AGL Component Library By Precision AGL Academy

PAPI

Precision Approach Path Indicator – a visual glide slope guidance system consisting of four light units arranged in a row. PAPI provides pilots with an accurate, intuitive indication of their position relative to the correct approach path, ensuring safe and stable approaches, particularly in marginal weather conditions.

PAPI (Precision Approach Path Indicator) four-unit red/white glide slope system

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Overview

What Is It?

The Precision Approach Path Indicator (PAPI) is a visual guidance system that helps pilots maintain the correct glide slope during final approach. It consists of four light units arranged in a row, typically installed on the left side of the runway (or both sides for Category II/III). Each unit projects a red or white light, depending on the pilot's viewing angle. The combination of red and white lights indicates whether the aircraft is above, below, or on the correct glide path.

PAPI is the most widely used visual glide slope system worldwide, providing a simple, unambiguous signal that requires no special equipment on the aircraft. It is essential for both precision and non‑precision runways, enhancing safety and operational efficiency during all weather conditions.

Purpose

Purpose & Function

PAPI's purpose is to let a pilot self-correct a descent angle to within a very tight margin using only a glance at the runway, without any onboard glide slope receiver or electronic aid — a capability that matters on every approach, but becomes essential in marginal weather, at night, or when an ILS glide path isn't available or isn't being used. The four-unit row translates a continuous descent-angle deviation into a simple, countable pattern of red and white lights, so a pilot can judge not just whether they're high or low but roughly by how much.

This combination of precision and universality — no aircraft equipment required, immediately readable by any pilot regardless of aircraft type — is why PAPI has become the default visual glide slope system at the overwhelming majority of the world's runways, serving as either the primary glide path reference or a critical backup to an electronic system.

Application

Where Is It Used?

PAPI is deployed on a wide range of runways and heliports:

  • Precision approach runways (CAT I, II, III) – providing primary visual glide slope guidance.
  • Non‑precision runways – enhancing approach safety for visual and circling approaches.
  • Military airfields – supporting tactical and training operations.
  • Heliports – providing glide path guidance for helicopter approaches (helicopter PAPI).
  • Regional and general aviation airports – improving approach accuracy and safety.
  • Runways with terrain or obstacle constraints – where a defined glide path is critical.
Placement

Installation & Location

The wing bar of four light units is mounted on one side of the runway (normally the left, viewed from the approach), at a fixed lateral offset from the runway edge chosen to keep the units clear of the obstacle-limitation surface, wingtip clearance envelope, and any blast zone. The bar is set back from the threshold along the runway at a distance derived from the design tables so the visual glide path crosses the threshold at the standard eye-to-wheel height for the aircraft the runway serves, all tied into the runway centreline and threshold survey. Each unit sits on its own frangible mount at equal lateral spacing along the bar, and is individually aimed in elevation during commissioning so the four units together produce a sharp two-red/two-white split exactly on the design glide angle, with the transition band between units kept tight. Cabling runs underground from each unit back to the constant current regulator, and the units and mounting frame must stay within the frangibility requirements for the runway's code number.

Function

How Does It Work?

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

  • Optical Design: Each light unit contains a lamp (halogen or LED) and a precision optical system that projects a beam with a distinct red/white transition. The transition angle is set to the desired glide slope (typically 3°).
  • Colour Indication: When the aircraft is on the correct glide path, the pilot sees two red lights (the units closest to the runway) and two white lights (the units farthest from the runway). Above the path, more white lights appear; below, more red lights appear. The system provides a four‑light display with the following meanings:
    • All white – aircraft is well above the glide path.
    • 3 white / 1 red – slightly above the glide path.
    • 2 white / 2 red – on the correct glide path.
    • 1 white / 3 red – slightly below the glide path.
    • All red – well below the glide path.
  • Power and Control: PAPI 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 to suit ambient light conditions (day, night, twilight).
  • Integration: PAPI is often integrated with runway approach lighting systems and may be controlled remotely via the ALCMS. Some systems include automatic brightness adjustment based on ambient light sensors.
Architecture

