AGL Component Library By Precision AGL Academy

APAPI

Abbreviated Precision Approach Path Indicator – a compact two‑unit visual glide slope system that provides pilots with a simple red/white indication of their position relative to the correct approach path. APAPI is an economical solution for smaller airfields, heliports, and as a backup to full PAPI systems.

APAPI (Abbreviated Precision Approach Path Indicator) two-unit red/white glide slope system

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Overview

What Is It?

The Abbreviated Precision Approach Path Indicator (APAPI) is a visual glide slope guidance system consisting of two light units arranged in a row, typically installed on the left side of the runway. 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, but with fewer lights than the standard four‑unit PAPI.

APAPI provides a simplified but effective glide path reference, making it ideal for smaller airports, general aviation fields, heliports, and temporary installations. It is also used as a backup system on larger runways. The two‑unit configuration reduces cost and footprint while still delivering clear guidance for visual approaches.

Purpose

Purpose & Function

APAPI exists to bring the same red/white, above/below/on-path logic that pilots already trust on standard PAPI to airfields where a full four-unit installation isn't warranted — smaller general aviation strips, heliports, or temporary sites. Using two light units instead of four means the pilot reads a coarser indication of glide slope deviation, but the fundamental colour-transition principle stays identical, so no new interpretation skill is required.

Because it mirrors standard PAPI so closely, APAPI also works well as a backup or supplementary indicator on larger runways, giving controllers and pilots an additional visual reference at reduced cost and physical footprint without introducing a system pilots would need to learn to read differently.

Application

Where Is It Used?

APAPI is deployed on a variety of airfields and landing sites:

  • General aviation airports – providing cost‑effective glide slope guidance.
  • Heliports – where a compact system is needed for helicopter approaches.
  • Regional and remote airstrips – with limited electrical capacity or space.
  • Military forward operating bases – requiring rapid deployment.
  • As a backup to PAPI – on precision runways for redundancy.
  • Temporary or emergency runways – where a full PAPI is not justified.
Placement

Installation & Location

The wing bar consists of two light units mounted on a single frangible mast, positioned on one side of the runway (normally the left, viewed from the approach) at a fixed lateral offset from the runway edge, clear of the obstacle-limitation surface and any propeller or jet-blast zone. The bar is set back from the threshold along the runway a distance chosen from the design tables to place the visual glide path over the threshold at the standard eye-to-wheel height, tied into the runway centreline and threshold survey so the resulting glide angle matches the promulgated approach path. Each unit sits on a frangible coupling at a set height and is individually aimed and levelled during commissioning to give a sharp red/white transition at the design angle. Cabling runs underground from the bar back to its constant current regulator, and units are set out with enough separation from the runway strip edge that a frangible failure does not intrude on the graded area.

Function

How Does It Work?

APAPI operates on the same optical principle as PAPI but with two light units:

  • Optical Design: Each light unit contains a lamp and a precision optical system that projects a beam with a sharp red/white transition. The transition angle is set to the desired glide slope (typically 3°).
  • Colour Indication: With only two units, the indication is coarser but still intuitive:
    • Both white – aircraft is well above the glide path.
    • Near unit red / far unit white – on the correct glide path. The unit nearest the runway is set to a higher transition angle than the far unit, so on the design glide path the near unit still reads red and the far unit has already gone white. This is the same near-red/far-white convention used by the standard four‑unit PAPI, just with only one pair of units instead of two.
    • Both red – aircraft is well below the glide path.
  • Power and Control: APAPI units are powered from the constant current series circuit via isolating transformers, with intensity controlled by the CCR (typically 3‑step). Brightness can be adjusted for day, twilight, and night operations.
  • Integration: APAPI is often deployed independently or integrated with the runway lighting system. It may be controlled remotely via the ALCMS if connected.
Architecture

System Architecture & Control Logic

APAPI carries the same control architecture as full PAPI, simply with fewer units to power and aim. Each of the two light units is levelled and its lens/shutter tilted so its red/white transition sits at a specific elevation, with the near unit set to a fractionally higher transition angle than the far one so the near unit reads red and the far unit reads white on the design glide path; that split is fixed optical hardware set at commissioning, not a runtime signal. Both units draw from the same constant current series circuit through their own isolating transformers, so the CCR (or ALCMS, if the site connects one) commands a single shared brightness step for the whole two-light array — it has no way to change which unit shows red versus white, only how bright both burn. Loop monitoring follows the standard series-circuit pattern: the CCR watches loop voltage against commanded current, and a rise reads back as a lamp or transformer fault on that loop, not a pinpointed unit or a misalignment — those are only caught by periodic ground or flight check of the fixed optical aim.

