AGL Component Library By Precision AGL Academy

Lead-on Light

A specialized taxiway centreline light that provides colour-coded guidance to pilots transitioning from a taxiway onto the runway. Lead-on lights form a single row of in-pavement fixtures approaching the runway holding position, alternately green and yellow once the centreline crosses onto the runway, guiding the pilot to the correct entry point and take-off position.

Lead-on Light

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Overview

What Is It?

A Lead-on Light is the length of taxiway centreline lighting, coloured alternately green and yellow, that runs along the taxiway centreline where it crosses onto the runway at an entry point or intersection departure position. It is the same L-852D-type in-pavement fixture used for ordinary green taxiway centreline lighting, laid as a single row — the yellow segments mark the portion of the path that is already, functionally, on the runway. Lead-on lights are essential for ensuring that aircraft are properly aligned with the runway centreline before beginning their take-off roll, particularly during low visibility operations.

Purpose

Purpose & Function

The lead-on light exists to ensure an aircraft is precisely aligned with the runway centreline before takeoff power is applied, a requirement that becomes far harder to judge visually at night or in low-visibility conditions when the pilot is transitioning from a taxiway onto the runway. The colour itself carries the guidance: yellow tells the pilot the centreline they are tracking has crossed onto the runway, giving an intuitive cue to line up rather than requiring them to estimate alignment from taxiway markings alone. Getting this alignment right before the takeoff roll begins matters because correcting a misaligned aircraft after power is applied and the aircraft is accelerating is far more difficult and time-critical than correcting it while still taxiing at low speed.

Application

Where Is It Used?

Lead-on lights are installed at runway holding positions where taxiways intersect the runway. They are used on:

  • Precision approach runways (CAT II and III) where accurate alignment is critical
  • Busy airports with complex taxiway layouts and multiple runway entry points
  • Runway intersections where taxiways enter the runway at an angle
  • Low visibility operations where visual guidance is essential
  • Military airfields requiring rapid and accurate aircraft positioning
Placement

Installation & Location

Fixtures are installed as a single row on the taxiway centreline where it crosses the runway holding position and continues onto the runway, with the final light positioned at or just before the point the aircraft lines up for departure. Each light mounts on an L-852 base can recessed flush with the pavement, fed by cable run in pavement ducting back to the taxiway lighting circuit on a dedicated isolating transformer tap so the lead-on sequence can be controlled or intensity-stepped independently of the general taxiway lighting. Fixtures on the runway side of the holding position show yellow, reinforcing to the pilot that they are in the transition zone on the runway rather than on ordinary taxiway alignment. Placement is coordinated with the holding position location and the runway entry geometry so the row of lights delivers the aircraft onto the runway centreline at the correct heading for departure.

Function

How Does It Work?

Lead-on lights operate as part of the taxiway and runway guidance system:

  • Installation: Lead-on lights form a single row on the taxiway centreline, typically at 15-30 metre intervals leading to the runway.
  • Lighting: The lights are typically green or yellow, providing directional guidance to the pilot. The lights may be steady burning or flashing, depending on the application.
  • Guidance: The switch to yellow along the centreline guides the pilot to align the aircraft with the runway centreline.
  • Integration: Lead-on lights are integrated with stop bar lights, runway guard lights, and other taxiway guidance systems.
Architecture

System Architecture & Control Logic

Lead-on lights sit on the same kind of loop-level architecture as the rest of the taxiway lighting circuit: an Airfield Lighting Control and Monitoring System (ALCMS) selects the intensity step, a CCR regulates the whole series loop to the corresponding fixed current, and every fixture on that loop — the whole row of lead-on lights, via their own isolating transformers — burns at the same intensity together. There is no per-fixture dimming; the yellow/green colour split comes from the lamp or filter fitted to each fixture, not from any independent control of individual lights. The distinguishing piece of control logic for lead-on lights is the stop bar interlock: where a lead-on light run leads up to a runway-holding position protected by a stop bar, the ALCMS suppresses the lead-on command whenever that stop bar is illuminated red, so a pilot is never shown a "proceed" cue while still required to hold. Only when the stop bar is selectively switched off to clear the aircraft does the interlock release, and the lead-on lights energize to guide the aircraft on to the runway. This interlock is implemented in the control system logic rather than in the fixture itself, so it applies uniformly to the whole lead-on run regardless of which CCR loop feeds it.

