AGL Component Library By Precision AGL Academy

Bidirectional / Omnidirectional Runway Edge Fixture

A versatile runway edge light that can be configured for either bidirectional (two opposite directions along the runway) or omnidirectional (360°) light distribution. This flexible design adapts to various runway configurations, providing clear edge delineation for pilots regardless of approach direction or aircraft position on the runway.

Bidirectional/Omnidirectional Runway Edge Fixture

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Overview

What Is It?

A Bidirectional/Omnidirectional Runway Edge Fixture is a runway edge light that offers selectable or fixed light distribution patterns to suit different operational requirements. In bidirectional mode, the fixture projects light in two opposite directions along the runway centreline, visible to pilots approaching from either end. In omnidirectional mode, the fixture emits light uniformly in all directions (360°), providing edge visibility from any angle — particularly useful at runway intersections, curved sections, or where aircraft may be positioned at various angles on the runway. This dual‑capability fixture reduces the need for separate inventory of bidirectional and omnidirectional lights, simplifying maintenance and logistics for airfield operators.

Purpose

Purpose & Function

A standard runway edge light assumes pilots only ever approach from one predictable direction and angle; the bidirectional/omnidirectional fixture exists for the geometries where that assumption breaks down. Its purpose is to eliminate the dark or ambiguous edge segments that would otherwise appear wherever a runway is operated from both ends, where taxiways or rapid-exit turns intersect the edge line at an angle, or where a curved section or displaced threshold puts the pilot's viewing angle outside a single fixed beam's coverage. By projecting a correctly coloured beam — white along the runway body, yellow in the final 600 m / 2,000 ft (or half the runway length, whichever is less) on instrument runways — toward every direction from which an aircraft can legitimately approach or occupy that point, the fixture preserves continuous, correctly coded lateral guidance exactly where a single-direction light would leave a gap. This also serves an operational purpose beyond the individual light: because one fixture design covers both bidirectional and omnidirectional roles, airfield operators can standardise on fewer part numbers, simplifying stock holding and reducing the chance of an incorrect fixture being installed at a critical, non-standard location.

Application

Where Is It Used?

This versatile fixture is used on runways where both approach directions are operational, requiring bidirectional visibility, as well as at runway intersections, rapid exit taxiway turnoffs, and curved sections where omnidirectional visibility is beneficial. It is also suitable for runways with displaced thresholds, where edge lights need to be visible from multiple angles. The fixture is available in both elevated (frangible pole) and inset (flush‑mounted) configurations, making it suitable for all runway pavement types. It is used on precision and non‑precision instrument runways, with white light output for the main runway section and yellow (amber) for the last 600 m (2,000 ft), or half the runway length if less, on runways where this caution zone applies.

Placement

Installation & Location

Fixtures are set out along the runway edge at standard spacing using an elevated frangible-mount base can or an inset base can depending on pavement type, positioned no more than 3 m outward from the runway edge and clear of the graded strip's load-bearing width, the same convention as other runway edge lights. Because the fixture must switch from white to yellow over the final 600 m (or half the runway length, whichever is less) on runways where this caution zone applies, setout for that section is tied precisely to the runway centreline survey measured back from the runway end, so the colour transition point lines up exactly across both edge rows rather than drifting between the two sides; cabling and isolating transformer arrangements otherwise follow the standard runway edge lighting series circuit.

Function

How Does It Work?

The fixture contains an optical system that can be configured for bidirectional or omnidirectional output. In bidirectional mode, a precision prism and reflector system directs light into two opposite narrow beams (typically 3° vertical × 6° horizontal each), aligned along the runway centreline. In omnidirectional mode, a diffuse reflector or multifaceted prism spreads the light uniformly in all horizontal directions (360°) with a controlled vertical spread (3°–6°). Some designs allow field‑adjustable optics to switch between modes, while others are fixed at manufacture. The light source is typically a high‑output LED array or halogen lamp, powered by the series circuit via an isolating transformer. Intensity is controlled by the CCR's current steps, with 5‑step (2.8A – 6.6A) operation. The frangible coupling (elevated version) or rugged housing (inset version) ensures safety and durability.

