AGL Component Library By Precision AGL Academy

CAT III Approach Lighting

The pinnacle of precision approach lighting systems, designed for Category III operations with the most demanding visibility requirements. Featuring a full 900‑metre configuration with high‑intensity barrettes, sequenced flashing lights, red side‑row bars, and enhanced centreline lighting, the CAT III system supports approaches with decision heights as low as 50ft (CAT IIIa) or zero (CAT IIIb/c) and RVR down to 200m or less, enabling safe landings in the world's most challenging weather conditions.

CAT III Approach Lighting System

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Overview

What Is It?

CAT III Approach Lighting is the most advanced precision approach lighting system available, designed to support Category III instrument approaches — the lowest visibility operations in commercial aviation. The system features a comprehensive 900‑metre configuration of high‑intensity barrettes, sequenced flashing lights, red side‑row bars, and enhanced centreline lighting. CAT III systems are distinguished by their exceptional reliability, redundancy, and light output, with multiple independent power feeds and backup systems to ensure continuous operation in the most critical conditions. They support operations with decision heights as low as 50 feet (CAT IIIa) or zero feet (CAT IIIb and CAT IIIc), and RVR down to 200 metres (CAT IIIa) or as low as 75 metres (CAT IIIb) and even zero (CAT IIIc).

Purpose

Purpose & Function

CAT III approach lighting exists to support the narrowest margins in commercial aviation, where decision heights as low as 50 feet or zero and RVR as low as 75 metres or zero leave essentially no room for a lighting failure or a momentarily degraded visual cue to go unnoticed. Its comprehensive combination of high-intensity barrettes, sequenced flashing lights, red side-row bars, and enhanced centreline lighting exists to give the pilot (or, at the lowest minimums, the autoland system and any last-second visual cross-check) the maximum achievable visual information in the shortest possible viewing window before touchdown. The purpose behind its redundant power feeds and backup systems is equally central: at these minimums, a lighting outage isn't a degraded-but-workable situation, it is potentially the loss of the only visual reference available, so the system is engineered specifically to keep functioning through failures that a less critical system could simply tolerate.

Application

Where Is It Used?

CAT III approach lighting systems are installed at the world's busiest and most advanced airports. They are typically used on:

  • Precision approach runways with CAT IIIa/b/c capability (50ft or zero DH, 200m RVR or less)
  • Major international hub airports in regions with frequent fog, heavy rain, or snow
  • Airports that serve as critical diversion points for long‑haul and transoceanic flights
  • Military airbases with all‑weather operational requirements
  • Runways with the highest traffic volumes where operational continuity is paramount
  • Airports implementing CAT IIIb/c for zero‑visibility operations (with appropriate taxiway guidance)
Placement

Installation & Location

Fixtures are set out along the extended runway centreline for the full 900 m length, on frangible stands graded to the approach slope; structures crossing roads, water, or depressions are elevated on piers or catwalks to keep the array on a consistent plane. Given the zero-tolerance for outage at CAT III minima, every stand is fed from dual, independently routed circuits in separate ductbanks, each backed by its own constant current regulator and standby power source, so that loss of a single feeder or regulator cannot take down the array. The red side-row bars in the final 300 m are tied into the runway's own lighting so the approach-to-runway transition reads as one continuous system. Setting-out follows the extended centreline and threshold survey to the same tolerance as the runway lighting it feeds into.

Function

How Does It Work?

The CAT III approach lighting system incorporates all the features of CAT II with enhanced reliability and performance for the lowest visibility:

  • High‑Intensity Barrettes: A series of light bars (typically 5 lights per bar) positioned at 30m/100 ft intervals along the full 731m/914m (2,400 ft/3,000 ft) approach path, with significantly higher luminous intensity than CAT I/II for penetration of dense fog.
  • Sequenced Flashing Lights (SFL): Ultra‑high‑intensity lights that flash in rapid sequence from the outer end toward the threshold, creating a highly visible "rolling" effect that indicates the approach direction. The SFL in CAT III has the highest intensity and fastest flash rate for maximum visibility in fog.
  • Red Side‑Row Bars: Red lights on both sides of the approach path in the final 300m segment, providing a critical visual warning of lateral deviation in very low visibility.
  • Enhanced Centreline Lighting: More frequent centreline barrettes and lights, providing precise lateral guidance with reduced spacing for improved continuity in low visibility.
  • Decision Bar: A row of lights at the decision height point, providing a clear visual reference for the pilot's go/no‑go decision.
  • Redundancy and Reliability: CAT III systems feature redundant power feeds, dual CCRs, and automatic failover to ensure uninterrupted operation. Many systems also include remote monitoring and diagnostics for proactive maintenance.
  • Automatic Intensity Control: The system automatically adjusts intensity based on real‑time RVR data, ensuring optimal visibility without blinding pilots in varying conditions.
Architecture

