Approach Lighting System (ALS) fault diagnosis — from a complete system outage through to partial/multiple fixture failures, flicker and intensity-step faults, colour and photometric compliance, circuit and cable faults, connector and transformer failure, alignment and structural damage (poles, crossbars, platforms), optical failure, control and remote-monitoring faults, earthing/lightning protection, and water ingress across the elevated mast and crossbar structures beyond the runway threshold. Each topic follows the full engineering diagnostic record: symptom → observation → measurement → decision → fault location → root cause → verification → corrective action → preventive action.
Symptom — The entire Approach Lighting System (ALS) fails to illuminate when commanded, reported via pilot report, ALCMS status, or routine night inspection — distinct from a partial or single-fixture outage.
Approach Lighting System (ALSF-2/MALSR/simplified configuration as installed) — elevated crossbar and centreline barrette fixtures on frangible masts/poles beyond the runway threshold, sequenced flasher units, dedicated ALS feeder circuit(s) and control cabinet, fed from the CCR/ALS regulator and ALCMS.
After repair, re-energise the system and confirm every crossbar, centreline barrette, and sequenced flasher operates correctly at all commanded intensity steps during a full night inspection.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-CCR-04 (CCR LOTO Procedure)
Standards: ICAO Annex 14 Vol I, FAA AC 150/5340-30, FAA AC 150/5345-46 (ALSF-2/MALSR series)
Diagram: ALS System Circuit and Structure Layout Drawing
Case Study: Division 01 — CCR Troubleshooting; Division 24 — Complete Runway Lighting Failure
Symptom — A defined section of the ALS — for example one or more crossbars, a segment of the centreline barrette run, or the sequenced flasher string — is dark or malfunctioning while the rest of the system operates normally.
The affected ALS sub-circuit or structural section (crossbar group, centreline segment, or flasher branch) and its dedicated feeder from the control cabinet.
Re-energise the section and confirm it matches the operating pattern (steady, sequenced, or intensity-stepped as applicable) of the rest of the system before closing out.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-ALS-02 (Sub-Circuit Isolation Procedure)
Standards: ICAO Annex 14 Vol I, FAA AC 150/5345-46
Diagram: ALS Sub-Circuit Distribution Drawing
Case Study: Division 01 — CCR Troubleshooting; Division 25 — Field Case Study Troubleshooting
Symptom — Two or more individual ALS fixtures — crossbar lights, centreline barrette elements, or flasher heads — are dark or malfunctioning together within an otherwise energised section, distinct from a full sub-circuit outage.
The group of individual ALS fixtures affected and the series/parallel wiring segment feeding them within their sub-circuit.
After repair, megger the full affected segment, re-energise, and confirm every fixture in the previously affected group operates correctly.
SOP: SOP-ALS-02 (Sub-Circuit Isolation Procedure), SOP-ALS-03 (Series Circuit Fault Location Procedure)
Standards: IEC 60364, ICAO Annex 14 Vol I, FAA AC 150/5345-46
Diagram: ALS Circuit and Structure Wiring Drawing
Case Study: Division 24 — Complete Runway Lighting Failure; Division 25 — Field Case Study Troubleshooting
Symptom — One or more ALS fixtures flicker, pulse, or vary in brightness instead of holding steady output (for steady-burning elements) or a consistent flash characteristic (for sequenced flashers) at the commanded intensity step.
ALS fixture, its isolation transformer or flasher driver, connector, and the circuit supplying it.
Monitor the repaired fixture over several operating cycles, including at least one period of the wind or weather condition previously associated with the flicker, before closing out.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure)
Standards: FAA AC 150/5345-46 (ALSF-2/MALSR), ICAO Annex 14 Vol I
Diagram: ALS Circuit Layout Drawing
Case Study: Division 01 — CCR Troubleshooting (intensity step control)
Symptom — An ALS fixture illuminates but appears noticeably dimmer than adjacent fixtures on the same crossbar or centreline run at the same commanded intensity step.
