FLIGHT INSPECTION
We perform the following types of
Flight Inspection:
Nav Aids:
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Instrument Landing System (ILS) Category I, II and III
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VHF Omni directional Radio Range (VOR)
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Distance Measuring Equipment (DME)
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Non-Directional Beacon (NDB)
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ILS Markers and FAN Markers
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GBAS Landing System (GLS)
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Transponder Landing Systems (TLS)
Airfield Ground Lighting and Visual Glideslope Indicator:
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Visual Approach Slope Indicator (VASI)
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Precision Approach Path Indicator (PAPI)
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Airfield Lighting Systems (ALS)
Procedures Validation:
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GPS Precision and Non Precision Approaches
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Area Navigation Procedures RNAV
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Instrument Approach Procedures RNP, including LNAV/VNAV, LP and LPV based on GNSS with SBAS/WAAS, GBAS or DME/DME
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Instrument Flight Procedures validation (SID, STAR, SIAP)
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GNSS with SBAS/WAAS evaluation
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Ground Based Augmentation System (GBAS/LAAS)
VHF / UHF:
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VHF Communications
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VHF Direction finding (VDF)
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UHF Communication
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UHF Direction Finding (UDF)
Radar:
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Surveillance Radar Element (SRE)
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Precision Approach Radar (PAR)
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Primary Surveillance Radar (PSR)
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Secondary Surveillance Radar (SSR/ MSSR) with dedicated Flight Inspection Transponder Mode A, C and S
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Multilateration Systems (MLAT) / Wide Area Multilateration (WAM)
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Precision Runway Monitor System (PRM)
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Automatic Dependent Surveillance Broadcast (ADS-B)
Military:
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Military facilities Tactical Air Navigation (TACAN)
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Scan DME/TACAN with up to 10 facilities
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Oscilloscope/Digital Spectrum Analyzer for DME/TACAN
Worldwide Flight Inspection
Our Automatic Flight Inspection System (AD-AFIS) is manufactured by Aerodata AG, the world's leader in the manufacturing of highly sophisticated flight inspection systems.
Key features and advantages:
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Meets the requirements of UK CAA CAP 670, ICAO Doc 8071, Annex 10, FAA Order 8200.1D, and the NATO STANAG.
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AD-AFIS coupled with Flight Director and Autopilot for precision guidance with minimum deviation from the set trajectory (ICAO Doc 8071 Ch 4 §4.3.17, §4.3.47).
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AD-AFIS to minimise human error factors.
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Independent flight inspection antennas (ICAO Doc 8071 Ch 4 §4.3.89, Attach A to Ch 1 §3.7 [c,e]).
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Measurement accuracy to within <10cm Phase Differential Global Positioning System (PDGPS).
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Dual set of receivers simultaneously provide redundancy and reduce errors (ICAO Doc 8071 Ch 4 §4.3.90, Attach A to Ch 1 §4.1).
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Independent onboard radio station (ICAO Doc 8071 Attach A to Ch 1 §4.4).
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Primary flight displays in-flight inspection console for full situational awareness of the operator.
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Instant post-processing by the time stamps synchronization for maximum accuracy.
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Automatically generated reports, to prevent operator errors.
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Certified by the EASA STCs.