Source: https://guides.developer.iata.org/docs/download-the-latest-standards

FuelDistribution

A procedure that defines the consecutive steps for fueling an aircraft and the quantities to distribute to each of the corresponding tanks at each step in case a fuel split calculation is required to be performed by the departure control system.

Properties

Name Description Type Required Generic Enum Ignore
aircraftGroupConfiguration A Specific Configuration of an Aircraft Group. AircraftGroupConfiguration true false
conditionName Further specification of the fuel distribution name, e.g. CASE A, CASE B, etc. string false false
fuelDensityMeasure Fuel density used in case fuel data is defined as weight/index, expressed as weight for a given fuel density volume unit. WeightMeasure false false
fuelDensityVolumeUnitCode Liquid volume unit used for fuel density calculation. When missing the standard aircraft fuel density volume unit is used. LiquidVolumeUnitCode false false
fuelDistributionName Specific name for the fuel distribution. string false false
fuelDistributionStep A step in the fueling of an aircraft describing the quantities to distribute to each of the corresponding tanks. array true FuelDistributionStep --- false
maximumVolumeMeasure Maximum fuel volume to distribute. LiquidVolumeMeasure false false
maximumWeightMeasure Maximum fuel weight to distribute. WeightMeasure false false
minimumVolumeMeasure Minimum fuel volume to distribute. LiquidVolumeMeasure false false
minimumWeightMeasure Minimum fuel weight to distribute. WeightMeasure false false
remark An additional, supplementary information about the document or service. array false Remark --- false

Referenced By

AircraftGroupConfiguration
FuelDistributionStep
Remark
{
  "aircraftGroupConfiguration" : {
    "aircraftGroup" : { },
    "asymmetricalLoadLimitationTable" : [ { } ],
    "balanceOutputRequirement" : [ { } ],
    "cabinComponent" : [ { } ],
    "cabinLayout" : { },
    "cargoHeatingDevice" : [ { } ],
    "cargoVentilationDevice" : [ { } ],
    "centerOfGravityLimitTable" : [ { } ],
    "combinedLoadLimitationTable" : [ { } ],
    "crewDistribution" : [ { } ],
    "cumulativeLoadLimitationTable" : [ { } ],
    "curtailmentTable" : [ { } ],
    "deck" : [ { } ],
    "defaultInd" : "boolean",
    "dowConfiguration" : [ { } ],
    "dowItem" : [ { } ],
    "dryOperatingAircraft" : [ { } ],
    "fleetBalanceArmMeasure" : { },
    "fleetIndexValue" : "number",
    "fleetMacPercent" : "number",
    "fleetWeightMeasure" : { },
    "flightDeckCrewLocation" : [ { } ],
    "floorLoadLimitationTable" : [ { } ],
    "fuelDistribution" : [ { } ],
    "fuelingProcedure" : [ { } ],
    "fuelTank" : [ { } ],
    "holdLayout" : { },
    "idealTrimLineTable" : [ { } ],
    "lateralImbalanceLimitTable" : [ { } ],
    "maximumWeightsTable" : [ { } ],
    "minimumWeightsTable" : [ { } ],
    "pantryDistribution" : [ { } ],
    "paxTrimOutputRequirement" : [ { } ],
    "potableWaterDistribution" : [ { } ],
    "potableWaterTank" : [ { } ],
    "runningLoadLimitationTable" : [ { } ],
    "saleableConfiguration" : [ { } ],
    "stabTable" : [ { } ],
    "startWeightTypeCode" : { },
    "supplementaryInfoRequirement" : [ { } ],
    "swa" : [ { } ],
    "taxiFuelProcedure" : [ { } ],
    "tippingLimitTable" : [ { } ]
  },
  "conditionName" : "string",
  "fuelDensityMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "fuelDensityVolumeUnitCode" : {
    "liquidVolumeUnitCodeEnum" : { }
  },
  "fuelDistributionName" : "string",
  "fuelDistributionStep" : [ {
    "fuelDistribution" : { },
    "fuelDistributionStepElement" : [ { } ],
    "stepName" : "string",
    "stepNumber" : "integer",
    "volumeRangeFromMeasure" : { },
    "volumeRangeToMeasure" : { },
    "weightRangeFromMeasure" : { },
    "weightRangeToMeasure" : { }
  } ],
  "maximumVolumeMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "maximumWeightMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "minimumVolumeMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "minimumWeightMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "remark" : [ {
    "aircraft" : { },
    "aircraftGroup" : { },
    "asymmetricalLoadLimitationTable" : { },
    "baggageStandardWeights" : { },
    "balanceOutputRequirement" : { },
    "cargoHeatingDevice" : { },
    "cargoVentilationDevice" : { },
    "centerOfGravityLimitTable" : { },
    "combinedLoadLimitation" : { },
    "combinedLoadLimitationTable" : { },
    "creationDateTime" : "string",
    "crewBaggageStandardWeights" : { },
    "crewDistribution" : { },
    "crewStandardWeights" : { },
    "cumulativeLoadLimitationTable" : { },
    "curtailmentTable" : { },
    "datedOperatingFlight" : { },
    "deck" : { },
    "displayInd" : "boolean",
    "dowConfiguration" : { },
    "dowItem" : { },
    "dryOperatingAircraft" : { },
    "fareRule" : { },
    "floorLoadLimitationTable" : { },
    "fuelDistribution" : { },
    "fuelingProcedure" : { },
    "idealTrimLineTable" : { },
    "lateralImbalanceLimitTable" : { },
    "maximumWeights" : { },
    "maximumWeightsTable" : { },
    "minimumWeights" : { },
    "minimumWeightsTable" : { },
    "missingRestraintRule" : { },
    "orderAmendment" : { },
    "otherPaymentMethod" : { },
    "pantryDistribution" : { },
    "pax" : { },
    "paxStandardWeights" : { },
    "paxTrimOutputRequirement" : { },
    "potableWaterDistribution" : { },
    "priceVarianceRule" : { },
    "promotion" : { },
    "responseParameters" : { },
    "runningLoadLimitationTable" : { },
    "specialLoadLimitation" : { },
    "stabTable" : { },
    "supplementaryInfoRequirement" : { },
    "swa" : { },
    "text" : "string",
    "tippingLimitTable" : { },
    "uldCompatibility" : { },
    "uldType" : { }
  } ]
}