AGL Component Library By Precision AGL Academy

Helicopter PAPI

A specialised visual glide slope system tailored for helicopter operations. Helicopter PAPI provides a steeper approach angle (typically 4° to 6°) compared to fixed‑wing PAPI, accommodating the unique flight profiles and landing requirements of rotorcraft. It offers the same intuitive red/white colour indication as standard PAPI, ensuring safe and precise approaches to helipads and helicopter landing zones.

Helicopter PAPI steep-angle red/white glide slope indicator for heliports

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Overview

What Is It?

The Helicopter PAPI (H‑PAPI) is a visual approach slope indicator system specifically designed for helicopter operations. It is structurally similar to the standard four‑unit PAPI used on fixed‑wing runways, but with a key difference: the glide path angle is set significantly steeper, typically between 4° and 6° (compared to the standard 3° for fixed‑wing). This steeper angle accommodates the typical descent profiles of helicopters, which often approach landing zones with a higher rate of descent and a steeper approach path.

Helicopter PAPI is installed at helipads, heliports, and helicopter landing zones (HLZs) to provide pilots with a clear, visual indication of their position relative to the correct approach slope. It is particularly valuable in low visibility conditions, at night, and in confined areas where terrain or obstacles require precise glide path control. The system uses the same red/white colour transition as standard PAPI, making it intuitive for pilots already familiar with the technology.

Purpose

Purpose & Function

Helicopter PAPI exists because a standard 3° fixed-wing glide slope doesn't match how helicopters actually fly an approach — rotary-wing aircraft typically descend more steeply and into confined landing zones where a shallow, extended approach path may not be physically available due to terrain or obstacles. Without a glide indicator matched to that steeper profile, a helicopter pilot would have to judge the correct descent angle by eye alone, which is far less reliable at night, in poor visibility, or when the landing zone is surrounded by buildings, wires, or rising ground.

By using the same intuitive red/white colour logic as fixed-wing PAPI but calibrated to the steeper angle helicopters need, H-PAPI lets pilots already trained on standard visual glide slope indicators apply that same skill directly to helicopter operations, reducing the risk of a too-high or too-low approach into a landing zone with little room for correction.

Application

Where Is It Used?

Helicopter PAPI is deployed on a variety of helicopter landing sites:

  • Heliports – providing standard visual glide slope guidance for commercial and private helicopter operations.
  • Hospital helipads – ensuring precise approaches for emergency medical services (EMS) in confined urban environments.
  • Offshore helipads – on ships or oil platforms where a steeper approach is often required.
  • Military helicopter landing zones – supporting tactical and training operations.
  • Confined area helipads – where obstacles require a steeper approach angle.
  • As a complement to GPS/RNP approaches – providing visual backup for instrument approaches.
Placement

Installation & Location

The wing bar is mounted to one side of the final approach and take-off area (FATO) or helipad touchdown point, positioned much closer in than a fixed-wing PAPI installation to suit the steeper helicopter approach angle and the confined dimensions of most helicopter sites. Units are set out on a survey tied to the FATO centreline and touchdown point, at a lateral offset and setback chosen to place the on-slope indication over the aiming point at the design approach angle (commonly steeper than the standard 3°, and adjustable for confined or obstacle-limited sites). Mounts are typically lower-profile than runway PAPI, and on rooftop or offshore helipads may be deck-mounted rather than on a frangible ground coupling, since impact frangibility requirements differ from runway environments. Cabling runs back to a compact constant current regulator suited to the shorter circuit lengths typical of helipad installations.

Function

How Does It Work?

Helicopter PAPI operates on the same principle as standard PAPI, but with a steeper glide path angle and specific installation considerations for helipad environments:

  • 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 steep glide slope (typically 4°–6°).
  • Colour Indication: The four‑light display provides the same intuitive red/white combination as standard PAPI:
    • 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.
  • Steeper Glide Path: The steeper angle (4°–6°) allows helicopters to clear obstacles more effectively and follow a descent profile that aligns with typical helicopter approach procedures. The angle is adjustable to suit specific site requirements.
  • Power and Control: Helicopter PAPI units are powered from the constant current series circuit (often a dedicated circuit) via isolating transformers, with intensity controlled by the CCR (typically 3‑step or 5‑step). Brightness can be adjusted for day, twilight, and night operations.
  • Integration: Helicopter PAPI is typically deployed independently or integrated with the helipad lighting system and ALCMS. It may be combined with other approach aids such as the Helicopter Approach Path Indicator (HAPI) or visual docking guidance systems.
Architecture

