AGL Component Library By Precision AGL Academy

Elevated Runway Edge Light

The most common runway edge light configuration, mounted on frangible poles or base plates above the runway shoulder. Provides high visibility and precise beam control for all weather operations, with a breakaway design to protect aircraft on impact.

Elevated runway edge light fixture on frangible coupling (L-861 type)

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

Overview

What Is It?

An Elevated Runway Edge Light is a visual aid mounted on a small pole or pedestal above the runway surface (typically 300–500 mm high). It is the standard configuration for runways where the shoulder is soft (grass or gravel) or where a raised light offers the best optical performance. The fixture includes a frangible coupling that shears on impact, reducing the risk of damage to an aircraft that veers off the runway. Elevated lights are used on both precision and non-precision runways, with white or yellow (last 600 m / 2,000 ft) beam outputs.

Purpose

Purpose & Function

The elevated configuration exists because raising the light head above grade generally gives the best possible optical performance for edge delineation, projecting a cleaner, more visible beam to an approaching or departing pilot than a flush fixture can achieve, and it is the default choice wherever the shoulder surface allows it. This benefit only holds where an aircraft veering off the paved surface won't be put at greater risk by striking the fixture, which is why the elevated light is fitted with a frangible coupling engineered to shear at a controlled, predetermined force: the design deliberately trades fixture survivability for aircraft safety in an off-runway excursion. Consequently, the elevated light's role is to be used wherever soft shoulders (grass, gravel) or unconstrained ground clearance make its superior optical output and frangible safety behaviour the right combination, reserving the inset alternative for surfaces where an elevated stem would itself be the hazard.

Application

Where Is It Used?

Installed on the runway shoulders, typically 1–3 metres outside the paved edge, at regular intervals (60 m / 200 ft for CAT I and above, up to 100 m / 300 ft for non-precision). Used on all airfields with grass, gravel, or compacted soil shoulders where an inset fixture is not feasible. Also common on taxiway edges and as standalone approach lighting support structures.

Placement

Installation & Location

Fixtures are set out along both runway edges at the design spacing, positioned on the shoulder just outside the paved surface and clear of the graded runway strip's load-bearing requirements. Each stem mounts on a frangible coupling atop an L-867 base can set flush with grade, with overall fitting height kept within the obstacle-limitation surface for the runway category so the raised head never intrudes on the clearance envelope. The base can is fed by armoured cable run in a trench back to the isolating transformer pit, with the transformer housed in its own secondary base can adjacent to the fixture to keep the series-circuit joint clear of standing water. Setting-out is tied to the runway centreline survey so the edge line stays parallel and true along the full runway length, and elevated fixtures are typically substituted with inset units within the runway end safety area, blast pads, and other zones where a raised obstacle cannot be tolerated.

Function

How Does It Work?

Each elevated light is powered from the series circuit via an isolating transformer buried near the fixture. The lamp or LED module projects light through a precision prism and lens assembly to create the required beam pattern (symmetric or asymmetric, depending on installation orientation). The intensity is controlled by the CCR's current steps. The frangible coupling is designed to break at a predetermined shear force (typically 250–450 kg), allowing the light head to detach cleanly without causing significant damage to an aircraft's wing or engine.

Architecture

System Architecture & Control Logic

Elevated runway edge lights are not individually addressable — control is exercised at the loop level through the constant current series circuit. An Airfield Lighting Control and Monitoring System (ALCMS), operated by the tower or an automated visibility-linked routine, selects the required brightness step based on prevailing RVR, ATC instruction, or (at smaller aerodromes) pilot-controlled lighting input. This command is passed to the CCR, which regulates the entire loop to the corresponding fixed current (one of 5 steps between 2.8A and 6.6A). Every fixture on that loop, via its own isolating transformer, draws from the same current and therefore burns at the same intensity simultaneously — there is no way to dim or brighten a single fixture independently of the rest of the circuit. Fault detection is likewise 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 rather than pinpointed to an exact fixture without further sectionalised testing. Because the elevated fitting sits on a frangible coupling, a sheared coupling looks electrically identical to any other open-circuit fault on the loop — the ALCMS reports it the same way, and only a field inspection confirms whether the cause was impact damage or a failed component.