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

CCR / ALCMS (IF CONNECTED) Selects shared brightness step SERIES CIRCUIT LOOP Same current to both units — brightness only ISOLATING TRANSFORMER (PER UNIT) Taps fixed loop current to each light unit LIGHT UNIT (×2, INDIVIDUALLY AIMED) Near unit set fractionally higher than far unit Fixed at commissioning — no runtime control SIGNAL IS OPTICAL, NOT ELECTRONIC The one-white/one-red split 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 Two-Light Glide Path Indication

Both White
Aircraft is well above the glide path
One White / One Red
On the correct glide path — a coarser reading than PAPI's four-light bar
Both Red
Aircraft is well below the glide path
2 Units, 3 States — A Simpler Read Than Full PAPI's 5-State Bar
Construction

Physical Construction

Each of the two APAPI units shares the same rectangular, box-section housing used on full PAPI installations, in die-cast aluminium alloy or louvred galvanised steel, weatherproofed against UV exposure and de-icing fluid. The light source sits behind a lower red filter glass and an upper clear (white) glass, split at a precise internal line so the beam changes sharply from red to white at the set glide-path angle, with a built-in spirit level and micrometer pitch adjuster used to set each unit during commissioning. The housing mounts on a frangible mast at a fixed, surveyed height, engineered to shear away cleanly on impact, and is typically installed on runways too narrow or too lightly trafficked to justify a full four-unit wing bar. Cabling runs underground in conduit to a dedicated isolating transformer per unit, housed in a nearby base can with sealed, direct-burial connectors and a drainage provision to protect the transformer and cable entries from moisture.

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 Units2 (standard APAPI)
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
Unit SynchronisationBoth units wired on the same series circuit/step to keep the red/white transition simultaneous
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)≥ 12,000 cd on-axis per unit, up to 15,000 cd at full intensity
Main Beam Intensity (Red)≥ 6,000 cd on-axis per unit, up to 8,000 cd at full intensity
Transition Sharpness (Red/White)≤ 3 arc-minutes vertical transition band per unit
Vertical Beam Spread2 units splayed about the 3° reference; coarser composite band than 4-unit PAPI
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

APAPI specifications and installation requirements

FAA AC 150/5345-28

Precision Approach Path Indicator (PAPI) systems – includes APAPI guidance

IEC/TS 61827

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

FAA Engineering Brief #67

Light Sources Other than Incandescent and Xenon for Airport and Obstruction Lighting Fixtures

Prerequisites

Installation Requirements

Wing Bar Setout
Civil

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

Frangible Mast Foundation
Civil

Install the footing for the single frangible mast carrying both units, clear of the obstacle-limitation surface and any propeller or jet-blast zone.

Duct & Cable Route to CCR
Electrical

Run underground cabling from the bar back to its constant current regulator.

Isolating Transformer Matching
Electrical

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

Two-Unit Aiming & Levelling
Mechanical

Aim and level each of the two units individually during commissioning to give a sharp red/white transition at the design glide angle.

Frangible Coupling Fixing
Mechanical

Torque the frangible coupling to the specified value, checking the fitting shears as designed under lateral load.

Strip-Edge Clearance Check
Documentation

Confirm the mast's separation from the runway strip edge is enough that a frangible failure does not intrude on the graded area.

Pre-Energisation Sign-off
Documentation

Record mast position, cable route, and torque values 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 both 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 both 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, confirming the two-unit indication reads correctly given the narrower box compared to a full four-unit wing bar.

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 both units alongside as-built position and aiming angles in the commissioning dossier.

Upkeep

Inspection & Maintenance

Beam Alignment Check
Annual

Calibrate each of the two units' beam angles with precision optical tools; with only two units, an alignment error has a proportionally larger effect on the indicated path.

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

Lamp / LED Module Inspection
Semi-annual

Check each unit's light source for failure and replace promptly to avoid a misleading indication from either unit.

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 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 for both units to keep the pair correctly positioned relative to the runway edge.

Field Notes

Common Field Issues

Beam Misalignment

With only two units, alignment errors are more critical – a small angular error can shift the effective glide path significantly. Regular alignment checks using precision optical tools are essential.

