AGL Component Library By Precision AGL Academy

Visual Glide Slope PAPI / VASI

The visual guidance that tells pilots if they are on the correct approach path — a row of lights that changes colour from red to white depending on the aircraft's angle relative to the ideal 3° glide slope.

PAPI System

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Overview

What Are They?

Visual Approach Slope Indicator (VASI) and Precision Approach Path Indicator (PAPI) are light systems that provide pilots with visible glide-slope guidance during the final approach segment. They are located beside the runway threshold and project a pattern of red and white light, enabling the pilot to determine whether the aircraft is above, on, or below the optimal descent path.

PAPI has largely replaced VASI on modern airfields because it offers more precise guidance with a single row of lights (typically four units) that all show the same colour for a given angle, whereas VASI uses a two-bar system with separate upwind and downwind bars. Both systems serve the same purpose: preventing approaches that are too high (risk of overshoot) or too low (risk of obstacle collision).

Purpose

Purpose & Function

The purpose of PAPI and VASI systems is to solve a problem that runway and approach lighting alone can't: telling a pilot not just where the runway is, but whether they are actually descending at the correct angle to reach it safely. An approach that looks visually fine to the eye can still be dangerously high (risking a long landing or a go-around) or dangerously low (risking obstacle or terrain collision short of the runway), and neither error is easy to judge from the runway's appearance alone, especially at night or in marginal visibility. By encoding glide-slope deviation directly into a simple red/white colour pattern that requires no calculation or instrument cross-check, PAPI (and its predecessor VASI) gives the pilot instantaneous, continuous feedback throughout the approach — which is why PAPI's single-row, four-unit design has displaced VASI's older two-bar system on most modern airfields, since a single glance at one row of lights is faster and less ambiguous to interpret than comparing two separate bars.

Application

Where Are They Used?

Visual glide slope systems are installed on the approach side of runways that serve instrument or visual approaches, and are particularly important for precision approaches:

  • PAPI: Typically a row of four light units, each projecting a red or white beam. Installed on the left side of the runway (or both sides for some configurations) at a defined distance from the threshold.
  • VASI: A two-bar system (near and far) showing red/red when below the glide path, white (near)/red (far) when on the correct path, and white/white when above it. Now less common, but still in use on some smaller or older airfields.
  • APAPI: Abbreviated PAPI with only two light units, used on non-precision or visual-only runways.
  • Tri-colour or PVASI: Other visual slope indicators, though PAPI is the international standard.

The system is sized and sited according to the approach category of the runway (e.g., CAT I, II, III) and the specific geometry of the approach obstacle-limitation surface.

Placement

Installation & Location

The four PAPI units are installed in a straight row perpendicular to the runway centreline, on the left side of the runway abreast of the touchdown zone at a fixed distance from the threshold, with even spacing between units set by the applicable design standard so the row reads as one continuous bar rather than separate lights. Each unit's foundation and frangible mounting are surveyed and levelled precisely, since PAPI's entire function depends on every unit being set to the exact same glide-slope elevation angle — the units are not simply bolted down and left, but individually adjusted and checked against the design glide path using a theodolite or the manufacturer's alignment tool before being accepted into service. Cabling to each unit runs in duct or direct-buried conduit back to its own isolating transformer and onward to the circuit's CCR, following the same series-circuit wiring practice as other precision approach lighting so all four units can be intensity-stepped together. Where VASI's older two-bar layout is retained on a legacy installation, the near and far bars are similarly surveyed to their respective design angles, with the greater physical separation between the two bars making precise siting even more critical to the system reading correctly from the cockpit.

Function

How Does It Work?

Each PAPI unit contains a lamp, a red filter, and a lens or reflector that projects a beam with a sharp cut-off angle. The beam is aimed so that below the glide path the pilot sees red, and above the glide path white. With four units, the pilot sees a combination of red and white lights that indicates the deviation from the nominal 3° glide slope.