System Architecture & Control Logic

At its core, CAT III control logic follows the same two-path architecture as CAT I and CAT II: steady-burning elements — high-intensity barrettes, red side-row bars, and enhanced centreline lighting — sit on a constant current series circuit, with the ALCMS selecting the intensity step and the CCR regulating the loop to a single fixed current shared by every fixture via its own isolating transformer, while the sequenced flashing lights and decision bar are driven by a separate flasher/sequencer controller discharging through each lamp in outer-to-threshold order at the highest rate and peak intensity in the approach lighting family. What sets CAT III apart is that this entire control chain — ALCMS, CCR, and sequencer — is duplicated rather than run as a single string, with automatic real-time adjustment against live RVR data on both subsystems. The mechanics of that duplication and the automatic failover between feeds are covered in the next section.

Same two-path control logic as CAT I/II — duplicated end-to-end for redundancy (see below)

AIRFIELD LIGHTING CONTROL SYSTEM (ALCMS) Automatic real-time step selection from live RVR data CONSTANT CURRENT REGULATOR Converts step command to fixed loop current STEADY-FIXTURE SERIES CIRCUIT LOOP Feeds high-intensity barrettes, side-rows & centreline ISOLATING TRANSFORMER (PER FIXTURE) Taps fixed loop current to each steady fixture HIGH-RATE SFL FLASHER / SEQUENCER Capacitor-discharge, fastest rate & highest peak intensity HIGH-INTENSITY BARRETTES / SIDE-ROWS Steady-burning — highest intensity in the ALS family SEQUENCED FLASHING LIGHTS + DECISION BAR Outer lamp to threshold, maximum fog penetration APPROACH LIGHT PATTERN TO PILOT Steady bars and rolling flash combine into one visual cue ENTIRE CHAIN DUPLICATED FOR REDUNDANCY — SEE NEXT SECTION
Redundancy Logic

Dual Feed & Automatic Failover — Why CAT III Never Goes Dark

Primary Power FEED LOST CCR A FAULT Secondary Power Independent feed CCR B Standby → Active Automatic Failover Detects fault → switches feed 731m/914m Approach Lighting Circuit Continuously powered — no interruption to pilot's visual cues Dual Feeds + Dual CCRs + Auto-Failover = Uninterrupted Illumination for CAT IIIb/c Zero-RVR Ops
Active / live path
Faulted primary path
Standby (idle) path
Construction

Physical Construction

Barrette stands are frangible structures carrying multiple lamp housings on a rigid bar, graded in height to keep the array on the approach slope; die-cast aluminium housings behind toughened, gasket-sealed lenses achieve an IP67/IP68 rating on each high-intensity LED array or 200W+ halogen lamp. The sequenced flashing heads use the highest-output xenon strobe tubes and trigger electronics in the approach lighting family, housed in weatherproof domes with correspondingly larger capacitor banks to sustain the ultra-high-intensity, rapid sequence required at CAT III minima. Red side-row bar fixtures in the final 300 m share construction with the runway's own edge lighting, tying the approach hardware directly into the runway system. Given the zero-tolerance for outage at CAT III minima, each stand and fixture is wired to accept dual, independently routed feeder cables in separate ductbanks, each terminating at its own isolating transformer, so the loss of a single feeder or transformer does not extinguish the fixture; stands crossing roads, water, or depressions are raised on piers or catwalks engineered to the same redundancy standard. Stainless-steel fasteners and corrosion-resistant finishes are used throughout to meet the reliability demands of CAT III operation.