ALCMS Selects intensity step + stop bar interlock logic CCR Regulates loop to fixed current step Series Circuit Loop Yellow + green fixtures on the same loop current Row — Yellow Segment Via own transformer Row — Green Segment Via own transformer Stop Bar Illuminated? Yes → lead-on command suppressed Loop-Level Control, Gated by Stop Bar Interlock Interlock releases only once the stop bar is switched off to clear the aircraft
Guidance Logic

Circuit & Colour-Transition Overview

CCR Series Circuit Isolating Transformer One per fixture · 45W/65W Taxiway Centreline — Single Row, 15–30m Spacing Holding Position / Runway Edge Green — approaching taxiway Yellow — on the runway Aircraft
Series circuit path
Green fixture — taxiway side
Yellow fixture — runway side
Construction

Physical Construction

The fixture body is typically a die-cast aluminium alloy housing, machined and anodised or powder-coated for corrosion resistance against de-icing fluids, fuel spillage, and UV exposure. The green (and where fitted, yellow) lens is a borosilicate glass or high-strength polycarbonate prism, gasket-sealed to the housing with an O-ring or silicone seal to achieve an IP67/IP68 rating against water and dust ingress, and shaped to project a uni- or bi-directional beam towards the approaching aircraft. Elevated units bolt to a frangible coupling engineered to shear cleanly under aircraft impact loads, seated on an L-867 base can set flush with the surrounding grade; flush-mounted (inset) units instead seat directly into an L-868 base can recessed into the pavement, with the top surface load-rated for aircraft wheel loading of up to 100,000 kg. Internal wiring terminates at L-823 primary connectors, sealed splice connectors rated for direct burial and continuous immersion, which mate to the secondary leads of the isolating transformer housed in its own base can nearby. Stainless-steel fasteners are used throughout to resist corrosion, 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 (green or yellow)
ColourGreen (taxiway side), transitioning to Yellow (on the runway)
IntensityControlled by CCR (typically 5-step)
Beam PatternUni-directional or bi-directional towards approaching aircraft
Spacing15-30 metre intervals along taxiway centreline
Mounting TypeFlush-mounted (inset) or elevated
Load Capacity100,000 kg (220,000 lbs) wheel load
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 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 (Green, 100%)≥ 20–150 cd per FAA AC 150/5345-46 Table 1 (applicable L-852 curved/wide-beam class) / IEC TS 61827
Main Beam Intensity (Yellow, 100%)≥ 20–150 cd per FAA AC 150/5345-46 Table 1 (applicable L-852 curved/wide-beam class) / IEC TS 61827
Intensity Steps (5-step)100% / 30% / 10% / 3% / 1% of rated peak intensity
Vertical Beam SpreadMain beam 2°–15° above horizontal (peak ~3°–4°)
Horizontal Beam Spread± 5° to ± 7.5° either side of the taxiway centreline, uni- or bi-directional per installation
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 Table 1 figures
Chromaticity (Green)Within ICAO Annex 14 green boundary (CIE coordinates)
Chromaticity (Yellow)Within ICAO Annex 14 yellow boundary (CIE coordinates)
DirectionalityAimed to guide approaching aircraft toward the runway along the taxiway centreline
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

Lead-on light requirements and installation standards

FAA AC 150/5345-46

Specification for Runway and Taxiway Light Fixtures (L-852D taxiway centreline, alternating green/yellow option)

IEC TS 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 L-867 (elevated) or L-868 (inset) base can, holding the can top flush and level within the taxiway centreline surface tolerance.

Drainage Provision
Civil

Provide a weep hole or drainage path at the base can to prevent water pooling around the transformer and cable entry, especially on flush-mounted installations.

Duct & Cable Route
Electrical

Lay the series circuit duct/cable route to design depth and separation from other services, 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 fully submersible-rated before backfill or reinstatement of the base can.

Isolating Transformer Matching
Electrical

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

Frangible Coupling / Flush-Fit Fixing
Mechanical

For elevated units, torque the frangible coupling to the specified value so it shears cleanly under lateral load; for inset units, torque the fixing bolts and seal the rim so the fixture sits flush and load-bearing.

Beam Orientation & Aim Setting
Mechanical

Orient the lens so the beam projects towards the approaching aircraft along the centreline, checking elevation and aim against the design diagram before final fixing.

Pre-Energisation Sign-off
Documentation

Record base can position, cable route, connector seal, and torque values 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 and LED driver primary wiring before energisation, confirming insulation resistance clears the acceptable minimum.

Loop Continuity Test
Pre-Energisation

Verify circuit continuity end to end, ruling out open circuits or high-resistance splices before the fixture is first powered.

