AGL Component Library By Precision AGL Academy

Simple Approach Lighting System (SALS)

A basic, cost‑effective approach lighting system consisting of a single row of lights extending from the runway threshold. Designed for non‑precision runways at smaller airfields, SALS provides pilots with essential visual guidance during final approach, enhancing safety without the complexity and cost of full precision approach lighting systems.

Simple Approach Lighting System (SALS)

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Overview

What Is It?

The Simple Approach Lighting System (SALS) is a basic approach lighting system designed for non‑precision runways. It consists of a single row of steady‑burning white lights extending from the runway threshold into the approach area, typically for a distance of 420 metres under the ICAO Simple Approach Lighting System standard (centreline at 60m intervals, with a single crossbar at 300m). Note: "SALS" is primarily an ICAO/historical term; the closest current FAA counterpart is the SSALS (Simplified Short Approach Lighting System), a 427m/1,400 ft truncated ALSF‑2 configuration — the two are not directly interchangeable and site documentation should confirm which standard actually applies. Unlike more complex systems such as ALSF‑1 or MALSR, SALS does not include sequenced flashing lights or crossbar lights. It provides pilots with a basic visual reference for aligning with the runway centreline during final approach, making it a practical and economical solution for smaller airports, regional airfields, and general aviation facilities.

Purpose

Purpose & Function

SALS exists to give smaller airports, regional airfields, and general aviation facilities a functional visual centreline reference for night and marginal-weather approaches, at a fraction of the cost and infrastructure demand of a precision system. Its deliberate simplicity — a single row of steady-burning lights with no crossbars or sequenced flashing — reflects a purpose scoped specifically to basic alignment rather than the fine distance, depth, and directional cues that ALSF-class systems provide, which are unnecessary at fields without the traffic volume or low-visibility operations that would justify them. Its purpose is therefore about accessibility: providing a meaningful safety improvement over having no approach lighting at all, calibrated to what smaller facilities can practically support.

Application

Where Is It Used?

SALS systems are installed at airports that support non‑precision approaches. They are typically used on:

  • Non‑precision runways with VOR, NDB, or GPS approaches
  • Regional and general aviation airports with lower traffic volumes
  • Smaller airfields with budget constraints for AGL infrastructure
  • Military airfields with basic approach requirements
  • Runways with visual approaches that benefit from enhanced night guidance
  • Airports transitioning to higher categories where SALS serves as a baseline
Placement

Installation & Location

Fixtures are mounted on lightweight frangible stands set out along the extended runway centreline at 60 m spacing, running from the threshold out to 420 m, with a single crossbar at the 300 m point. With no flashing circuit or crossbar structures to coordinate, the array is wired as a single steady-burning series circuit, with cable run in duct from each stand back to the regulator. Stand loads are modest, so elevated piers are needed only where the extended centreline crosses a road, ditch, or similar minor obstacle. Setting-out is tied to the runway centreline extended and threshold survey.

Function

How Does It Work?

The SALS system operates on a simple principle: a row of lights provides a visual centreline reference for the pilot:

  • Single Row of Lights: A row of steady‑burning white lights (typically 30m to 60m spacing) extends from the runway threshold out into the approach area, providing a visual centreline reference.
  • Length: The system typically extends 420 metres from the threshold under the ICAO standard, with a single crossbar at 300m. The nearest FAA equivalent, SSALS, extends 427 metres (1,400 ft) — the two standards use different fixture spacing and are not identical.
  • Lateral Guidance: The row of lights helps the pilot align the aircraft with the runway centreline during the final approach segment.
  • Distance Reference: The spacing of the lights provides a rough distance reference, helping the pilot judge the approach path.
  • Intensity Control: The lights are typically controlled by a CCR with intensity steps (usually 3‑step or 5‑step), allowing the ATC to adjust brightness for visibility conditions.
  • Simplicity: The system has no flashing lights, crossbars, or complex sequencing, making it simple to install, operate, and maintain.
Architecture

System Architecture & Control Logic

SALS runs on a single series circuit loop with no sequencer stage — every fixture along the 420 m row (plus its single 300m crossbar) is wired into the same loop and switches and dims together as one system, making it the most straightforward control chain in the approach lighting family. An Airfield Lighting Control and Monitoring System (ALCMS), operated by the tower or an automated visibility-linked routine, selects the required brightness step; this command is passed to the CCR, which regulates the whole row to the corresponding fixed current. Every fixture, via its own isolating transformer, draws from the same current and therefore burns at the same intensity simultaneously — there is no way to command an individual light, or a section of the row, independently of the rest. Fault detection follows the same loop-based principle used across the AGL series circuit family: the CCR continuously monitors loop voltage against the commanded current, and a voltage rise at constant current signals increased circuit impedance, typically an open-circuit lamp or a failed isolating transformer, reported to the ALCMS as a loop fault rather than pinpointed to an exact fixture without further sectionalised testing.

