AGL Component Library By Precision AGL Academy

VASI

Visual Approach Slope Indicator – a two‑bar or three‑bar visual guidance system that provides pilots with a red/white indication of their position relative to the correct glide path. VASI is a proven, simple system that has been in use for decades, offering reliable approach guidance for both day and night operations.

VASI (Visual Approach Slope Indicator) two-bar red/white glide slope lights

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Overview

What Is It?

The Visual Approach Slope Indicator (VASI) is a visual guidance system that helps pilots maintain the correct glide path during final approach. It consists of a series of light units arranged in bars (typically two or three bars) on the left side of the runway. Each bar projects a red or white light depending on the pilot's viewing angle. The combination of red and white bars indicates whether the aircraft is above, below, or on the correct glide slope.

VASI is one of the oldest and most widely used visual glide slope systems. It provides a clear, unambiguous signal that requires no special equipment on the aircraft. The system is simple, reliable, and cost‑effective, making it suitable for a wide range of airports, from small general aviation fields to larger commercial airports.

Purpose

Purpose & Function

VASI exists to answer one question for an approaching pilot — am I on the correct glide path, or am I too high or too low — using nothing more than red and white light and the aircraft's own eyes, without requiring any onboard equipment or electronic glide slope receiver. This makes it usable by any aircraft regardless of avionics fit, which is part of why it became one of the most widely adopted visual glide slope systems at airports of every size.

The multi-bar arrangement gives the pilot a graduated read: the relationship between the near and far bars shifts as the aircraft moves above or below the ideal path, letting a pilot correct smoothly and early rather than discovering a deviation only once it has become significant, which is especially valuable during the final stages of approach when altitude for correction is limited.

Application

Where Is It Used?

VASI is deployed on a wide range of runways and landing sites:

  • Non‑precision runways – providing essential visual glide slope guidance.
  • General aviation airports – where cost and simplicity are key.
  • Military airfields – supporting training and operational approaches.
  • Regional and remote airstrips – with limited infrastructure.
  • As a backup to PAPI – on precision runways for redundancy.
  • Heliports – where a simple glide path reference is needed.
Placement

Installation & Location

VASI uses two light bars — a near (downwind) bar and a far (upwind) bar — mounted on one side of the runway, normally the left, at a fixed lateral offset from the runway edge clear of the obstacle-limitation surface and blast zones. The bars are set back from the threshold at distances derived from the design tables, spaced apart along the runway so that on the correct glide path the near bar shows white and the far bar shows red, with the vertical separation between the two producing the visual "on-slope" cue. Setting-out is tied to the runway centreline and threshold survey so both bars sit on the same design glide path, and each unit within a bar is mounted on its own frangible coupling and individually aimed and levelled during commissioning. Cabling from each bar runs underground back to its constant current regulator, and on wide-body runways a second pair of bars may be installed on the opposite side to give a full box configuration.

Function

How Does It Work?

VASI operates on a simple optical principle that provides immediate visual feedback to the pilot:

  • Configuration: VASI typically consists of two or three light bars (e.g., 2‑bar VASI or 3‑bar VASI). Each bar contains multiple light units that project a beam with a distinct red/white transition. The bars are positioned at different distances from the runway threshold and set to slightly different angles.
  • Colour Indication: The pilot sees a combination of red and white bars. For a standard 2‑bar VASI (one near bar and one far bar):
    • Both white – aircraft is well above the glide path.
    • Near bar white / Far bar red – on the correct glide path.
    • Both red – aircraft is well below the glide path.
    For a 3‑bar VASI, the indication is more nuanced, with the middle bar providing a reference for specific aircraft types (e.g., high‑wing vs. low‑wing).
  • Power and Control: VASI units are powered from the constant current series circuit via isolating transformers, with intensity controlled by the CCR (typically 3‑step or 5‑step). Brightness can be adjusted for day, twilight, and night operations.
  • Integration: VASI is typically deployed independently or integrated with the runway lighting system. It may be controlled remotely via the ALCMS if connected.
Architecture

