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Ground‑Based Augmentation System (GBAS)

A satellite‑based navigation system that provides differential corrections and integrity monitoring for Global Positioning System (GPS) signals, enabling precision approaches (CAT I, II, III) with lateral and vertical guidance. GBAS enhances GPS accuracy, integrity, continuity, and availability, making it a vital component of modern air navigation infrastructure.

GBAS

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Overview

What Is It?

The Ground‑Based Augmentation System (GBAS) is a ground‑based system that augments the Global Positioning System (GPS) to provide enhanced navigation performance for aircraft. A GBAS installation typically consists of:

  • Reference Receivers: A network of GPS reference receivers located at surveyed positions around the airport. These receivers measure GPS signal errors (ionospheric, tropospheric, satellite clock, and ephemeris errors).
  • Central Processing Station: A ground computer that processes the reference receiver data to generate differential corrections and integrity parameters.
  • VHF Data Broadcast (VDB): A VHF transmitter that broadcasts the correction and integrity data to aircraft within the coverage area (typically about 20 nautical miles).

Aircraft equipped with a GBAS receiver use the broadcast data to compute a highly accurate, integrity‑monitored position, enabling precision approaches (CAT I, II, III) with lateral and vertical guidance. GBAS is increasingly positioned as a longer-term successor to the Instrument Landing System (ILS), with a growing number of installations at major airports worldwide, offering multiple approach paths and greater flexibility than a fixed ILS beam can provide.

Purpose

Purpose & Function

GBAS exists to deliver the same category of precision approach guidance as ILS, lateral and vertical, down to CAT III minima, from a single ground installation that can support every runway and multiple approach paths at an airport rather than requiring a dedicated localizer and glide slope pair for each runway end. Its purpose is achieved by applying the same correction-and-integrity principle as wide-area SBAS, but concentrated locally around one airport using its own reference receivers and VHF broadcast, which gives it tighter local accuracy and lower latency than a wide-area system could provide for approach-critical guidance. That local scope is also what lets GBAS support curved or offset approach paths that a fixed ILS beam geometry cannot offer, giving airports more flexibility in how aircraft are guided to each runway.

Application

Where Is It Used?

GBAS is used for a wide range of applications across all phases of flight:

  • Precision Approaches: GBAS supports CAT I, II, and III precision approaches, providing lateral and vertical guidance to the runway. It allows for multiple approach paths (e.g., curved approaches) and can serve all runway ends from a single installation.
  • Terminal Area Navigation: GBAS provides accurate positioning for departure and arrival procedures, including RNAV/RNP operations.
  • En‑route Navigation: GBAS corrections can improve en‑route GPS accuracy, though coverage is typically limited to the airport vicinity.
  • Surface Navigation: GBAS can provide accurate positioning for airport surface movement guidance, including A‑SMGCS applications.
  • Remote and Offshore Operations: GBAS is particularly valuable in areas where ILS installations are impractical or expensive, such as offshore heliports or remote airstrips.
Placement

Installation & Location

Reference receivers are distributed around the airfield on surveyed monuments, spaced apart and sited with a clear view of the sky to minimise multipath and ensure the array as a whole sees consistent satellite geometry; their antennas are mounted on short masts or building rooftops away from large reflective surfaces. The central processing station and VHF data broadcast (VDB) transmitter are housed together in an equipment building, with the VDB antenna mounted on a mast sited to give unobstructed line of sight over the runway and approach/departure paths it serves. Cabling from each reference receiver back to the processing station is run in duct, and the facility is connected to airport standby power in the same way as other critical navigation aids, given its role in supporting precision approaches.

Function

How Does It Work?

The GBAS system operates through a multi‑step process:

  • Reference Measurements: The reference receivers track all visible GPS satellites and measure pseudorange and carrier‑phase observables. These measurements are compared with the known positions of the receivers to calculate ranging errors.
  • Differential Corrections: The central processing station computes differential corrections for each satellite in view. These corrections include ionospheric delay, tropospheric delay, satellite clock errors, and ephemeris errors.
  • Integrity Monitoring: The system continuously monitors the health of the GPS constellation and the ground equipment. It generates integrity parameters — a ground accuracy designator (σ_pr_gnd) and per-receiver B-values derived by cross-checking the redundant reference receivers against each other — that allow the aircraft receiver to assess the reliability of the corrections and detect a faulty measurement before it propagates into the position solution.
  • Data Broadcast: The VDB transmitter broadcasts the corrections, integrity data, and approach path information (waypoints, glide path angle, etc.) on a VHF frequency (108.025–117.950 MHz, in 25 kHz channel steps, paired with the approach procedure).
  • Aircraft Processing: The aircraft's GBAS receiver uses the broadcast data to correct its GPS measurements, compute a precise position, and generate lateral and vertical deviation signals for the cockpit display (similar to ILS).
Architecture