Specification

Technical Parameters

ParameterTypical Value
System TypeCAT IIIa/b/c precision approach lighting
Light SourceHigh‑intensity LED array or 200W+ halogen
ColourWhite (steady and flashing), Red (side‑row bars)
Configuration Length731 metres / 2,400 ft (standard) – 914 metres / 3,000 ft (shallow-slope sites)
Barrette Spacing30m/100 ft intervals along full length
Barrette Lights per Bar5 lights (for maximum visibility)
Sequenced Flashing LightsUltra‑high‑intensity, rapid sequence toward threshold
Side‑Row BarsRed lights on both sides of the final 300m segment
Centreline LightingEnhanced spacing (closer than CAT II) for continuity
Decision BarPresent at decision height point
Intensity Steps5‑step (2.8A – 6.6A) CCR controlled, with automatic RVR‑based dimming
Beam PatternUni‑directional towards approach, very narrow beam for maximum intensity
Mounting TypeElevated or flush‑mounted (inset)
Isolating Transformer200W – 300W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
RedundancyDual power feeds, dual CCRs, automatic failover
SupportCAT IIIa (50ft DH, 200m RVR) / CAT IIIb (zero DH, 75m RVR) / CAT IIIc (zero DH, zero RVR)
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeIndependent series circuits (dual CCR fed, automatic failover) for centreline, side-row bars, and SFL/strobe array
Rated Series Current6.6A per circuit (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A)
IsolationDedicated isolating transformer (200W – 300W) per fixture; SFL heads fed from dedicated capacitor-discharge units
Transformer SecondaryMatched to fixture wattage; sized to series circuit rating
SFL Power SupplyUltra-high-output capacitor-discharge trigger units driving xenon strobes, synchronised by a flasher controller at the rapid CAT III sequence rate
Cable TypeL-824 single-conductor, direct-burial rated, 5kV per circuit; shielded trigger cable for SFL synchronisation
ConnectorL-823 primary connector, submersible-rated splice
Insulation Resistance≥ 50 MΩ (megger test, cable-to-ground)
Earthing/GroundingFixture body, stands, and base cans bonded to airfield earth grid
Fault ProtectionDual CCR-level ground fault and open-circuit detection with automatic failover between primary and standby regulator
Standby PowerDual mains feeds with automatic transfer, backed by airfield standby generation to meet CAT III continuity-of-supply requirements
Power SourceDual CCR output per circuit, regulated per ICAO/FAA RVR-based intensity step schedule
Optical Performance

Photometric Requirements

ParameterTypical Value
Centreline Barrette Intensity10,000 – 20,000 cd (white), 5-step: 100% / 30% / 10% / 3% / 1%, tightly regulated
Red Side-Row Bar Intensity≥ 2,000 cd (red) over the last 1,000 ft to touchdown
SFL Peak Effective IntensityUltra-high-output, ≥ 20,000 effective cd (white xenon strobe)
SFL Flash RateRapid sequence rate synchronised outward-to-threshold along the centreline, per CAT III schedule
Vertical Beam SpreadMain beam 1°–12° above horizontal (peak ~2°–3°)
Horizontal Beam Spread± 4.5° either side of runway centreline extended, plus red side-row spread
ChromaticityWhite (centreline/SFL) and red (side-row bars) within ICAO Annex 14 boundaries
RVR-Based Intensity ControlAutomatic step selection tied to reported RVR, with dual-regulator monitoring to guarantee CAT III output continuity
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5340-30 CAT III configuration figures
Compliance

Applicable Standards

ICAO Annex 14

CAT III approach lighting configuration, spacing, colour, intensity, and redundancy requirements

FAA AC 150/5345-46

Specification for CAT III approach lighting components and systems

IEC 61827

Electrical and photometric performance for AGL luminaires (CAT III grade)

FAA Engineering Brief #67

LED CAT III component performance and reliability requirements

Prerequisites

Installation Requirements

Frangible Stand Footing & Slope Grading
Civil

Set each stand footing along the full 900 m run to the design height so the array follows the approach slope, holding tolerance through to the threshold.

Elevated Piers & Catwalks Over Obstacles
Civil

Install piled structures or catwalks wherever the approach crosses roads, water, or depressions, built to the same redundancy standard as the rest of the array.

Dual Independent Ductbank Routing
Electrical

Lay dual, independently routed duct runs to every stand and fixture, each ductbank terminating at its own isolating transformer so loss of a single feeder cannot extinguish a fixture.

L-823 Connector Termination
Electrical

Terminate and seal primary connectors on both primary and secondary feeds per manufacturer procedure, keeping every splice fully submersible-rated before backfill.

Redundant CCR & Standby Power Verification
Electrical

Confirm each circuit is backed by its own constant current regulator and standby power source, with dual feeds independently traceable back to source before energisation.