System Architecture & Control Logic

VASI's glide path signal is generated entirely by fixed optics, with the circuit doing nothing more than powering the lamps. Every light unit's lens/shutter assembly is levelled and tilted at commissioning so its red/white transition falls at a specific elevation, and the bars — near and far in a 2-bar system, or near/middle/far in a 3-bar system — are aimed at slightly different angles from each other so that, together, they straddle the design glide path. That geometry is permanent hardware alignment, checked periodically by ground or flight inspection, not something any control system adjusts in real time. All units across all bars are powered from the same constant current series circuit through their own isolating transformers, and the CCR (or ALCMS where connected) sets one shared brightness step for day, twilight, or night — a command that changes overall brightness only, never which bar or unit shows red or white. Loop-level fault detection works as on any series circuit: the CCR watches loop voltage against commanded current, and a rise reports an open lamp or failed transformer as a loop fault, sectionalised by further testing rather than pinpointed automatically.

CCR / ALCMS → Series Circuit Loop → Isolating Transformer → Bar (Near / Far / Middle, each fixed to its own angle)

CCR / ALCMS Selects shared brightness step SERIES CIRCUIT LOOP Same current to every bar — brightness only ISOLATING TRANSFORMER (PER UNIT) Taps fixed loop current to each light unit BAR (NEAR / FAR / MIDDLE) Each bar aimed at its own fixed elevation Fixed at commissioning — no runtime control SIGNAL IS OPTICAL, NOT ELECTRONIC The near/far colour combination comes from fixed aim, not from any command the circuit sends LOOP FEEDBACK CCR tracks loop voltage against commanded current; a rise flags a lamp/transformer fault, not misaim
Pilot's View

Reading the Glide Path from Bar Colour

2‑Bar VASI — Near Bar (closer to threshold) & Far Bar
Far Bar
Near Bar
Above Glide Path

Both bars appear white — aircraft is flying too high on approach.

Far Bar
Near Bar
On Glide Path

Near bar white, far bar red — aircraft is on the correct 3° slope.

Far Bar
Near Bar
Below Glide Path

Both bars appear red — aircraft is flying too low on approach.

A 3‑bar VASI adds a middle bar so high‑wing and low‑wing aircraft, which sit the pilot's eye at different heights, each read the correct near/far pairing for their own cockpit position.

Construction

Physical Construction

Each VASI unit in a wing bar is a wide, box-section housing in die-cast aluminium alloy or louvred galvanised steel, containing several lamp/optic pairs side by side so the bar presents as a single elongated light source rather than a row of separate fixtures. The optics are split into an upper clear (white) glass and a lower red filter glass, precisely positioned so the beam transitions from white to red at the set glide-path angle, with a built-in levelling and pitch-adjustment mechanism used to aim each bar during commissioning. Downwind and upwind bars are mounted on separate frangible masts set at surveyed heights either side of the touchdown zone, engineered to shear away cleanly if struck. Cabling runs underground in conduit to isolating transformers housed in nearby base cans, with sealed, direct-burial connectors and a drainage provision to keep the transformer and cable entries free of standing water.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array or 45W/65W halogen lamp
ColourWhite (upper beam) and Red (lower beam) per unit
Luminous IntensityUp to 15,000 cd (white) and 8,000 cd (red) depending on setting
Intensity Steps3‑step (day, twilight, night) or 5‑step (2.8A – 6.6A) CCR controlled
Glide Path AngleTypically 3° (2.5° to 4° adjustable)
Beam PatternNarrow vertical beam with a sharp red/white transition
Number of Bars2 (standard) or 3 (3‑bar VASI)
Mounting TypeElevated (frangible poles) – typically 10–20 m from runway edge
Isolating Transformer45W – 65W (6.6A series circuit) per unit
Protection ClassIP67 / IP68 (weather‑resistant)
Operating Temperature-40°C to +55°C
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) or 3-step equivalent
IsolationVia dedicated isolating transformer (45W/65W) per unit
Bar SynchronisationUpwind and downwind bars powered from circuits synchronised to the same intensity step
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
Main Beam Intensity (White)≥ 10,000 cd on-axis per unit, up to 15,000 cd at full intensity
Main Beam Intensity (Red)≥ 5,000 cd on-axis per unit, up to 8,000 cd at full intensity
Transition Sharpness (Red/White)≤ 4 arc-minutes vertical transition band per bar
Vertical Beam SpreadNear and far bars set at slightly different elevations (typically ~20 arc-minutes apart) to build the composite signal
Horizontal Beam Spread± 5° to ± 10° either side of runway centreline plane
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures
Chromaticity (White)Within ICAO Annex 14 white boundary (CIE coordinates)
Chromaticity (Red)Within ICAO Annex 14 red boundary (CIE coordinates)
Intensity Tolerance± 25% of rated value at each CCR step (field measurement)
Maintenance Factor≥ 50% of new-fixture intensity before lamp/lens replacement is due
Test MethodMobile photometric van/goniophotometer or fixed test bench per bar
Compliance