System Architecture & Control Logic

A GBAS ground facility's control logic centres on redundant reference receivers feeding a central integrity processor. Multiple GNSS reference receivers, sited around the airfield, each independently compute pseudorange corrections; the processor cross-checks these against one another to detect a faulty receiver or a satellite anomaly before it can propagate to an aircraft. Corrections, approach path definitions and integrity parameters are packaged and broadcast continuously over the VHF Data Broadcast (VDB) link at the required message rate, so aircraft are never operating on stale data. If the processor cannot certify the correction data within the required integrity bounds, it withholds or flags the broadcast rather than transmit an unverified correction, with status reported to the ATC and maintenance monitoring system.

Reference Receivers → Integrity Processor → VDB Broadcast → Aircraft GBAS Receiver

GNSS REFERENCE RECEIVERS Multiple, redundant — independently track satellites INTEGRITY PROCESSOR Cross-checks receivers, computes corrections CORRECTION & INTEGRITY DATA PACKAGING Approach path plus integrity bounds per satellite VDB TRANSMITTER Broadcasts continuously at required message rate AIRCRAFT GBAS RECEIVER Applies corrections to onboard GNSS position INTEGRITY-GATED BROADCAST Unverified corrections are withheld or flagged rather than broadcast to aircraft CROSS-CHECK Processor continuously cross-checks receiver data; failed integrity check withholds the broadcast
Architecture

Signal & Data Flow

Space Segment
GPS Satellites
L1/L2/L5 ranging signals broadcast to all visible receivers
→
Ground Segment
Reference Receivers
Track satellites, measure pseudorange & carrier‑phase, derive ranging errors
→
Processing
Central Facility
Computes differential corrections + integrity monitoring (σ_pr_gnd, B-values)
→
Broadcast
VDB Transmitter
Sends corrections, integrity data & approach path on VHF (108.025–117.950 MHz)
→
Aircraft
GBAS Receiver
Corrects GPS fix, outputs lateral/vertical deviation to cockpit display
Construction

Physical Construction

The GBAS ground facility comprises a small number of precisely surveyed GPS reference receiver antennas mounted on short masts around the airfield, each connected via shielded, lightning-protected cabling back to a central processing cabinet housing the redundant reference receivers, integrity-monitoring processors, and VHF Data Broadcast (VDB) transmitter. The VDB transmit antenna is mounted at an elevated, unobstructed location to achieve its rated coverage radius, with the equipment cabinet built as a weatherproof, temperature-controlled enclosure similar to other NAVAID ground stations. Internally, the reference receivers and VDB transmitter chains are duplicated for hot-standby redundancy, with automatic switchover logic and continuous integrity monitoring built into the processing electronics to meet the stringent CAT I/II/III integrity and continuity requirements. Surge protection and isolation are fitted at every antenna feed and external interface given the facility's exposure to lightning and RF interference, and the cabinet's power section connects to mains, UPS, and generator backup for uninterrupted operation.

Specification

Technical Parameters

ParameterTypical Value
Frequency (GPS)L1 (1575.42 MHz), L2 (1227.60 MHz), L5 (1176.45 MHz)
VDB Frequency Range108.025 MHz – 117.950 MHz, 25 kHz channel spacing (paired with approach procedure)
VDB ModulationD8PSK (Data‑8 Phase Shift Keying)
VDB Data Rate31.5 kbps (10.5 kbaud × 3 bits/symbol, D8PSK)
VDB CoverageTypically up to 20 NM (37 km) radius
Approach Accuracy95% position error: Lateral ≤ 16 m, Vertical ≤ 4 m (CAT I / GAST-C, per ICAO Annex 10)
IntegrityIntegrity risk < 10⁻⁷ per approach (CAT I)
Continuity> 99.99%
Availability> 99.9% (CAT I)
CAT CapabilityCAT I, II, III (depending on installation and certification)
Standby SystemDual redundant (hot standby) for critical components
Power SupplyMains with UPS and generator backup
Protection ClassIP65 / IP67 (weatherproof for outdoor equipment)
Power Supply