System Architecture & Control Logic

PAPI has no per-unit electronic addressing — the "control logic" that produces the glide path signal is set optically at commissioning, not by any processor. Each of the four light units is levelled and its internal lens/shutter assembly is precisely tilted so its red/white transition occurs at a specific elevation angle, with the units aimed a fraction of a degree apart from one another so that, taken together, they straddle the design glide path (typically 3°). Once set, that elevation is fixed hardware, not a software parameter. All four units are powered from the same constant current series circuit through their own isolating transformers, with the ALCMS or local CCR setting the shared brightness step for day, twilight, or night; that command changes how bright the whole array is, never which unit shows which colour. Where automatic brightness control is fitted, an ambient light sensor feeds the CCR/ALCMS to select the appropriate step. Loop monitoring works the same way as any series circuit — the CCR watches loop voltage against commanded current, and a rise flags an open-circuit lamp or failed transformer as a loop fault for maintenance to isolate, rather than the system detecting or correcting a misaimed unit itself. Optical alignment is verified periodically by ground or flight check, not by any feedback sensor in the fixture.

ALCMS / CCR → Series Circuit Loop → Isolating Transformer → Light Unit (elevation fixed optically per unit)

ALCMS / LOCAL CCR Selects shared brightness step (day/twilight/night) SERIES CIRCUIT LOOP Same current to all four units — brightness only ISOLATING TRANSFORMER (PER UNIT) Taps fixed loop current to each light unit LIGHT UNIT (×4, INDIVIDUALLY AIMED) Lens/shutter tilt sets that unit's red/white split Fixed at commissioning — no runtime control SIGNAL IS OPTICAL, NOT ELECTRONIC The 4-light colour pattern 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
Reading The Signal

The Four-Light Glide Path Indication

All White
Aircraft is well above the glide path
3 White / 1 Red
Slightly above the glide path
2 White / 2 Red
On the correct glide path (target indication)
1 White / 3 Red
Slightly below the glide path
All Red
Aircraft is well below the glide path
2 White / 2 Red — On the Correct 3° Glide Path
Construction

Physical Construction

Each of the four PAPI units is a rectangular, box-section housing in die-cast aluminium alloy or louvred galvanised steel, weatherproofed and finished to resist UV degradation and de-icing fluid over years of outdoor service. Inside, the light source sits behind a two-part optical system: a lower red filter glass and an upper clear (white) glass, precisely separated so the beam transitions sharply between colours at the set glide-path angle, with a mechanical spirit-level and micrometer adjuster built into the housing so each unit can be levelled and pitched to within fractions of a degree during commissioning. The housing bolts to a frangible mounting mast set at a fixed, surveyed height above the runway shoulder, positioned so a shear point lets the mast break away cleanly if struck by an aircraft or vehicle. Primary cabling runs underground in conduit from each unit to its own isolating transformer, housed in a nearby L-867/L-868 base can, with sealed direct-burial connectors and a drainage provision to keep moisture away from the transformer and cable entries.

Specification

Technical Parameters

ParameterTypical Value
Light SourceLED array or 100W / 150W halogen lamp
ColourWhite (upper beam) and Red (lower beam) per unit
Luminous IntensityUp to 25,000 cd (white) and 12,000 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 (approx. 3 arc‑minutes)
Number of Units4 (standard PAPI); 2 (APAPI); 6+ for some configurations
Mounting TypeElevated (frangible poles) – typically 10–20 m from runway edge
Isolating Transformer65W – 150W (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 (65W–150W) per unit
Unit SynchronisationAll units in the wing bar wired on the same series circuit/step to present a consistent glide-path indication
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)≥ 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 arc-minutes vertical transition band per unit
Vertical Beam SpreadEach of the 4 units splayed at fixed increments about the 3° 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

PAPI specifications including beam angles, colours, and installation requirements

FAA AC 150/5345-28

Precision Approach Path Indicator (PAPI) systems

FAA AC 150/5345-46

Specification for Runway, Taxiway, Heliport, and Vertiport Light Fixtures (covers PAPI fixture qualification)

IEC/TS 61827

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

Prerequisites

Installation Requirements

Wing Bar Setout
Civil

Position the four-unit wing bar on one side of the runway at a fixed lateral offset, set back from the threshold at the distance derived from the design tables, tied to the runway centreline and threshold survey.