System Architecture & Control Logic

Helicopter PAPI shares the same control architecture as standard PAPI — the glide path signal is fixed optically per unit, not switched electronically. Each of the four units is levelled and its lens/shutter tilted so its red/white transition sits at a specific elevation, with the four angles set apart to straddle the steeper 4°–6° approach rather than the standard 3°; that steeper aim is set once at commissioning and adjusted on site if the helipad's obstacle environment changes. Units are powered from a constant current series circuit — often a dedicated circuit rather than one shared with fixed-wing runway lighting — through their own isolating transformers, with the CCR or ALCMS setting one shared brightness step for day, twilight, or night across all four units. As with fixed-wing PAPI, that command changes overall brightness only; it cannot alter which unit shows red or white. Loop monitoring is standard series-circuit practice: the CCR tracks loop voltage against commanded current and reports a voltage rise as a loop fault (open lamp or failed transformer) for maintenance to trace, while the fixed optical aim itself is verified by periodic ground or flight check rather than by any onboard sensor.

CCR / ALCMS → Dedicated Series Circuit → Isolating Transformer → Light Unit (elevation fixed to steep angle)

CCR / ALCMS Selects shared brightness step DEDICATED SERIES CIRCUIT LOOP Often separate from fixed-wing runway circuits ISOLATING TRANSFORMER (PER UNIT) Taps fixed loop current to each light unit LIGHT UNIT (×4, STEEP-ANGLE AIM) Elevations set to straddle the 4°–6° approach 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
Approach Geometry

Why Steeper? Glide Path Angle Comparison

Fixed-Wing PAPI
3°
Shallow ~3° Approach
Helicopter PAPI (H-PAPI)
H 4–6°
Steeper 4–6° Approach
Steeper Angle = Shorter Final Approach & Better Obstacle Clearance for Confined Helipads
Construction

Physical Construction

Each unit shares the same rectangular, box-section housing used on fixed-wing PAPI installations — die-cast aluminium alloy or louvred galvanised steel, weatherproofed against UV exposure and de-icing fluid — but is set up for the steeper approach angle used at a helipad. The optics are split into 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 built-in spirit level and micrometer pitch adjuster used to aim each unit during commissioning. The housing mounts on a frangible mast at a fixed, surveyed height, positioned close to the helipad centreline compared to a runway installation, and engineered to shear away cleanly if struck. 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 keep the transformer and cable entries free of standing water.

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 4° – 6° (adjustable; steeper than standard PAPI)
Beam PatternNarrow vertical beam with a sharp red/white transition
Number of Units4 (standard helicopter PAPI), some configurations use 2 (like APAPI)
Mounting TypeElevated (frangible poles) – typically 10–20 m from the helipad centreline
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 array 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 heliport/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)≥ 18,000 cd on-axis per unit, up to 25,000 cd at full intensity
Main Beam Intensity (Red)≥ 9,000 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 SpreadUnits splayed about the steeper 4°–6° reference to build the composite on-slope band
Horizontal Beam Spread± 5° to ± 10° either side of the helipad approach centreline
Isocandela DistributionPer ICAO Annex 14 Attachment A (heliport supplement) / 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, Volume II

Heliport specifications – Helicopter PAPI requirements

FAA AC 150/5345-28

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

UK CAA CAP 437

Standards for Offshore Helicopter Landing Areas – includes helideck approach/PAPI lighting specifications

IEC/TS 61827

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

Prerequisites

Installation Requirements

FATO/Helipad Setout
Site

Tie the wing bar position to the FATO or helipad touchdown-point survey, set closer in than a fixed-wing PAPI installation, at the lateral offset and setback needed for the design approach angle (commonly 4°–6°, adjustable for confined or obstacle-limited sites).

Foundation or Deck-Mount Fixing
Civil

Install the frangible ground coupling, or on rooftop or offshore helipads the deck-mounted fixing, per the site's own impact requirements rather than runway frangibility standards.

Duct & Cable Route to Compact CCR
Electrical

Run cabling suited to the shorter circuit lengths typical of helipad sites back to the compact 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.

Unit-by-Unit Aiming & Levelling
Mechanical

Aim and level each unit during commissioning for the steeper, confined-site approach angle rather than the standard 3° runway glide path.

Low-Profile Mount Fixing
Mechanical

Torque the lower-profile mounts to the specified value, appropriate to the helipad environment rather than a standard elevated frangible pole.