Electrical Requirements

RequirementTypical Value
Primary SupplyMains AC feed to the ground facility, backed by UPS and standby generator
ChangeoverAutomatic transfer between mains, UPS, and generator with no interruption to VDB transmission or reference receiver operation
CablingDedicated feeder from the airfield distribution point to the ground facility, sized to the equipment's rated load
Circuit ProtectionDedicated circuit breaker/isolator at the facility distribution board
Surge ProtectionSPDs fitted at the power, antenna, and reference-receiver cable entries
Insulation Resistance≥ 50 MΩ (megger test, cable-to-ground, at commissioning)
Earthing/GroundingFacility, mast, and reference receiver antennas bonded to the airfield earth grid
Fault ProtectionContinuous self-monitoring with alarm reporting to the remote status panel on power or subsystem fault
Compliance

Applicable Standards

ICAO Annex 10

GBAS frequency, modulation, and performance requirements

FAA Order 6884.1

Siting Criteria for Ground Based Augmentation System (GBAS) Ground Facility

EUROCAE ED-114

GBAS ground station performance and monitoring standards

RTCA DO-253

Minimum Operational Performance Standards (MOPS) for GBAS airborne receiver equipment

Prerequisites

Installation Requirements

Reference Receiver Monument Survey
Site

Establish surveyed monument positions distributed around the airfield, spaced apart with a clear view of the sky to minimise multipath and ensure consistent satellite geometry across the array.

Reference Antenna Mast/Rooftop Mounting
Civil

Mount each reference antenna on a short mast or building rooftop, away from large reflective surfaces.

VDB Antenna Mast Siting
Civil

Site the VDB antenna mast for unobstructed line of sight over the runway and the approach/departure paths it serves.

Duct & Cable Route to Processing Station
Electrical

Run cabling from each reference receiver back to the central processing station in duct.

Standby Power Connection
Electrical

Connect the facility to airport standby power, matching the arrangement used for other critical navigation aids.

Equipment Building Fit-Out
Mechanical

Install the central processing station and VDB transmitter together within the equipment building.

Satellite Geometry/Multipath Check
Documentation

Verify the reference receiver array as a whole sees consistent satellite geometry before commissioning.

Pre-Energisation Sign-off
Documentation

Record monument survey coordinates, mast positions, and cable routes as-built before the facility is closed up.

Verification

Testing & Commissioning

Reference Receiver Position Survey Verification
Pre-Energisation

Confirm each reference antenna's surveyed position meets the accuracy required for GBAS correction data before the receivers are brought into service.

VDB Frequency & Power Output Test
Commissioning

Verify the VHF Data Broadcast transmits on its assigned frequency at the correct power and modulation (D8PSK) to achieve rated coverage.

Integrity Monitoring Function Test
Commissioning

Inject simulated fault conditions and confirm the integrity-monitoring processors detect and flag them within the required time to meet CAT I/II/III integrity requirements.

Redundancy Switchover Test
Commissioning

Simulate a fault on the primary reference receiver or VDB transmitter chain and confirm automatic switchover to the hot-standby unit.

Data Broadcast Message Verification
Commissioning

Decode the broadcast correction and approach path data with a test receiver to confirm message content matches the published procedure.

Approach Accuracy Flight Check
Final Acceptance

Verify lateral and vertical guidance accuracy against the certified tolerance using a calibrated flight-check aircraft before operational release.

Documentation & As-Built Sign-off
Final Acceptance

Record survey data, VDB test results, integrity monitoring performance, and flight-check results in the commissioning dossier.

Upkeep

Inspection & Maintenance

GPS Signal Environment Survey
Annual

Survey the site for new sources of GPS interference or jamming that could affect signal integrity.

VDB Coverage Check
Annual

Verify VHF data broadcast coverage across the approach area, checking for multipath-affected zones.

Reference Receiver Calibration Check
Annual

Verify reference receiver calibration against a known-position benchmark.

Integrity Monitoring Function Test
Semi-annual

Test integrity monitoring functions to confirm faults would be correctly detected and flagged.

Field Notes

Common Field Issues

GPS Signal Interference and Jamming

GBAS is dependent on GPS signals, which are vulnerable to interference (intentional or unintentional) and ionospheric scintillation. Sites must be carefully surveyed for potential interference sources, and mitigation measures (e.g., antenna filtering, site shielding) are essential.

VDB Coverage and Multipath

The VHF data broadcast is line‑of‑sight and can be affected by terrain, buildings, and aircraft shadowing. Proper antenna placement and power selection are critical to ensure coverage over the entire approach path.