Frangible Mount Foundations
Civil

Install footings for each of the four units at equal lateral spacing along the bar, clear of the obstacle-limitation surface and wingtip clearance envelope.

Duct & Cable Route to CCR
Electrical

Run underground cabling from each unit back to the constant current regulator.

Isolating Transformer Matching
Electrical

Confirm each unit's 65W–150W isolating transformer matches the series circuit's rated current step before connection.

Four-Unit Aiming & Levelling
Mechanical

Individually aim each unit in elevation during commissioning so the four units together produce a sharp two-red/two-white split exactly on the design glide angle, with the transition band kept tight.

Frangible Coupling Fixing
Mechanical

Torque each unit's frangible mount to the specified value, keeping the units and mounting frame within the frangibility requirements for the runway's code number.

Wingtip/OLS Clearance Check
Documentation

Verify the bar's lateral offset keeps all four units clear of the obstacle-limitation surface and wingtip clearance envelope before energisation.

Pre-Energisation Sign-off
Documentation

Record unit spacing, cable routes, and torque values for the full bar as-built before the site is closed.

Verification

Testing & Commissioning

Insulation Resistance (Megger) Test
Pre-Energisation

Megger-test each unit's isolating transformer 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 all four units 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 unit's 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 all four units respond correctly and in unison at each step.

Glide Path Angle & Unit Aiming Verification
Final Acceptance

Set each unit's red/white transition angle with a calibrated PAPI aiming tool or theodolite, staggering the four units by the design increment so the two-red/two-white on-path indication reads correctly from the threshold.

Photometric Commissioning Test
Final Acceptance

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

Frangibility & Mounting Verification
Pre-Energisation

Confirm each frangible mast's 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 four units alongside as-built position and aiming angles in the commissioning dossier.

Upkeep

Inspection & Maintenance

Beam Alignment Check
Annual

Verify each unit's beam angle with a theodolite or specialised alignment tool, especially after maintenance or ground disturbance, since a small angular error shifts the glide path significantly at the threshold.

Photometric Intensity Check
Annual

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

Lens Cleaning
Quarterly

Clean dust, rubber deposits, de-icing fluids, and UV haze from each unit's lens to maintain output and colour transition clarity.

Lamp / LED Module Inspection
Semi-annual

Check halogen lamps for imminent burnout and LED arrays for individual diode failure, since either can distort the beam pattern and mislead pilots.

Frangible Coupling Check
Annual

Inspect couplings for fatigue from wind loading and thermal cycling and replace per manufacturer schedule to ensure safe breakaway on impact.

Insulation Resistance Test
Annual

Megger-test each unit'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 across all four units to keep the array correctly positioned relative to the runway edge.

Field Notes

Common Field Issues

Beam Misalignment

The accuracy of PAPI depends critically on the precise alignment of each unit's beam. Even a small angular error can shift the effective glide path by several feet at the runway threshold. Regular alignment checks (using a theodolite or specialised alignment tool) are essential, especially after maintenance or ground disturbance.

Lens Contamination and Optical Degradation

Lenses can become dirty or hazy due to dust, rubber deposits, de‑icing fluids, or UV exposure. This reduces the light output and can alter the colour transition. Routine cleaning and periodic photometric testing are required to maintain performance.

Lamp or LED Module Failure

In halogen‑based systems, lamp burnout is common. In LED systems, individual LEDs can fail, affecting the beam pattern. Regular inspections and prompt replacement are necessary to avoid misleading indications.

