controlled by the CCR's current steps, with higher intensities used during low visibility operations.

Architecture

System Architecture & Control Logic

Centreline lights are wired on their own dedicated series circuit, kept separate from the runway edge, threshold, and end light loops, since their close 15 m standard spacing and role in low-visibility operations call for brightness stepping that is independent of the rest of the runway lighting system. Colour is not a real-time control function: the white, alternating red/white, and solid red zones are fixed by the coloured filter or dichroic lens built into each fixture according to its distance from the runway end, so the colour pattern along the runway never changes regardless of which CCR step is commanded — only the overall intensity of every fixture on the loop rises or falls together. An Airfield Lighting Control and Monitoring System (ALCMS), operated by the tower or an automated visibility-linked routine, selects the intensity step appropriate to prevailing RVR; the CCR regulates the entire centreline loop to that fixed current, and every fixture's isolating transformer draws from the same current and burns at the same intensity simultaneously — there is no way to command an individual fixture, or a single colour zone, independently of the rest of the line. Fault detection is loop-based: the CCR continuously monitors loop voltage against the commanded current, and a voltage rise at constant current signals increased circuit impedance, typically an open-circuit lamp or a failed isolating transformer, which is reported to the ALCMS as a loop fault to be sectionalised by further field testing rather than resolved to an exact fixture from the control room.

ALCMS → CCR → Dedicated Centreline Circuit Loop → Isolating Transformer → Centreline Fixture (colour fixed by lens, not by command)

AIRFIELD LIGHTING CONTROL SYSTEM (ALCMS) Selects intensity step from prevailing RVR CONSTANT CURRENT REGULATOR Converts step command to fixed current DEDICATED CENTRELINE CIRCUIT LOOP Independent of edge / threshold / end loops ISOLATING TRANSFORMER (PER FIXTURE) Taps fixed loop current to fixture secondary CENTRELINE FIXTURE (WHITE / RED-WHITE / RED) Colour set by fitted lens, not by CCR step DEDICATED LOOP — NOT SHARED WITH OTHER CIRCUITS Colour zoning is fixed wiring, not real-time control Faults are isolated by loop testing, not fixture ID LOOP FEEDBACK CCR tracks loop voltage against commanded current Voltage rise flags an open circuit or failed transformer
Function

Circuit & Beam Overview

CONSTANT CURRENT REGULATOR Series Circuit — 6.6A ISOLATING TRANSFORMER 45W / 65W RUNWAY CENTRELINE LIGHT FIXTURE Flush-Mounted (Inset) — IP67 / IP68 FORWARD BEAM Toward Approach Direction AFT BEAM Toward Roll-Out Direction BI-DIRECTIONAL GUIDANCE TO PILOT Beam Pattern: 4° Vertical × 6° Horizontal COLOUR CODING BY DISTANCE FROM RUNWAY END THRESHOLD RUNWAY END 900m 300m WHITE RED / WHITE ALTERNATING RED
Zone widths are schematic and not drawn to scale.
Construction

Physical Construction

Centreline fixtures use a low-profile, load-rated aluminium alloy housing sunk into the pavement so the top surface sits flush with the runway and tolerates repeated aircraft wheel loading without cracking or displacement. The lens is a shallow, toughened-glass or polycarbonate dome shaped to shed water and resist jet-blast erosion while still projecting a usable beam angle. Where the fixture must show two colours (the alternating red/white and solid-red zones), the optical assembly is split internally by a fixed filter or divided LED array, so red and white segments share one sealed unit rather than requiring separate fixtures. The housing seats into an L-868 base can recessed into the pavement, gasket-sealed against surface water and fuel ingress for an IP67/IP68 rating. Internal leads terminate at L-823 primary connectors, sealed for direct burial and continuous immersion, mating to the isolating transformer's secondary in a base can set clear of the light itself, with stainless-steel fasteners used throughout to resist corrosion.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array or 45W / 65W halogen
Colour CodingWhite (runway body, from threshold up to 900m before the runway end), Alternating Red/White (900m–300m before the runway end), Red (final 300m before the runway end)
Spacing15m standard (all precision categories); up to 30m where permitted for RVR ≥ 350m operations
Beam PatternBi-directional (4° vertical x 6° horizontal)
Mounting TypeFlush-mounted (inset) in pavement
Load CapacityGoverning case per FAA Engineering Brief 83A: fully loaded A380-800 tyre (59,400 lb / ≈27,000 kg wheel load) imparts ≈24,700 lb (≈11,200 kg) onto the fixture footprint
Isolating Transformer45W / 65W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
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), 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
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 and open-circuit detection
Power SourceCCR output, regulated per ICAO/FAA intensity step schedule
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity (100%)≥ 10,000 cd (white), ≥ 2,000 cd (red) per ICAO Annex 14 / IEC 61827
Intensity Steps (5-step)100% / 30% / 10% / 3% / 1% of rated peak intensity
Vertical Beam SpreadMain beam 1°–15° above horizontal (peak ~4°), low-profile inset lens
Horizontal Beam Spread± 5° to ± 7.5° either side of runway centreline plane
DirectionalityBi-directional, symmetric intensity in both directions of travel
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures
Chromaticity (White)Within ICAO Annex 14 white boundary (CIE coordinates)
Chromaticity (Red)Within ICAO Annex 14 red boundary (CIE coordinates)
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

