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SSALS

A simplified short approach lighting system designed for non‑precision runways, typically consisting of a truncated, high-intensity centreline light-bar pattern extending 427 metres (1,400 ft) from the runway threshold. SSALS provides essential visual guidance for night and low‑visibility operations, offering a cost‑effective solution for smaller airports while maintaining safety standards.

SSALS - Simplified Short Approach Lighting System

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Overview

What Is It?

SSALS (Simplified Short Approach Lighting System) is a basic approach lighting system for non‑precision runways. It consists of a single row of steady‑burning white lights extending from the runway threshold into the approach area, for a distance of 427 metres (1,400 ft) under the FAA standard — effectively a truncated, high-intensity ALSF‑2 configuration with no crossbar or flashers. SSALS is a shorter, medium/high-intensity configuration designed for airfields with lower approach speeds and less demanding operational requirements than a full precision system. It provides pilots with a visual centreline reference during final approach, enhancing safety during night operations and marginal weather conditions without the complexity and cost of full precision approach lighting systems.

Purpose

Purpose & Function

SSALS exists to bring a basic centreline visual reference to smaller airfields where the traffic volume, approach speeds, and operational demands don't justify the length, or the cost, of a full-length approach lighting system. Its shortened configuration reflects a deliberate scaling decision: since lower approach speeds and simpler traffic patterns at these fields mean pilots need less lead distance to establish and confirm alignment, a shorter system still achieves the core purpose — giving a clear centreline reference during night and marginal-weather approaches — without the installation and maintenance burden of the full-length system. Its purpose is therefore about matching lighting infrastructure to the actual operational profile of smaller airfields rather than under-serving them with no system at all.

Application

Where Is It Used?

SSALS 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 and smaller aircraft
  • 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 where a shorter approach lighting system is sufficient due to terrain or approach speed considerations
Placement

Installation & Location

Fixtures are mounted on lightweight frangible stands set out along the extended runway centreline at 30 m (100 ft) spacing, running from the threshold out to 427 m (1,400 ft). 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. Its shorter 427 m length keeps the number of stands and the total cable run smaller than a full ALSF-2 installation, which suits smaller airfields with tighter budgets. 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 SSALS 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 at 30m (100 ft) spacing extends from the runway threshold out into the approach area for 427 metres (1,400 ft), providing a visual centreline reference.
  • Shorter Length: At 427 metres (1,400 ft), SSALS is a truncated version of the ALSF‑2 pattern, making it suitable for smaller airfields and lower approach speeds.
  • 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

SSALS runs on a single series circuit loop with no crossbar branch and no sequencer stage — every fixture along the shorter 427 m row is wired into the same loop and switches and dims together as one system, exactly as with the full-length ALSF-2 it truncates, just over a shorter run. 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 entire 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. Because the array is shorter than the full ALSF-2, the loop carries fewer fixtures and a lower total load, which is one of the reasons SSALS suits smaller airfields, but the control principle is identical. 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 → SSALS Series Circuit Loop (427 m) → 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 SSALS SERIES CIRCUIT LOOP (427 M) Shorter run, fewer fixtures, same control logic ISOLATING TRANSFORMER (PER FIXTURE) Taps fixed loop current to fixture secondary APPROACH ROW FIXTURE Steady white light at the commanded step SAME CONTROL LOGIC AS FULL-LENGTH SALS 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
Diagram

Array Length & SALS Comparison

Threshold (0 m) 30–60 m spacing → 427 m end
SSALS — 427 m Full ALSF-2 extends to 731–914 m
Solid = this system Hatched = longer alternative

Result: A shorter, single-row centreline reference sized for lower approach speeds — sufficient guidance without the cost of a full 731–914 m ALSF-2/MALSR precision system.

Construction

Physical Construction

Each fixture follows the same die-cast aluminium construction as a standard SALS unit: an LED array or 45–100W halogen lamp behind a toughened, gasket-sealed lens rated IP67/IP68, mounted on a frangible aluminium or composite stand bolted to a shallow footing or ground screw anchor. With no flasher stage or crossbar structures, all stands are wired into a single steady-burning series circuit through L-823 connectors and individual isolating transformers, with cable run in duct back to the regulator. Because the SSALS configuration is shorter than a full SALS array, the total number of stands, transformers, and cable runs is correspondingly smaller, reducing both material cost and installation time — a deliberate design trade that suits smaller airfields with tighter budgets. Stainless-steel fasteners and corrosion-resistant finishes are used throughout for continuous outdoor exposure.

Specification

Technical Parameters

ParameterTypical Value
System TypeSimplified Short Approach Lighting System (SSALS)
Light SourceLED array or halogen (45W – 100W)
ColourWhite (steady‑burning)
Configuration Length427 metres / 1,400 ft (FAA standard)
Light Spacing30m / 100 ft intervals (matches the parent ALSF‑2 pattern it truncates)
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 SSALS configuration figures
Test MethodMobile photometric van/goniophotometer or fixed test bench per fixture
Compliance

Applicable Standards

ICAO Annex 14

SSALS configuration, spacing, and photometric requirements

FAA AC 150/5345-46

Specification for SSALS components

IEC 61827

Electrical and photometric performance for AGL luminaires

FAA Engineering Brief #67

LED SSALS component performance requirements

Prerequisites

Installation Requirements

Frangible Stand Footing
Civil

Set each stand footing at 30 m (100 ft) spacing out to 427 m (1,400 ft), on shallow footings or ground screw anchors sized for the shorter array.