Frangible Coupling Fatigue

PAPI units are mounted on frangible poles. Wind loading and thermal cycling can weaken the couplings over time. Regular inspection and replacement per manufacturer schedules ensure the units will break away safely on impact.

Diagnostics

Troubleshooting Guide

One Unit Dark, Others Normal
Likely Cause
Failed LED module / lamp in that unit, or an open isolating transformer feeding it.
Diagnostic Steps
Confirm series loop continuity through the affected unit'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 four-unit 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 between units 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.
Misleading Red/White Split (Wrong Glide Path Indicated)
Likely Cause
One or more units have drifted from their commissioned elevation setting, or a lens/shutter assembly has 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 lens/shutter assembly for movement or damage.
Corrective Action
Re-aim and re-level the affected unit(s) to the surveyed angle using a theodolite or specialised alignment tool, then re-verify with a follow-up inspection.
Reduced or Uneven Light Output
Likely Cause
Hazy or contaminated lens, 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 lens; confirm the CCR is set to the correct intensity step for prevailing conditions.
Corrective Action
Clean or replace the lens, replace a degraded lamp/LED module, or correct the CCR step setting; re-verify with a follow-up photometric reading.
Unit Leaning, Loose, or Misaligned
Likely Cause
Frangible coupling has begun to fatigue or partially shear, or the base can/mast footing has settled due to ground movement.
Diagnostic Steps
Visually and physically check the frangible coupling for cracking or play; re-check unit aim against tolerance; inspect the surrounding ground for settlement or heave.
Corrective Action
Replace the frangible coupling on schedule if fatigued, re-level and re-aim the unit, and address any footing settlement to prevent recurrence.
Reliability

Failure Modes & Root Causes

LED Module / Lamp Failure
High Severity
Root Cause
Solder-joint fatigue from thermal cycling, moisture ingress through a compromised board seal, or ordinary end-of-life lumen depreciation.
Effect
Single unit goes dark or drops below minimum intensity while the rest of the four-light array continues to operate normally, shifting the readable red/white split.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and visual confirmation that all four units are 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; can darken the single unit or, if the open extends to the loop itself, take down the entire bar.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and loop-resistance testing from the CCR output.
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 red/white split across the four-light array, giving pilots an on-slope indication that no longer matches the surveyed glide path.
Detection Method
Ground or flight inspection of the glide-path angle against the design value, and periodic check of each unit's levelling and pitch-adjustment setting.
Series Cable / Connector Insulation Breakdown
Medium Severity
Root Cause
Cable jacket damage from excavation or rodent activity, age-related insulation degradation, or prolonged standing water in the duct run.
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 Contamination or Erosion
Low Severity
Root Cause
Prolonged UV exposure, abrasive particulate erosion, and grime or rubber-deposit build-up on the outer lens surface.
Effect
Reduced or hazy light output and a softened colour transition on the affected unit, which can fall below ICAO/FAA photometric thresholds.
Detection Method
Scheduled photometric intensity testing and visual inspection of the lens 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 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 PAPI bar runs 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 where a unit will be 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.

Aim Verification Before Return to Service
Operational

After any maintenance that touched pitch adjustment or levelling, confirm the unit's elevation setting against the design glide-path angle before closing out the work, since a single unit out of tolerance shifts the readable red/white split for approaching pilots.

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 unit out of aim tolerance, at reduced intensity, or otherwise non-compliant after maintenance; verify photometric and positional conformance across all four units before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Box-to-Box Intensity Matching Matters as Much as Absolute Intensity
Photometric

A box that is noticeably dimmer than its neighbours can still individually meet minimum candela while the imbalance itself creates a visible anomaly across the row; match relative intensity between boxes during maintenance, not just each box against the minimum spec.

A Level Box Can Still Have the Wrong Aim
Alignment

A box that has settled or tilted slightly can still display correct red and white colours from directly in front while its transition angle has shifted; verify each box's aim independently with a theodolite rather than relying on a visual walk-by check.