Centreline light spacing, colours, and photometric requirements

FAA AC 150/5345-46

Specification for runway centreline 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 Recess & Grade
Civil

Cut and compact the recess to the L-868 base can profile, holding the can top flush with the pavement surface and grade so no lip or depression is left to catch a wheel.

Centreline Survey & Spacing Set-out
Civil

Set out fixture positions from the runway centreline survey at the design spacing — 15 m standard, or up to 30 m only where permitted for RVR ≥ 350 m operations — confirming the white/alternating-red-white/red colour transitions land at the correct chainage before any cutting begins.

Drainage & Sealing
Civil

Seal the base can against surface water and jet-blast erosion, and locate the isolating transformer clear of the light base so the series-circuit joint stays out of standing water.

Duct & Cable Route
Electrical

Run the series circuit duct through pavement ducting to design depth, avoiding sharp bends that could stress the L-823 connector at final termination.

L-823 Connector Termination
Electrical

Terminate and seal the primary connector per manufacturer procedure, keeping the splice submersible-rated before the base can is closed and backfilled.

Isolating Transformer Matching
Electrical

Confirm the isolating transformer wattage matches the fixture and the series circuit's rated current step before connection.

Load-Rated Housing Seating
Mechanical

Seat the fixture housing fully home in the base can and confirm it sits flush and level, since the flush-mounted design must carry full aircraft wheel load without cracking or displacing.

Pre-Sealing Sign-off
Documentation

Record base can position, cable route, connector seal, and colour-zone chainage as-built before the recess is finally sealed, since these are not inspectable once the pavement is closed.

Verification

Testing & Commissioning

Insulation Resistance (Megger) 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.

Photometric & Colour Test (Red/White)
Final Acceptance

Verify intensity and chromaticity of both white and red-segment optics where alternating colour sections apply, against ICAO/FAA thresholds.

CCR Brightness Step Response
Energisation

Cycle the CCR through every intensity step and confirm the fixture responds correctly at each.

Load Rating & Recess Fit Verification
Pre-Energisation

Confirm the fixture and recessed housing meet wheel-load tolerances for the centreline before pavement is finally sealed.

Alignment & Levelling Verification
Final Acceptance

Confirm the fixture sits flush, level, and correctly centred within the recess before final backfill.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, and photometric readings alongside as-built position in the commissioning dossier for handover.

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Measure beam intensity and colour output against ICAO/FAA thresholds to confirm the fixture still meets minimum candela requirements under normal traffic wear.

Lens Cleaning & Rubber Deposit Removal
Quarterly

Clear rubber deposits, dirt, and film build-up from the lens with approved solvents and soft brushes so light output stays within spec.

Seal & Gasket Inspection
Annual

Check top-lens O-rings and body gaskets for cracking or compression set, and re-torque fasteners to keep the flush-mounted housing watertight.

Load Rating & Recess Inspection
Annual

Inspect the pavement recess, mounting can, and surrounding surface for cracking, spalling, or settlement that could compromise wheel-load rating or drainage.

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.

Alignment & Levelling
Semi-annual

Confirm the fixture sits flush with the pavement surface and that beam aim remains within tolerance so light stays correctly projected along the centreline.

Cable & Connector Inspection
Annual

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

Field Notes

Common Field Issues

Colour Filter Degradation

The red and white filters in centreline lights are subject to UV degradation and thermal stress. Over time, the colour intensity can fade or shift, compromising the colour coding that pilots rely on for distance estimation. Regular photometric testing is essential.

Lens Contamination from Rubber Deposits

Aircraft tyres deposit rubber on the runway surface, which can accumulate on the centreline light lenses, reducing light output. Regular cleaning with approved solvents and soft brushes is required to maintain photometric performance.

Misalignment Due to Pavement Settlement

Pavement settlement can cause centreline lights to tilt, altering the beam pattern and reducing visibility. Regular alignment checks using a digital level or specialized alignment jig are recommended.