Reference Receiver Calibration

The reference receivers must be precisely surveyed and regularly calibrated to maintain system accuracy. Any shift in the reference receiver position can degrade the differential corrections.

Integrity Monitoring Failures

The integrity monitoring subsystem must reliably detect and alert on any satellite or ground system failures. False alarms can reduce system availability, while missed detections can compromise safety. Regular testing and validation are required.

Diagnostics

Troubleshooting Guide

Loss of GPS Signal Tracking or Sudden Availability Drop
Likely Cause
GPS interference or jamming (intentional or unintentional), or ionospheric scintillation affecting satellite signal reception at the reference receivers.
Diagnostic Steps
Review the reference receiver logs for satellite dropouts and carrier-to-noise ratio trends; check for known interference sources or scintillation activity reports for the region; confirm all reference receivers are affected equally versus a single-unit fault.
Corrective Action
Coordinate with spectrum management if interference is confirmed; if scintillation-related, this may be a transient condition — monitor and report per procedure rather than replacing hardware prematurely.
VDB Coverage Gaps on the Approach Path
Likely Cause
Terrain, buildings, or aircraft shadowing the line-of-sight VHF data broadcast, or a VDB transmitter power/antenna fault.
Diagnostic Steps
Check VDB transmitter power output and antenna VSWR against baseline; review coverage complaints against known obstructions on the approach; confirm broadcast content and burst timing are correct at the antenna.
Corrective Action
Adjust antenna placement or power if within design margins, clear or mitigate new obstructions where possible, or repair the transmitter/antenna if a hardware fault is confirmed.
Differential Corrections Appear Degraded
Likely Cause
A reference receiver has shifted from its precisely surveyed position, or its calibration has drifted, corrupting the pseudorange corrections it broadcasts.
Diagnostic Steps
Compare each reference receiver's reported position against its surveyed benchmark; check for recent site work, settlement, or physical disturbance near the antenna; review correction residuals for a single outlier receiver.
Corrective Action
Re-survey and recalibrate the affected reference receiver, or physically re-secure its antenna mount if displacement is confirmed; validate corrected output before returning the receiver to the active set.
Integrity Monitor Triggers False Alarms or Fails to Alert
Likely Cause
Miscalibrated integrity thresholds, a faulty monitoring subsystem, or a genuine but undetected satellite/ground fault depending on which failure mode is occurring.
Diagnostic Steps
Review the integrity monitor's alarm history against known system events; run the required periodic integrity test/validation procedure; check monitor firmware/configuration against the latest approved baseline.
Corrective Action
Recalibrate or replace the integrity monitoring subsystem if it is generating false alarms or missing genuine faults, and do not return the system to service for CAT-level operations until validation passes.
Reliability

Failure Modes & Root Causes

GPS Interference or Ionospheric Scintillation
High Severity
Root Cause
GPS interference or jamming, intentional or unintentional, or ionospheric scintillation affecting satellite signal reception at the reference receivers.
Effect
Loss of GPS signal tracking or a sudden availability drop across the reference network.
Detection Method
Review of reference receiver logs for satellite dropouts and carrier-to-noise trends, and a check for known interference or scintillation activity in the region.
VDB Coverage Obstruction or Transmitter Fault
Medium Severity
Root Cause
Terrain, buildings, or aircraft shadowing the line-of-sight VHF data broadcast, or a VDB transmitter power/antenna fault.
Effect
VDB coverage gaps on the approach path that can affect approaches at specific segments.
Detection Method
VDB transmitter power and antenna VSWR checks against baseline, and a review of coverage complaints against known obstructions.
Reference Receiver Position Drift
High Severity
Root Cause
A reference receiver shifting from its precisely surveyed position, or its calibration drifting, corrupting the pseudorange corrections it broadcasts.
Effect
Differential corrections appear degraded, reducing the accuracy of the guidance provided to aircraft.
Detection Method
Comparison of each reference receiver's reported position against its surveyed benchmark, and a check for recent site work or physical disturbance near the antenna.
Integrity Monitor Miscalibration
High Severity
Root Cause
Miscalibrated integrity thresholds, a faulty monitoring subsystem, or an undetected satellite/ground fault.
Effect
The integrity monitor triggers false alarms or, more seriously, fails to alert on a genuine fault.
Detection Method
Review of the integrity monitor's alarm history against known system events, and the required periodic integrity test/validation procedure.
Precautions

Safety & Operational Notes

RF Exposure Near the VDB Antenna
Personnel Safety

Follow the facility's RF safety procedure and any posted exclusion distance when working near the VHF Data Broadcast transmit antenna, and confirm the transmitter is placed in maintenance/standby mode before working at or above the antenna mast.