ALCMS → CCR → Series Circuit Loop → Isolating Transformer → Elevated Fixture (with loop-level feedback)

AIRFIELD LIGHTING CONTROL SYSTEM (ALCMS) Selects brightness step (RVR / ATC / PCL) CONSTANT CURRENT REGULATOR Converts step command to fixed current SERIES CIRCUIT LOOP Same current for every fixture — no individual control ISOLATING TRANSFORMER (PER FIXTURE) Taps fixed loop current to fixture secondary ELEVATED FIXTURE (FRANGIBLE) Emits beam at the commanded intensity step LOOP-LEVEL CONTROL — NOT PER-FIXTURE All fixtures on a loop switch and dim together A sheared coupling reads as an open-circuit loop fault 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 2.8A – 6.6A series bus ISOLATING TRANSFORMER 45W / 65W, buried at fixture FRANGIBLE COUPLING Shears at 250–450 kg ELEVATED LIGHT HEAD (LED / HALOGEN) Prism & lens assembly BEAM PROJECTED TO PILOT 3°V x 6°H sym. / asym. BREAKAWAY EVENT — AIRCRAFT / VEHICLE IMPACT IMPACT FORCE APPLIED TO LIGHT HEAD e.g. snowplow, wingtip contact COUPLING SHEARS CLEANLY Predetermined shear point LIGHT HEAD DETACHES FROM BASE Minimises impact to aircraft TRANSFORMER & SERIES CIRCUIT REMAIN INTACT Buried below shear point — no circuit disruption Note: the coupling is designed to fail before load reaches the fixture base, keeping the buried transformer and series cable undamaged.

Top row: normal power and beam path from the CCR through to the projected beam. Bottom row: the frangible-coupling breakaway sequence that occurs on aircraft or ground-vehicle contact, isolating the mechanical failure at the fixture head while the buried transformer and series circuit continue operating undisturbed.

Construction

Physical Construction

The fixture head is a die-cast aluminium alloy housing, anodised or powder-coated for corrosion resistance, mounted atop a short stem or pedestal (typically 300–500 mm) that raises the optics clear of grass or gravel shoulders for a cleaner beam path. The optical assembly sits under a borosilicate glass or high-strength polycarbonate prism, gasket-sealed to the housing with an O-ring or silicone seal for an IP67/IP68 rating against rain, dust, and fuel exposure. The stem attaches to the base through a frangible coupling, an aluminium or composite fitting engineered to shear cleanly at a defined load if struck by an aircraft, wheel, or ground vehicle, minimising damage to both the aircraft and the fixture's electrical connections below the break point. The coupling in turn seats on an L-867 base can set flush with the surrounding grade. Internal wiring terminates at L-823 primary connectors, sealed for direct burial and continuous immersion, mating to the isolating transformer's secondary in an adjacent base can, with stainless-steel fasteners used throughout and a drainage provision in the base can to keep the connector joint clear of standing water.

Specification

Technical Parameters

ParameterTypical Value
Mounting Height300–500 mm above ground (pole / pedestal)
Light SourceLED array or 50W / 100W halogen
ColourWhite (full runway), Yellow (last 600m / 2,000ft on CAT II/III)
Intensity Steps5-step (2.8A – 6.6A) CCR controlled
Beam PatternSymmetric (3° vertical x 6° horizontal) or asymmetric for approach
Frangible CouplingShear force 250–450 kg (breakaway design)
Isolating Transformer45W / 65W (6.6A series circuit)
Protection ClassIP67 / IP68 (hermetically sealed)
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, stem, 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 (100%)≥ 10,000 cd (white), ≥ 5,000 cd (yellow) per ICAO Annex 14 / IEC 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 runway centreline plane
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures
Chromaticity (White)Within ICAO Annex 14 white boundary (CIE coordinates)
Chromaticity (Yellow)Within ICAO Annex 14 yellow 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

Elevated light mounting heights, colours, and spacing requirements

FAA AC 150/5345-46F

Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures (covers elevated L-861-type fixtures; supersedes -46E)

IEC 61827

Electrical and photometric characteristics for inset and elevated AGL luminaires

FAA AC 150/5345-53

Airport Lighting Equipment Certification Program — qualified fixture listing

Prerequisites

Installation Requirements

Base Can Excavation & Grade
Civil

Excavate and compact the sub-grade to design depth before setting the L-867 base can, holding the can top flush with the surrounding grade so the pedestal rises to the correct mounting height.