LED Driver Output Verification
Energisation

Confirm the LED driver delivers rated output current and voltage to the array once power is applied.

Photometric Intensity Test
Final Acceptance

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

Alignment & Levelling Verification
Final Acceptance

Confirm the fixture is aimed and levelled to correctly guide the pilot onto the runway along the design path.

CCR/Power Supply Step Response
Energisation

Cycle through available brightness steps and confirm the fixture responds correctly at each.

Frangibility & Base Frame Verification
Pre-Energisation

Confirm the frangible coupling and base frame meet as-built tolerances before the site is finally backfilled.

Documentation & As-Built Sign-off
Final Acceptance

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

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify beam intensity and colour (green or yellow) against ICAO / FAA thresholds using a calibrated photometer; degraded output usually points to lens contamination or an ageing LED array.

Lens Cleaning
Quarterly

Clean rubber deposits and de-icing fluid residue from the lens with approved solvents and soft brushes so beam shape and colour stay within spec.

LED Driver Inspection
Annual

Check the LED driver for signs of thermal stress or surge damage and replace on schedule, since driver failure is a common cause of a dark or flickering fixture.

Alignment & Levelling
Semi-annual

Confirm fixture aim remains within tolerance using a digital level or alignment jig so the beam stays correctly oriented along the approach path for approaching aircraft.

Seal & Gasket Inspection
Annual

Check housing O-rings and gaskets for cracking or compression set to maintain the fixture's IP67/IP68 rating against moisture ingress.

Insulation Resistance Test
Annual

Megger-test the isolating 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.

Base Frame & Pavement Inspection
Annual

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

Field Notes

Common Field Issues

Lens Contamination

Lead-on lights are exposed to rubber deposits from aircraft tyres and de-icing fluids. Regular cleaning with approved solvents and soft brushes is required to maintain light output and visibility.

Misalignment

Lead-on lights can become misaligned due to pavement settlement or impact damage, shifting the beam off the approach path and reducing guidance effectiveness. Regular alignment checks using a digital level or specialized alignment jig are recommended.

LED Driver Failure

LED drivers in lead-on 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

Single Fixture Dark, Rest of Circuit Normal
Likely Cause
Failed LED driver or LED array, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding).
Diagnostic Steps
Confirm series loop continuity is unbroken through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised.
Corrective Action
Replace the LED driver/array if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before backfill.
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 fixture or connector has degraded insulation resistance, creating a short or a partial ground fault on the series loop.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect fixtures for cracked gaskets, condensation, or damaged secondary cable jackets.
Corrective Action
Dry out or replace the affected fixture/connector, renew O-rings and gaskets, and confirm insulation resistance is back above the acceptable minimum before re-energising.
Reduced or Uneven Light Output
Likely Cause
Rubber deposits, tyre debris, or de-icing fluid residue built up on the lens is blocking or scattering light output.
Diagnostic Steps
Visually inspect the lens for contamination; run a photometric intensity check against ICAO/FAA thresholds to quantify the loss.
Corrective Action
Clean the lens with approved solvents and a soft brush; re-verify intensity with a follow-up photometric reading.
Fixture Aim Misaligned
Likely Cause
Pavement settlement or impact damage has shifted the fixture's aim off the designed approach path.
Diagnostic Steps
Check fixture aim against the design angle using a digital level or alignment jig; inspect the flush-mounted frame and surrounding pavement for settlement or cracking.
Corrective Action
Re-align the fixture to the specified beam angle and address any frame or subgrade settlement to prevent recurrence.
Fixture Flickering or Intermittent
Likely Cause
Loose or corroded primary/secondary crimp connections, or an LED driver cycling under thermal stress.
Diagnostic Steps
Inspect and re-torque all cable connections at the fixture base can; check for corrosion on crimps; monitor driver output and temperature once the CCR has warmed up.
Corrective Action
Re-terminate corroded connections with new crimps and sealant, or replace the LED driver if thermal cycling is confirmed under load.
Reliability