Equipment Cabinet Isolation
Electrical Safety

De-energise and lock out the reference receiver or VDB transmitter chain before working inside the processing cabinet, and verify zero energy before disturbing internal connections.

Reference Receiver Antenna Survey Integrity
Compliance

Do not move, re-mount, or replace a reference receiver antenna without re-surveying its position; the system's integrity depends on each antenna's surveyed location being accurate to a high tolerance.

Lightning Exposure at Mast-Mounted Antennas
Electrical Safety

Verify surge protection is in place and intact at every antenna feed before working on cabling, given the facility's exposure to lightning, and avoid antenna or mast work during an active electrical storm.

NOTAM for Service Interruption
Operational

Issue a NOTAM before taking the GBAS facility out of service or below integrity tolerance for maintenance, since aircraft rely on it for precision approach guidance.

Verify Integrity Monitoring Before Return to Service
Compliance

Confirm the integrity processor correctly detects a faulty receiver or out-of-tolerance correction and withholds the broadcast before returning the facility to service after maintenance affecting the reference receivers or processor.

PPE & Grounding
Personnel Safety

Use appropriate PPE and confirm the facility, mast, and reference receiver antennas remain bonded to the airfield earth grid before closing out cabling work.

Restore to Compliant State
Compliance

Do not leave the facility broadcasting corrections outside CAT I/II/III integrity and continuity requirements after maintenance; verify monitored parameters before closing out the work and cancelling the associated NOTAM.

Field Insight

Engineering & Expert Notes

Multipath Faults Look Like Receiver Faults
Diagnostics

An intermittent integrity flag that clears on receiver reset is frequently a multipath issue from a new reflective surface near the reference receivers, such as a parked vehicle or vehicle mast, rather than an actual receiver fault. Check the site line-of-sight environment before swapping hardware.

Reference Receiver Antenna Survey Drifts Over Time
Precision

Ground settlement or minor structural movement of a reference receiver antenna mount over years of service can introduce a small but real position error into the correction message. Periodic re-survey of antenna coordinates belongs in the maintenance cycle, not just at commissioning.

VDB Coverage Complaints Often Trace to Siting, Not Power
Troubleshooting

A reported VHF data broadcast coverage gap along a particular approach is more often caused by terrain or structure shadowing at that specific bearing than by transmitter power. Check the site's coverage prediction against the reported bearing before adjusting transmit power.

Trend Integrity Alarms, Don't Just Clear Them
Process

A GBAS integrity alarm that self-clears on the next cycle can still be an early indicator of a satellite geometry or ionospheric issue recurring at a predictable time of day. Log alarm timing and conditions rather than treating each clear as resolved.

Ionospheric Activity Drives Seasonal Alarm Patterns
Environment

Integrity alarm rates for GBAS installations tend to rise during periods of high ionospheric disturbance. When troubleshooting a spike in alarms, check regional space-weather activity before assuming a local equipment fault.

Keep Redundant Receiver Data Independently Logged
Design

Where multiple reference receivers feed a single processing path, log each receiver's raw data independently rather than only the combined output. This makes it possible to isolate which specific receiver degraded first when a fault eventually shows up in the combined correction.

Quick Answers

Frequently Asked Questions

Short answers about the Ground-Based Augmentation System (GBAS): what it is, how it works, typical specifications, standards, maintenance and common faults.

Q1What is a Ground-Based Augmentation System (GBAS)?

The Ground‑Based Augmentation System (GBAS) is a ground‑based system that augments the Global Positioning System (GPS) to provide enhanced navigation performance for aircraft. A GBAS installation typically consists of: Reference Receivers: A network of GPS reference receivers located at surveyed positions around the airport. These receivers measure GPS signal errors (ionospheric, tropospheric, satellite clock, and ephemeris errors). Central Processing Station: A ground computer that processes the reference receiver data to generate differential corrections and integrity parameters.

Q2What is the purpose of a Ground-Based Augmentation System (GBAS)?

GBAS exists to deliver the same category of precision approach guidance as ILS, lateral and vertical, down to CAT III minima, from a single ground installation that can support every runway and multiple approach paths at an airport rather than requiring a dedicated localizer and glide slope pair for each runway end.

Q3Where is a Ground-Based Augmentation System (GBAS) used and installed?