Lens Contamination

Dirt, dust, and de‑icing fluids can reduce light output and alter the 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

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

Diagnostics

Troubleshooting Guide

One Unit Dark, Other Normal
Likely Cause
Failed LED module / lamp, or an open isolating transformer feeding that unit — with only two units, a single failure removes half the array.
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 two-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 the cable run between the two units.
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 both 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
Likely Cause
One or both units have drifted from their commissioned elevation setting. Because the array only has two units, even a small angular error shifts the effective glide path significantly.
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.
Corrective Action
Re-aim and re-level the affected unit(s) to the surveyed angle using precision optical tools, then re-verify with a follow-up inspection.
Reduced or Hazy Light Output
Likely Cause
Contaminated or eroded 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
With only two units in the array, loss of one unit removes half the indication rather than a fraction of a larger array, making a single failure far more disruptive than in a 4-light PAPI.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and visual confirmation that both units are alight during routine inspection.
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 the entire two-unit circuit.
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 settlement of the mounting footing, vibration-induced loosening of the pitch-adjustment mechanism, or an aiming error introduced during maintenance.
Effect
A misleading red/white split at the design glide path — because APAPI has only two units instead of four, even a small angular error on one unit shifts the effective indication significantly.
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, corroded L-823 splices, or prolonged standing water in the duct run between the two units.
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, which can make the on-slope indication harder to read at range.
Detection Method
Scheduled photometric intensity testing against ICAO/FAA thresholds 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 the light out of aim tolerance or out of service entirely.
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 APAPI array 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 while a unit is dark or out of tolerance; with only two units in the array, taking one out of service removes half the glide-path indication, so schedule work accordingly.

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

Because the two-unit array is more sensitive to a single aiming error than a four-light PAPI, confirm elevation setting and level on the adjusted unit against the design glide-path angle before closing out any maintenance that touched pitch adjustment.

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 the remaining healthy unit 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 on both units before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Two-Box Configuration Leaves No Redundancy
Design

Losing one unit on a two-box APAPI removes half the visual indication, unlike a four-box PAPI where a single dark unit still leaves a usable partial picture; treat any single-unit fault on APAPI as an urgent restoration item rather than a routine ticket.

Tighter Aim Tolerance Between the Two Units
Alignment

With only two reference points, an aim mismatch between the pair reads to a pilot as an ambiguous transition far more readily than the same mismatch would across four PAPI boxes; verify both units against one shared theodolite baseline rather than sequentially against slightly different references.

General Aviation Sites See Longer Gaps Between Visits
Maintenance

APAPI often serves smaller fields without daily airport operations staff on site, so base settling, vegetation encroachment, or slow leveling drift can go unnoticed for longer; extend the inspection checklist with an explicit box-leveling check rather than relying on someone reporting an issue.

Backup Role Doesn't Relax the Duty Cycle
Compliance

Where APAPI is fitted as a secondary indicator alongside a primary PAPI on a larger runway, it's tempting to defer its calibration cycle; the abbreviated unit still has to meet the same photometric tolerance for the moments it's the active indicator.

Heliport Ground Reflections Can Skew Photocell Readings
Calibration

Installed near helipad surfaces, an ambient-light photocell can pick up reflected light off adjacent pads or apron lighting, causing premature or delayed intensity step changes; site the photocell away from reflective surfaces during initial placement, not just away from direct light sources.

Simplified Power Feeds Still Need Full Bonding Rigor
Electrical

Some APAPI installs at temporary or general aviation strips use simplified power runs without a full isolating-transformer series loop; don't skip earthing and bonding checks just because the installation looks temporary or small-scale.

Quick Answers

Frequently Asked Questions

Short answers about the APAPI (Abbreviated Precision Approach Path Indicator): what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is an APAPI (Abbreviated Precision Approach Path Indicator)?

The Abbreviated Precision Approach Path Indicator (APAPI) is a visual glide slope guidance system consisting of two light units arranged in a row, typically installed on the left side of the runway. Each unit projects a red or white light depending on the pilot's viewing angle.

Q2What is the purpose of an APAPI (Abbreviated Precision Approach Path Indicator)?

APAPI exists to bring the same red/white, above/below/on-path logic that pilots already trust on standard PAPI to airfields where a full four-unit installation isn't warranted — smaller general aviation strips, heliports, or temporary sites. Using two light units instead of four means the pilot reads a coarser indication of glide slope deviation, but the fundamental colour-transition principle stays identical, so no new interpretation skill is required.

Q3Where is an APAPI (Abbreviated Precision Approach Path Indicator) used and installed?