One power path, two optical configurations at the same current

CCR Series Circuit

5-step operation, 2.8A–6.6A

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Isolating Transformer

45W / 65W / 100W, feeds the fixture's LED array or halogen source

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Optical Configuration

Fixed at manufacture, or field-adjustable on some designs

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Bidirectional Mode

Precision prism & reflector split output into two opposite narrow beams (3°V × 6°H each), aligned to the centreline

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Up to 10,000 cd per beam at 6.6A

Omnidirectional Mode

Diffuse reflector or multifaceted prism spreads light 360° horizontally with 3°–6° vertical spread

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Up to 2,000 cd average at 6.6A

Architecture

System Architecture & Control Logic

Control-wise, this fixture behaves exactly like a standard runway edge light — it is not individually addressable, and its optical mode (bidirectional or omnidirectional) has no bearing on how it is controlled. An ALCMS command selects a brightness step, the CCR regulates the entire series circuit loop to the corresponding fixed current, and every fixture on that loop draws the same current through its own isolating transformer and burns at the same intensity at the same moment. Whether a given unit is configured for two opposing narrow beams or a 360° diffuse spread is a fixed (or field-set) property of its internal optics, decided at installation rather than commanded at runtime, so it plays no part in the loop's control logic. A loop fault — an open circuit or a failed transformer — is detected the same way as on any other series circuit, through a voltage rise at the CCR relative to the commanded current, and is reported at the loop level rather than pinned to one fixture without further sectionalised testing.

ALCMS Selects the brightness step for the loop Constant Current Regulator Regulates the entire loop to one fixed current Series Circuit Loop Same current for every fixture on the loop Isolating Transformer (Per Fixture) Taps the fixed loop current to the fixture Fixture (Bidirectional or Omnidirectional Optic) Beam pattern fixed at install — not part of the control loop LOOP-LEVEL CONTROL — NOT PER-FIXTURE Optical mode never changes what the ALCMS actually commands

Bidirectional vs. omnidirectional is an optical configuration decided at install — the control loop treats every fixture on it identically.

Construction

Physical Construction

This fixture is built on the same die-cast aluminium housing platform as a standard runway edge light, but with an optical assembly configured for either a bidirectional or omnidirectional light distribution. Bidirectional units house two separate lamp and lens assemblies within the housing, angled back-to-back so each projects its beam along the runway centreline in opposite directions, with the housing and internal wiring sized to accommodate the additional light source. Omnidirectional units instead use a single light source paired with a specially shaped reflector or diffusing lens that spreads the beam through a full 360° horizontal arc, trading peak beam intensity for all-round visibility. In both configurations, the optical assembly is gasket-sealed behind a hardened glass or polycarbonate lens to achieve an IP67/IP68 rating, and the fixture mounts on the same frangible coupling and L-867 base can, or L-868 inset can, arrangement as a standard edge light. Internal wiring terminates at sealed L-823 connectors feeding the isolating transformer in the base can, and stainless-steel fasteners and corrosion-resistant coatings are used throughout consistent with the rest of the runway edge lighting family.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array or 50W / 100W halogen
ColourWhite (full runway) / Yellow (last 600m or half runway length, whichever less, on instrument runways)
Beam Pattern (Bidirectional)Two opposite beams: 3° vertical x 6° horizontal each
Beam Pattern (Omnidirectional)360° horizontal with 3°–6° vertical spread
Intensity (Max, Bidirectional)Up to 10,000 cd per beam at 6.6A
Intensity (Max, Omnidirectional)Up to 2,000 cd (average) at 6.6A
Intensity Steps5‑step (2.8A – 6.6A) CCR controlled
Mounting TypeElevated (frangible pole) or Inset (flush)
Spacing60m on straight sections, reduced to 30m on curves or at higher-category precision runways
Frangible Coupling (Elevated)Shear force 250–450 kg
Load Capacity (Inset)≈27,000 kg (59,400 lbs) wheel load — governing case: fully loaded A380-800 tyre, per FAA Engineering Brief 83A
Isolating Transformer45W / 65W / 100W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries airfield 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 / 100W)
Cable TypeL-824 single-conductor, direct-burial rated
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 (Bidirectional, White)≥ 6,500 cd per beam, up to 10,000 cd at full intensity
Main Beam Intensity (Bidirectional, Yellow)≥ 6,500 cd per beam (last 600m caution zone, instrument runways)
Main Beam Intensity (Omnidirectional)≥ 1,200 cd average, up to 2,000 cd at full intensity
Beam Pattern (Bidirectional)Two opposed beams, 3° vertical × 6° horizontal each
Beam Pattern (Omnidirectional)360° horizontal coverage, 3°–6° vertical spread
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5340-30 figures for the selected configuration
ChromaticityWithin ICAO Annex 14 white or yellow boundary as applicable (CIE coordinates)
Intensity Tolerance± 25% of rated value at each CCR step (field measurement)
Maintenance Factor≥ 50% of new-fixture intensity before lens/LED replacement is due
Test MethodMobile photometric van/goniophotometer or fixed test bench per fixture
Compliance

