AVASI
Abbreviated Visual Approach Slope Indicator – a simplified single‑bar or two‑bar visual glide slope system that provides pilots with a basic red/white indication of their position relative to the approach path. AVASI is an economical and compact solution for smaller airfields, heliports, and temporary operations where full VASI or PAPI is not justified.
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What Is It?
The Abbreviated Visual Approach Slope Indicator (AVASI) is a simplified visual glide slope guidance system. Unlike the multi‑bar VASI or the four‑unit PAPI, AVASI typically consists of a single light bar or a simplified two‑bar configuration with fewer light units. It provides a basic but effective red/white indication to help pilots maintain a safe descent angle during final approach.
AVASI is designed for smaller airfields, heliports, and temporary operations where a full‑scale system is not economically or logistically justified. It offers a compact footprint, lower power consumption, and simpler installation while still delivering the essential visual cue needed for safe approaches.
Purpose & Function
AVASI exists to bring basic glide slope guidance to airfields and temporary operations where the cost, power requirements, or physical footprint of a full VASI or PAPI installation can't be justified. By reducing the light units to a single bar or simplified two-bar layout, it keeps the essential red/white on-path indication pilots need while cutting the infrastructure and maintenance burden considerably.
This trade-off is deliberate: AVASI accepts a coarser glide slope indication in exchange for being deployable at smaller general aviation fields, heliports, and short-term operations that would otherwise have no visual glide guidance at all, which is a meaningful safety improvement over relying on unaided visual approach judgement.
Where Is It Used?
AVASI is deployed on a variety of smaller and specialised landing sites:
- General aviation airports – with low traffic volumes and limited budgets.
- Heliports – where a compact system is needed for helicopter approaches.
- Remote and regional airstrips – with limited electrical infrastructure.
- Military forward operating bases – requiring rapid deployment and simplicity.
- Temporary or emergency runways – where a lightweight, portable system is advantageous.
- As a backup to PAPI or VASI – on larger runways for additional redundancy.
Installation & Location
AVASI reduces the standard VASI arrangement to a single light bar, mounted on one side of the runway at a fixed lateral offset from the edge, clear of the obstacle-limitation surface and any blast zone. The bar is set back from the threshold at the distance needed to place the resulting on-slope indication over the threshold at the correct height, tied into the runway centreline and threshold survey. Units sit on frangible mounts and are individually aimed and levelled during commissioning to give the correct red/white split at the design glide angle. Cabling runs underground back to the constant current regulator, and the single-bar footprint suits sites where space, budget, or traffic volume don't justify a full two-bar system.
How Does It Work?
AVASI operates on the same fundamental optical principle as VASI and PAPI, but with a simplified configuration:
- Configuration: AVASI typically uses a single bar of lights (or two bars in some configurations) installed on the left side of the runway or helipad. The bar contains one or more light units that project a beam with a distinct red/white transition.
- Colour Indication: The pilot sees a single bar that changes colour based on the viewing angle. The indication is typically:
- All white – aircraft is above the glide path.
- White/red transition (or one white, one red in two‑bar setups) – on the correct glide path.
- All red – aircraft is below the glide path.
- Power and Control: AVASI units are powered from the constant current series circuit via isolating transformers, with intensity controlled by the CCR (typically 3‑step). The reduced number of units means lower overall power demand.
- Integration: AVASI is typically deployed independently and can be easily integrated with the runway lighting system. It is often controlled manually or via a basic ALCMS interface.
System Architecture & Control Logic
AVASI's control logic is the same fixed-optics principle as full VASI, scaled down to a single bar (or two reduced bars). Each light unit's lens/shutter assembly is tilted at commissioning so its red/white transition falls at a specific elevation; where more than one unit or bar is fitted, they're aimed a fraction of a degree apart so the ensemble straddles the glide path. That aim is mechanical and permanent — nothing in the circuit changes which colour a unit shows. All units on a bar share a constant current series circuit through their own isolating transformers, and the CCR (often a basic 3-step unit, sometimes only manually switched) sets one brightness level for the whole bar; with the reduced unit count, total loop power demand is correspondingly lower than a full VASI or PAPI installation. Fault detection is loop-based as with any series circuit — a voltage rise at constant current signals an open lamp or failed transformer — and because AVASI is often deployed as a standalone installation rather than through a full ALCMS, that fault may be reported to only a basic local panel or noted on next inspection rather than flagged in real time to the tower.