APAPI is deployed on a variety of airfields and landing sites: General aviation airports – providing cost‑effective glide slope guidance. Heliports – where a compact system is needed for helicopter approaches. Regional and remote airstrips – with limited electrical capacity or space. Military forward operating bases – requiring rapid deployment. As a backup to PAPI – on precision runways for redundancy. Temporary or emergency runways – where a full PAPI is not justified.

Q4How does an APAPI (Abbreviated Precision Approach Path Indicator) work?

APAPI operates on the same optical principle as PAPI but with two light units: Optical Design: Each light unit contains a lamp and a precision optical system that projects a beam with a sharp red/white transition. The transition angle is set to the desired glide slope (typically 3°). Colour Indication: With only two units, the indication is coarser but still intuitive: Both white – aircraft is well above the glide path. Near unit red / far unit white – on the correct glide path.

Q5What are the typical technical parameters of an APAPI (Abbreviated Precision Approach Path Indicator)?

Typical values are — Light Source: LED array or 45W/65W halogen lamp; Colour: White (upper beam) and Red (lower beam) per unit; Luminous Intensity: Up to 15,000 cd (white) and 8,000 cd (red) depending on setting; Intensity Steps: 3‑step (day, twilight, night) or 5‑step (2.8A – 6.6A) CCR controlled; Glide Path Angle: Typically 3° (2.5° to 4° adjustable); Beam Pattern: Narrow vertical beam with a sharp red/white transition; Number of Units: 2 (standard APAPI); Mounting Type: Elevated (frangible poles) – typically 10–20 m from runway edge; Isolating Transformer: 45W – 65W (6.6A series circuit) per unit; Protection Class: IP67 / IP68 (weather‑resistant).

Q6What are the electrical requirements for an APAPI (Abbreviated Precision Approach Path Indicator)?

Typical requirements are — Circuit Type: Series circuit, constant current (CCR fed); Rated Series Current: 6.6A (5-step: 2.8A / 3.4A / 4.1A / 5.2A / 6.6A) or 3-step equivalent; Isolation: Via dedicated isolating transformer (45W/65W) per unit; Unit Synchronisation: Both units wired on the same series circuit/step to keep the red/white transition simultaneous; Transformer Secondary: Matched to fixture wattage; sized to series circuit rating; Cable Type: L-824 single-conductor, direct-burial rated, 5kV or 600V per circuit design; Connector: L-823 primary connector, submersible-rated splice; Insulation Resistance: ≥ 50 MΩ (megger test, cable-to-ground).

Q7What photometric requirements apply to an APAPI (Abbreviated Precision Approach Path Indicator)?

Typical requirements are — Main Beam Intensity (White): ≥ 12,000 cd on-axis per unit, up to 15,000 cd at full intensity; Main Beam Intensity (Red): ≥ 6,000 cd on-axis per unit, up to 8,000 cd at full intensity; Transition Sharpness (Red/White): ≤ 3 arc-minutes vertical transition band per unit; Vertical Beam Spread: 2 units splayed about the 3° reference; coarser composite band than 4-unit PAPI; 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).

Q8Which standards apply to an APAPI (Abbreviated Precision Approach Path Indicator)?

The main references are ICAO Annex 14 — APAPI specifications and installation requirements; FAA AC 150/5345-28 — Precision Approach Path Indicator (PAPI) systems – includes APAPI guidance; IEC/TS 61827 — Characteristics of inset and elevated luminaires used on aerodromes and heliports (photometric & electrical performance); FAA Engineering Brief #67 — Light Sources Other than Incandescent and Xenon for Airport and Obstruction Lighting Fixtures. Always verify the current edition and your aerodrome's approved requirements.

Q9How often should an APAPI (Abbreviated Precision Approach Path Indicator) be inspected and maintained?

Typical maintenance tasks and intervals are: Beam Alignment Check (annual); Photometric Intensity Check (annual); Lens Cleaning (quarterly); Lamp / LED Module Inspection (semi-annual); Frangible Coupling Check (annual); Insulation Resistance Test (annual); Cable & Connector Inspection (annual); Mounting Pole Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common APAPI (Abbreviated Precision Approach Path Indicator) faults?

Common symptoms covered are: One Unit Dark, Other Normal; Entire Series Circuit Dark / CCR Will Not Regulate; CCR Trips on Overcurrent or Ground Fault; Misleading Red/White Split; Reduced or Hazy Light Output; Unit Leaning, Loose, or Misaligned. For example, for "One Unit Dark, Other Normal": Likely Cause: Failed LED module / lamp, or an open isolating transformer feeding that unit — with only two units, a single failure removes half the array. 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.

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