ALS fixture optical/lamp assembly, isolation transformer or driver output, and lens condition.
Re-measure luminance output after corrective action and compare against neighbouring fixtures and the manufacturer's rated output for the commanded step.
SOP: SOP-ALS-04 (Lens Cleaning and Inspection Procedure)
Standards: ICAO Annex 14 Vol I (light intensity requirements), FAA AC 150/5340-30
Diagram: ALS Photometric Specification Sheet
Case Study: Division 26 — Photometric & Intensity Compliance
Symptom — An ALS fixture shows a colour other than specified for its position — for example, a white steady-burning light showing amber/red-tinted output, or a fixture in the last 300 m section not showing the correct red side-row colour where applicable.
ALS fixture lens/filter and lamp/LED module colour characteristics relative to its position in the approach lighting configuration (e.g., red terminating/side row barrettes in ALSF-2 systems).
Visually confirm the correct colour is displayed at the correct position during a night inspection, alongside the fixtures immediately either side.
SOP: SOP-ALS-04 (Lens Cleaning and Inspection Procedure)
Standards: ICAO Annex 14 Vol I (approach lighting colour requirements), FAA AC 150/5340-30
Diagram: ALS Colour-Scheme Layout Drawing
Case Study: Division 26 — Photometric & Intensity Compliance
Symptom — The ALS fails to change output correctly when a different intensity step is commanded — either remaining at a fixed intensity, failing to reach the commanded step, or responding incorrectly compared to neighbouring circuits.
ALS regulator/CCR step control output and the fixture/transformer response across the system's intensity range.
Cycle through every available intensity step and confirm correct field output and correct ALCMS feedback at each before returning the system to normal operation.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-CCR-08 (Intensity Step Verification)
Standards: ICAO Annex 14 Vol I, FAA AC 150/5345-46
Diagram: ALS Regulator Step-Control Schematic
Case Study: Division 01 — CCR Troubleshooting (Intensity Step Control)
Symptom — A defined ALS circuit — a series loop, sub-circuit, or feeder branch — shows a confirmed electrical fault (open circuit, short circuit, or protection trip) at the circuit level, distinct from an individual fixture or cable-segment fault already isolated to a single point.
The affected ALS circuit as a whole, including its protective device, feeder, and the fixture group it serves.
After repair, re-energise the circuit and confirm the protective device holds under normal load, and that every fixture on the circuit operates correctly across all intensity steps.
SOP: SOP-ALS-02 (Sub-Circuit Isolation Procedure), SOP-ALS-03 (Series Circuit Fault Location Procedure)
Standards: IEC 60364, ICAO Annex 14 Vol I
Diagram: ALS Circuit Schematic
Case Study: Division 01 — CCR Troubleshooting; Division 24 — Complete Runway Lighting Failure
Symptom — A confirmed insulation or conductor fault in ALS feeder or series cable, requiring cable-level repair or replacement, distinct from a connector or fixture fault.
ALS feeder and series cable routed through ducts, pull boxes, and structures across the approach lighting area, which frequently spans unpaved, wetland, or difficult-access terrain beyond the runway threshold.
After repair, megger the full repaired segment and the adjoining sections, re-energise, and confirm all fixtures on the loop operate correctly across all intensity steps.
SOP: SOP-ALS-03 (Series Circuit Fault Location Procedure), SOP-ALS-05 (Cable Splice and Repair Procedure)
Standards: IEC 60502 (power cable), ICAO Annex 14 Vol I, FAA AC 150/5340-30
Diagram: ALS Cable Route and Structure Drawing
Case Study: Division 24 — Complete Runway Lighting Failure
Symptom — The individual isolation transformer feeding an ALS fixture has failed — open-circuit, short-circuit, or significantly out of tolerance on secondary output — distinct from a fixture lamp/LED or connector fault.