Drainage Provision
Civil

Provide a weep hole or drainage path at the base can to prevent water pooling around the transformer and cable entry beneath the pedestal.

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 / Pedestal Fixing
Mechanical

Torque the frangible coupling and pedestal fixing bolts to the specified value, checking the fitting shears cleanly under lateral load and does not bind before the stem is loaded.

Mounting Height & Aim Setting
Mechanical

Set the pedestal height and beam aim (elevation and azimuth) against the design aiming diagram, keeping the fixture within the frangibility height limit above grade.

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 (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 Intensity Test
Final Acceptance

Measure beam intensity with a calibrated photometer against ICAO/FAA thresholds before the fixture is handed over.

Mounting Height & Alignment Verification
Final Acceptance

Confirm fixture height and aim match the design elevation profile so the beam clears obstacles and stays within the aiming tolerance.

Frangible Coupling & Pole Stability Check
Pre-Energisation

Confirm the frangible coupling shears at the correct load and the pole/pedestal is stable before the site is finally backfilled.

CCR Brightness Step Response
Energisation

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

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

Frangible Coupling Check
Annual

Inspect the coupling for cracking, corrosion, or shear fatigue and replace on schedule (or after any plough/impact event) to keep breakaway force within the 250–450 kg design range.

Lens & Prism Cleaning
Annual

Clean dust, mud, and bird droppings off the optical prism with an optics-safe solution so beam intensity and shape stay within photometric spec.

Cable Gland & Base Seal Check
Annual

Inspect the base cable gland and seals for wear, and re-torque the base connection to prevent moisture ingress and internal corrosion.

Photometric Intensity Check
Annual

Measure beam intensity and colour with a calibrated photometer against ICAO / FAA thresholds; a shortfall usually traces back to lens contamination or LED ageing.

Insulation Resistance Test
Annual

Megger-test the isolating transformer and series circuit to confirm insulation resistance stays above minimum, catching moisture ingress before it trips the series circuit.

Mounting Height & Alignment
Semi-annual

Verify the fixture sits at the correct 300–500 mm mounting height and beam aim remains within tolerance for the approach and runway path.

Pole / Pedestal Stability
Annual

Check the mounting stake or pedestal for looseness, corrosion, or settlement in surrounding ground that could tilt the fixture or compromise frangibility.

Vegetation & Debris Clearance
Quarterly

Clear grass, snow, or debris around the base so the beam is unobstructed and the frangible coupling stays accessible for inspection.

Field Notes

Common Field Issues

Frangible Coupling Fatigue

Repeated snowplow impacts or vibration from nearby aircraft can weaken the frangible coupling. It is recommended to replace couplings every 5 years or after any significant impact event to ensure breakaway performance.

Prism / Lens Contamination

Elevated fixtures are exposed to dust, mud, and bird droppings. Annual cleaning with approved optics-safe solutions is necessary to maintain photometric performance and avoid intensity degradation.

Moisture Ingress via Cable Gland

Water ingress through the base cable gland is a common failure point. Periodic inspection of gland seals and re-torquing of the base connection can prevent internal corrosion and short circuits.