CCR (Basic/Manual) → Series Circuit Loop → Isolating Transformer → Light Unit (elevation fixed optically)
How a Single Bar Encodes Glide Angle
Above Glide Path
Line of sight looks into the upper part of the beam — bar reads all white.
On Glide Path
Sight line sits right at the sharp red/white split — the bar shows the transition itself, or one bar white and the other red in a two‑bar setup.
Below Glide Path
Line of sight drops into the lower part of the beam — bar reads all red.
AVASI trades the near/far bar comparison of a full VASI (and the four-unit precision of PAPI) for a single bar's own red/white transition — coarser guidance, but far fewer units, less power, and a footprint suited to small or temporary sites.
Physical Construction
Each AVASI bar is a wide, box-section housing in die-cast aluminium alloy or louvred galvanised steel, built the same way as a full VASI bar but deployed as a single downwind bar (or a simplified two-bar pair) rather than a full multi-bar system. The optics are split into an upper clear (white) glass and a lower red filter glass, precisely positioned so the beam transitions from white to red at the set glide-path angle, with a built-in levelling and pitch-adjustment mechanism used to aim the bar during commissioning. The housing mounts on a frangible mast set at a fixed, surveyed height beside the runway, engineered to shear away cleanly if struck. Cabling runs underground in conduit to an isolating transformer 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.
Technical Parameters
| Parameter | Typical Value |
|---|---|
| Light Source | LED array or 45W halogen lamp |
| Colour | White (upper beam) and Red (lower beam) per unit |
| Luminous Intensity | Up to 8,000 cd (white) and 4,000 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 Bars/Units | 1 bar (single unit) or 2 bars (simplified two‑bar) |
| 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 |
| Bar Synchronisation | Where a second bar is fitted, both bars share the same series step to keep the transition aligned |
| 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) | ≥ 6,000 cd on-axis per unit, up to 8,000 cd at full intensity |
| Main Beam Intensity (Red) | ≥ 3,000 cd on-axis per unit, up to 4,000 cd at full intensity |
| Transition Sharpness (Red/White) | ≤ 4 arc-minutes vertical transition band per bar |
| Vertical Beam Spread | Single bar (or reduced 2-bar) set at the 3° reference; coarser composite signal than full VASI |
| Horizontal Beam Spread | ± 5° to ± 10° either side of runway centreline plane |
| Isocandela Distribution | Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 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 bar |
Applicable Standards
ICAO Annex 14
Guidance for abbreviated visual slope indicators (AVASI)
FAA AC 150/5340-25
Visual Approach Slope Indicator (VASI) Systems – includes abbreviated (AVASI) configurations
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
Bar Setout
CivilSet out the single bar (or simplified two-bar arrangement) at a fixed lateral offset from the runway edge, set back from the threshold to place the on-slope indication at the correct height, tied to the runway centreline and threshold survey.
Frangible Pole Foundation
CivilInstall footings clear of the obstacle-limitation surface and any blast zone for the reduced-footprint array.
Duct & Cable Route to CCR
ElectricalRun underground cabling back to the constant current regulator.
Isolating Transformer Matching
ElectricalConfirm each unit's 45W–65W isolating transformer matches the series circuit's rated current step before connection.
Unit Aiming & Levelling
MechanicalIndividually aim and level each unit during commissioning to give the correct red/white split at the design glide angle.
Frangible Coupling Fixing
MechanicalTorque frangible mount couplings to the specified value, confirming the fitting shears as designed under lateral load.
Reduced-Footprint Clearance Check
DocumentationConfirm the single- or two-bar footprint sits within available clearance margins before energisation.
Pre-Energisation Sign-off
DocumentationRecord bar position, cable route, and torque values as-built before the site is closed.
Testing & Commissioning
Insulation Resistance (Megger) Test
Pre-EnergisationMegger-test the bar'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 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 the bar'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 the bar responds correctly at each step.
Glide Path Angle Verification
Final AcceptanceSet the bar's red/white transition angle with a calibrated aiming tool or theodolite, confirming the abbreviated single- or two-bar indication reads correctly given the reduced guidance compared to a full VASI wing bar.
Photometric Commissioning Test
Final AcceptanceMeasure red and white beam intensity, colour, and transition sharpness with a calibrated photometer against ICAO/FAA commissioning tolerances.
Frangibility & Mounting Verification
Pre-EnergisationConfirm the 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 alongside as-built position and aiming angle in the commissioning dossier.