Key functional aspects include:

  • Colour Coding: On a four-unit PAPI, the number of white vs. red lights indicates the deviation:
    • 4 White: Too high (steep approach)
    • 3 White / 1 Red: Slightly high
    • 2 White / 2 Red: On glide slope (correct)
    • 1 White / 3 Red: Slightly low
    • 4 Red: Too low (shallow approach)
  • Light Source: Traditionally halogen lamps, but increasingly LED modules for longer life and lower maintenance.
  • Power Supply: Fed from the AGL series circuit (like other runway lighting) via isolating transformers, with intensity steps controlled from the CCR.
  • Adjustment: Each unit can be mechanically tilted to set the exact glide-slope angle (typically 3°).
  • Frangibility: PAPI units are mounted on frangible supports so they break away on impact, reducing the risk to aircraft.
Architecture

System Architecture & Control Logic

The PAPI or VASI light bar is controlled the same way a runway edge light circuit is: at the loop level, not per fixture. All units in the bar — typically four for PAPI — are wired into the same constant current series circuit and fed through their own isolating transformers, so a single ALCMS-commanded brightness step changes every unit's intensity simultaneously. This is not incidental — a pilot reading the four-light pattern is comparing red and white across units in the same glance, so if one unit ran at a different intensity to the others (rather than simply switching between red and white internally) the comparison itself would be unreliable. The glide-path angle each unit indicates is set mechanically during aiming and calibration, not by the ALCMS; the control system's only real-time influence is the shared brightness step and on/off state for the whole bar, with loop-level fault detection identifying an open circuit or failed transformer the same way it would on any other series circuit.

ALCMS Selects on/off state and brightness step for the bar Constant Current Regulator Regulates the whole loop to one fixed current Series Circuit Loop All 4 PAPI/VASI units wired in series Isolating Transformer (Per Unit) Taps the fixed loop current to each unit PAPI / VASI Unit Red/white split set internally at the commanded intensity LOOP-LEVEL CONTROL — ALL 4 UNITS TOGETHER Keeping every unit at identical intensity is what keeps the glide-path indication trustworthy

Glide-path angle is set by mechanical aiming, not by the control system — ALCMS only ever switches the whole bar together.

Function

Reading the Four-Light Bar

4 White
Too High
3 White / 1 Red
Slightly High
2 White / 2 Red
On Glide Slope
1 White / 3 Red
Slightly Low
4 Red
Too Low
Each Unit's Sharp Red/White Cut-Off Sets the 3° Glide Path

Fed from the series circuit via an isolating transformer; frangible-mounted to break away on impact

Construction

Physical Construction

Each PAPI or VASI unit is a weatherproof, elongated housing, typically die-cast aluminium, containing two or three separate light sources (halogen or LED) each viewed through its own precisely positioned optical system. A split-colour lens or a combination of a red filter over the lower portion of each lamp's beam and clear glass over the upper portion, positioned to a fraction of a degree of accuracy, creates the sharp red/white transition that defines the glide path angle for that unit. The housing mounts on a frangible support structure similar to elevated runway edge lights, engineered to break away cleanly under aircraft impact, with the unit's angular tilt precisely set and locked using shims or an integrated adjustment mechanism during commissioning to establish the correct glide path. The optical compartment is gasket-sealed against the housing to protect the lamps and precision optics from moisture and dust, and the units in a wing bar are installed on a common baseline with tightly controlled spacing and levelling so their combined light pattern reads consistently from the approach.

Specification

Technical Parameters

ParameterTypical Value
Number of Units (PAPI)4 (standard), 2 (APAPI) for some applications
Number of Units (VASI)2 bars (near and far), each with multiple lights
Glide Slope AngleTypically 3° (adjustable 2.5°–4°)
Colour TransitionRed below glide path, white above (PAPI)
Light SourceHalogen or LED, fed via isolating transformer
Intensity ControlSelectable steps via CCR (same as runway lighting)
MountingFrangible support, elevated above ground
Visibility RangeDay: 5–8 km; Night: up to 20 km (depending on intensity)
StandardsICAO Annex 14, FAA AC 150/5345-28, IS 7785
Power Supply