Barrette, SFL & Side-Row Assembly
Mechanical

Fix lamp housings to barrette bars, mount ultra-high-intensity SFL heads, and install red side-row bar fixtures in the final 300 m, torquing all frangible fittings to spec.

Setting-Out & Runway Transition
Mechanical

Tie stand positions to the extended centreline and threshold survey to the same tolerance as the runway lighting it feeds into, keeping the approach-to-runway transition continuous.

Pre-Energisation Sign-off
Documentation

Record stand positions, dual cable routes, connector seals, 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 steady circuit, the ultra-high-intensity SFL circuit, and the red side-row bar circuit on both primary and secondary power feeds before backfill.

Loop Continuity & Resistance Test
Pre-Energisation

Verify series loop continuity and record total loop resistance for the full 731m/914m run, including the enhanced-spacing centreline and side-row bars, before first energisation.

Dual Feed & Automatic Failover Test
Energisation

Energise from the primary CCR/power feed, then force a failure and confirm the secondary CCR/feed picks up automatically within the required changeover time with no perceptible loss of guidance.

Automatic RVR-Linked Dimming Verification
Energisation

Simulate a range of RVR inputs to the ALCMS and confirm the CCR automatically adjusts intensity in line with CAT III visibility-linked control logic down to zero-RVR settings.

Sequenced Flashing & Decision Bar Response
Energisation

Confirm the ultra-high-intensity SFL sequence fires correctly toward the threshold and that the decision bar illuminates and aligns with the decision-height reference point.

Side-Row Bar & Barrette Alignment Verification
Final Acceptance

Check elevation, azimuth, and colour segregation of every barrette and red side-row light against the design aiming diagram, correcting any deviation before sign-off.

Photometric Commissioning Test
Final Acceptance

Measure beam intensity and colour of white and red elements with a calibrated photometer against ICAO/FAA CAT IIIa/b/c commissioning tolerances.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, failover-time, dimming-response, and photometric readings alongside as-built positions in the commissioning dossier for handover.

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify barrette, side-row bar, and centreline beam intensity against ICAO / FAA thresholds using a calibrated photometer across the full 731m/914m ultra-high-intensity configuration.

Barrette & Side-Row Lens Cleaning
Quarterly

Clear dust, insect residue, and weathering film from barrette, side-row, and enhanced-spacing centreline lenses so beam output stays within spec at CAT III intensity levels.

Sequenced Flasher Timing Test
Semi-annual

Confirm the ultra-high-intensity sequenced flashers fire in the correct rapid outer-to-threshold order, since a stuck or mistimed flasher is critical at near-zero visibility.

Dual CCR & Automatic Failover Test
Semi-annual

Simulate loss of the primary power feed or CCR and confirm the redundant feed and CCR take over automatically without a lighting gap, per the CAT III redundancy requirement.

RVR-Based Dimming Verification
Semi-annual

Confirm the automatic RVR-based dimming logic steps intensity correctly against simulated visibility inputs, since this directly affects crew visual reference at decision height.

Decision Bar Function Check
Semi-annual

Verify the decision bar at the decision height point illuminates correctly and at the specified intensity, since this is the critical go/no-go visual reference in CAT IIIb/c operations.

Insulation Resistance Test
Annual

Megger-test the isolation transformers and series circuit feeding the configuration to confirm resistance stays above minimum, flagging moisture ingress before it causes a circuit-wide fault.

Cable & Connector Inspection
Annual

Examine primary and secondary cable connections across the array for corrosion or loose crimps, a common source of intermittent series-circuit faults over a run this long.

Field Notes

Common Field Issues

Lens Contamination in Fog and Snow

CAT III components operate in the most severe weather conditions. Fog, snow, and de‑icing chemicals can rapidly contaminate lenses, reducing light output. Regular cleaning with approved solvents and soft brushes is essential, with some airports implementing automated cleaning systems for critical components.

SFL Synchronisation Drift

The SFL system relies on precise timing. Control units can drift over time, causing the sequence to become irregular or out of sync. Regular calibration and testing of the SFL system is critical for CAT III operations, with redundant controllers recommended.

Misalignment of Elevated Fixtures

Elevated approach lights can be knocked out of alignment by wind, wildlife, or maintenance vehicles. Regular alignment checks using a theodolite or laser alignment system are essential, especially for the side‑row bars which must be precisely positioned.

