Parameter Tolerance Profile Measurement to be made Transmitter tobe checked
PowerDensity along runway Greater than 5 dB above the value in ICAO Annex 10 Volume 1 paragraph 3.11.4.10.1 for one degreeor 9 dB for 2 degree or larger beam width antennas at 2.5 m (8 ft) above the runway surface, at theMLS datum point, or at the farthest point of therunway centre line which is in line of sight of the azimuth antenna Ground spot check Direct read off groundequipment CommissioningBothRoutineBoth
Multipath relativepowerdensity Within theMLS azimuth coverage at60 m (200 ft)or more abovethreshold The duration of a reflected scanning beam signal whose power density is higher than 4 dB belowthe azimuth guidance scanning beam signal power density shall be shorter than one second Level Slice on centreline from 20NM at 0.3 theta to intersect a Fly down from 7 NM on azimuth and elevation to ARD Plot or analysis CommissioningOne TXBiennial OneTX
Multipath relativepowerdensityWithin theMLS azimuth proportional guidancesector, below 60 m (200 ft)above threshold The power density of any reflected approachazimuth guidance scanning beam signal shall be less than 10 dB above the power density of the approach azimuth guidance scanning beam signal Ground check on centreline between ARD and along runway From plot CommissioningOne TXBiennial OneTX
Parameter Tolerance Profile Measurement to be made Transmitter tobe checked
Monitor Verification Ground check Spot check CommissioningBothRoutineBoth
Identification Ground check Spot check CommissioningBothRoutineBoth
Parameter Tolerance Profile Measurement to be made Transmitter tobe checked
Accuracy at ApproachReference Datum Mean Glidepath Error (MGE) ± 0.3mNote: The ICAO Standard in Annex 10 Volume 1 paragraph 3.11.5.3.5.1 is for ground equipmentcontribution. Checks in the far field would include the effects of multipath. Due to the similarity withILS it is assumed that this requirement includes multipath effectsMGE standard needs to be clarified by ICAO Static antenna at the ARD Direct reading CommissioningBothRoutineBoth
Parameter Tolerance Profile Measurement to be made Transmitter tobe checked
AngleAccuracyEdge ofcoverage to ARD PFE and PFN PFE ± 0.6m at ARDPFN ± 0.4m at ARDThe PFE limit and PFN limit, expressed in angular terms at 37 km (20 NM) from the runway threshold on the minimum glide path, shall degrade linearly to 0.2 degreesCMNCMN ± 0.3m at ARDThe CMN limit, expressed in angular terms at 37 km (20 NM) from the runway threshold on the minimum glide path, shall degrade linearly to 0.1 degreesFly up deflection shall exist at all angles betweenlower limit of coverage and 2.2 degrees, thereafterAnnex 10 Volume 1 Standard applies between 2.2 degrees and theta This is a two-part testLevel Slice on centreline from 20NM at 0.3 theta to 1.75 theta ofthe elevationFly down from 7 NM on azimuth and elevation to ARD Plot from 0.3 theta to 1.75theta, and;Plot from 7NM to ARD CommissioningBothRoutineBoth
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