Electrical Requirements

RequirementTypical Value
Circuit TypeSeries airfield circuit, constant current (CCR fed), same loop as runway lighting
Primary Loop Current6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A)
Isolating TransformerOne per light unit, matched to the fixture's rated wattage
Cable TypeL-824 single-conductor, direct-burial or duct-routed, matched to loop voltage class
ConnectorL-823 primary connector, submersible-rated splice, encapsulated after mating
Unit-to-Unit CablingIndividual home-run leads from each of the 4 units back to their own isolating transformer
Earthing/GroundingFrangible mounts and fixture bodies bonded to airfield earth grid
Fault ProtectionCCR-level ground fault and open-circuit detection on the primary loop
Power SourceCCR output, intensity-stepped in unison with the associated approach/runway lighting
Optical Performance

Photometric Requirements

ParameterTypical Value
Main Beam Intensity (White)≥ 16,000 cd on-axis per unit, up to 25,000 cd at full intensity
Main Beam Intensity (Red)≥ 8,000 cd on-axis per unit, up to 12,000 cd at full intensity
Transition Sharpness (Red/White)≤ 3–4 arc-minutes vertical transition band per unit, tighter for PAPI than VASI
Vertical Beam SpreadUnits (PAPI) or bars (VASI) splayed about the 3° glide slope reference to build the composite on-slope band
Horizontal Beam Spread± 5° to ± 10° either side of runway centreline plane
Isocandela DistributionPer ICAO Annex 14 Attachment A / FAA AC 150/5345-28 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 unit
Compliance

Applicable Standards

ICAO Annex 14

International standards for PAPI and VASI siting, angle, and colour requirements

FAA AC 150/5345-28

U.S. specification for Precision Approach Path Indicators (PAPI)

FAA AC 150/5340-25

Visual Approach Slope Indicator (VASI) Systems (mostly superseded by PAPI)

IS 7785

Indian Standard for airfield lighting, including visual slope indicators

DGCA CAR Section 4

Indian regulatory requirements for aerodrome visual aids

Prerequisites

Installation Requirements

Baseline Spacing & Levelling
Civil

Set out and level all units in the wing bar on a common baseline with the tightly controlled spacing the design calls for, so the combined light pattern reads consistently from the approach.

Offset Distance from Runway
Civil

Confirm each unit's lateral offset from the runway edge and its distance from the threshold match the design siting, since these dimensions directly set the geometry of the glide path.

Frangible Support Fixing
Mechanical

Torque the frangible support fixing bolts to the specified value, checking the fitting shears as designed under lateral load and does not bind.

Preliminary Angle Setting
Mechanical

Set each unit's angular tilt to the design glide slope angle using shims or the integrated adjustment mechanism, ready for precision verification during commissioning.

Isolating Transformer & Connector Termination
Electrical

Terminate and seal the primary connector at each unit, confirming the isolating transformer wattage and ratio match the fixture and the series circuit's rated current step.

Optical Compartment Seal Check
Mechanical

Confirm the gasket seal on the optical compartment is intact, protecting the precision optics and split-colour lens from moisture and dust before commissioning.

Pre-Commissioning Sign-off
Documentation

Record baseline spacing, offset distances, preliminary angle settings, and connector seal as-built before final glide-path calibration and energisation.

Verification

Testing & Commissioning

Glide Slope Angle Verification
Final Acceptance

Set and verify each unit's elevation angle so the four-unit array produces the correct red/white transition at the nominal glide slope.

Unit-to-Unit Angle Increment Check
Final Acceptance

Confirm the angular increment between adjacent units is correct, since an uneven step distorts the on-slope indication band.

Colour Transition Sharpness Test
Final Acceptance

Fly or simulate an approach through the transition zone to confirm the red/white cut-off is sharp, without a broad or fuzzy pink band.

Photometric Intensity Test
Final Acceptance

Measure beam intensity and colour with a calibrated photometer against ICAO/FAA commissioning tolerances for both red and white sectors.

Wing-Bar Levelling Verification
Final Acceptance

Confirm the four units sit at equal height and are correctly spaced perpendicular to the runway centreline per the design layout.