Confined-Site Clearance Check
Documentation

Verify obstacle and space clearance for the confined dimensions typical of helicopter sites before energisation.

Pre-Energisation Sign-off
Documentation

Record FATO/touchdown survey reference, cable route, and fixing 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 all 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 each unit responds correctly and in unison at each step.

Steep Glide Path Angle Verification
Final Acceptance

Set each unit's red/white transition to the steeper helicopter approach angle (typically 4°–6°) with a calibrated aiming tool or theodolite, confirming the on-path indication reads correctly from the helipad approach direction.

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 proximity to the helipad centreline 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 units alongside as-built position and aiming angles in the commissioning dossier.

Upkeep

Inspection & Maintenance

Glide Path Angle Verification
Annual

Re-check the steep 4°–6° angle setting with a theodolite or precision alignment tool, since even a small error significantly shifts the indicated path in confined helipad environments.

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, marine salt, and urban airborne contaminants from each unit's lens to maintain light 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 sharp red/white transition.

Frangible Coupling Check
Annual

Inspect couplings for fatigue from wind loading, rotor wash vibration, and thermal cycling, and replace on schedule to preserve breakaway performance.

Obstacle Clearance Review
Annual

Confirm the indicated glide path still provides safe clearance from surrounding obstacles, re-surveying if the helipad environment has changed.

Insulation Resistance Test
Annual

Megger-test the isolating transformer and series circuit to confirm insulation resistance stays above the minimum, flagging moisture ingress before it causes a fault.

Mounting Pole & Base Inspection
Annual

Check pole verticality, base corrosion, and surrounding ground condition to ensure units remain correctly positioned relative to the helipad centreline.

Field Notes

Common Field Issues

Steep Angle Calibration

The steeper glide path angle (4°–6°) requires precise calibration. Even a small angular error can significantly affect the approach path, especially in confined helipad environments. Regular alignment checks using precision optical tools are essential.

Lens Contamination

Helipads are often located in dusty, marine, or urban environments with high levels of airborne contaminants. Lenses must be cleaned regularly to maintain light output and colour transition integrity.

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.

Frangible Coupling Fatigue

Helicopter PAPI units are mounted on frangible poles. Wind loading, vibration from helicopter rotor wash, and thermal cycling can weaken couplings. Regular inspection ensures breakaway performance on impact.

Obstacle Clearance

The steeper glide path is often selected to clear obstacles, but the visual indication must be carefully aligned with the actual obstacle environment. Site‑specific calibration is critical to ensure the indicated path provides safe obstacle clearance.

Diagnostics

Troubleshooting Guide

One Unit Dark, Others Normal
Likely Cause
Failed LED module / lamp in that unit, or an open isolating transformer feeding it on the dedicated helipad circuit.
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 Dedicated Circuit Dark / CCR Will Not Regulate
Likely Cause
Open-circuit fault in the dedicated series loop feeding the helipad 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.
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 — often accelerated by marine or urban airborne contaminants around helipads — has degraded insulation resistance.
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.
Steep Glide Path Indication Reads Incorrectly
Likely Cause
One or more units have drifted from their commissioned steep-angle (4°–6°) setting, which is more sensitive to small errors given the confined helipad approach environment.
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; confirm obstacle clearance assumptions still match the site.
Corrective Action
Re-aim and re-level the affected unit(s) to the surveyed steep angle using precision optical tools, then re-verify against the obstacle environment with a follow-up inspection.
Reduced or Hazy Light Output
Likely Cause
Lens contamination from dust, marine salt, or urban pollutants common in helipad environments, an aging LED array, or the CCR running on a lower brightness step than required.
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 — accelerated by rotor wash vibration — or the base footing has settled.
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
A unit within the wing bar goes dark or drops below minimum intensity, degrading the red/white split that indicates the steep 4-6° helicopter glide path.
Detection Method
Megger test of the transformer, secondary voltage check with the CCR energised, and visual confirmation that all wing-bar 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; darkens the affected unit or, given the shorter dedicated helipad circuits, can take down the whole wing 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 / Approach Angle Drift
High Severity
Root Cause
Vibration-induced loosening of the pitch-adjustment mechanism on a deck-mounted unit, footing settlement on a ground-mounted installation, or an aiming error introduced during maintenance.
Effect
A misleading red/white split at the steep design approach angle, which is more consequential in the confined dimensions typical of helicopter sites.
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 splices, or water ingress in the duct run — on offshore or rooftop helipads, salt spray accelerates jacket and connector degradation.
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
Salt spray on offshore installations, rotor downwash-driven grime and dust, or ordinary UV exposure and erosion of the lens surface.
Effect
Reduced or hazy light output and a softened colour transition, harder to read given the closer-in, steeper approach used at most helipads.
Detection Method
Scheduled photometric intensity testing against ICAO/FAA thresholds and visual inspection of the lens during quarterly cleaning.
Mount / Deck Fixing Fatigue
Medium Severity
Root Cause
Cyclic vibration loading on a deck- or rooftop-mounted fixing, corrosion at fasteners in a marine environment, or frangible coupling fatigue on ground-mounted units.
Effect
Unit loosens or shifts alignment, taking the light out of aim tolerance; on ground-mounted units the frangible coupling may separate entirely.
Detection Method
Physical inspection of the mount or coupling for cracking, corrosion, or play, and periodic fixture-aim/level checks against tolerance.
Precautions