Applicable Standards

ICAO Annex 14

VASI specifications and installation requirements

FAA AC 150/5340-25

Visual Approach Slope Indicator (VASI) Systems

FAA AC 150/5345-46

Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures

IEC/TS 61827

Characteristics of inset and elevated luminaires used on aerodromes and heliports (photometric & electrical performance)

Prerequisites

Installation Requirements

Near/Far Bar Setout
Civil

Set out the near (downwind) and far (upwind) bars at the design-table distances from the threshold, tied to the runway centreline and threshold survey so both bars sit on the same design glide path.

Frangible Pole Foundations
Civil

Install footings at a fixed lateral offset from the runway edge, clear of the obstacle-limitation surface and blast zones, for the near and far bar poles (and the second pair, where a full box configuration is specified).

Duct & Cable Route to CCR
Electrical

Run underground cabling from each bar back to its constant current regulator, keeping the near and far bar circuits separately traceable.

Isolating Transformer Matching
Electrical

Confirm each unit's 45W–65W isolating transformer matches the series circuit's rated current step before connection.

Unit-by-Unit Aiming & Levelling
Mechanical

Aim and level each unit within both bars during commissioning so the correct on-slope condition shows white on the near bar and red on the far bar.

Frangible Coupling Fixing
Mechanical

Torque frangible pole couplings to the specified value for every unit in both bars.

Box Configuration Verification
Documentation

Where a second bar pair is installed on the opposite side for a full box configuration, confirm both pairs are set out to the same design glide path before commissioning.

Pre-Energisation Sign-off
Documentation

Record survey coordinates, cable routes, and torque values for both bars as-built before the site is closed.

Verification

Testing & Commissioning

Insulation Resistance (Megger) Test
Pre-Energisation

Megger-test each bar's isolating transformer(s) and the series loop before energisation, 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 downwind and upwind bars 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 bar's connectors 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 all bars respond correctly and in unison at each step.

Bar-to-Bar Glide Path Angle Verification
Final Acceptance

Set the downwind and upwind bars' red/white transition angles with a calibrated aiming tool or theodolite, confirming the correct angular offset between bars so the on-path (or on-slope) indication reads correctly from the approach.

Photometric Commissioning Test
Final Acceptance

Measure red and white beam intensity, colour, and transition sharpness on each bar with a calibrated photometer against ICAO/FAA commissioning tolerances.

Frangibility & Mounting Verification
Pre-Energisation

Confirm each bar's frangible mast shear point, base height, and surveyed position meet as-built tolerances before the site is finally backfilled.

Documentation & As-Built Sign-off
Final Acceptance

Record insulation, continuity, voltage, and photometric readings for all bars alongside as-built position and aiming angles in the commissioning dossier.

Upkeep

Inspection & Maintenance

Bar Alignment & Setting Check
Annual

Calibrate each bar's beam angle with precision optical tools, since an incorrect setting on any bar can produce a misleading glide slope indication.