CCR Brightness Step Response
Energisation

Cycle the CCR through every intensity step and confirm all four units respond together without any unit lagging or failing to switch.

Documentation & As-Built Sign-off
Final Acceptance

Record unit angles, photometric readings, and flight/ground verification results in the commissioning dossier for handover.

Upkeep

Inspection & Maintenance

Glide Slope Angle Verification
Annual

Confirm the promulgated glide slope angle across all units using calibrated theodolite or inclinometer equipment, since a shifted angle misleads pilots on the approach.

Unit-to-Unit Consistency Check
Semi-annual

Verify all PAPI units (or both VASI bars) present a consistent red/white transition and intensity, since a mismatched unit undermines the visual glide path picture.

Photometric Intensity Check
Annual

Verify beam intensity and colour against ICAO / FAA thresholds using a calibrated photometer to catch lens haze or lamp/LED degradation.

Frangible Mount & Structure Inspection
Annual

Check frangible support couplings and elevated structures for corrosion, brittleness, or shear fatigue, particularly given their exposed siting.

CCR & Intensity Step Check
Semi-annual

Confirm the feeding CCR steps the array through all selectable intensity levels correctly and that steps match across all units.

Isolating Transformer & Cable Check
Annual

Megger-test isolating transformers and inspect cable connections feeding each unit, since a fault in one leg can darken an entire glide slope indication.

Approach Terrain & Sightline Check
Annual

Confirm vegetation growth, new structures, or terrain changes haven't obstructed the sightline between units and the approach path.

Lens & Optical Window Cleaning
Quarterly

Wipe lenses and optical windows free of dust, film, and insect residue so light output stays within spec across all units.

Field Notes

Common Field Issues

Misalignment / Incorrect Aiming

Each PAPI unit must be precisely aligned to the correct glide-slope angle. Vibration or ground settlement can knock units out of alignment, giving misleading indications.

Lamp or LED Failure

A single failed unit in a PAPI row can cause ambiguous indications (e.g., 3 lights instead of 4). Regular inspections and prompt replacement are essential.

Dirt or Lens Degradation

Dust, bird droppings, or UV degradation can reduce light output or shift colour, compromising the system's effectiveness, especially in low visibility.

Frangible Mount Damage

During snow clearing or vehicle operations, frangible supports can be damaged without breaking, leaving the unit misaligned or unstable.

Intensity Mismatch

If different units on the same row are replaced with mismatched lamps or LEDs, the perceived brightness across the row can vary, making the colour change less distinct.

Electrical Supply Issues

PAPI units are fed from the series circuit, so a fault in the primary cable or isolating transformer can knock out individual units or the entire system.

Diagnostics

Troubleshooting Guide

Ambiguous or Inconsistent Glide-Slope Indication
Likely Cause
One or more PAPI units have drifted out of alignment due to vibration or ground settlement.
Diagnostic Steps
Check the aiming angle of each unit in the row against the specified glide-slope angle using an alignment jig or digital level; compare readings across all units for consistency.
Corrective Action
Re-aim any unit found outside tolerance, and investigate ground settlement if multiple units in the row have drifted.
Row Shows Fewer Lit Units Than Expected
Likely Cause
Lamp or LED failure in one unit of the row, producing an ambiguous count (e.g., 3 lights instead of 4).
Diagnostic Steps
Visually inspect the row for a dark unit; verify supply voltage is present at the affected unit; check the lamp/LED module for failure.
Corrective Action
Replace the failed lamp/LED module promptly, since a single dark unit can materially change the indicated glide-slope reading.
Reduced Visibility or Colour Shift in Low Visibility Conditions
Likely Cause
Dirt, bird droppings, or UV-related lens degradation reducing light output or shifting colour.
Diagnostic Steps
Inspect the lens for contamination or discolouration; take a photometric reading before and after a test clean.
Corrective Action
Clean or replace the lens as needed, and re-verify photometric and colour compliance with a follow-up test.
Unit Found Misaligned or Unstable Without Visible Breakage
Likely Cause
The frangible mount has been struck (e.g., during snow clearing or vehicle operations) and damaged internally without fully breaking away.
Diagnostic Steps
Inspect the frangible coupling/mount for hairline damage, looseness, or partial fatigue; check unit stability and aim against tolerance.
Corrective Action
Replace the damaged frangible mount and re-level/re-aim the unit, even if it did not fully break away, since partial damage compromises both stability and breakaway performance.
Perceived Brightness Uneven Across the Row
Likely Cause
Mismatched lamp or LED replacement units fitted to individual PAPI units in the same row.
Diagnostic Steps
Check part numbers and output bins of lamps/LEDs across all units in the row for consistency; take comparative photometric readings.
Corrective Action
Replace mismatched units with manufacturer-approved, matched-output lamps or LEDs so brightness and colour transition are consistent across the row.
Multiple Units or Entire Row Dark
Likely Cause
A fault in the series circuit's primary cable or isolating transformer feeding the PAPI units.
Diagnostic Steps
Check the CCR/series circuit status for a fault indication; megger the feeder cable and test the isolating transformer for the affected units.
Corrective Action
Repair or replace the faulted cable section or isolating transformer, and re-verify all units in the row illuminate correctly before returning to service.
Reliability

