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.
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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 & 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.
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.
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.
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.
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.
Glide-path angle is set by mechanical aiming, not by the control system — ALCMS only ever switches the whole bar together.
Reading the Four-Light Bar
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
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.
Technical Parameters
| Parameter | Typical 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 Angle | Typically 3° (adjustable 2.5°–4°) |
| Colour Transition | Red below glide path, white above (PAPI) |
| Light Source | Halogen or LED, fed via isolating transformer |
| Intensity Control | Selectable steps via CCR (same as runway lighting) |
| Mounting | Frangible support, elevated above ground |
| Visibility Range | Day: 5–8 km; Night: up to 20 km (depending on intensity) |
| Standards | ICAO Annex 14, FAA AC 150/5345-28, IS 7785 |
Electrical Requirements
| Requirement | Typical Value |
|---|---|
| Circuit Type | Series airfield circuit, constant current (CCR fed), same loop as runway lighting |
| Primary Loop Current | 6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A) |
| Isolating Transformer | One per light unit, matched to the fixture's rated wattage |
| Cable Type | L-824 single-conductor, direct-burial or duct-routed, matched to loop voltage class |
| Connector | L-823 primary connector, submersible-rated splice, encapsulated after mating |
| Unit-to-Unit Cabling | Individual home-run leads from each of the 4 units back to their own isolating transformer |
| Earthing/Grounding | Frangible mounts and fixture bodies bonded to airfield earth grid |
| Fault Protection | CCR-level ground fault and open-circuit detection on the primary loop |
| Power Source | CCR output, intensity-stepped in unison with the associated approach/runway lighting |
Photometric Requirements
| Parameter | Typical 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 Spread | Units (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 Distribution | Per 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 Method | Mobile photometric van/goniophotometer or fixed test bench per unit |
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
Installation Requirements
Baseline Spacing & Levelling
CivilSet 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
CivilConfirm 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
MechanicalTorque 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
MechanicalSet 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
ElectricalTerminate 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
MechanicalConfirm 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
DocumentationRecord baseline spacing, offset distances, preliminary angle settings, and connector seal as-built before final glide-path calibration and energisation.
Testing & Commissioning
Glide Slope Angle Verification
Final AcceptanceSet 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 AcceptanceConfirm the angular increment between adjacent units is correct, since an uneven step distorts the on-slope indication band.
Colour Transition Sharpness Test
Final AcceptanceFly 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 AcceptanceMeasure beam intensity and colour with a calibrated photometer against ICAO/FAA commissioning tolerances for both red and white sectors.
Wing-Bar Levelling Verification
Final AcceptanceConfirm the four units sit at equal height and are correctly spaced perpendicular to the runway centreline per the design layout.
CCR Brightness Step Response
EnergisationCycle 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 AcceptanceRecord unit angles, photometric readings, and flight/ground verification results in the commissioning dossier for handover.
Inspection & Maintenance
Glide Slope Angle Verification
AnnualConfirm 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-annualVerify 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
AnnualVerify beam intensity and colour against ICAO / FAA thresholds using a calibrated photometer to catch lens haze or lamp/LED degradation.
Frangible Mount & Structure Inspection
AnnualCheck frangible support couplings and elevated structures for corrosion, brittleness, or shear fatigue, particularly given their exposed siting.
CCR & Intensity Step Check
Semi-annualConfirm the feeding CCR steps the array through all selectable intensity levels correctly and that steps match across all units.
Isolating Transformer & Cable Check
AnnualMegger-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
AnnualConfirm vegetation growth, new structures, or terrain changes haven't obstructed the sightline between units and the approach path.
Lens & Optical Window Cleaning
QuarterlyWipe lenses and optical windows free of dust, film, and insect residue so light output stays within spec across all units.
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.
Troubleshooting Guide
Ambiguous or Inconsistent Glide-Slope Indication
Row Shows Fewer Lit Units Than Expected
Reduced Visibility or Colour Shift in Low Visibility Conditions
Unit Found Misaligned or Unstable Without Visible Breakage
Perceived Brightness Uneven Across the Row
Multiple Units or Entire Row Dark
Failure Modes & Root Causes
Row Alignment Divergence Between Units
Single-Unit Outage Within the Row
Lens or Filter Contamination Across the Row
Undetected Mechanical Instability
Brightness Imbalance Across the Row
Shared Circuit or Power Fault
Safety & Operational Notes
Series Circuit Isolation
Electrical SafetyPAPI/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
ComplianceThe 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
MechanicalNever 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
OperationalPAPI/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 SafetyAllow 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 SafetyAfter 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 SafetyUse 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
ComplianceDo 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.
Engineering & Expert Notes
Aim From the Design Sheet, Not the Neighbouring Unit
ComplianceNever 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
PhotometricThe 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
DurabilityAs 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
OperationalPAPI/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
ElectricalSwapping 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
TroubleshootingMoisture 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.
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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