Applicable Standards

ICAO Annex 14

Runway edge light beam patterns, intensities, and colour requirements

FAA AC 150/5345-46

Specification for bidirectional/omnidirectional runway edge lights

IEC TS 61827

Characteristics of inset and elevated AGL luminaires

IES LM-79 / LM-80

LED edge light electrical/photometric performance and lumen-maintenance durability testing

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 level and, for inset units, flush with the pavement.

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 in flush/inset installations.

Duct & Cable Route
Electrical

Lay the series circuit duct/cable route to design depth, sizing the cable entry for the additional wiring a bidirectional unit's second lamp assembly requires.

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 matches the fixture's combined lamp load (both beams, for bidirectional units) and the series circuit's rated current step.

Frangible Coupling / Base Can Fixing
Mechanical

Torque the frangible coupling (elevated) or fixture fixing bolts (inset) to the specified value, checking the fitting shears as designed under lateral load and does not bind.

Beam Orientation Setting
Mechanical

Orient bidirectional units so both back-to-back beams align precisely along the runway centreline, or level omnidirectional units for even 360° coverage, before backfill.

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 ahead of backfill.

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.

CCR Brightness Step Response
Energisation

Cycle the CCR through every intensity step and confirm the fixture responds correctly at each, ruling out marginal transformers or loose connections.

Beam Pattern Verification
Final Acceptance

For bidirectional units, confirm both opposing beams are correctly aligned along the runway centreline; for omnidirectional units, confirm even light distribution through the full 360° arc with no dark sectors.

Photometric Commissioning Test
Final Acceptance

Measure beam intensity, colour, and pattern with a calibrated photometer against ICAO/FAA commissioning tolerances prior to operational handover.

Frangibility/Flush-Mount Verification
Pre-Energisation

For elevated units, confirm the frangible coupling shear point and mast height meet as-built tolerances; for inset units, confirm the fixture sits flush with the surrounding pavement.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, and photometric readings alongside as-built configuration (bidirectional or omnidirectional) in the commissioning dossier.

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify beam intensity against ICAO / FAA thresholds for both directions on bidirectional units, and across the full 360° spread on omnidirectional units, using a calibrated photometer.

Lens & Prism Cleaning
Quarterly

Clean both beam faces (bidirectional) or the full lens circumference (omnidirectional) of dust, rubber deposits, and film build-up so output stays within spec.

CCR Intensity Step Verification
Semi-annual

Confirm the fixture responds correctly across all 5 CCR steps (2.8A–6.6A), since intermittent failure at higher steps can mask a developing series-circuit fault.

Seal & Gasket Inspection
Annual

Check top-cap or housing seals for cracking or compression set, and re-torque fasteners to keep the fixture watertight.