Failure Modes & Root Causes

Row Alignment Divergence Between Units
High Severity
Root Cause
One or more units in the row drifted in azimuth or elevation independently since the last formal alignment check.
Effect
Ambiguous or inconsistent glide-slope indication, since the array's combined red/white presentation depends on all units in the row agreeing.
Detection Method
Field verification of azimuth and elevation on every unit in the row relative to each other and to the approved glide path setting.
Single-Unit Outage Within the Row
High Severity
Root Cause
Lamp/LED failure, a connector fault, or a series circuit interruption affecting one unit while the rest of the row continues normally.
Effect
Row shows fewer lit units than expected, which can be misread by a pilot as an incorrect glide-slope indication rather than a fault.
Detection Method
Photometric comparison across all units in the row to identify the one that is dark or under-performing, and prompt corrective dispatch.
Lens or Filter Contamination Across the Row
Medium Severity
Root Cause
Rubber deposits, dust, and de-icing fluid residue building up on the lenses over successive operating seasons, often affecting the whole row unevenly.
Effect
Reduced visibility or a colour shift in low-visibility conditions, weakening the glide-slope cue exactly when it matters most.
Detection Method
Scheduled photometric intensity and chromaticity testing across the row, and visual inspection during routine cleaning.
Undetected Mechanical Instability
High Severity
Root Cause
Foundation settlement, a loosened mounting base, or a partially fatigued frangible coupling that has not yet failed outright.
Effect
Unit found misaligned or unstable without visible breakage, a fault that can escape a quick visual check but still degrades the presented glide path.
Detection Method
Physical stability check of the mount and coupling during scheduled maintenance, in addition to the routine alignment reading.
Brightness Imbalance Across the Row
Medium Severity
Root Cause
Uneven lumen depreciation between units of different ages, or a mix of replacement lamps/LEDs with differing output.
Effect
Perceived brightness uneven across the row, making the glide-slope indication harder to read cleanly on approach.
Detection Method
Photometric comparison of intensity across all units in the row against the rated tolerance.
Shared Circuit or Power Fault
High Severity
Root Cause
A CCR fault, a failed isolating transformer, or a series cable insulation breakdown affecting the circuit feeding multiple units.
Effect
Multiple units or the entire row dark, removing the glide-slope indication entirely rather than degrading it.
Detection Method
CCR output verification, full-circuit megger testing, and sectionalised fault-location testing to isolate the affected segment.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

PAPI/VASI units run on the same constant-current series loop as the associated runway or approach lighting and can carry several kV. De-energise and lock out the CCR, then verify zero energy at the unit before opening its housing.

Aim-Angle Calibration Integrity
Compliance

The vertical aim angle of each unit sets the published glide path; never adjust a unit without a calibrated theodolite/clinometer and the design elevation setting sheet, since even a small angular error can put approaching aircraft below the intended glide slope.