ALS series-circuit isolation transformer (rated per the specific fixture type — crossbar, centreline barrette, or flasher unit — within the ALSF-2/MALSR configuration).
After replacement with the correctly rated transformer, re-energise and confirm the fixture operates correctly across all intensity steps, and re-check insulation resistance at the next scheduled maintenance visit.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-ALS-06 (Transformer Test and Replacement Procedure)
Standards: FAA AC 150/5345-26 (isolation transformers), ICAO Annex 14 Vol I
Diagram: ALS Circuit Design Specification
Case Study: Division 01 — CCR Troubleshooting (series circuit fundamentals)
Symptom — A fixture, transformer, or junction connector within the ALS is found failed — corroded, cracked, arced, or not maintaining a reliable connection.
Fixture, transformer, and junction connectors within ALS structure bases, junction boxes, and mast-mounted enclosures.
Re-test insulation resistance and contact integrity after reconnection, and schedule a follow-up check after the next significant weather event to confirm the seal is holding.
SOP: SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-ALS-07 (Connector Maintenance Procedure)
Standards: FAA AC 150/5345-26 (connectors), ICAO Annex 14 Vol I
Diagram: ALS Structure and Enclosure Wiring Detail Drawing
Case Study: Division 25 — Field Case Study Troubleshooting
Symptom — An ALS fixture (crossbar element, centreline barrette, or flasher head) is correctly powered and mechanically sound, but is not correctly aimed relative to the approach path and design sightline, reducing apparent intensity to an approaching aircraft.
ALS fixture mounting/aiming on its mast, crossbar, or ground-level frangible base relative to the design approach azimuth and elevation.
Re-inspect from the design approach sightline at night after realignment, and confirm the fixture remains correctly aligned after the next scheduled maintenance interval, particularly following any significant wind event.
SOP: SOP-ALS-08 (Fixture Alignment Verification Procedure)
Standards: ICAO Annex 14 Vol I Appendix 2 (approach light beam characteristics), FAA AC 150/5340-30
Diagram: ALS Aiming and Alignment Reference Drawing
Case Study: Division 26 — Photometric & Intensity Compliance
Symptom — An ALS support pole (mast supporting a crossbar or individual fixture) is found physically damaged — bent, cracked, corroded, or partially collapsed — distinct from wider structural damage affecting the crossbar or platform itself (ALS-284).
ALS support pole/mast, its frangible base coupling, and immediate foundation.
After pole repair or replacement, confirm correct electrical operation (megger and functional test) and correct fixture alignment per ALS-282 before returning the section to service.
SOP: SOP-ALS-09 (Pole Replacement Procedure), SOP-ALS-10 (Frangible Coupling Inspection)
Standards: FAA AC 150/5345-46 (frangibility requirements), ICAO Annex 14 Vol I
Diagram: ALS Pole and Frangible Coupling Assembly Drawing
Case Study: Division 27 — FOD & Physical Damage Case Studies
Symptom — A wider ALS structural element — a crossbar, elevated platform, walkway, or support framework carrying multiple fixtures — is found damaged, distinct from damage isolated to a single support pole (ALS-283).
ALS crossbar, elevated platform/walkway, and support framework carrying multiple fixtures and their associated wiring.
After structural repair and re-certification (where a formal assessment was required), confirm correct electrical operation and alignment of every fixture on the structure before returning it to service.
SOP: SOP-ALS-11 (Structural Damage Assessment and Repair Procedure)
Standards: FAA AC 150/5345-46, ICAO Annex 14 Vol I, applicable structural design codes
Diagram: ALS Structure Engineering Drawing
Case Study: Division 27 — FOD & Physical Damage Case Studies
Symptom — An ALS fixture receives correct electrical power and the lamp/LED/flash source operates, but the fixture fails to produce the correct beam pattern — light appears scattered, absent in the expected direction, or grossly asymmetric.
