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.
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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 & 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.
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.
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.
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.
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)
The Two-Light Glide Path Indication
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.
Technical Parameters
| Parameter | Typical Value |
|---|---|
| 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) |
| Operating Temperature | -40°C to +55°C |
Electrical Requirements
| Requirement | Typical Value |
|---|---|
| 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) |
| Earthing/Grounding | Fixture body and base can bonded to airfield earth grid |
| Fault Protection | CCR-level ground fault and open-circuit detection |
| Power Source | CCR output, regulated per ICAO/FAA intensity step schedule |
Photometric Requirements
| Parameter | Typical 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 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) |
| 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
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
Installation Requirements
Wing Bar Setout
CivilPosition 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
CivilInstall 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
ElectricalRun underground cabling from the bar back to its constant current regulator.
Isolating Transformer Matching
ElectricalConfirm each unit's 45W–65W isolating transformer matches the series circuit's rated current step before connection.
Two-Unit Aiming & Levelling
MechanicalAim 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
MechanicalTorque the frangible coupling to the specified value, checking the fitting shears as designed under lateral load.
Strip-Edge Clearance Check
DocumentationConfirm 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
DocumentationRecord mast position, cable route, and torque values as-built before the site is closed.
Testing & Commissioning
Insulation Resistance (Megger) Test
Pre-EnergisationMegger-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-EnergisationVerify 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
EnergisationWith 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
EnergisationCycle 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 AcceptanceSet 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 AcceptanceMeasure 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-EnergisationConfirm 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 AcceptanceRecord insulation, continuity, voltage, and photometric readings for both units alongside as-built position and aiming angles in the commissioning dossier.
Inspection & Maintenance
Beam Alignment Check
AnnualCalibrate 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
AnnualVerify white and red beam intensity and the red/white transition against ICAO thresholds using a calibrated photometer.
Lens Cleaning
QuarterlyClean dirt, dust, and de-icing fluid residue from each unit's lens to maintain colour transition integrity.
Lamp / LED Module Inspection
Semi-annualCheck each unit's light source for failure and replace promptly to avoid a misleading indication from either unit.
Frangible Coupling Check
AnnualInspect couplings for fatigue from wind loading and thermal cycling and replace on schedule to preserve breakaway performance.
Insulation Resistance Test
AnnualMegger-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
AnnualExamine primary and secondary cable connections for corrosion or loose crimps, a common source of intermittent series-circuit faults.
Mounting Pole Inspection
AnnualCheck pole verticality and base condition for both units to keep the pair correctly positioned relative to the runway edge.
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.
Troubleshooting Guide
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
Failure Modes & Root Causes
LED Module / Lamp Failure
Isolating Transformer Failure
Unit Elevation Drift
Series Cable / Connector Insulation Breakdown
Lens Contamination or Erosion
Frangible Coupling Fatigue
Safety & Operational Notes
Series Circuit Isolation
Electrical SafetyThe 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
OperationalAny 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
MechanicalNever 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
OperationalBecause 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
OperationalKeep 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 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 the remaining healthy unit on the same circuit.
PPE & Grounding
Personnel SafetyUse 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
ComplianceDo 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.
Engineering & Expert Notes
Two-Box Configuration Leaves No Redundancy
DesignLosing 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
AlignmentWith 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
MaintenanceAPAPI 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
ComplianceWhere 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
CalibrationInstalled 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
ElectricalSome 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.
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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