Diagnostics

Troubleshooting Guide

Single Fixture Dark, Rest of Circuit Normal
Likely Cause
Failed LED module/lamp, or an open isolating transformer (blown primary link or failed secondary winding) inside the pole base.
Diagnostic Steps
Confirm series loop continuity is unbroken through the transformer primary; megger the transformer; check secondary voltage at the base 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 base cable gland before closing up the pole.
Entire Series Circuit Dark / CCR Will Not Regulate
Likely Cause
Open-circuit fault in the series loop, often at a sheared frangible coupling that has also parted the internal cable connection.
Diagnostic Steps
Check the CCR fault/open-circuit indication first; walk the row for any leaning, missing, or knocked-over fixtures; loop-resistance test to isolate the faulted segment.
Corrective Action
Replace the sheared coupling and reconnect the internal cable, or repair the faulted cable section; re-test insulation resistance before reinstating the circuit.
CCR Trips on Overcurrent or Ground Fault
Likely Cause
Moisture ingress through a worn cable gland or base seal has degraded insulation resistance, creating a short or partial ground fault.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect fixtures for a loose gland, cracked base seal, or condensation inside the pole.
Corrective Action
Dry out or replace the affected fixture, renew the gland seal and re-torque the base connection, and confirm insulation resistance is back above minimum before re-energising.
Reduced or Uneven Light Output
Likely Cause
Prism contaminated with dust, mud, or bird droppings; an ageing LED array; or the fixture aim drifted off tolerance.
Diagnostic Steps
Run a photometric intensity check against ICAO/FAA thresholds; inspect and clean the prism with an optics-safe solution; verify beam aim against the approach/runway path.
Corrective Action
Clean the prism, replace a degraded LED module, or re-aim the fixture; re-verify with a follow-up photometric reading.
Fixture Leaning, Loose, or Height Out of Tolerance
Likely Cause
Frangible coupling has begun to fatigue or partially shear, or the pole/pedestal mounting has loosened or settled in the surrounding ground.
Diagnostic Steps
Check the coupling for cracking, corrosion, or play; measure mounting height against the 300–500 mm design range; inspect the base for settlement or corrosion.
Corrective Action
Replace the coupling if fatigued, re-level and re-set the fixture to correct height, and address any base or subgrade settlement to prevent recurrence.
Coupling Shears Below Expected Impact Force
Likely Cause
Coupling material has become brittle from age, weather exposure, or accumulated micro-fractures from repeated low-level impacts, dropping breakaway force below the 250–450 kg design range.
Diagnostic Steps
Examine the sheared coupling face for corrosion or fatigue striations; review the fixture's service history and last replacement date; check nearby fixtures for similar ageing.
Corrective Action
Fit a new coupling to design spec, and bring forward the replacement interval for other couplings from the same batch or installation date.
Reliability

Failure Modes & Root Causes

LED Module / Lamp Failure
High Severity
Root Cause
Solder-joint fatigue from thermal cycling, moisture ingress at the LED board 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 base connector.
Isolating Transformer Winding Failure
High Severity
Root Cause
Moisture ingress into the pole base leading to insulation breakdown, a manufacturing winding defect, or a blown primary 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.
Frangible Coupling Fatigue / Fracture
High Severity
Root Cause
Cyclic loading from vehicle or plough contact, material fatigue over the service interval, or corrosion at the coupling threads.
Effect
Fixture leans, loosens, or shears off entirely, often parting the internal cable connection and taking down the full series loop.
Detection Method
Physical inspection of the coupling for cracking, corrosion, or play, and a walk of the row to spot any leaning or knocked-over fixtures.
Premature Coupling Shear
Medium Severity
Root Cause
Coupling material has become brittle from age, weather exposure, or accumulated micro-fractures, dropping the breakaway force below the 250–450 kg design range.
Effect
Coupling shears under lighter-than-intended contact, causing nuisance outages and unplanned fixture replacement.
Detection Method
Examination of sheared coupling faces for corrosion or fatigue striations, and a service-history review of the coupling's batch and last replacement date.
Base Seal / Cable Gland Failure
Medium Severity
Root Cause
A worn or loosened cable gland, or a cracked base seal, that lets moisture track into the pole from ground level.
Effect
Degraded insulation resistance producing a short or partial ground fault, and internal corrosion of the base connection.
Detection Method
Full-circuit megger testing to identify the low-resistance segment, and a visual check of the gland and base seal at suspect fixtures.
Prism Contamination or Aim Drift
Low Severity
Root Cause
Dust, mud, or bird droppings accumulating on the prism, or gradual aim drift from vibration or minor impacts.
Effect
Reduced or uneven light output and a beam pattern that can fall out of alignment with the approach/runway path.
Detection Method
Photometric intensity testing, visual prism inspection, and a beam-aim check against the design path during scheduled maintenance.
Pole / Pedestal Mounting Settlement
Medium Severity
Root Cause
Loosened mounting hardware, or the surrounding ground settling due to poor sub-grade compaction, frost heave, or drainage failure.
Effect
Fixture height drifts out of the 300–500 mm design range, or the pole leans, both of which push the beam out of tolerance.
Detection Method
Mounting-height measurement against design range, and a visual check of the base and surrounding ground for settlement.
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