Test the Anti-Fog Heater as Its Own Check Item
Maintenance

Many PAPI units include internal heaters to prevent lens condensation in cold or humid climates; a failed heater shows up as reduced apparent intensity only in certain weather rather than an outright fault, so test heater function separately from the light source.

Dual-Side Installations Need Cross-Side Consistency
Verification

Where PAPI is installed on both sides of the runway for higher-category operations, aim and intensity between the two rows must be verified as matching each other, not just independently in-spec on each side.

A Low Sun Angle Can Mimic or Mask a Real Aim Fault
Verification

Seasonal low sun angles near sunrise or sunset can wash out or alter the perceived colour transition during a visual check, either mimicking a fault that isn't there or masking one that is; schedule photometric verification rather than relying solely on visual checks at those times of day.

Spacing Errors Compound Across the Row
Installation

A small spacing error between adjacent boxes, if repeated across all four units during a re-install, shifts the effective on-slope indication more than the same error would in a single box; verify spacing against the original survey data, not just against the neighbouring box.

Quick Answers

Frequently Asked Questions

Short answers about PAPI lights: signal meaning, specifications, circuits, standards, maintenance and common faults.

Q1What is a PAPI?

The Precision Approach Path Indicator is a visual glide slope guidance system made of four light units in a row, typically on the left side of the runway (both sides for Category II/III). Each unit shows red or white depending on the pilot's approach angle.

Q2How do pilots read PAPI signals?

On the correct glide path the pilot sees two red and two white units. More white units mean the aircraft is above the slope, and more red units mean it is below. All white indicates well above and all red indicates well below.

Q3Why is PAPI used?

It lets a pilot self-correct descent angle to a tight margin with a glance at the runway, without any onboard glide slope receiver. That matters most in marginal weather, at night, or where no ILS glide path is available.

Q4Where are PAPI systems installed?

On precision approach runways (CAT I, II, III), on non-precision runways to improve visual and circling approaches, at military airfields and at heliports.

Q5What are the typical specifications of a PAPI unit?

Typical values are an LED array or 100/150 W halogen lamp, up to 25,000 cd white and 12,000 cd red, a 3 degree glide path (adjustable 2.5-4 degrees), a red/white transition of about 3 arc-minutes, and frangible elevated mounting typically 10-20 m from the runway edge.

Q6How is a PAPI powered and controlled?

PAPI units are fed from a constant current series circuit, with each unit isolated by its own 65-150 W isolating transformer. Intensity follows the CCR steps, for example a 5-step schedule of 2.8, 3.4, 4.1, 5.2 and 6.6 A, and all units are wired on the same circuit or step so the indication stays consistent.

Q7What photometric performance should a PAPI meet?

Typical on-axis intensity is at least 16,000 cd white and 8,000 cd red per unit, a red/white transition of 3 arc-minutes or less, and a field intensity tolerance of ±25% at each CCR step. Chromaticity must fall within the ICAO Annex 14 white and red boundaries.

Q8Which standards apply to PAPI?

ICAO Annex 14 (beam angles, colours and installation), FAA AC 150/5345-28 (PAPI systems), FAA AC 150/5345-46 (fixture specification) and IEC/TS 61827 (luminaire characteristics).

Q9How often should a PAPI be inspected and maintained?

Typical intervals are quarterly for lens cleaning, semi-annual for lamp or LED module inspection, and annual for beam alignment with a theodolite or alignment tool, photometric checks, frangible coupling checks and insulation resistance testing.

Q10Why is PAPI beam alignment so critical?

A small angular error in a unit's beam shifts the indicated glide path significantly at the threshold, so alignment should be re-verified after maintenance or any ground disturbance.

Q11What should I check if one PAPI unit is dark and the others are normal?

The usual causes are a failed LED module or lamp in that unit, or an open isolating transformer. Confirm series loop continuity through the transformer primary, megger the transformer, and check the secondary voltage at the connector with the CCR energised.

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