Failure Modes & Root Causes

LED Driver Failure
High Severity
Root Cause
Thermal cycling stress inside the driver housing, moisture ingress through a compromised seal, or ordinary end-of-life drift in the driver's output regulation.
Effect
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 leading to insulation breakdown, a manufacturing defect in the winding, or a blown primary fuse-wire link from a transient surge.
Effect
Open-circuit point in the series loop; can darken the single fixture or, if the open extends to the loop itself, take down the entire circuit.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
L-823 Connector / Splice Degradation
Medium Severity
Root Cause
Improper seating or crimping during installation, gasket failure allowing groundwater ingress, or corrosion building up on the pins over time.
Effect
Intermittent operation, flickering, or a partial ground fault that degrades circuit insulation resistance.
Detection Method
Insulation resistance (megger) testing of the circuit and visual inspection of connectors at the fixture base can during maintenance.
Series Cable Insulation Breakdown
High Severity
Root Cause
Cable jacket damage from nearby excavation or rodent activity, age-related insulation degradation, or prolonged standing water in the duct run.
Effect
Ground fault or short circuit that trips the CCR or darkens the entire series loop.
Detection Method
Full-circuit megger test to flag the low-resistance segment, followed by sectionalised testing or time-domain reflectometry to pinpoint the fault location.
Fixture Aim Misalignment / Frame Settlement
Medium Severity
Root Cause
Pavement settlement, impact damage from ground vehicles, or subgrade movement shifting the flush-mounted frame off its designed aim.
Effect
Fixture aim drifts outside tolerance along the approach path, weakening guidance to the flight crew.
Detection Method
Periodic fixture-aim checks using a digital level or alignment jig, and visual inspection of the frame and surrounding pavement for settlement or cracking.
Optical Lens Contamination / Degradation
Low Severity
Root Cause
Rubber deposits from aircraft tyres, de-icing fluid residue, and abrasive particulate erosion accumulating on the flush-mounted lens.
Effect
Reduced or uneven light output and an altered beam pattern that can fall below ICAO/FAA photometric thresholds.
Detection Method
Scheduled photometric intensity testing and visual inspection of the lens during quarterly cleaning.
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

Dedicated Circuit Isolation
Electrical Safety

Lead-on lights are typically fed from their own isolating transformer tap so the sequence can be controlled independently; confirm which tap and CCR feeds the fixture before isolating, and verify zero energy before opening a base can or handling connectors.

Holding Position Coordination
Operational

These fixtures guide aircraft toward the runway entry point; work here requires ATC coordination and a NOTAM where lights will be dark, with personnel and vehicles kept clear of the holding position and runway entrance.

Flush Fit & Wheel-Load Tolerance
Mechanical

The inset fixture must sit precisely flush with the pavement; a proud edge or depression becomes a wheel-impact point as aircraft manoeuvre along the row toward the runway.

Yellow Lens Verification
Compliance

Confirm the yellow lens is correctly fitted and distinct from the green taxiway centreline lenses further back along the taxi route, since a mismatched colour blurs the transition-zone cue the lead-on system relies on.

Insulation Test Before Re-Energisation
Electrical Safety

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

Restore to Compliant State
Compliance

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

Field Insight

Engineering & Expert Notes

Lens Colour Drift Is Easy to Miss at Night
Compliance

Yellow lenses that have UV-aged toward a paler, washed-out tone can still pass a casual daylight glance but read ambiguously against green centreline lenses after dark; check lens colour under actual night viewing conditions, not just in daylight during walkdowns.

Colour Transition Point Matters as Much as Individual Fixtures
Design

Lead-on lights work by the point where the row switches from green to yellow, cueing the pilot that they've reached the runway; a single fixture can test within spec yet still misplace that cue if its position has drifted relative to the holding position marking, so check the transition point against the design layout, not just each unit in isolation.

Flushness Degrades Gradually Under Wheel Loading
Mechanical

Repeated wheel loading at the pavement interface can settle an inset fixture below flush over time, well before any visible cracking appears. Include a flushness check with a straightedge in routine inspections rather than waiting for a reported "bump."

Confirm the Feed Before Assuming Sequencing Control
Electrical

Because lead-on lights are often tapped separately so their sequence can be controlled independently from the rest of the taxiway circuit, don't assume which transformer or CCR feeds a given fixture from as-built drawings alone; field-verify the tap before isolating or troubleshooting sequencing complaints.

Inset Housings See More Standing Water Than Elevated Fixtures
Durability

Flush-mounted lead-on housings sit in a pavement low point more often than elevated fixtures nearby, so seals and drainage paths take on a heavier moisture load. Prioritise these units when scheduling gasket and connector inspections rather than treating all inset fixtures on a loop as equal risk.

Log Insulation Readings to Catch Slow Faults
Troubleshooting

A degrading connector at an inset fixture usually shows up first as a gradual decline in loop insulation resistance rather than an abrupt fault; trend megger readings across maintenance visits so a failing splice is caught before it darkens the row.