Elevated edge 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

Any work on or near an active runway requires ATC/airside coordination and a NOTAM where the fixture will be dark or out of tolerance, with vehicle and personnel movement kept clear of the runway strip.

Frangibility Not to Be Defeated
Mechanical

Never substitute the frangible coupling with a rigid fitting or over-torque it during installation or repair; the coupling must still shear cleanly on aircraft impact to limit damage to an aircraft that veers off the runway.

Hot Lamp / Housing Contact
Personnel Safety

Allow the fixture housing and lamp/LED module to cool before handling after an active period; incandescent units retain significant heat and can cause burns during lens or lamp replacement.

Mower & Ground-Vehicle Strike
Operational

Because the fixture stands 300–500 mm proud of grade, brief mowing and snow-clearance crews on its location and keep the pole height within the design limit so it stays visible and shears rather than becomes a hidden strike hazard.

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 damage healthy fixtures on the same circuit.

Restore to Compliant State
Compliance

Do not leave a fixture out of aim tolerance, leaning, or at reduced intensity after maintenance; verify photometric and positional conformance before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

LED Retrofit Step Matching
Retrofit

When retrofitting an LED head onto an existing elevated stem, check that the fixture's brightness-step curve actually tracks the CCR's current steps the way the original incandescent lamp did; a mismatched curve leaves the edge line looking uneven between steps even though every fixture measures within spec at each step individually.

Size the Transformer to the Load, Not the Legacy Lamp
Electrical

Reusing an isolating transformer sized for the old incandescent wattage on a much lower-draw LED head is a common source of premature transformer failure and nuisance loop trips; re-select VA rating against the actual LED load rather than assuming the existing transformer is close enough.

Frangible Couplings Age, Even Without Impact
Mechanical

UV and thermal cycling can shift the shear characteristics of a composite or aluminium frangible coupling over years of service. A coupling that looks visually fine can no longer shear at its rated load, so periodic torque/shear verification belongs in the overhaul cycle, not just the post-impact inspection.

Balance Loops Sharing One CCR
Design

Where multiple series loops run off a single CCR, unequal loop lengths or lamp counts between loops can produce visibly uneven edge-light brightness runway-to-runway even though each individual fixture tests within photometric tolerance. Balance loop impedance at the design stage, not after commissioning complaints.

A Sheared Coupling Reads the Same as Any Other Open Circuit
Troubleshooting

Because the elevated fitting sits on a frangible coupling, a sheared coupling looks electrically identical to any other open-circuit fault to the CCR and ALCMS — both report as a loop voltage rise at constant current. Don't assume impact damage or a failed lamp from the control-room alert alone; a field inspection is what actually distinguishes the two.

De-Icing Fluid Ages Seals Faster Than UV Alone
Durability

Repeated exposure to glycol-based de-icing fluid degrades gaskets and lens seals faster than sun and weather alone, especially on stems near taxiway/runway intersections that see heavy de-icing traffic. Specify seal materials rated for glycol contact and inspect gasket condition at overhaul, not only at initial install.

Quick Answers

Frequently Asked Questions

Short answers about the Elevated Runway Edge Light (L-861/L-862): what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is an Elevated Runway Edge Light (L-861/L-862)?

An Elevated Runway Edge Light is a visual aid mounted on a small pole or pedestal above the runway surface (typically 300–500 mm high). It is the standard configuration for runways where the shoulder is soft (grass or gravel) or where a raised light offers the best optical performance. The fixture includes a frangible coupling that shears on impact, reducing the risk of damage to an aircraft that veers off the runway. Elevated lights are used on both precision and non-precision runways, with white or yellow (last 600 m / 2,000 ft) beam outputs.