Safety & Operational Notes

Series Circuit Isolation
Electrical Safety

The wing 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.

Helipad Work Coordination
Operational

Any work on or near an active helipad requires coordination with the operator or ATC and a NOTAM while a unit is dark or out of tolerance, with personnel kept clear of the touchdown/lift-off area during any approach.

Rotor Downwash Hazard
Personnel Safety

Never carry out maintenance on the wing bar while a helicopter is operating nearby; loose fasteners, gaskets, or tools become foreign object hazards under rotor downwash and downwash forces can also destabilise personnel working at a deck edge.

Deck Edge & Marine Environment Precautions
Personnel Safety

On rooftop or offshore helipads, use fall protection and follow the platform's permit-to-work procedure when accessing units near a deck edge, and expect accelerated corrosion at fasteners and connectors that warrants closer inspection intervals.

Frangibility / Mount Integrity Not to Be Defeated
Mechanical

On ground-mounted units, never substitute the frangible coupling with a rigid fitting; on deck- or rooftop-mounted units, restore the fixing to its specified torque and corrosion protection so the mount performs as designed under vibration and wind loading.

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 other 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 mounting structure 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 the wing bar before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Confined-Area Siting Increases Obstruction Sensitivity
Siting

Helicopter landing zones often sit closer to buildings and trees than fixed-wing runways; verify line-of-sight to the full beam sector at the actual steep glide angle in use, not just at the heights and distances used for standard fixed-wing PAPI siting.

Steeper Angle Setups Deserve Their Own Aim Charts
Alignment

At 4°–6° instead of the standard 3°, absolute aim tolerance at typical viewing distances behaves differently than on a fixed-wing PAPI; use the manufacturer's aim data for the steeper-angle configuration rather than reusing setup notes written for standard PAPI.

Rotor Downwash Loosens Fasteners Faster
Mechanical

Repeated helicopter operations close to the fixture subject H-PAPI mounts to more sustained vibration than a typical fixed-wing PAPI site sees; increase the fastener torque-check frequency at high-cycle helipads rather than following the standard PAPI interval.

NVG Compatibility Needs Its Own Verification
Optical

Many helicopter operations use night vision goggles; where that applies to the operating fleet, confirm the fixture's output profile still meets NVG compatibility requirements separately from the standard daylight and twilight intensity-step checks.

Unimproved Pads See More Particulate Ingress
Durability

HLZs on unimproved or semi-improved surfaces expose the fixture to more dust and debris from rotor wash than a paved runway does; inspect lens condition and seals on a shorter cycle at these sites.

Verify the Angle Against That Site's Own Obstacle Study
Compliance

The 4°–6° glide angle is set per HLZ based on its specific obstacle environment, so confirm the as-built angle against that site's own obstacle assessment at each major check rather than assuming a generic helicopter PAPI default applies.

Quick Answers

Frequently Asked Questions

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

Q1What is a Helicopter PAPI (Helicopter Precision Approach Path Indicator)?

The Helicopter PAPI (H‑PAPI) is a visual approach slope indicator system specifically designed for helicopter operations. It is structurally similar to the standard four‑unit PAPI used on fixed‑wing runways, but with a key difference: the glide path angle is set significantly steeper, typically between 4° and 6° (compared to the standard 3° for fixed‑wing). This steeper angle accommodates the typical descent profiles of helicopters, which often approach landing zones with a higher rate of descent and a steeper approach path.

Q2What is the purpose of a Helicopter PAPI (Helicopter Precision Approach Path Indicator)?