Inspection & Maintenance
Beam Alignment Check
AnnualCalibrate the single or two-bar beam angle with precision tools; with fewer lights than full PAPI or VASI, alignment accuracy matters more per unit.
Photometric Intensity Check
AnnualVerify white and red beam intensity and the red/white transition against ICAO thresholds using a calibrated photometer.
Lens Cleaning
QuarterlyClean dust, rubber deposits, 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, since the coarser resolution of AVASI leaves less margin for a degraded 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 the 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 to ensure the single or two-bar array remains correctly positioned relative to the runway edge.
Common Field Issues
Limited Resolution
With fewer lights, AVASI provides a coarser indication than full PAPI or VASI. Pilots must be aware of the reduced resolution, particularly in marginal weather. This is a design trade‑off for cost and simplicity.
Beam Alignment
Accurate calibration of the single bar's beam angle is critical. Even a small error can shift the effective glide path significantly. Regular alignment checks using precision tools are essential.
Lens Contamination
Dust, rubber deposits, and de‑icing fluids can reduce light output and affect the colour transition. Routine cleaning and photometric testing are required to maintain the integrity of the indication.
Frangible Coupling Fatigue
AVASI units are mounted on frangible poles. Wind loading and thermal cycling can weaken couplings. Regular inspection ensures breakaway performance on impact.
Troubleshooting Guide
Bar Dark or Partially Dark
Entire Series Circuit Dark / CCR Will Not Regulate
CCR Trips on Overcurrent or Ground Fault
Coarse or Misleading Glide Path Indication
Reduced or Hazy Light Output
Unit Leaning, Loose, or Misaligned
Failure Modes & Root Causes
LED Module / Lamp Failure
Isolating Transformer Failure
Bar Unit Elevation Drift
Series Cable / Connector Insulation Breakdown
Lens Contamination or Erosion
Frangible Coupling Fatigue
Safety & Operational Notes
Series Circuit Isolation
Electrical SafetyThe AVASI bar runs on a constant-current series circuit that can carry several kV across the loop. De-energise and lock out the CCR, then verify zero energy at the fixture before opening a base can or handling cable connectors.
Airside Work Coordination
OperationalAny work on or near an active runway requires ATC/airside coordination and a NOTAM while a unit is dark or out of tolerance; because a single bar carries the whole glide-path cue, an out-of-service unit degrades the indication more than it would on a multi-bar VASI, 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
OperationalConfirm elevation setting and level on any adjusted unit against the design glide-path angle before closing out maintenance; with only one bar encoding the angle, a small aiming error is more consequential than in a multi-bar installation.
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 units 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 across the bar before closing out the work and cancelling the associated NOTAM.
Engineering & Expert Notes
Single-Bar Configuration Has No Independent Cross-Check
DesignUnlike a multi-bar VASI, a single-bar AVASI has no second reference to catch a slowly developing angle drift by comparison; rely on scheduled theodolite verification as the primary drift-detection method rather than pilot reports.
Lower Power Draw Doesn't Mean Lower Voltage-Drop Tolerance
ElectricalAVASI's reduced power consumption is often paired with lighter-gauge feeder cable; on longer runs to a remote threshold this increases voltage drop, so cable sizing still has to be recalculated for run length even though the connected load itself is small.
Temporary Installs Still Need a Rated Frangible Base
MechanicalShort-term or portable AVASI installs sometimes get a rigid or improvised mount because the fixture is expected to be temporary; if it sits within the obstacle-free area for any length of time it still needs a frangible mount rated to the same standard as a permanent unit.
The Colour Transition Band Is the Whole Signal
OpticalWith only one light unit carrying the indication, the sharpness of the red-to-white transition matters more than it would in a multi-bar system; check optical calibration for a crisp transition, not just correct colour at each extreme.
Battery or Solar Variants Need a Duty-Cycle Log
MaintenanceTemporary AVASI installs commonly run on batteries or solar panels; track discharge and recharge cycles as a standing maintenance item rather than waiting for a low-intensity complaint to reveal a power problem.
Each Heliport Repositioning Is Effectively a New Install
AlignmentBecause AVASI is frequently redeployed between heliports or temporary sites, calibration data from the previous location doesn't carry over; re-survey and re-aim at every repositioning rather than reusing prior settings.
Frequently Asked Questions
Short answers about the AVASI (Abbreviated Visual Approach Slope Indicator): what it is, how it works, typical specifications, standards, maintenance and common faults.