Frangible Coupling Check (Elevated)
Annual

On elevated mounts, inspect the frangible coupling for corrosion or fatigue that could shift the 250–450 kg shear threshold.

Load Capacity Check (Inset)
Annual

On inset mounts, check the housing and pavement interface for damage that could compromise the rated wheel load capacity.

Insulation Resistance Test
Annual

Megger-test the isolating transformer and series circuit connection to confirm insulation resistance stays above minimum, flagging moisture ingress early.

Cable & Connector Inspection
Annual

Examine primary and secondary cable connections and transformer terminals for corrosion or loose crimps, a common source of intermittent faults.

Field Notes

Common Field Issues

Optical Mode Misconfiguration

If the fixture is field‑adjustable, incorrect selection of bidirectional vs. omnidirectional mode can lead to poor visibility for pilots. Clear labeling and verification during installation are essential to ensure the correct beam pattern for each location.

Uneven Intensity in Omnidirectional Mode

Omnidirectional fixtures may have slight variations in intensity around the 360° circle due to optical asymmetries or contamination. Regular photometric testing using a goniophotometer is recommended to verify uniformity.

Prism Alignment Drift in Bidirectional Mode

Vibration from aircraft and thermal cycling can cause the prism or reflector to shift, misaligning the bidirectional beams. Regular alignment checks using a digital level and alignment jig are necessary to maintain beam accuracy.

Lens Contamination Affecting Both Patterns

Regardless of the mode, the optical window is exposed to runway debris, rubber deposits, and de‑icing fluids. Routine cleaning with approved solvents and soft brushes is critical to maintain photometric performance and beam quality.

Diagnostics

Troubleshooting Guide

Single Fixture Dark, Rest of Loop Normal
Likely Cause
Failed lamp/LED source, or an open isolating transformer at that fixture (blown primary link or failed secondary winding).
Diagnostic Steps
Confirm series loop continuity through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised.
Corrective Action
Replace the lamp/LED source if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before backfill.
Entire Loop Dark / CCR Reports Voltage Rise
Likely Cause
Open-circuit fault in the series loop (severed cable, corroded splice, or a failed transformer acting as an open point), detected at the CCR as a voltage rise relative to the commanded current.
Diagnostic Steps
Check the CCR's fault/voltage-rise 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.
Fixture Showing the Wrong Beam Pattern for Its Location
Likely Cause
The optical mode — bidirectional or omnidirectional — is incorrectly set on a field-adjustable unit, or a fixed-mode fixture was installed at a location requiring the other pattern.
Diagnostic Steps
Visually confirm the beam pattern in the field against the required mode for that location on the layout drawing; check the field-adjustable optics setting if the unit supports it.
Corrective Action
Reconfigure field-adjustable optics to the correct mode, or replace the unit with one manufactured for the correct fixed mode; re-verify against the site layout drawing.
Uneven Intensity Around the 360° Circle (Omnidirectional Mode)
Likely Cause
Optical asymmetry from a manufacturing tolerance, or lens contamination unevenly affecting the diffuse reflector's 360° spread.
Diagnostic Steps
Run a goniophotometric test around the full 360° circle to map the intensity variation; inspect the lens and reflector for localised contamination or damage.
Corrective Action
Clean the optical window if contamination is the cause; replace the reflector/lens assembly if the asymmetry persists after cleaning and re-test.
Bidirectional Beams Misaligned from the Runway Centreline
Likely Cause
Vibration from aircraft operations and thermal cycling has shifted the internal prism or reflector out of alignment.
Diagnostic Steps
Check beam alignment with a digital level and alignment jig against the runway centreline; compare the two opposing beams for symmetry.
Corrective Action
Re-align the prism/reflector assembly per the manufacturer's procedure, or replace the optical assembly if it cannot be brought back within tolerance.
CCR Trips on Overcurrent or Ground Fault
Likely Cause
Moisture ingress at the fixture or connector has degraded insulation resistance, creating a short or partial ground fault on the series loop.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect the suspect fixture 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 Hazy Light Output in Either Mode
Likely Cause
Contamination of the optical window from runway debris, rubber deposits, or de-icing fluids, regardless of which mode the fixture is configured for.
Diagnostic Steps
Run a photometric intensity check against ICAO/FAA thresholds for the configured mode; inspect the lens for visible contamination.
Corrective Action
Clean the optical window with approved solvents and soft brushes per the maintenance schedule; re-verify with a follow-up photometric reading.
Reliability