ALS fixture optical assembly — reflector, lens system, and internal beam-forming components, including flash-tube reflector assemblies on sequenced flasher units.
Verify beam pattern visually from the design approach sightline (or with a goniophotometer if available) after repair, and re-inspect after several operating cycles, including a windy period, to confirm the fix is stable.
SOP: SOP-ALS-12 (Optical Assembly Inspection Procedure)
Standards: FAA AC 150/5345-46 (photometric requirements), ICAO Annex 14 Vol I Appendix 2
Diagram: ALS Fixture Optical Assembly Diagram
Case Study: Division 26 — Photometric & Intensity Compliance
Symptom — An ALS fixture or section, while electrically and mechanically functional, fails to meet the required photometric output (intensity, beam spread, or flash characteristics for sequenced flashers) when measured against ICAO/FAA standards during a compliance survey.
ALS fixture photometric performance as measured against ICAO Annex 14 Appendix 2 / FAA AC 150/5340-30 specifications for approach lighting.
Conduct a follow-up photometric survey of the corrected fixtures, and cross-check a sample of unaffected neighbouring fixtures to confirm the survey and correction are consistent.
SOP: SOP-ALS-13 (Photometric Compliance Survey Procedure)
Standards: ICAO Annex 14 Vol I Appendix 2, FAA AC 150/5340-30
Diagram: ALS Photometric Specification Sheet
Case Study: Division 26 — Photometric & Intensity Compliance
Symptom — The ALS master controller or sequenced flasher control unit fails to correctly command the system — for example, incorrect flash sequencing, failure to synchronise with the runway lighting state, or failure to respond to ALCMS commands — while field power distribution itself is confirmed sound.
ALS master controller / sequenced flasher control unit and its command interface to the CCR/ALCMS and field circuits.
Observe the ALS through at least one full commanded cycle (including any intensity-step and flasher-sequencing changes) to confirm correct, stable operation before closing out.
SOP: SOP-ALS-14 (Master Controller Fault Diagnosis Procedure)
Standards: ICAO Annex 14 Vol I, FAA AC 150/5345-46 (sequenced flasher systems)
Diagram: ALS Master Controller Wiring and Communication Schematic
Case Study: Division 01 — CCR Troubleshooting; Division 28 — Control System Diagnostics
Symptom — The ALCMS or remote monitoring system shows incorrect, missing, or stale status for the ALS — for example, reporting a fault when the field system is actually operating correctly, or failing to report a genuine field fault — indicating a monitoring/reporting issue rather than a true field fault.
ALS remote monitoring interface — status sensors, communication links, and the ALCMS display/logging system as it relates to ALS status reporting.
Monitor ALCMS status against independently verified field condition over a follow-up period, including at least one intensity-step change and, if applicable, a flasher sequencing cycle, to confirm the fix is stable.
SOP: SOP-ALS-15 (Remote Monitoring Verification Procedure)
Standards: ICAO Annex 14 Vol I, FAA AC 150/5345-46
Diagram: ALS Remote Monitoring and Communication Schematic
Case Study: Division 28 — Control System Diagnostics
Symptom — An ALS structure, fixture, or circuit is found with an earthing/bonding fault — high resistance to earth, a broken earth conductor, or a missing bond — identified either during a scheduled earth resistance test or following an electrical fault or lightning event.
ALS earthing and bonding system, including structure earth electrodes, bonding conductors between structural elements, and the connection to the overall airfield earthing grid.
Re-test earth resistance and full bonding continuity after repair, and repeat the test at the next scheduled interval to confirm the result remains stable, particularly through a seasonal soil-moisture cycle.
SOP: SOP-ALS-16 (Earthing and Bonding Test Procedure)
Standards: IEC 62305 (lightning protection), ICAO Annex 14 Vol I, applicable national electrical earthing standards
Diagram: ALS Structure Earthing and Bonding Drawing
Case Study: Division 29 — Earthing & Lightning Protection
Symptom — Water is found inside a fixture housing, junction box, or structure base enclosure during inspection or maintenance, with or without an associated electrical fault already having occurred.