Photometric Intensity Check
Annual

Verify white and red beam intensity and the red/white transition across all bars against ICAO thresholds using a calibrated photometer.

Lens Cleaning
Quarterly

Clean dust, rubber deposits, and de-icing fluid residue from each unit's lens to maintain colour transition integrity.

Lamp / LED Module Inspection
Semi-annual

Check each bar's light source for failure and replace promptly to avoid a misleading glide slope indication.

Frangible Coupling Check
Annual

Inspect couplings for fatigue from wind loading and thermal cycling and replace on schedule to preserve breakaway performance.

Insulation Resistance Test
Annual

Megger-test each bar's isolating transformer and series circuit 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.

Mounting Pole Inspection
Annual

Check pole verticality and base condition for each of the two or three bars to keep the array correctly positioned relative to the runway edge.

Field Notes

Common Field Issues

Bar Alignment and Setting

VASI requires precise alignment of each bar's beam angle. Incorrect settings can lead to misleading glide slope indications. Regular calibration using precision optical tools is essential.

Lens Contamination

Dust, rubber deposits, and de‑icing fluids can reduce light output and affect colour transition. Routine cleaning and photometric testing are required.

Lamp or LED Failure

In halogen systems, lamp burnout is common. In LED systems, individual LEDs may fail. Regular inspections and prompt replacement are necessary to avoid misleading indications.

Frangible Coupling Fatigue

VASI units are mounted on frangible poles. Wind loading and thermal cycling can weaken couplings. Regular inspection ensures breakaway performance on impact.

Diagnostics

Troubleshooting Guide

Single Bar Dark, Other Bar(s) Normal
Likely Cause
Failed LED array / lamp within one or more units of that bar, or an open isolating transformer feeding it.
Diagnostic Steps
Confirm series loop continuity through the affected bar's transformer primary; megger the transformer; check secondary voltage at the connector with the CCR energised.
Corrective Action
Replace the failed lamp/LED module if the transformer checks healthy; otherwise swap the isolating transformer and re-seal the connectors before backfill.
Entire Series Circuit Dark / CCR Will Not Regulate
Likely Cause
Open-circuit fault in the series loop feeding the VASI bars (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 between bars 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 unit, connector, or base can has degraded insulation resistance, creating a short or partial ground fault on the series loop.
Diagnostic Steps
Megger the full circuit to identify the low-resistance segment; visually inspect suspect units for cracked gaskets, condensation, or damaged secondary cable jackets.
Corrective Action
Dry out or replace the affected unit/connector, renew O-rings and gaskets, and confirm insulation resistance is back above the acceptable minimum before re-energising.
Ambiguous or Incorrect Red/White Indication
Likely Cause
Bar aim or pitch has drifted from its commissioned setting, or the red filter glass has faded, cracked, or shifted, moving the red/white transition off the design glide-path angle.
Diagnostic Steps
Carry out a ground or flight inspection of the glide-path angle against the design value; check each unit's levelling and pitch-adjustment setting; inspect the red filter glass for fading, cracking, or seal failure.
Corrective Action
Re-aim and re-level the affected unit(s) to the surveyed angle, or replace a degraded filter glass, then re-verify the transition with a follow-up inspection.
Reduced or Hazy Light Output
Likely Cause
Contaminated or eroded upper/lower lens glass, an aging LED array or halogen lamp, or the CCR running on a lower brightness step than the operational requirement.
Diagnostic Steps
Run a photometric intensity check against ICAO/FAA thresholds; inspect and clean the upper (white) and lower (red) lens glass; confirm the CCR is set to the correct intensity step for prevailing conditions.
Corrective Action
Clean or replace the lens glass, replace a degraded lamp/LED module, or correct the CCR step setting; re-verify with a follow-up photometric reading.
Bar Leaning, Loose, or Misaligned
Likely Cause
Frangible mast coupling has begun to fatigue or partially shear, or the base can/mast footing has settled due to ground movement or wind loading.
Diagnostic Steps
Visually and physically check the frangible coupling for cracking or play; re-check bar aim and pitch against tolerance; inspect the surrounding ground for settlement or heave around the mast footing.
Corrective Action
Replace the frangible coupling on schedule if fatigued, re-level and re-aim the bar, and address any footing settlement to prevent recurrence.
Reliability