Red Filter Degradation

The red side‑row bars use colour filters that can degrade over time due to UV exposure and thermal stress. The red colour may fade or shift toward orange. Regular photometric testing and filter replacement are essential to maintain ICAO chromaticity requirements.

CCR and Power Supply Failure

CAT III systems draw significant power and require precise current regulation. Voltage fluctuations, CCR faults, or cable damage can cause inconsistent brightness or total failure. Regular power quality monitoring, cable testing, and CCR maintenance are essential. Redundant power feeds and automatic failover must be tested regularly.

Communication Network Latency

CAT III systems rely on real‑time communication between RVR sensors, ALCMS, and CCRs. Network latency or failures can delay intensity adjustments or cause system errors. Regular network performance monitoring and redundant communication paths are critical.

Diagnostics

Troubleshooting Guide

Single Light/Bar Dark, Rest of Array 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 Array Dark / CCR Will Not Regulate
Likely Cause
Open-circuit fault in the series loop feeding the approach lights (severed cable, corroded splice, or a failed transformer acting as an open point).
Diagnostic Steps
Check the CCR fault/open-circuit indication first; loop-resistance test from the CCR output to isolate the faulted segment; sectionalise and megger cable runs along the approach centreline 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.
SFL Sequence Irregular or Out of Step
Likely Cause
Timing drift in the sequenced flashing light controller, or a failed flasher unit, has broken the rolling flash pattern.
Diagnostic Steps
Verify controller timing against the specified sequence rate; check each flasher head in turn for correct firing order; inspect flasher control cabling for damage.
Corrective Action
Recalibrate or replace the SFL controller, or replace the faulty flasher head; confirm the rolling sequence is restored end to end.
Red Side-Row Bar Faded or Shifted Toward Orange
Likely Cause
UV exposure and thermal stress have degraded the red colour filter on a side-row bar, shifting its chromaticity out of tolerance.
Diagnostic Steps
Run a photometric/chromaticity check against ICAO colour limits for red; visually compare the suspect bar to a known-good reference fixture.
Corrective Action
Replace the red filter or lens assembly; re-verify chromaticity with a follow-up test before returning the bar to service.
CCR/Power Feed Failure — Redundant Failover Not Confirmed
Likely Cause
The primary CCR or power feed has failed and the automatic failover to the redundant feed has not engaged correctly, a critical gap for CAT III readiness.
Diagnostic Steps
Confirm the fault indication on the primary CCR; manually test that the redundant feed and failover relay operate correctly; check ALCMS logs for the failover event.
Corrective Action
Repair or replace the failed CCR/feed component, and re-test the automatic failover sequence before returning the system to full CAT III readiness.
ALCMS/RVR Communication Latency or Loss
Likely Cause
A network fault or delay in the link between RVR sensors, ALCMS, and CCRs is delaying or preventing intensity adjustments.
Diagnostic Steps
Check network link status and latency between ALCMS and each CCR; verify RVR sensor data is being received and timestamped correctly.
Corrective Action
Restore or reroute the communication path and confirm redundant links are active; re-verify intensity commands are executing in real time.
Reliability