Q1What is an AVASI (Abbreviated Visual Approach Slope Indicator)?
The Abbreviated Visual Approach Slope Indicator (AVASI) is a simplified visual glide slope guidance system. Unlike the multi‑bar VASI or the four‑unit PAPI, AVASI typically consists of a single light bar or a simplified two‑bar configuration with fewer light units. It provides a basic but effective red/white indication to help pilots maintain a safe descent angle during final approach. AVASI is designed for smaller airfields, heliports, and temporary operations where a full‑scale system is not economically or logistically justified.
Q2What is the purpose of an AVASI (Abbreviated Visual Approach Slope Indicator)?
AVASI exists to bring basic glide slope guidance to airfields and temporary operations where the cost, power requirements, or physical footprint of a full VASI or PAPI installation can't be justified. By reducing the light units to a single bar or simplified two-bar layout, it keeps the essential red/white on-path indication pilots need while cutting the infrastructure and maintenance burden considerably.
Q3Where is an AVASI (Abbreviated Visual Approach Slope Indicator) used and installed?
AVASI is deployed on a variety of smaller and specialised landing sites: General aviation airports – with low traffic volumes and limited budgets. Heliports – where a compact system is needed for helicopter approaches. Remote and regional airstrips – with limited electrical infrastructure. Military forward operating bases – requiring rapid deployment and simplicity. Temporary or emergency runways – where a lightweight, portable system is advantageous. As a backup to PAPI or VASI – on larger runways for additional redundancy.
Q4How does an AVASI (Abbreviated Visual Approach Slope Indicator) work?
AVASI operates on the same fundamental optical principle as VASI and PAPI, but with a simplified configuration: Configuration: AVASI typically uses a single bar of lights (or two bars in some configurations) installed on the left side of the runway or helipad. The bar contains one or more light units that project a beam with a distinct red/white transition. Colour Indication: The pilot sees a single bar that changes colour based on the viewing angle.
Q5What are the typical technical parameters of an AVASI (Abbreviated Visual Approach Slope Indicator)?
Typical values are — Light Source: LED array or 45W halogen lamp; Colour: White (upper beam) and Red (lower beam) per unit; Luminous Intensity: Up to 8,000 cd (white) and 4,000 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 Bars/Units: 1 bar (single unit) or 2 bars (simplified two‑bar); Mounting Type: Elevated (frangible poles) – typically 10–20 m from runway edge; Isolating Transformer: 45W – 65W (6.6A series circuit) per unit.
Q6What are the electrical requirements for an AVASI (Abbreviated Visual Approach Slope 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; Bar Synchronisation: Where a second bar is fitted, both bars share the same series step to keep the transition aligned; 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 AVASI (Abbreviated Visual Approach Slope Indicator)?
Typical requirements are — Main Beam Intensity (White): ≥ 6,000 cd on-axis per unit, up to 8,000 cd at full intensity; Main Beam Intensity (Red): ≥ 3,000 cd on-axis per unit, up to 4,000 cd at full intensity; Transition Sharpness (Red/White): ≤ 4 arc-minutes vertical transition band per bar; Vertical Beam Spread: Single bar (or reduced 2-bar) set at the 3° reference; coarser composite signal than full VASI; Horizontal Beam Spread: ± 5° to ± 10° either side of runway centreline plane; Isocandela Distribution: Per ICAO Annex 14 Attachment A / FAA AC 150/5345-46 figures; Chromaticity (White): Within ICAO Annex 14 white boundary (CIE coordinates).
Q8Which standards apply to an AVASI (Abbreviated Visual Approach Slope Indicator)?
The main references are ICAO Annex 14 — Guidance for abbreviated visual slope indicators (AVASI); FAA AC 150/5340-25 — Visual Approach Slope Indicator (VASI) Systems – includes abbreviated (AVASI) configurations; 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 AVASI (Abbreviated Visual Approach Slope 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 AVASI (Abbreviated Visual Approach Slope Indicator) faults?
Common symptoms covered are: Bar Dark or Partially Dark; Entire Series Circuit Dark / CCR Will Not Regulate; CCR Trips on Overcurrent or Ground Fault; Coarse or Misleading Glide Path Indication; Reduced or Hazy Light Output; Unit Leaning, Loose, or Misaligned. For example, for "Bar Dark or Partially Dark": Likely Cause: Failed LED module / lamp in one or more units, or an open isolating transformer feeding the bar. Diagnostic Steps: Confirm series loop continuity through the 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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