Failure Modes & Root Causes

LED Module / Lamp Failure
Medium Severity
Root Cause
Solder-joint fatigue from thermal cycling, moisture ingress through a compromised board seal, or ordinary end-of-life lumen depreciation.
Effect
A dark unit within the near or far bar weakens that bar's colour cue, potentially skewing the white/red reading pilots use to judge above, on, or below the glide path.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and visual confirmation that both bars are fully alight.
Isolating Transformer 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; darkens the affected unit or, if the open extends to the loop itself, can take down an entire bar.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
Bar Unit Elevation Drift
High Severity
Root Cause
Gradual footing settlement, vibration-induced loosening of the pitch-adjustment mechanism, or an aiming error introduced during maintenance.
Effect
A shifted white/red split between the near and far bars, giving pilots an on-slope indication that no longer matches the surveyed glide path.
Detection Method
Ground or flight inspection of the two-bar (or three-bar) indication against design values, and periodic check of each unit's levelling and pitch-adjustment setting.
Series Cable / Connector Insulation Breakdown
Medium Severity
Root Cause
Cable jacket damage, corroded splices, or prolonged standing water in the duct run between the near and far bars.
Effect
Ground fault or short circuit that trips the CCR, or an intermittent partial fault that degrades insulation resistance across the loop.
Detection Method
Full-circuit megger test to flag the low-resistance segment, followed by sectionalised testing to pinpoint the fault location.
Lens / Colour Filter Degradation
Low Severity
Root Cause
Prolonged UV exposure fading the red colour filter, abrasive particulate erosion, or grime build-up on the outer lens surface.
Effect
A weakened or ambiguous white/red distinction — since VASI's entire indication depends on colour rather than a variable split, filter fading is especially consequential.
Detection Method
Scheduled photometric and colorimetric testing against ICAO/FAA thresholds, and visual inspection of the lens and filter during quarterly cleaning.
Frangible Coupling Fatigue
Medium Severity
Root Cause
Cyclic loading from mower or vehicle contact, material fatigue over the service interval, or corrosion at the coupling threads.
Effect
Unit leans, loosens, or separates from its base, taking that bar light out of aim tolerance or out of service.
Detection Method
Physical inspection for cracking or play in the coupling, and periodic fixture-aim/level checks against tolerance.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

The near and far bars run on a constant-current series circuit that can carry several kV across the loop. De-energise and lock out the CCR, then verify zero energy at the fixture before opening a base can or handling cable connectors.

Airside Work Coordination
Operational

Any work on or near an active runway requires ATC/airside coordination and a NOTAM while a bar unit is dark or out of tolerance, with vehicle and personnel movement kept clear of the runway strip per the aerodrome's safety management procedures.

Frangibility Not to Be Defeated
Mechanical

Never substitute the frangible coupling with a rigid fitting or over-torque it during installation or repair; the coupling must still shear cleanly on aircraft impact to limit damage under the frangibility requirement.

Colour Filter Handling
Operational

Handle red colour filters carefully during lens or lamp replacement and verify colorimetric output before closing out the work; since VASI's entire indication depends on colour rather than a variable split, a faded or improperly seated filter is especially consequential to the on-slope reading.

FOD Control at the Base Can
Operational

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

Insulation Test Before Re-Energisation
Electrical Safety

After any cable, connector, or transformer work, megger test the affected series loop before restoring power, since a residual fault at re-energisation can trip the CCR or damage healthy units on the same circuit.

PPE & Grounding
Personnel Safety

Use insulated tools and appropriate PPE when working on series-circuit connections, and confirm the fixture and base can are bonded/grounded per the electrical design before reconnecting the loop.