Failure Modes & Root Causes

LED Module / Lamp Failure
High Severity
Root Cause
Solder-joint fatigue from thermal cycling, moisture ingress through a compromised LED board seal, or ordinary end-of-life lumen depreciation.
Effect
Single fixture goes dark while the rest of the loop continues to operate normally, and the CCR reports a voltage rise consistent with the loop absorbing the open fixture.
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.
Prism Alignment Drift (Bidirectional Mode)
Medium Severity
Root Cause
Manufacturing tolerance, impact, or thermal-cycling movement of the internal prism assembly that splits the fixture's output into its two directional beams.
Effect
Bidirectional beams become misaligned from the runway centreline, weakening the directional cue that mode depends on.
Detection Method
Beam pattern verification against the design bearing, checked during commissioning and periodic photometric testing.
Optical Mode Misconfiguration
Medium Severity
Root Cause
A fixture installed with its internal optic set to the wrong mode for its intended location, or a mode changed during a repair without being reset.
Effect
The fixture shows the wrong beam pattern for its location, presenting bidirectional beams where an omnidirectional 360° pattern was intended, or vice versa.
Detection Method
Beam pattern verification against the design specification for that fixture's location, checked at commissioning and after any repair.
Lens / Prism Contamination
Low Severity
Root Cause
Dust, rubber deposits, or general weathering building up on the lens or internal prism surfaces.
Effect
Reduced or hazy light output in either mode, and uneven intensity around the 360° circle in omnidirectional mode as contamination isn't always uniform.
Detection Method
Photometric intensity check against ICAO/FAA thresholds, and visual inspection and cleaning of the lens and prism.
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 the CCR tripping on overcurrent or ground fault.
Detection Method
CCR self-diagnostic/fault indication, output current verification, and a load-bank test to confirm regulation across all intensity steps.
Frangible Coupling Fatigue / Seal Failure
Medium Severity
Root Cause
On elevated units, cyclic loading and corrosion fatiguing the frangible coupling; on inset units, gasket compression set or housing cracking under wheel loading.
Effect
Elevated units lean, loosen, or shear off their base; inset units allow water ingress that accelerates connector corrosion.
Detection Method
Frangible coupling check on elevated units, or seal and gasket inspection on inset units, as part of scheduled maintenance.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

These fixtures run 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 cable 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 per the aerodrome's safety management procedures.

Confirm Optical Mode Before Installation
Compliance

Verify the fixture's internal optic is set to the correct mode — bidirectional or omnidirectional — for its intended location before installing or returning it to service after repair; a mode mismatch can present the wrong beam pattern without any other indication of fault.

Frangibility Not to Be Defeated
Mechanical

On elevated units, never substitute the frangible coupling with a rigid fitting or over-torque it during installation or repair; on inset units, ensure the housing and seal are restored to their rated wheel-load capacity before reopening the surface to traffic.

Verify Beam Pattern After Prism Work
Operational

After any work affecting the internal prism assembly, check the beam pattern against the design bearing before returning the fixture to service, since a drifted prism weakens the directional cue in bidirectional mode without necessarily darkening the fixture.

FOD Control at the Base Can
Operational

Keep tools, fasteners, and removed gaskets accounted for at all times when the base can is open, and secure or remove any loose material before reinstating the fixture, to prevent foreign object debris on the movement area.

