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.
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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 & 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.
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.
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.
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.
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)
Circuit & Beam Overview
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.
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.
Technical Parameters
| Parameter | Typical Value |
|---|---|
| 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) |
Electrical Requirements
| Requirement | Typical Value |
|---|---|
| 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 |
| Fault Protection | CCR-level ground fault and open-circuit detection |
| Power Source | CCR output, regulated per ICAO/FAA intensity step schedule |
Photometric Requirements
| Parameter | Typical 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 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) |
| 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 Method | Mobile photometric van/goniophotometer or fixed test bench per fixture |
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
Installation Requirements
Base Can Excavation & Grade
CivilExcavate 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
CivilProvide 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
ElectricalLay 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
ElectricalTerminate 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
ElectricalConfirm the isolating transformer wattage and ratio match the fixture and the series circuit's rated current step before connection.
Frangible Coupling / Pedestal Fixing
MechanicalTorque 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
MechanicalSet 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
DocumentationRecord base can position, cable route, connector seal, and torque values as-built before backfill, since these are not inspectable once the site is closed.
Testing & Commissioning
Insulation Resistance (Megger) Test
Pre-EnergisationMegger-test the isolating transformer and series loop before the circuit is energised, confirming insulation resistance clears the acceptable minimum.
Loop Continuity & Resistance Test
Pre-EnergisationVerify 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
EnergisationWith 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 AcceptanceMeasure beam intensity with a calibrated photometer against ICAO/FAA thresholds before the fixture is handed over.
Mounting Height & Alignment Verification
Final AcceptanceConfirm 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-EnergisationConfirm the frangible coupling shears at the correct load and the pole/pedestal is stable before the site is finally backfilled.
CCR Brightness Step Response
EnergisationCycle the CCR through every intensity step and confirm the fixture responds correctly at each.
Documentation & As-Built Sign-off
Final AcceptanceRecord insulation, continuity, voltage, and photometric readings alongside as-built position in the commissioning dossier for handover.
Inspection & Maintenance
Frangible Coupling Check
AnnualInspect 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
AnnualClean 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
AnnualInspect the base cable gland and seals for wear, and re-torque the base connection to prevent moisture ingress and internal corrosion.
Photometric Intensity Check
AnnualMeasure 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
AnnualMegger-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-annualVerify 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
AnnualCheck the mounting stake or pedestal for looseness, corrosion, or settlement in surrounding ground that could tilt the fixture or compromise frangibility.
Vegetation & Debris Clearance
QuarterlyClear grass, snow, or debris around the base so the beam is unobstructed and the frangible coupling stays accessible for inspection.
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.
Troubleshooting Guide
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
Failure Modes & Root Causes
LED Module / Lamp Failure
Isolating Transformer Winding Failure
Frangible Coupling Fatigue / Fracture
Premature Coupling Shear
Base Seal / Cable Gland Failure
Prism Contamination or Aim Drift
Pole / Pedestal Mounting Settlement
CCR Regulation Fault
Safety & Operational Notes
Series Circuit Isolation
Electrical SafetyElevated 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
OperationalAny 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
MechanicalNever 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 SafetyAllow 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
OperationalBecause 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 SafetyAfter 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
ComplianceDo 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.
Engineering & Expert Notes
LED Retrofit Step Matching
RetrofitWhen 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
ElectricalReusing 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
MechanicalUV 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
DesignWhere 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
TroubleshootingBecause 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
DurabilityRepeated 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.
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.
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Please read before relying on any content on this page.
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