ALS fixture housing, junction box, structure base enclosure, and their gasket/seal systems, across an area that frequently includes low-lying, unpaved, or wetland-adjacent terrain beyond the runway threshold.
Re-test insulation resistance after drying and resealing, and re-inspect the enclosure after the next significant rainfall or flood-risk period to confirm the ingress path has been fully resolved.
SOP: SOP-ALS-17 (Water Ingress Response Procedure)
Standards: FAA AC 150/5345-46 (environmental sealing requirements), ICAO Annex 14 Vol I
Diagram: ALS Structure and Enclosure Detail Drawing
Case Study: Division 25 — Field Case Study Troubleshooting
Quick answers about Approach Lighting System (ALS) troubleshooting in the AGL Troubleshooting Atlas.
Division 10 is the Approach Lighting System (ALS) Troubleshooting reference. It publishes 20 diagnostic topics, ALS-271 to ALS-290, for Approach Lighting System (ALS) faults on airfield ground lighting systems.
Every topic follows the same diagnostic record: the symptom, equipment/system, possible causes ranked by likelihood (high, medium or low), required tools, safety precautions, diagnostic procedure, test points, root cause verification, corrective action, preventive action and related references (SOPs, standards, diagrams and case studies).
The 20 topics are ALS-271 to ALS-290: Approach Light System Not Working; Partial Approach Light Failure; Multiple Approach Lights Failure; Approach Light Flickering; Approach Light Dim; Approach Light Wrong Color; Approach Light Intensity Step Failure; Approach Light Circuit Failure; Approach Light Cable Failure; Approach Light Transformer Failure; Approach Light Connector Failure; Approach Light Alignment Error; Approach Light Pole Damage; Approach Light Structural Damage; Approach Light Optical Failure; Approach Light Photometric Failure; Approach Light Control Failure; Approach Light Remote Monitoring Failure; Approach Light Earthing Failure; Approach Light Water Ingress.
Each procedure starts with observation before any intervention. For example, ALS-271 (Approach Light System Not Working) begins: Check the ALCMS/CCR panel to confirm whether the ALS regulator is commanded on and whether it is showing an output fault, a feedback fault, or genuinely zero output.
Each topic lists its own precautions. For example, ALS-271 (Approach Light System Not Working) starts with: Coordinate all approach-area access through ATC/airfield operations — ALS structures are frequently in the approach surface and may require additional clearance beyond a standard runway/taxiway closure.
Related references in the topics include SOP-ALS-01 (ALS Fault Isolation Procedure), SOP-CCR-04 (CCR LOTO Procedure), SOP-ALS-02 (Sub-Circuit Isolation Procedure), SOP-ALS-03 (Series Circuit Fault Location Procedure), SOP-ALS-04 (Lens Cleaning and Inspection Procedure), SOP-CCR-08 (Intensity Step Verification), SOP-ALS-05 (Cable Splice and Repair Procedure) and SOP-ALS-06 (Transformer Test and Replacement Procedure), and 11 more.
Where a standard applies, it appears in the topic's Related References. Those cited in this division include ICAO Annex 14 Vol I, FAA AC 150/5340-30, FAA AC 150/5345-46, IEC 60364, IEC 60502, FAA AC 150/5345-26, ICAO Annex 14 Vol I Appendix 2 and IEC 62305.
Use the search box at the top of the page to filter the 20 published topics by code, fault name or keyword; matching topics open automatically. Each diagnostic record can also be downloaded as a Word (.doc) file.
Approach lighting faults can disrupt sequenced flashing, crossbars, or centreline bars — each with different failure signatures.
Build the technical knowledge to understand approach lighting circuit topology, sequencing logic, and how to isolate a fault within a large, multi-fixture system under time pressure.
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Please read before relying on any content on this page or on any record downloaded from it.