StabTable
A set of related stabilizer trim settings for given flap settings or thrust ratings.
Properties
Name |
Description |
Type |
Required |
Generic |
Enum |
Ignore |
aircraftGroupConfiguration |
A Specific Configuration of an Aircraft Group. |
AircraftGroupConfiguration |
true |
|
|
false |
flapsSettingValue |
The Flaps Setting to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
macPercent |
The maximum %MAC value to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
maximumFlapsSettingValue |
The maximum value of the Flaps Setting range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
maximumMacPercent |
The maximum value of the %MAC range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
maximumThrustRatingValue |
The maximum value of the Thrust Rating range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
minimumFlapsSettingValue |
The minimum value of the Flaps Setting range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
minimumMacPercent |
The minimum value of the %MAC range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
minimumThrustRatingValue |
The minimum value of the Thrust Rating range to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
remark |
An additional, supplementary information about the document or service. |
array |
false |
Remark |
--- |
false |
stab |
A stabilizer Trim Setting. The required position of the horizontal stabilizer depending on the aircrafts weight and center of gravity (%MAC/RC). |
array |
true |
Stab |
--- |
false |
stabText |
A text to be appended to the stabilizer trim value printed on the load sheet depending on the stabilizer trim range it belongs to. |
array |
false |
StabText |
--- |
false |
tableName |
Specific name for the table of stabilizer trim settings. |
string |
false |
|
|
false |
thrustRatingValue |
The Thrust Rating to which the specific stabilizer trim table applies. |
number |
false |
|
|
false |
{
"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" : [ { } ]
},
"flapsSettingValue" : "number",
"macPercent" : "number",
"maximumFlapsSettingValue" : "number",
"maximumMacPercent" : "number",
"maximumThrustRatingValue" : "number",
"minimumFlapsSettingValue" : "number",
"minimumMacPercent" : "number",
"minimumThrustRatingValue" : "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" : { }
} ],
"stab" : [ {
"changePerPctmacValue" : "number",
"macPercent" : "number",
"stabTable" : { },
"towMeasure" : { },
"value" : { }
} ],
"stabText" : [ {
"noseIndicationText" : "string",
"stabFromValue" : "number",
"stabTable" : { },
"stabToValue" : "number"
} ],
"tableName" : "string",
"thrustRatingValue" : "number"
}