Helicopter PAPI exists because a standard 3° fixed-wing glide slope doesn't match how helicopters actually fly an approach — rotary-wing aircraft typically descend more steeply and into confined landing zones where a shallow, extended approach path may not be physically available due to terrain or obstacles.

Q3Where is a Helicopter PAPI (Helicopter Precision Approach Path Indicator) used and installed?

Helicopter PAPI is deployed on a variety of helicopter landing sites: Heliports – providing standard visual glide slope guidance for commercial and private helicopter operations. Hospital helipads – ensuring precise approaches for emergency medical services (EMS) in confined urban environments. Offshore helipads – on ships or oil platforms where a steeper approach is often required. Military helicopter landing zones – supporting tactical and training operations. Confined area helipads – where obstacles require a steeper approach angle. As a complement to GPS/RNP approaches – providing visual backup for instrument approaches.

Q4How does a Helicopter PAPI (Helicopter Precision Approach Path Indicator) work?

Helicopter PAPI operates on the same principle as standard PAPI, but with a steeper glide path angle and specific installation considerations for helipad environments: 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 steep glide slope (typically 4°–6°).

Q5What are the typical technical parameters of a Helicopter PAPI (Helicopter Precision Approach Path Indicator)?

Typical values are — Light Source: LED array or 100W / 150W halogen lamp; Colour: White (upper beam) and Red (lower beam) per unit; Luminous Intensity: Up to 25,000 cd (white) and 12,000 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 4° – 6° (adjustable; steeper than standard PAPI); Beam Pattern: Narrow vertical beam with a sharp red/white transition; Number of Units: 4 (standard helicopter PAPI), some configurations use 2 (like APAPI); Mounting Type: Elevated (frangible poles) – typically 10–20 m from the helipad centreline.

Q6What are the electrical requirements for a Helicopter PAPI (Helicopter 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 (65W–150W) per unit; Unit Synchronisation: All units in the array wired on the same series circuit/step to present a consistent glide-path indication; 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 a Helicopter PAPI (Helicopter Precision Approach Path Indicator)?

Typical requirements are — Main Beam Intensity (White): ≥ 18,000 cd on-axis per unit, up to 25,000 cd at full intensity; Main Beam Intensity (Red): ≥ 9,000 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 Spread: Units splayed about the steeper 4°–6° reference to build the composite on-slope band; Horizontal Beam Spread: ± 5° to ± 10° either side of the helipad approach centreline; Isocandela Distribution: Per ICAO Annex 14 Attachment A (heliport supplement) / FAA AC 150/5345-28 figures; Chromaticity (White): Within ICAO Annex 14 white boundary (CIE coordinates).

Q8Which standards apply to a Helicopter PAPI (Helicopter Precision Approach Path Indicator)?

The main references are ICAO Annex 14, Volume II — Heliport specifications – Helicopter PAPI requirements; FAA AC 150/5345-28 — Precision Approach Path Indicator (PAPI) systems – includes helicopter PAPI guidance; UK CAA CAP 437 — Standards for Offshore Helicopter Landing Areas – includes helideck approach/PAPI lighting specifications; IEC/TS 61827 — Characteristics of inset and elevated luminaires used on aerodromes and heliports (photometric & electrical performance). Always verify the current edition and your aerodrome's approved requirements.

Q9How often should a Helicopter PAPI (Helicopter Precision Approach Path Indicator) be inspected and maintained?

Typical maintenance tasks and intervals are: Glide Path Angle Verification (annual); Photometric Intensity Check (annual); Lens Cleaning (quarterly); Lamp / LED Module Inspection (semi-annual); Frangible Coupling Check (annual); Obstacle Clearance Review (annual); Insulation Resistance Test (annual); Mounting Pole & Base Inspection (annual). Your airport's approved maintenance programme takes precedence.

Q10How do I troubleshoot common Helicopter PAPI (Helicopter Precision Approach Path Indicator) faults?

Common symptoms covered are: One Unit Dark, Others Normal; Entire Dedicated Circuit Dark / CCR Will Not Regulate; CCR Trips on Overcurrent or Ground Fault; Steep Glide Path Indication Reads Incorrectly; Reduced or Hazy Light Output; Unit Leaning, Loose, or Misaligned. For example, for "One Unit Dark, Others Normal": Likely Cause: Failed LED module / lamp in that unit, or an open isolating transformer feeding it on the dedicated helipad circuit. 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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