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

AIRFIELD LIGHTING CONTROL SYSTEM (ALCMS) Selects brightness step (RVR / ATC / PCL) CONSTANT CURRENT REGULATOR Converts step command to fixed current SALS SERIES CIRCUIT LOOP No crossbar branch, no sequencer stage ISOLATING TRANSFORMER (PER FIXTURE) Taps fixed loop current to fixture secondary APPROACH ROW FIXTURE Steady white light at the commanded step SIMPLEST CONTROL CHAIN IN THE AGL FAMILY Whole row switches and dims as one unit Faults are isolated by loop testing, not fixture ID LOOP FEEDBACK CCR tracks loop voltage against commanded current Voltage rise flags an open circuit or failed transformer
Engineering View

Approach Row Length Overview

Approach direction → RUNWAY THRESHOLD STEADY WHITE, 30–60m SPACING — NO FLASHING ICAO STANDARD — 420m FAA SSALS — 427m

The entire system is one steady-burning row on a single series circuit. ICAO's SALS (420m, 60m spacing, single 300m crossbar) and the FAA's nearest counterpart, SSALS (427m, no crossbar), are different configurations of the same basic idea, not the same fixture carried a different distance — verify which standard actually applies to a given site rather than treating the figures as interchangeable. There's nothing sequenced in either, which is what keeps this family cheap to install and maintain relative to ALSF-type systems.

Construction

Physical Construction

Each fixture is a die-cast aluminium housing containing an LED array or 45–100W halogen lamp behind a toughened lens, gasket-sealed with an O-ring or silicone seal to achieve an IP67/IP68 rating, mounted on a frangible aluminium or composite stand bolted to a shallow concrete footing or ground screw anchor. With no flasher stage or crossbar structures to build, the array consists of identical stands at uniform spacing, all wired into a single steady-burning series circuit. Internal wiring terminates at L-823 primary connectors sealed for direct burial, which mate to the secondary leads of the isolating transformer housed at the base of each stand, with cable run in duct back to the regulator. Stainless-steel fasteners and corrosion-resistant finishes are used throughout to withstand continuous outdoor exposure over unprepared approach terrain.

Specification

Technical Parameters

ParameterTypical Value
System TypeSimple Approach Lighting System (SALS)
Light SourceLED array or halogen (45W – 100W)
ColourWhite (steady‑burning)
Configuration Length420m (ICAO SALS standard, with a single crossbar at 300m) — nearest FAA counterpart is SSALS at 427m/1,400 ft (no crossbar)
Light Spacing60m intervals (ICAO SALS)
FlashingNone (steady‑burning only)
Crossbar LightsNot included
Intensity Steps3‑step or 5‑step CCR controlled (2.8A – 6.6A)
Beam PatternUni‑directional towards approach
Mounting TypeElevated or flush‑mounted (inset)
Isolating Transformer45W – 100W (6.6A series circuit)
Protection ClassIP67 / IP68 (submersible)
SupportNon‑precision approaches (VOR, NDB, GPS)
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries circuit, constant current (CCR fed)
Rated Series Current6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A)
IsolationVia dedicated isolating transformer (45W – 100W), not directly connected to series loop
Transformer SecondaryMatched to fixture wattage; sized to series circuit rating
Cable TypeL-824 single-conductor, direct-burial rated, 5kV or 600V per circuit design
ConnectorL-823 primary connector, submersible-rated splice
Insulation Resistance≥ 50 MΩ (megger test, cable-to-ground)
Earthing/GroundingFixture body 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
Centreline Bar Intensity200 – 1,500 cd (white, low-to-medium intensity)
Intensity Steps100% / 30% / 10% of rated peak intensity (3-step typical)
Vertical Beam SpreadMain beam 2°–10° above horizontal (peak ~3°–4°)
Horizontal Beam Spread± 4.5° either side of runway centreline extended
ChromaticityWhite within ICAO Annex 14 boundary
Maintenance Factor≥ 50% of new-fixture intensity before replacement/cleaning is due
Intensity Tolerance± 25% of rated value at each CCR step (field measurement)
Isocandela DistributionPer ICAO Annex 14 Attachment A SALS configuration figures
Test MethodMobile photometric van/goniophotometer or fixed test bench per fixture
Compliance

Applicable Standards

ICAO Annex 14

SALS configuration, spacing, and photometric requirements

FAA AC 150/5345-46

Specification for SALS components

IEC 61827

Electrical and photometric performance for AGL luminaires

FAA Engineering Brief #67

LED SALS component performance requirements

Prerequisites

Installation Requirements

Frangible Stand Footing
Civil

Set each stand footing at 60 m spacing out to 420 m (ICAO SALS), or per the applicable local standard if a different configuration is specified, on shallow concrete footings or ground screw anchors.