Frangibility Not to Be Defeated
Mechanical

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

Glide Path Work Coordination
Operational

PAPI/VASI is a primary visual glide path reference; obtain ATC/airside coordination and issue a NOTAM before taking a unit out of service or adjusting its aim, and keep vehicles and personnel clear of the beam and the runway strip during aircraft operations.

Hot Lamp / Housing Contact
Personnel Safety

Allow the housing, lens, and lamp/LED module to cool before handling after an active period; the internal light source and optical filter run hot during normal operation and can cause burns during lens or lamp replacement.

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 unit and frangible base are bonded/grounded per the electrical design before reconnecting the loop.

Restore to Compliant State
Compliance

Do not leave a unit out of aim tolerance, at reduced intensity, or with an uneven red/white transition across the bar after maintenance; verify photometric and angular conformance before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Aim From the Design Sheet, Not the Neighbouring Unit
Compliance

Never re-aim a unit by eye-matching it to its bar-mates; always aim from the original design elevation setting sheet and a calibrated theodolite, since a neighbouring unit could itself be out of tolerance.

Match the Red/White Transition Across the Bar
Photometric

The width and angle of the colour transition must be consistent unit-to-unit; a single unit with a narrower or wider transition band creates an ambiguous "pink" sector that different pilots will read differently on approach.

Colour Transition Drifts With Source Aging
Durability

As the lamp or LED source ages it can dim unevenly through the red and white filter halves, shifting the perceived transition angle even though the physical aim hasn't moved; treat transition angle as a parameter to retest at overhaul, not just total intensity.

Low-Mounted Units Are Vulnerable to Line-of-Sight Obstruction
Operational

PAPI/VASI units sit low and well off the runway edge; snow berms, standing water reflection, or growing vegetation in the beam path can attenuate one or two units in a bar without it showing up on a check made from directly on the extended centreline.

Keep Isolation Transformers Matched Across the Bar
Electrical

Swapping in a transformer with a different VA rating than the rest of the bar during a repair can leave one unit measurably dimmer or brighter than its neighbours even when its own current is within spec; treat the bar as a matched electrical set.

Trend Loop Readings, Don't Just Spot-Check
Troubleshooting

Moisture ingress at an L-823 connector usually shows up first as a slow drift in loop insulation resistance, not a hard fault. Logging megger readings over successive maintenance cycles catches a failing splice months before it takes the loop down.

Quick Answers

Frequently Asked Questions

Short answers about PAPI and VASI visual glide slope systems: how to read them, layout, standards, maintenance and common faults.

Q1What is the difference between PAPI and VASI?

Both are visual glide slope indicators that use red and white lights beside the runway. PAPI uses a single row of typically four units, while VASI uses a two-bar system with separate near and far bars. PAPI has largely replaced VASI because it gives more precise guidance.

Q2How do you read a four-light PAPI?

Four white lights mean too high, three white and one red slightly high, two white and two red on the glide slope, one white and three red slightly low, and four red too low.

Q3What is an APAPI?

An APAPI (abbreviated PAPI) uses only two light units and is used on non-precision or visual-only runways.

Q4What glide slope angle do PAPI systems use?

Typically 3°, adjustable from about 2.5° to 4° to suit the runway and obstacle environment.

Q5How far can pilots see PAPI lights?

Typical visibility is 5 to 8 km by day and up to about 20 km at night, depending on the intensity setting.

Q6Where are PAPI units installed?

The four units are installed in a straight row perpendicular to the runway centreline, usually on the left side, abreast of the touchdown zone at a fixed distance from the threshold. They are mounted on frangible supports and fed from the series circuit.

Q7Which standards apply to PAPI and VASI?

The main references are ICAO Annex 14, FAA AC 150/5345-28 (PAPI), FAA AC 150/5340-25 (VASI, mostly superseded), IS 7785 and DGCA CAR Section 4 for India. Always verify the current edition.

Q8What are the common faults on PAPI systems?

Typical problems are misaligned aiming from vibration or settlement, a failed lamp or LED that leaves an ambiguous indication, lens dirt or degradation, damaged frangible mounts, mismatched replacement sources and electrical faults in the series circuit or isolating transformer.

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