Field Notes

Troubleshooting Guide

Single Fixture Dark, Rest of Circuit Normal
Likely Cause
Failed LED module/lamp, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding) at that 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/lamp if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before lowering the fixture back into the can.
Entire Series Circuit Dark / CCR Will Not Regulate
Likely Cause
Open-circuit fault in the series loop (severed cable, corroded L-823 splice, or a failed transformer acting as an open point).
Diagnostic Steps
Check the CCR fault/open-circuit indication first; loop-resistance test from the CCR output to isolate the faulted segment; sectionalise and megger cable runs to narrow down the break.
Corrective Action
Excavate and repair or replace the faulted cable section and connector; re-test insulation resistance before reinstating the circuit.
CCR Trips on Overcurrent or Ground Fault
Likely Cause
Moisture ingress at a flush-mounted can or connector, often from a cracked seal or a failed drain, has degraded insulation resistance and created a short or partial ground fault.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect fixture cans for standing water, cracked gaskets, or damaged secondary cable jackets.
Corrective Action
Pump out and dry the affected can, renew top-lens O-rings and body gaskets, and confirm insulation resistance is back above the acceptable minimum before re-energising.
Reduced, Uneven, or Colour-Shifted Light Output
Likely Cause
Rubber-deposit film or scratching on the top lens, a UV-degraded red/white colour filter, or an aging LED array running below its rated candela.
Diagnostic Steps
Run a photometric intensity and colour check against ICAO/FAA thresholds; inspect the lens for rubber build-up, pitting, or filter fade; confirm the CCR is set to the correct intensity step.
Corrective Action
Clean the lens with approved solvents, replace a faded filter or degraded LED module, or correct the CCR step setting; re-verify with a follow-up photometric reading.
Fixture Flickering or Intermittent
Likely Cause
Loose or corroded primary/secondary crimp connections inside the can, or a marginal transformer winding under thermal and wheel-load vibration.
Diagnostic Steps
Inspect and re-torque all cable connections at the base can; check crimps for corrosion; monitor secondary voltage for drop under load once the CCR has warmed up.
Corrective Action
Re-terminate corroded connections with new crimps and sealant, or replace the transformer if voltage sag is confirmed under load.
Fixture Not Flush, Cracked Top, or Water Pooling in Recess
Likely Cause
Repeated aircraft wheel loading has fatigued the mounting flange or recess, or subgrade/pavement settlement has left the fixture proud, sunken, or holding water above the top lens.
Diagnostic Steps
Check flush tolerance and cracking around the recess edge with a straightedge; verify the drain path is clear; inspect the mounting flange and fasteners for fatigue or shear.
Corrective Action
Re-set or replace the mounting can and re-pour the surrounding pavement to restore flushness, clear or re-grade the drain path, and replace a cracked top assembly before it admits water into the circuit.
Reliability

Failure Modes & Root Causes

LED Module / Lamp Failure
High Severity
Root Cause
Solder-joint fatigue from thermal cycling and wheel-load vibration inside the can, moisture ingress past a degraded seal, or ordinary end-of-life lumen depreciation.
Effect
Single fixture goes dark or drops below minimum intensity while the rest of the series circuit continues to operate normally.
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 into the base can leading to insulation breakdown, a manufacturing winding defect, or a blown primary fuse-wire link from a transient surge.
Effect
Open-circuit point in the series loop, darkening the single fixture or, if the open extends further, taking 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.
Base Can Seal / Drain Failure
Medium Severity
Root Cause
Cracked top-lens O-rings or body gaskets, or a blocked drain path, allowing surface water to collect and stand inside the flush-mounted can.
Effect
Degraded insulation resistance producing a short or partial ground fault that can trip the CCR.
Detection Method
Full-circuit megger testing to identify the low-resistance segment, and a visual check for standing water or cracked gaskets at suspect cans.
Colour Filter / Lens Degradation
Low Severity
Root Cause
UV exposure fading the red/white colour filter, or rubber-deposit film and scratching building up on the top lens from tyre contact.
Effect
Reduced or colour-shifted light output that can fall outside ICAO/FAA photometric and chromaticity thresholds, particularly at the red-segment transition.
Detection Method
Photometric intensity and colour check, and visual inspection of the lens for rubber build-up, pitting, or filter fade during cleaning.
Crimp Connection Corrosion
Medium Severity
Root Cause
Loose or corroded primary/secondary crimp connections inside the can, aggravated by thermal cycling and constant wheel-load vibration.
Effect
Fixture flickers or operates intermittently, and voltage can sag under load once the CCR has warmed up.
Detection Method
Inspection and re-torque of cable connections at the base can, and monitoring secondary voltage for drop under load.
Mounting Flange Fatigue / Recess Settlement
High Severity
Root Cause
Repeated aircraft wheel loading fatiguing the mounting flange, or subgrade/pavement settlement around the recess over time.
Effect
Fixture sits proud, sunken, or cracked at the recess, creating an FOD risk and allowing water to pool above the top lens.
Detection Method
Flush-tolerance and cracking check with a straightedge, drain-path verification, and inspection of the mounting flange and fasteners for fatigue or shear.
Series Cable Insulation Breakdown
High Severity
Root Cause
Cable jacket damage from nearby excavation, age-related insulation degradation, or prolonged standing water in the duct run between cans.
Effect
Ground fault or short circuit that trips the CCR or darkens the entire centreline series loop.
Detection Method
Full-circuit megger test to flag the low-resistance segment, followed by sectionalised testing to pinpoint the fault location.
CCR Regulation Fault
High Severity
Root Cause
Internal component failure (control board or output stage), a load mismatch after circuit modification, or a firmware/setpoint fault.
Effect
Incorrect brightness step, failure to hold regulated current across the loop, or nuisance tripping on healthy circuits.
Detection Method
CCR self-diagnostic/fault indication, output current verification, and a load-bank test to confirm regulation across all intensity steps.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