Elevated Piers at Minor Obstacles
Civil

Install piers only where the extended centreline crosses a road, ditch, or similar minor obstacle, since the shorter run has fewer such crossings to manage.

Duct & Cable Route
Electrical

Lay the duct run from each stand back to the regulator, sized for a single steady-burning series circuit with a smaller total cable run than a full SALS installation.

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 row stays true across the full 427 m run.

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 the isolating transformers 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 across the full 427m (1,400 ft) array 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 fixture in the array responds correctly and uniformly at each step.

Fixture Alignment & Aim Verification
Final Acceptance

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

Photometric Commissioning Test
Final Acceptance

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

Array Spacing & Configuration Check
Pre-Energisation

Survey light spacing along the 427m (1,400 ft) centreline against the as-designed 30m (100 ft) intervals, confirming the configuration meets the applicable FAA standard.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, and photometric readings alongside as-built array 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 SSALS 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

SSALS 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 SSALS 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.

Short Length Limitations

At 427 metres (1,400 ft), SSALS may not provide sufficient guidance for higher‑speed aircraft or for pilots requiring longer lead‑in. Airfields with faster traffic or more demanding operations may need to upgrade to a longer system like MALSR/ALSF‑1 (731m/914m) or a full precision system.

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 an elevated fixture base 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 or Off-Beam
Likely Cause
Wind loading, wildlife strike, or contact from a maintenance vehicle has knocked an elevated bar 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 short 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 shortened 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 over SSALS's shorter array length.
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 (Loose Crimp Connections)
Medium Severity
Root Cause
Loose or corroded primary/secondary crimp connections, or a marginal transformer winding under thermal load.
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

SSALS 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 before opening any enclosure.

Off-Runway Access
Personnel Safety

SSALS bars are positioned in the short 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

Shorter Length Doesn't Mean Lower Tolerance for Aim Error
Structural

Because SSALS's 427m configuration serves airfields with lower approach speeds, it's tempting to assume alignment tolerance is more forgiving; treat aim verification with the same rigor as a longer system since pilots still depend on it as their primary visual reference.

Verify Segment Isolation Even on a Short Run
Electrical

A short single-row loop still benefits from being wired so a fault can be localised rather than only detected as a general dimming or dark segment; this matters even more at smaller airfields with less frequent maintenance coverage.

Smaller Airfields Often Mean Less Frequent Maintenance Visits
Durability

SSALS installations at smaller, lower-traffic airfields can go longer between scheduled maintenance visits than systems at busier airports; weight the inspection interval to reflect the actual visit cadence rather than a generic schedule that assumes more frequent attention.

Track Intensity Trend Even at Lower-Traffic Fields
Photometric

It's easy to under-prioritise photometric trending at a smaller airfield with less regulatory scrutiny, but the pilots using this approach still depend on it as their primary visual reference; maintain consistent survey discipline regardless of traffic volume.

Rule Out CCR Output Before Replacing Multiple Lamps
Troubleshooting

Several fixtures appearing simultaneously dim is more often a CCR output issue than multiple coincidental lamp failures; verify regulator output directly before committing to lamp replacement across the row.

Keep As-Built Records Current for Future Category Upgrades
Upgrade Planning

If the airfield's traffic or category requirements grow, accurate current documentation of the SSALS as-built configuration makes planning an upgrade to a full SALS or MALS system considerably more straightforward.

Quick Answers

Frequently Asked Questions

Short answers about SSALS (Simplified Short Approach Lighting System): use, length, standards, maintenance and common faults.

Q1What is SSALS?

SSALS (Simplified Short Approach Lighting System) is a basic approach lighting system for non-precision runways. It uses steady-burning white lights extending from the runway threshold into the approach area to give a visual centreline reference.

Q2How long is an SSALS installation?

427 metres (1,400 ft) from the runway threshold.

Q3Does SSALS have flashing lights or a crossbar?

No. It is steady-burning only and does not include crossbar lights.

Q4Where is SSALS used?

On non-precision runways with VOR, NDB or GPS approaches, regional and general aviation airports with lower traffic, smaller airfields with limited AGL budgets and military airfields with basic approach requirements.

Q5What light sources does SSALS use?

White LED arrays or halogen lamps of about 45 W to 100 W.

Q6Which standards apply to SSALS?

The main references are ICAO Annex 14, FAA AC 150/5345-46, IEC TS 61827 and FAA Engineering Brief 67 for LED components. Always verify the current edition and your aerodrome's approved requirements.

Q7How often should SSALS be maintained?

Typically quarterly lens cleaning, semi-annual alignment checks with a theodolite or laser system and annual photometric intensity checks. Your airport's approved maintenance programme takes precedence.

Q8What are the common problems with SSALS?

Lens contamination, misalignment of elevated fixtures, power supply or CCR problems, and vegetation or obstruction growth around the lights at smaller airfields.

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