Elevated Piers at Minor Obstacles
Civil

Install piers only where the extended centreline crosses a road, ditch, or similar minor obstacle, since stand loads are modest across the rest of the run.

Duct & Cable Route
Electrical

Lay the duct run from each stand back to the regulator, sized for a single steady-burning series circuit with no flasher or crossbar circuits to coordinate.

L-823 Connector Termination
Electrical

Terminate and seal the primary connector at each stand per manufacturer procedure, keeping every splice fully submersible-rated before backfill.

Isolating Transformer Matching
Electrical

Confirm each fixture's isolating transformer wattage matches the series circuit's rated current step before connection.

Stand & Fixture Assembly
Mechanical

Fix the die-cast fixture housing to each frangible stand, torquing fittings to spec so the stand shears cleanly under lateral load.

Setting-Out to Extended Centreline
Mechanical

Tie stand positions to the extended runway centreline and threshold survey so the uniformly spaced row stays true across the full configuration length.

Pre-Energisation Sign-off
Documentation

Record stand positions, cable route, 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 each isolating transformer and the full 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 across the full 420m run 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 each 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 every stand along the row responds together, ruling out marginal transformers or loose connections.

Fixture Alignment & Aim Verification
Final Acceptance

Check elevation and azimuth of each stand against the design aiming diagram, correcting any deviation before sign-off.

Photometric Commissioning Test
Final Acceptance

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

Frangibility & Mounting Verification
Pre-Energisation

Confirm the frangible coupling, footing or ground screw depth, and stand height meet as-built tolerances before the site is finally backfilled.

Documentation & As-Built Sign-off
Final Acceptance

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

Upkeep

Inspection & Maintenance

Photometric Intensity Check
Annual

Verify beam intensity against ICAO / FAA thresholds using a calibrated photometer; degraded output usually points to lens haze or an aging light source.

Lens Cleaning
Quarterly

Clean environmental pollutants, bird droppings, and de-icing residue from each fixture, especially the more distant lights which must remain clearly visible.

Alignment Check
Semi-annual

Verify fixture aim using a theodolite or laser alignment system, since wind, wildlife, or vehicle strikes can knock elevated fixtures out of tolerance.

Site Survey & Vegetation Clearance
Semi-annual

Walk the approach line to confirm no vegetation or structures have grown up to obstruct the light output since the last inspection.

CCR & Power Quality Check
Annual

Monitor voltage stability and CCR step response, since even a simple system like SALS can suffer inconsistent brightness under power fluctuation.

Insulation Resistance Test
Annual

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

Cable & Connector Inspection
Annual

Examine primary and secondary cable connections for corrosion or loose crimps, a common source of intermittent series-circuit faults.

Housing & Base Inspection
Annual

Check base cans, mounting stakes, and surrounding pavement or turf for settlement, cracking, or debris that could affect frangibility or drainage.

Field Notes

Common Field Issues

Lens Contamination

SALS components are exposed to environmental pollutants, bird droppings, and de‑icing chemicals. Regular cleaning with approved solvents and soft brushes is essential to maintain light output and visibility, especially for the distant lights which must be clearly seen.

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 to maintain the correct beam direction.

Power Supply and CCR Issues

Even a simple system like SALS requires reliable power. Voltage fluctuations, CCR faults, or cable damage can cause inconsistent brightness or total failure. Regular power quality monitoring and cable testing are recommended.

Vegetation and Obstruction Growth

At smaller airfields, vegetation or structures can grow up around approach lights, obstructing the light output. Regular site inspections and vegetation management are essential to maintain clear lines of sight.