Centreline 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.

Airside Work Coordination
Operational

Working directly on the centreline means working in the physical wheel track of every landing and departing aircraft; this requires runway closure or a protected work window with full ATC coordination and a NOTAM, never a live-traffic gap.

Flush Fit & Wheel-Load Tolerance
Mechanical

The L-850-series fitting must sit precisely flush with the pavement surface; even a small proud edge or depression becomes a repeated wheel-impact point and a FOD source under sustained tyre loading.

Colour-Zone Accuracy
Compliance

Confirm the replacement fixture's lens/filter matches the correct colour for its zone (white, alternating red/white, or solid red) before closing out; an incorrect colour at the wrong distance from the runway end misleads the remaining-length cue pilots rely on, particularly in CAT II/III operations.

Base Can Seal Integrity
Mechanical

Reseal the base can and cable gland fully watertight after any work, since standing water at a centreline can degrades insulation quickly under continuous tyre and jet-blast exposure.

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 a long run of centreline lights.

Restore to Compliant State
Compliance

Do not leave a fixture proud, dark, or with an incorrect colour after maintenance; verify flushness, colour, and photometric conformance before closing out and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Colour-Segment Orientation Is Rotation-Sensitive
Optical

Where the fixture's internal filter or LED array splits red and white segments for the touchdown-zone and last-300 m transitions, the segment split only reads correctly if the housing is seated in the exact rotational orientation the optical design assumes. A fixture reinstated a few degrees off its seated orientation after base-can work can show the wrong colour proportion to one direction of traffic without failing a simple on/off check.

Highest Wheel-Load Concentration on the Field
Mechanical

Centreline fixtures take direct wheel crossings from every landing and departure, more than any other inset type, so housing and lens fatigue here tends to show up earlier than the standard inspection interval assumes. Weight centreline inspection frequency toward wheel-load fatigue signs (hairline lens cracking, base-can seating movement), not just optical output.

Diagnosing Faults Ahead of a Hard Failure
Troubleshooting

Because CAT II/III runways are held at the tighter 15 m standard spacing (rather than the 30 m allowed for less demanding operations), a single failed centreline fixture is far more noticeable to a pilot than an equivalent gap elsewhere on the field. Trend loop insulation readings through this zone specifically, so a developing connector fault is caught before it creates a visible gap at the highest-scrutiny part of the runway.

Transformer Sizing on LED Retrofit
Retrofit

An isolating transformer sized for the legacy incandescent lamp is typically oversized for an LED centreline retrofit, which invites early transformer failure and nuisance loop-current faults. Re-select VA rating against the actual dual-colour LED module's draw, not the lamp it replaces.

Grade and Seating Tolerance Compounds Over a Long Run
Civil

A base can set a few millimetres proud or recessed is a minor issue in isolation, but repeated along a full-length centreline run it becomes a visible ride-quality and jet-blast erosion pattern. Hold seating tolerance consistently along the run rather than treating each cut-in as an independent installation.

Fuel and Rubber Deposit Build-Up in the Touchdown Zone
Durability

The dome lens through the touchdown zone accumulates rubber and fuel residue faster than the white-only sections further down the runway, which can dull the red/white split before it dulls overall output. Clean and re-verify colour segmentation on its own shorter cycle through this zone rather than relying on a field-wide cleaning interval.