GBAS is used for a wide range of applications across all phases of flight: Precision Approaches: GBAS supports CAT I, II, and III precision approaches, providing lateral and vertical guidance to the runway. It allows for multiple approach paths (e.g., curved approaches) and can serve all runway ends from a single installation. Terminal Area Navigation: GBAS provides accurate positioning for departure and arrival procedures, including RNAV/RNP operations. En‑route Navigation: GBAS corrections can improve en‑route GPS accuracy, though coverage is typically limited to the airport vicinity.

Q4How does a Ground-Based Augmentation System (GBAS) work?

The GBAS system operates through a multi‑step process: Reference Measurements: The reference receivers track all visible GPS satellites and measure pseudorange and carrier‑phase observables. These measurements are compared with the known positions of the receivers to calculate ranging errors. Differential Corrections: The central processing station computes differential corrections for each satellite in view. These corrections include ionospheric delay, tropospheric delay, satellite clock errors, and ephemeris errors. Integrity Monitoring: The system continuously monitors the health of the GPS constellation and the ground equipment.

Q5What are the typical technical parameters of a Ground-Based Augmentation System (GBAS)?

Typical values are — Frequency (GPS): L1 (1575.42 MHz), L2 (1227.60 MHz), L5 (1176.45 MHz); VDB Frequency Range: 108.025 MHz – 117.950 MHz, 25 kHz channel spacing (paired with approach procedure); VDB Modulation: D8PSK (Data‑8 Phase Shift Keying); VDB Data Rate: 31.5 kbps (10.5 kbaud × 3 bits/symbol, D8PSK); VDB Coverage: Typically up to 20 NM (37 km) radius; Approach Accuracy: 95% position error: Lateral ≤ 16 m, Vertical ≤ 4 m (CAT I / GAST-C, per ICAO Annex 10); Integrity: Integrity risk < 10⁻⁷ per approach (CAT I); Continuity: > 99.99%; Availability: > 99.9% (CAT I); CAT Capability: CAT I, II, III (depending on installation and certification).

Q6What are the electrical requirements for a Ground-Based Augmentation System (GBAS)?

Typical requirements are — Primary Supply: Mains AC feed to the ground facility, backed by UPS and standby generator; Changeover: Automatic transfer between mains, UPS, and generator with no interruption to VDB transmission or reference receiver operation; Cabling: Dedicated feeder from the airfield distribution point to the ground facility, sized to the equipment's rated load; Circuit Protection: Dedicated circuit breaker/isolator at the facility distribution board; Surge Protection: SPDs fitted at the power, antenna, and reference-receiver cable entries; Insulation Resistance: ≥ 50 MΩ (megger test, cable-to-ground, at commissioning).

Q7Which standards apply to a Ground-Based Augmentation System (GBAS)?

The main references are ICAO Annex 10 — GBAS frequency, modulation, and performance requirements; FAA Order 6884.1 — Siting Criteria for Ground Based Augmentation System (GBAS) Ground Facility; EUROCAE ED-114 — GBAS ground station performance and monitoring standards; RTCA DO-253 — Minimum Operational Performance Standards (MOPS) for GBAS airborne receiver equipment. Always verify the current edition and your aerodrome's approved requirements.

Q8How often should a Ground-Based Augmentation System (GBAS) be inspected and maintained?

Typical maintenance tasks and intervals are: GPS Signal Environment Survey (annual); VDB Coverage Check (annual); Reference Receiver Calibration Check (annual); Integrity Monitoring Function Test (semi-annual). Your airport's approved maintenance programme takes precedence.

Q9How do I troubleshoot common Ground-Based Augmentation System (GBAS) faults?

Common symptoms covered are: Loss of GPS Signal Tracking or Sudden Availability Drop; VDB Coverage Gaps on the Approach Path; Differential Corrections Appear Degraded; Integrity Monitor Triggers False Alarms or Fails to Alert. For example, for "Loss of GPS Signal Tracking or Sudden Availability Drop": Likely Cause: GPS interference or jamming (intentional or unintentional), or ionospheric scintillation affecting satellite signal reception at the reference receivers. Diagnostic Steps: Review the reference receiver logs for satellite dropouts and carrier-to-noise ratio trends; check for known interference sources or scintillation activity reports for the region; confirm all reference receivers are affected equally versus a single-unit fault. Corrective Action: Coordinate with spectrum management if interference is confirmed; if scintillation-related, this may be a transient condition — monitor and report per procedure rather than replacing hardware prematurely.

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