Quick Answers

Frequently Asked Questions

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

Q1What is a Lead-on Light?

A Lead-on Light is the length of taxiway centreline lighting, coloured alternately green and yellow, that runs along the taxiway centreline where it crosses onto the runway at an entry point or intersection departure position. It is the same L-852D-type in-pavement fixture used for ordinary green taxiway centreline lighting, laid as a single row — the yellow segments mark the portion of the path that is already, functionally, on the runway. Lead-on lights are essential for ensuring that aircraft are properly aligned with the runway centreline before beginning their take-off roll, particularly during low visibility operations.

Q2What is the purpose of a Lead-on Light?

The lead-on light exists to ensure an aircraft is precisely aligned with the runway centreline before takeoff power is applied, a requirement that becomes far harder to judge visually at night or in low-visibility conditions when the pilot is transitioning from a taxiway onto the runway. The colour itself carries the guidance: yellow tells the pilot the centreline they are tracking has crossed onto the runway, giving an intuitive cue to line up rather than requiring them to estimate alignment from taxiway markings alone.

Q3Where is a Lead-on Light used and installed?

Lead-on lights are installed at runway holding positions where taxiways intersect the runway. They are used on: Precision approach runways (CAT II and III) where accurate alignment is critical Busy airports with complex taxiway layouts and multiple runway entry points Runway intersections where taxiways enter the runway at an angle Low visibility operations where visual guidance is essential Military airfields requiring rapid and accurate aircraft positioning.

Q4How does a Lead-on Light work?

Lead-on lights operate as part of the taxiway and runway guidance system: Installation: Lead-on lights form a single row on the taxiway centreline, typically at 15-30 metre intervals leading to the runway. Lighting: The lights are typically green or yellow, providing directional guidance to the pilot. The lights may be steady burning or flashing, depending on the application. Guidance: The switch to yellow along the centreline guides the pilot to align the aircraft with the runway centreline. Integration: Lead-on lights are integrated with stop bar lights, runway guard lights, and other taxiway guidance systems.

Q5What are the typical technical parameters of a Lead-on Light?

Typical values are — Light Source: LED array (green or yellow); Colour: Green (taxiway side), transitioning to Yellow (on the runway); Intensity: Controlled by CCR (typically 5-step); Beam Pattern: Uni-directional or bi-directional towards approaching aircraft; Spacing: 15-30 metre intervals along taxiway centreline; Mounting Type: Flush-mounted (inset) or elevated; Load Capacity: 100,000 kg (220,000 lbs) wheel load; Isolating Transformer: 45W / 65W (6.6A series circuit); Protection Class: IP67 / IP68 (submersible).

Q6What are the electrical requirements for a Lead-on 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 base can bonded to airfield earth grid.

Q7What photometric requirements apply to a Lead-on Light?

Typical requirements are — Main Beam Intensity (Green, 100%): ≥ 20–150 cd per FAA AC 150/5345-46 Table 1 (applicable L-852 curved/wide-beam class) / IEC TS 61827; Main Beam Intensity (Yellow, 100%): ≥ 20–150 cd per FAA AC 150/5345-46 Table 1 (applicable L-852 curved/wide-beam class) / IEC TS 61827; Intensity Steps (5-step): 100% / 30% / 10% / 3% / 1% of rated peak intensity; Vertical Beam Spread: Main beam 2°–15° above horizontal (peak ~3°–4°); Horizontal Beam Spread: ± 5° to ± 7.5° either side of the taxiway centreline, uni- or bi-directional per installation; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 Table 1 figures.

Q8Which standards apply to a Lead-on Light?

The main references are ICAO Annex 14 — Lead-on light requirements and installation standards; FAA AC 150/5345-46 — Specification for Runway and Taxiway Light Fixtures (L-852D taxiway centreline, alternating green/yellow option); IEC TS 61827 — Electrical and photometric performance for AGL luminaires; FAA AC 150/5345-53 — Airport Lighting Equipment Certification Program. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should a Lead-on Light be inspected and maintained?

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

Q10How do I troubleshoot common Lead-on 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 or Uneven Light Output; Fixture Aim Misaligned; Fixture Flickering or Intermittent. For example, for "Single Fixture Dark, Rest of Circuit Normal": Likely Cause: Failed LED driver or LED array, or an open isolating transformer (blown primary fuse-wire link or failed secondary winding). Diagnostic Steps: Confirm series loop continuity is unbroken through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised. Corrective Action: Replace the LED driver/array if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before backfill.

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