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, at reduced intensity, in the wrong optical mode, or otherwise non-compliant after maintenance; verify photometric, positional, and mode conformance before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

A Mode Mismatch Hides Behind a Passing Photometric Test
Compliance

A fixture set to the wrong optical mode can still measure within tolerance on a straight-ahead intensity check, since the test doesn't necessarily probe the beam from the angle where the mismatch actually matters; verify optical mode by design record cross-reference at commissioning and after any repair, not by intensity reading alone.

Prism Drift in Bidirectional Mode Is Subtle
Optical

A slightly rotated or shifted internal prism weakens the directional cue for one approach direction while the fixture still appears lit and roughly on-aim from the other; check bidirectional beam pattern from both directions of travel after any work on the optic assembly, not just the direction the technician happens to be standing in.

Record Mode at the Fixture, Not Just in the Design Drawing
Documentation

Where a spare unit can be configured either bidirectional or omnidirectional before installation, a labelling gap between the physical fixture and the design drawing is an easy way for the wrong mode to go unnoticed for years; mark the configured mode on the fixture or base can itself as a cross-check against the drawing.

LED Retrofit Needs Its Optic Matched, Not Just Its Driver
Retrofit

When retrofitting these fixtures to LED, confirm the replacement optic reproduces the correct bidirectional or omnidirectional pattern for that specific position; a generic LED retrofit kit sized for wattage and step-matching alone can quietly change the beam distribution even while passing a basic on-aim intensity check.

Mixed-Mode Runs Complicate Loop Balancing
Design

A series loop mixing bidirectional and omnidirectional fixtures can draw slightly differently depending on optic design even at the same rated wattage; account for this at the design and commissioning stage rather than assuming uniform electrical behaviour across every fixture on the loop.

Seal Integrity Matters More on Inset Variants
Durability

Where this fixture is installed as an inset unit rather than an elevated one, de-icing fluid and standing water exposure at the seal is a bigger long-term risk to the optic assembly than UV alone; specify glycol-rated seals for inset installations and inspect them on a shorter interval than elevated units at the same site.

Quick Answers

Frequently Asked Questions

Short answers about the Bidirectional/Omnidirectional Runway Edge Fixture: what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is a Bidirectional/Omnidirectional Runway Edge Fixture?

A Bidirectional/Omnidirectional Runway Edge Fixture is a runway edge light that offers selectable or fixed light distribution patterns to suit different operational requirements. In bidirectional mode , the fixture projects light in two opposite directions along the runway centreline, visible to pilots approaching from either end. In omnidirectional mode , the fixture emits light uniformly in all directions (360°), providing edge visibility from any angle — particularly useful at runway intersections, curved sections, or where aircraft may be positioned at various angles on the runway.

Q2What is the purpose of a Bidirectional/Omnidirectional Runway Edge Fixture?

A standard runway edge light assumes pilots only ever approach from one predictable direction and angle; the bidirectional/omnidirectional fixture exists for the geometries where that assumption breaks down. Its purpose is to eliminate the dark or ambiguous edge segments that would otherwise appear wherever a runway is operated from both ends, where taxiways or rapid-exit turns intersect the edge line at an angle, or where a curved section or displaced threshold puts the pilot's viewing angle outside a single fixed beam's coverage.

Q3Where is a Bidirectional/Omnidirectional Runway Edge Fixture used and installed?

This versatile fixture is used on runways where both approach directions are operational, requiring bidirectional visibility, as well as at runway intersections, rapid exit taxiway turnoffs, and curved sections where omnidirectional visibility is beneficial. It is also suitable for runways with displaced thresholds, where edge lights need to be visible from multiple angles. The fixture is available in both elevated (frangible pole) and inset (flush‑mounted) configurations, making it suitable for all runway pavement types.

Q4How does a Bidirectional/Omnidirectional Runway Edge Fixture work?