Q2What is the purpose of an Elevated Runway Edge Light (L-861/L-862)?

The elevated configuration exists because raising the light head above grade generally gives the best possible optical performance for edge delineation, projecting a cleaner, more visible beam to an approaching or departing pilot than a flush fixture can achieve, and it is the default choice wherever the shoulder surface allows it.

Q3Where is an Elevated Runway Edge Light (L-861/L-862) used and installed?

Installed on the runway shoulders, typically 1–3 metres outside the paved edge, at regular intervals (60 m / 200 ft for CAT I and above, up to 100 m / 300 ft for non-precision). Used on all airfields with grass, gravel, or compacted soil shoulders where an inset fixture is not feasible. Also common on taxiway edges and as standalone approach lighting support structures.

Q4How does an Elevated Runway Edge Light (L-861/L-862) work?

Each elevated light is powered from the series circuit via an isolating transformer buried near the fixture. The lamp or LED module projects light through a precision prism and lens assembly to create the required beam pattern (symmetric or asymmetric, depending on installation orientation). The intensity is controlled by the CCR's current steps. The frangible coupling is designed to break at a predetermined shear force (typically 250–450 kg), allowing the light head to detach cleanly without causing significant damage to an aircraft's wing or engine.

Q5What are the typical technical parameters of an Elevated Runway Edge Light (L-861/L-862)?

Typical values are — Mounting Height: 300–500 mm above ground (pole / pedestal); Light Source: LED array or 50W / 100W halogen; Colour: White (full runway), Yellow (last 600m / 2,000ft on CAT II/III); Intensity Steps: 5-step (2.8A – 6.6A) CCR controlled; Beam Pattern: Symmetric (3° vertical x 6° horizontal) or asymmetric for approach; Frangible Coupling: Shear force 250–450 kg (breakaway design); Isolating Transformer: 45W / 65W (6.6A series circuit); Protection Class: IP67 / IP68 (hermetically sealed).

Q6What are the electrical requirements for an Elevated Runway Edge Light (L-861/L-862)?

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, stem, and base can bonded to airfield earth grid.

Q7What photometric requirements apply to an Elevated Runway Edge Light (L-861/L-862)?

Typical requirements are — Main Beam Intensity (100%): ≥ 10,000 cd (white), ≥ 5,000 cd (yellow) per ICAO Annex 14 / IEC 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 runway centreline plane; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures; Chromaticity (White): Within ICAO Annex 14 white boundary (CIE coordinates); Chromaticity (Yellow): Within ICAO Annex 14 yellow boundary (CIE coordinates).

Q8Which standards apply to an Elevated Runway Edge Light (L-861/L-862)?

The main references are ICAO Annex 14 — Elevated light mounting heights, colours, and spacing requirements; FAA AC 150/5345-46F — Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures (covers elevated L-861-type fixtures; supersedes -46E); IEC 61827 — Electrical and photometric characteristics for inset and elevated AGL luminaires; FAA AC 150/5345-53 — Airport Lighting Equipment Certification Program — qualified fixture listing. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should an Elevated Runway Edge Light (L-861/L-862) be inspected and maintained?

Typical maintenance tasks and intervals are: Frangible Coupling Check (annual); Lens & Prism Cleaning (annual); Cable Gland & Base Seal Check (annual); Photometric Intensity Check (annual); Insulation Resistance Test (annual); Mounting Height & Alignment (semi-annual); Pole / Pedestal Stability (annual); Vegetation & Debris Clearance (quarterly). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Elevated Runway Edge Light (L-861/L-862) 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 Leaning, Loose, or Height Out of Tolerance; Coupling Shears Below Expected Impact Force. For example, for "Single Fixture Dark, Rest of Circuit Normal": Likely Cause: Failed LED module/lamp, or an open isolating transformer (blown primary link or failed secondary winding) inside the pole base. Diagnostic Steps: Confirm series loop continuity is unbroken through the transformer primary; megger the transformer; check secondary voltage at the base 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 base cable gland before closing up the pole.

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 advice on elevated runway edge light selection or installation?

Precision AGL Academy provides expert guidance on frangible coupling choice, photometric alignment, and field testing.