Failure Modes & Root Causes

Light Source (Lamp/LED) Failure
High Severity
Root Cause
Solder-joint fatigue from repeated thermal cycling, moisture ingress through a compromised fixture seal, or ordinary end-of-life lumen depreciation.
Effect
Single light or bar within the approach, side-row, or decision bar array goes dark or drops below minimum intensity while the rest of the array continues to operate normally.
Detection Method
Nighttime visual patrol along the approach centreline, 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 array or side-row circuit.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
L-823 Connector / Splice Degradation
Medium Severity
Root Cause
Improper seating or crimping during installation, gasket failure allowing groundwater ingress, or corrosion building up on the pins over time.
Effect
Intermittent operation, flickering, or a partial ground fault that degrades circuit insulation resistance.
Detection Method
Insulation resistance (megger) testing of the circuit and visual inspection of connectors at each fixture base can during maintenance.
Series Cable Insulation Breakdown
High Severity
Root Cause
Cable jacket damage from nearby excavation or wildlife activity, age-related insulation degradation, or prolonged standing water in the duct run.
Effect
Ground fault or short circuit that trips a CCR or darkens a series loop feeding the approach, side-row, or decision bar circuits.
Detection Method
Full-circuit megger test to flag the low-resistance segment, followed by sectionalised testing or time-domain reflectometry to pinpoint the fault location.
Elevated / Side-Row Fixture Frangible Coupling Fatigue
Medium Severity
Root Cause
Cyclic wind loading, wildlife strike, or contact from a maintenance vehicle, combined with ordinary material fatigue over the service interval.
Effect
Fixture leans, loosens, or separates from its mounting stake, pulling the light out of the tight aim tolerance required for CAT III minima.
Detection Method
Physical inspection for cracking or play in the coupling, and periodic fixture-aim checks with a theodolite or laser alignment system.
Dual CCR / Automatic Failover Fault
High Severity
Root Cause
Failure of the standby CCR to pick up load on primary-unit trip, a fault in the automatic transfer/failover logic, or a mismatched current setpoint between the primary and redundant units.
Effect
Loss of redundancy leaves the circuit vulnerable to a single-point outage; in the worst case, a primary CCR trip is not covered and the circuit darkens outright, which is unacceptable at CAT III minima.
Detection Method
Scheduled failover drill forcing a transfer from primary to standby CCR, output current verification on both units, and confirmation the ALCMS correctly reports failover status.
RVR-Based Automatic Dimming Fault
Medium Severity
Root Cause
A fault in the RVR sensor feed, a software/logic error in the automatic step-selection algorithm, or a stale or lost data link between the RVR system and the lighting control cabinet.
Effect
Intensity step fails to match prevailing runway visual range, either under-lighting the approach in low-visibility conditions or over-lighting and causing pilot glare.
Detection Method
Cross-check commanded intensity step against reported RVR values, verify the RVR data feed is current, and exercise a manual step-selection test to confirm dimming logic responds correctly.
ALCMS Communications / Network Latency or Loss
Medium Severity
Root Cause
Degraded fibre or copper link between the lighting control cabinet and the ALCMS, a switch or gateway fault, or contention on a shared control network.
Effect
Delayed or lost command/status exchange between the tower and field cabinet, which can mask a fault indication or delay a required intensity change during a CAT III approach.
Detection Method
Network link diagnostics and latency testing between the ALCMS and field cabinet, and verification that fault/status reporting is being received in real time.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

Centreline bar, crossbar, and red side row circuits run on constant-current series loops that can carry several kV. De-energise and lock out the associated CCR, then verify zero energy at the tower base or barrette before opening any enclosure.

Sequenced Flasher Capacitor Discharge
Electrical Safety

Condenser discharge units driving the sequenced flashing lights on a CAT III configuration store a high-energy charge even after the master flasher controller is switched off; discharge each unit through its bleed resistor and confirm zero voltage before servicing a flasher head.

Elevated Tower & Off-Runway Access
Personnel Safety

Light bar towers extend along the extended centreline over terrain that may be uneven, waterlogged, or off the paved movement area; use fall protection when climbing frangible towers and assess ground conditions before positioning vehicles or ladders.

Frangibility Not to Be Defeated
Mechanical

Never substitute a frangible coupling or tower base with a rigid fitting, and do not over-torque connections during installation or repair; the structure must still break away cleanly on aircraft impact within the runway safety area.

Zero-Visibility Work Coordination
Operational

CAT III operations tolerate essentially no degradation in the light pattern; obtain ATC/airside coordination and issue a NOTAM before any bar, crossbar, or flasher is taken out of service, and keep personnel and vehicles clear of the approach surface during aircraft operations.

FOD Control Along the Approach
Operational

Account for tools, fasteners, and hardware at every tower and barrette worked on, and remove or secure loose material before leaving the site, since debris in the approach area can be ingested or strike an aircraft on short final.

Insulation Test Before Re-Energisation
Electrical Safety

After any cable, connector, or transformer work on a bar, crossbar, or flasher circuit, megger test the affected series loop before restoring power, since a residual fault can trip the CCR or damage healthy fixtures on the same circuit.

Restore to Compliant State
Compliance

Do not leave the system with a bar out of aim tolerance, a dark flasher, or an out-of-sequence discharge pattern; verify photometric output and flasher timing against CAT III requirements before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Test the Full Failover Chain, Not Individual Components
Redundancy

CAT III's multiple independent power feeds only deliver their intended reliability if the transfer logic between them has been tested end-to-end under realistic fault conditions, not just verified as individually functional in isolation.