The fixture contains an optical system that can be configured for bidirectional or omnidirectional output. In bidirectional mode , a precision prism and reflector system directs light into two opposite narrow beams (typically 3° vertical × 6° horizontal each), aligned along the runway centreline. In omnidirectional mode , a diffuse reflector or multifaceted prism spreads the light uniformly in all horizontal directions (360°) with a controlled vertical spread (3°–6°). Some designs allow field‑adjustable optics to switch between modes, while others are fixed at manufacture.

Q5What are the typical technical parameters of a Bidirectional/Omnidirectional Runway Edge Fixture?

Typical values are — Light Source: LED array or 50W / 100W halogen; Colour: White (full runway) / Yellow (last 600m or half runway length, whichever less, on instrument runways); Beam Pattern (Bidirectional): Two opposite beams: 3° vertical x 6° horizontal each; Beam Pattern (Omnidirectional): 360° horizontal with 3°–6° vertical spread; Intensity (Max, Bidirectional): Up to 10,000 cd per beam at 6.6A; Intensity (Max, Omnidirectional): Up to 2,000 cd (average) at 6.6A; Intensity Steps: 5‑step (2.8A – 6.6A) CCR controlled; Mounting Type: Elevated (frangible pole) or Inset (flush).

Q6What are the electrical requirements for a Bidirectional/Omnidirectional Runway Edge Fixture?

Typical requirements are — Circuit Type: Series airfield 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 / 100W); Cable Type: L-824 single-conductor, direct-burial rated; 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; Fault Protection: CCR-level ground fault and open-circuit detection; Power Source: CCR output, regulated per ICAO/FAA intensity step schedule.

Q7What photometric requirements apply to a Bidirectional/Omnidirectional Runway Edge Fixture?

Typical requirements are — Main Beam Intensity (Bidirectional, White): ≥ 6,500 cd per beam, up to 10,000 cd at full intensity; Main Beam Intensity (Bidirectional, Yellow): ≥ 6,500 cd per beam (last 600m caution zone, instrument runways); Main Beam Intensity (Omnidirectional): ≥ 1,200 cd average, up to 2,000 cd at full intensity; Beam Pattern (Bidirectional): Two opposed beams, 3° vertical × 6° horizontal each; Beam Pattern (Omnidirectional): 360° horizontal coverage, 3°–6° vertical spread; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5340-30 figures for the selected configuration.

Q8Which standards apply to a Bidirectional/Omnidirectional Runway Edge Fixture?

The main references are ICAO Annex 14 — Runway edge light beam patterns, intensities, and colour requirements; FAA AC 150/5345-46 — Specification for bidirectional/omnidirectional runway edge lights; IEC TS 61827 — Characteristics of inset and elevated AGL luminaires; IES LM-79 / LM-80 — LED edge light electrical/photometric performance and lumen-maintenance durability testing. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should a Bidirectional/Omnidirectional Runway Edge Fixture be inspected and maintained?

Typical maintenance tasks and intervals are: Photometric Intensity Check (annual); Lens & Prism Cleaning (quarterly); CCR Intensity Step Verification (semi-annual); Seal & Gasket Inspection (annual); Frangible Coupling Check (Elevated) (annual); Load Capacity Check (Inset) (annual); Insulation Resistance Test (annual); Cable & Connector Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Bidirectional/Omnidirectional Runway Edge Fixture faults?

Common symptoms covered are: Single Fixture Dark, Rest of Loop Normal; Entire Loop Dark / CCR Reports Voltage Rise; Fixture Showing the Wrong Beam Pattern for Its Location; Uneven Intensity Around the 360° Circle (Omnidirectional Mode); Bidirectional Beams Misaligned from the Runway Centreline; CCR Trips on Overcurrent or Ground Fault; Reduced or Hazy Light Output in Either Mode. For example, for "Single Fixture Dark, Rest of Loop Normal": Likely Cause: Failed lamp/LED source, or an open isolating transformer at that fixture (blown primary link or failed secondary winding). Diagnostic Steps: Confirm series loop continuity through the fixture's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised. Corrective Action: Replace the lamp/LED source if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the L-823 connectors before backfill.

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