Restore to Compliant State
Compliance

Do not leave a bar unit out of aim tolerance, at reduced intensity, or otherwise non-compliant after maintenance; verify photometric, colorimetric, and positional conformance across the near and far bars before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Older Installations May Predate Current Photometric Standards
Compliance

Many VASI systems have been in continuous service for decades; a unit that was compliant at installation may no longer meet current intensity or angle tolerances, so benchmark against the current standard at each major inspection rather than the original commissioning spec.

The Downwind Bar Serves a Different Aircraft Category
Design

In a three-bar system, the far bar exists to give a different glide path reference for aircraft with a higher cockpit eye height; treat it as a distinct calibration target rather than a redundant copy of the near and middle bars.

LED Retrofits Can Sharpen the Colour Transition Pilots Are Used To
Retrofit

Swapping legacy incandescent VASI lamps for LED sources can sharpen the red-to-white transition band compared with what pilots at that field are accustomed to seeing; verify the transition still falls within the specified angular tolerance rather than assuming a brighter, similar-looking LED is automatically equivalent.

One Site Survey Underpins Every Bar — an Error There Propagates
Verification

Because VASI relies on relative angles between bars, an error in the original site survey affects every bar consistently and is hard to catch from any single bar's individual test; cross-check the full multi-bar geometry periodically against as-built survey data.

Vegetation Growth Affects Sightline Before It Affects the Fixture
Siting

The light units can remain in perfect calibration while grass, crops, or shrub growth in the approach path progressively obstructs a pilot's view of the lower bars; include an approach sightline check as its own maintenance item, not just a fixture check.

Trend Readings Over Years, Not Just Pass/Fail at Each Visit
Maintenance

Given how long many VASI installations stay in service, keep historical photometric and angle readings on file so gradual drift shows up as a trend across years rather than only as a binary pass or fail at each individual visit.

Quick Answers

Frequently Asked Questions

Short answers about VASI: two-bar and three-bar systems, specifications, circuits, standards and maintenance.

Q1What is a VASI?

The Visual Approach Slope Indicator is a visual glide path guidance system using light units arranged in two or three bars, typically on the left side of the runway. It shows red and white light to indicate the approach angle.

Q2What question does VASI answer for the pilot?

Whether the aircraft is on the correct glide path, too high or too low, using red and white light and the pilot's own eyes without any onboard equipment.

Q3What is the difference between 2-bar and 3-bar VASI?

A 2-bar VASI is the standard configuration and a 3-bar VASI adds a further bar. Near and far bars are set at slightly different elevations, typically about 20 arc-minutes apart, to build the composite signal.

Q4Where is VASI used?

On non-precision runways, at general aviation airports where cost and simplicity matter, and at military airfields for training and operations.

Q5What are the typical specifications?

An LED array or 45/65 W halogen lamp, up to 15,000 cd white and 8,000 cd red, a 3 degree glide path (adjustable 2.5-4 degrees), and frangible elevated mounting typically 10-20 m from the runway edge.

Q6How is VASI powered?

From a constant current series circuit through a 45-65 W isolating transformer per unit, with upwind and downwind bars on circuits synchronised to the same intensity step.

Q7What photometric performance is expected?

At least 10,000 cd white and 5,000 cd red on-axis, a red/white transition of 4 arc-minutes or less per bar, and a ±25% field tolerance at each CCR step.

Q8Which standards apply to VASI?

ICAO Annex 14, FAA AC 150/5340-25 (Visual Approach Slope Indicator Systems), FAA AC 150/5345-46 (fixture specification) and IEC/TS 61827.

Q9How often should VASI be maintained?

Quarterly lens cleaning, semi-annual lamp or LED inspection, and annual bar alignment, photometric checks, frangible coupling inspection and insulation resistance tests.

Q10How does VASI differ from PAPI?

Both use red and white light, but VASI uses two or three bars of light units at different elevations, while PAPI uses a single row of four units.

Q11What if one VASI bar is dark and the others are normal?

Look for a failed LED array or lamp within that bar's units, or an open isolating transformer feeding it. Confirm loop continuity through the transformer primary and megger the transformer.

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