Quick Answers

Frequently Asked Questions

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

Q1What is a Runway Centreline Light?

A Runway Centreline Light is a series of flush-mounted inset lights installed along the exact centre of the runway. These lights provide critical longitudinal guidance to pilots, particularly during low-visibility operations. The colour coding is standardized: white lights from the threshold to 900 metres from the runway end, alternating red and white from 900 to 300 metres from the runway end, and all red from 300 metres to the runway end. This colour transition gives pilots a visual cue of the remaining runway length.

Q2What is the purpose of a Runway Centreline Light?

Centreline lights exist to keep an aircraft tracking the exact longitudinal axis of the runway when the pilot's outside visual references are degraded, most critically during CAT II/III landings and low-visibility takeoffs where edge lights alone cannot provide fine enough lateral guidance.

Q3Where is a Runway Centreline Light used and installed?

Installed on precision approach runways (CAT I, II, and III) and many non-precision runways where centreline guidance is required. Per ICAO Annex 14, the standard longitudinal spacing is 15 metres; a wider 30-metre spacing may only be used where the centreline lighting's serviceability meets the specified maintenance objectives and the runway is intended for use in RVR conditions of 350 m or greater (i.e., less demanding, non-CAT II/III operations). CAT II/III precision approach and low-visibility runways are therefore kept at the 15-metre spacing.

Q4How does a Runway Centreline Light work?

Each centreline light is powered from the constant current series circuit via an isolating transformer. The lights use a bi-directional optical system to project a narrow beam (typically 4° vertical x 6° horizontal) both ahead and behind the fixture, ensuring visibility to pilots on approach and during roll-out. The colour transition is achieved using coloured filters or dichroic lenses. The intensity is controlled by the CCR's current steps, with higher intensities used during low visibility operations.

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

Typical values are — Light Source: LED array or 45W / 65W halogen; Colour Coding: White (runway body, from threshold up to 900m before the runway end), Alternating Red/White (900m–300m before the runway end), Red (final 300m before the runway end); Spacing: 15m standard (all precision categories); up to 30m where permitted for RVR ≥ 350m operations; Beam Pattern: Bi-directional (4° vertical x 6° horizontal); Mounting Type: Flush-mounted (inset) in pavement; Load Capacity: Governing case per FAA Engineering Brief 83A: fully loaded A380-800 tyre (59,400 lb / ≈27,000 kg wheel load) imparts ≈24,700 lb (≈11,200 kg) onto the fixture footprint.

Q6What are the electrical requirements for a Runway Centreline Light?

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), 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; Insulation Resistance: ≥ 50 MΩ (megger test, cable-to-ground); Earthing/Grounding: Fixture body and inset base can bonded to airfield earth grid.

Q7What photometric requirements apply to a Runway Centreline Light?

Typical requirements are — Main Beam Intensity (100%): ≥ 10,000 cd (white), ≥ 2,000 cd (red) per ICAO Annex 14 / IEC 61827; Intensity Steps (5-step): 100% / 30% / 10% / 3% / 1% of rated peak intensity; Vertical Beam Spread: Main beam 1°–15° above horizontal (peak ~4°), low-profile inset lens; Horizontal Beam Spread: ± 5° to ± 7.5° either side of runway centreline plane; Directionality: Bi-directional, symmetric intensity in both directions of travel; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures; Chromaticity (White): Within ICAO Annex 14 white boundary (CIE coordinates).

Q8Which standards apply to a Runway Centreline Light?

The main references are ICAO Annex 14 — Centreline light spacing, colours, and photometric requirements; FAA AC 150/5345-46 — Specification for runway centreline 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 Centreline Light be inspected and maintained?

Typical maintenance tasks and intervals are: Photometric Intensity Check (annual); Lens Cleaning & Rubber Deposit Removal (quarterly); Seal & Gasket Inspection (annual); Load Rating & Recess Inspection (annual); Insulation Resistance Test (annual); Alignment & Levelling (semi-annual); Cable & Connector Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Runway Centreline Light faults?

Common symptoms covered are: Single Fixture Dark, Rest of Circuit Normal; Entire Series Circuit Dark / CCR Will Not Regulate; CCR Trips on Overcurrent or Ground Fault; Reduced, Uneven, or Colour-Shifted Light Output; Fixture Flickering or Intermittent; Fixture Not Flush, Cracked Top, or Water Pooling in Recess. For example, for "Single Fixture Dark, Rest of Circuit Normal": Likely Cause: Failed LED module/lamp, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding) at that 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/lamp if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before lowering the fixture back into the can.

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