Diagnostics

Troubleshooting Guide

Single Bar/Light 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 array (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.
CCR Trips on Overcurrent or Ground Fault
Likely Cause
Moisture ingress at a fixture or connector has degraded insulation resistance, creating a short or a partial ground fault on the series loop.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect fixtures 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 on Distant Bars
Likely Cause
Lens contamination from environmental pollutants or de-icing residue, or an aging light source, is most noticeable on the furthest bars from the runway threshold.
Diagnostic Steps
Run a photometric intensity check against ICAO/FAA thresholds; inspect and clean the lens; confirm the CCR is set to the correct intensity step for prevailing conditions.
Corrective Action
Clean or replace the lens, replace a degraded light source, or correct the CCR step setting; re-verify with a follow-up photometric reading.
Elevated Fixture Misaligned
Likely Cause
Wind loading, wildlife strike, or contact from a maintenance vehicle has knocked an elevated fixture off its aiming tolerance, or the frangible coupling has begun to fatigue.
Diagnostic Steps
Re-check fixture aim with a theodolite or laser alignment system against the approach centreline; inspect the frangible coupling and mounting stake for cracking, play, or settlement.
Corrective Action
Re-level and re-aim the fixture, replace the frangible coupling if fatigued, and address any base or subgrade settlement to prevent recurrence.
Flickering or Intermittent Brightness
Likely Cause
Loose or corroded primary/secondary crimp connections, or CCR power-quality instability upstream of the array.
Diagnostic Steps
Inspect and re-torque cable connections at the fixture base can; check for corrosion on crimps; monitor CCR supply voltage and step response under load.
Corrective Action
Re-terminate corroded connections with new crimps and sealant, or address the upstream power-quality issue if CCR step response is confirmed unstable.
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 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.
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 the CCR or darkens the entire series loop feeding the approach lights.
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 Bar 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
Bar leans, loosens, or separates from its mounting stake, pulling the light out of aim tolerance along the approach centreline.
Detection Method
Physical inspection for cracking or play in the coupling, and periodic fixture-aim checks with a theodolite or laser alignment system.
CCR Regulation Fault
High Severity
Root Cause
Internal component failure (control board or output stage), a load mismatch after circuit modification, or a firmware/setpoint fault.
Effect
Incorrect brightness step, failure to hold regulated current across the loop, or nuisance tripping on an otherwise healthy circuit.
Detection Method
CCR self-diagnostic/fault indication, output current verification, and a load-bank test to confirm regulation across all intensity steps.
Lens Contamination / Reduced Intensity on Distant Bars
Low Severity
Root Cause
Environmental pollutants, de-icing residue, or airborne particulate building up on the lens surface, an effect that shows up first on the outermost bars furthest from routine ground-crew traffic.
Effect
Reduced or hazy light output on the distant bars that can fall below the photometric thresholds needed to maintain a continuous visual reference along the approach.
Detection Method
Scheduled photometric intensity testing and visual inspection of the lens on each bar during routine cleaning, with particular attention to the furthest fixtures.
Flickering / Intermittent Brightness from Loose Connections
Medium Severity
Root Cause
Loose or corroded primary/secondary crimp connections, or a marginal transformer winding under thermal load, common on older SALS installations nearing the end of their service life.
Effect
Bar flickers or shows intermittent brightness rather than a hard failure, which can be mistaken for a healthy fixture on a quick visual check.
Detection Method
Inspect and re-torque all cable connections at the fixture base can, check for corrosion on crimps, and monitor secondary voltage for drop under load once the CCR has warmed up.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

SALS bar circuits run on a constant-current series loop that can carry several kV. De-energise and lock out the associated CCR, then verify zero energy at the bar or crossbar before opening any enclosure.

Off-Runway Access
Personnel Safety

SALS bars are positioned in the approach area beyond the runway end, often on unpaved or uneven ground; assess ground conditions before positioning vehicles or personnel near a bar.

Frangibility Not to Be Defeated
Mechanical

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

Airside Work Coordination
Operational

Work on approach lighting affects an active runway's usable minima; obtain ATC/airside coordination and issue a NOTAM before any bar is taken out of service, and keep personnel and vehicles clear of the approach surface during aircraft operations.

Hot Lamp / Housing Contact
Personnel Safety

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

FOD Control at the Bar
Operational

Account for tools, fasteners, and hardware at every bar 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 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 a bar out of aim tolerance or at reduced intensity; verify photometric and positional conformance before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Simplicity Doesn't Reduce the Need for Aim Verification
Structural

Because SALS has no SFL or crossbar complexity to draw attention, its basic centreline aim can drift unnoticed for longer than on a more actively monitored precision system. Keep alignment checks on a defined schedule rather than deprioritising them because the system is 'simple.'