Zero-Visibility Operations Leave No Margin for Gradual Degradation
Photometric

At CAT IIIb/IIIc minimums, lumen depreciation that would be a minor concern on a CAT I system can matter operationally. Trend intensity data aggressively and replace on a predictive schedule rather than waiting for a failed survey.

Automated Cleaning Systems Still Need Manual Verification
Structural

Where automated lens cleaning is deployed for reliability in severe fog and snow, confirm actual cleaning effectiveness periodically by direct inspection; an automated system that's stopped working can mask degrading light output for longer than a manually-cleaned array would.

Map Every Independent Feed to Its Actual Failure Domain
Electrical

Two power feeds documented as 'independent' can still share a common failure point upstream — the same substation, the same trench run, the same transformer bank. Verify true independence physically, not just on the single-line diagram.

Redundant Controllers Need Cross-Checking, Not Just Individual Health Checks
Troubleshooting

A redundant SFL controller that reports healthy in isolation can still be silently out of sync with its primary; verify the two agree on actual sequence timing, not just that each independently passes its own self-test.

Category Approval Rides on Documented Reliability History
Compliance

Because CAT III approval depends heavily on demonstrated system reliability over time, gaps or inconsistencies in maintenance and outage records can jeopardise category status independent of the system's present physical condition.

Quick Answers

Frequently Asked Questions

Short answers about CAT III approach lighting: minima, redundancy, RVR control, standards and maintenance.

Q1What is CAT III approach lighting?

It is the highest-specification precision approach lighting system, for Category III operations in the lowest visibility. It combines high-intensity barrettes, ultra-high-intensity sequenced flashing lights, red side-row bars, enhanced centreline lighting and a decision bar, with redundant power and controls.

Q2What operating minima does CAT III support?

CAT IIIa supports a 50 ft decision height with 200 m RVR, CAT IIIb zero decision height with 75 m RVR, and CAT IIIc zero decision height with zero RVR. At these minima there is essentially no room for a lighting failure or degraded visual cue to go unnoticed.

Q3How does CAT III differ from CAT II?

CAT III adds higher luminous intensity, five lights per barrette, closer-spaced enhanced centreline lighting, the fastest and highest-intensity sequenced flashers, 200 to 300 W isolating transformers, and full redundancy: dual power feeds, dual CCRs, automatic failover and standby power.

Q4What redundancy does a CAT III system have?

Dual mains feeds with automatic transfer, backed by airfield standby generation, dual CCRs with automatic failover between primary and standby regulators, and independent series circuits for the centreline, side-row bars and flasher array. Many systems add remote monitoring and diagnostics for proactive maintenance.

Q5How is CAT III intensity controlled?

By five CCR steps (2.8 A to 6.6 A) with automatic dimming based on real-time RVR data, so brightness suits the visibility without blinding pilots. This relies on real-time communication between RVR sensors, the ALCMS and the CCRs.

Q6How long is a CAT III system and how are the lights spaced?

The configuration is typically 731 m (2,400 ft) as standard up to 914 m (3,000 ft) on shallow-slope sites, with barrettes of 5 lights at 30 m (100 ft) intervals and red side-row bars on both sides of the final 300 m.

Q7Where is CAT III approach lighting used?

At major international hubs, particularly in regions with frequent fog, heavy rain or snow, airports that serve as critical diversion points for long-haul and transoceanic flights, high-traffic runways where operational continuity is paramount, military airbases, and airports implementing CAT IIIb/c operations with appropriate taxiway guidance.

Q8Which standards apply to CAT III approach lighting?

The main references are ICAO Annex 14 (configuration, spacing, colour, intensity and redundancy requirements), FAA AC 150/5345-46 (CAT III components and systems), IEC 61827 and FAA Engineering Brief #67 (LED CAT III performance and reliability). Always verify the current edition and your aerodrome's approved requirements.

Q9How often should CAT III approach lighting be maintained?

Typical practice is quarterly lens cleaning, semi-annual sequenced flasher timing tests, dual CCR and automatic failover tests, RVR-based dimming verification and decision bar checks, and annual photometric intensity checks, insulation resistance tests and cable and connector inspection. Your airport's approved maintenance programme takes precedence.

Q10What are the common CAT III approach lighting problems?

Rapid lens contamination in fog, snow and de-icing chemicals, sequenced flasher synchronisation drift, misaligned elevated fixtures, red filter degradation, CCR and power supply failure, and communication network latency or failure that delays RVR-driven intensity changes.

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