A Single-Row Loop Still Deserves Segment Fault Isolation
Electrical

Even a basic single-row configuration benefits from being wired so a fault can be localised to a segment rather than only detected as 'something in the row is dark'; this shortens troubleshooting time considerably on longer runs.

Distant Lights See the Most Neglect on Simple Systems
Durability

The lights furthest from the threshold are the least visible from the airport operations area and the easiest to under-inspect on a basic system; without a deliberate weighting, they accumulate contamination and misalignment fastest.

Track Intensity Even Where There's No Precision-Approach Requirement to Force It
Photometric

Because SALS isn't tied to a precision-approach category with strict periodic survey requirements, intensity trending can slip in practice. Maintain the same discipline as a regulated system since pilots are still relying on this as their primary visual reference.

Verify CCR Output Before Assuming Multiple Lamp Failures
Troubleshooting

A CCR operating below its rated output can present as several fixtures being simultaneously dim rather than one obviously failed unit; check regulator output directly before replacing several lamps that may not actually be at fault.

Document Baseline Condition Before Any Future MALS/MALSR Upgrade
Upgrade Planning

If an upgrade to a more capable system is ever planned, having current, well-documented survey and as-built records for the existing SALS installation makes scoping that upgrade considerably faster and more accurate.

Quick Answers

Frequently Asked Questions

Short answers about the Simple Approach Lighting System (SALS): layout, use on non-precision runways, intensity, standards, maintenance and common faults.

Q1What is a Simple Approach Lighting System (SALS)?

SALS is a basic approach lighting system for non-precision runways. It is a single row of steady-burning white lights extending from the runway threshold into the approach area, typically 420 m under the ICAO standard, with centreline lights at 60 m intervals and a single crossbar at 300 m.

Q2Is SALS the same as the FAA's SSALS?

No. SALS is primarily an ICAO/historical term. The nearest current FAA counterpart is SSALS (Simplified Short Approach Lighting System), a 427 m (1,400 ft) truncated ALSF-2 configuration with no crossbar. The two use different fixture spacing and are not interchangeable, so site documentation should confirm which standard applies.

Q3Why use SALS instead of a precision approach lighting system?

It gives smaller airports, regional airfields and general aviation facilities a functional visual centreline reference for night and marginal-weather approaches at a fraction of the cost and infrastructure of a precision system. It provides basic alignment rather than the fine distance and depth cues of precision systems.

Q4Which runways use SALS?

Non-precision runways with VOR, NDB or GPS approaches, regional and general aviation airports, smaller budget-constrained airfields, military airfields with basic approach requirements, and airports transitioning to higher categories where SALS is a baseline.

Q5Does SALS flash?

No. It is steady-burning only, with no sequenced flashing and, in the FAA-style layout, no crossbars. It is wired as a single steady-burning series circuit.

Q6How bright is SALS?

Centreline bar intensity is 200–1,500 cd (white, low-to-medium intensity), with a typical 3-step (100%, 30%, 10%) intensity control, or 3- or 5-step CCR control (2.8–6.6 A). The beam is unidirectional toward the approach, about ±4.5° either side of the extended centreline.

Q7How is SALS installed?

Fixtures are on lightweight frangible stands set along the extended runway centreline at 60 m spacing out to 420 m, with a single crossbar at 300 m. Each fixture has a 45–100 W isolating transformer on a 6.6 A series circuit, and cable runs in duct back to the regulator. Elevated or flush-mounted fixtures may be used.

Q8Which standards apply to SALS?

The main references are ICAO Annex 14 (SALS configuration, spacing and photometrics), FAA AC 150/5345-46, IEC 61827 and FAA Engineering Brief #67 (LED component performance). Always verify the current edition and your approved requirements.

Q9How often should SALS be maintained?

Typical intervals are quarterly for lens cleaning, semi-annual for alignment checks with a theodolite or laser and site survey and vegetation clearance, and annual for photometric intensity checks and CCR and power quality checks. Your approved maintenance programme takes precedence.

Q10Why is one light dark while the rest of the array works?

A failed lamp or LED source, or an open isolating transformer at that fixture. Confirm loop continuity through the transformer primary, megger the transformer and check secondary voltage at the connector, then replace the lamp or swap the transformer and re-seal the L-823 connectors.

Q11Why is the whole array dark or the CCR unable to regulate?

An open circuit in the series loop, such as a severed cable, corroded splice or a failed transformer acting as an open point. Check the CCR fault indication first, then loop-resistance test from the CCR output to isolate the faulted segment.

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