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

Stab

A stabilizer Trim Setting. The required position of the horizontal stabilizer depending on the aircrafts weight and center of gravity (%MAC/RC).

Properties

Name Description Type Required Generic Enum Ignore
changePerPctmacValue Stabilizer trim setting change for each percent reduction in PCTMAC. When this field is used, only one PCTMAC (the maximum value) and corresponding STAB must be specified in the table for a given take-off weight. number false false
macPercent %MAC value for which the stabilizer trim setting applies. number false false
stabTable A set of related stabilizer trim settings for given flap settings or thrust ratings. StabTable true false
towMeasure Take-off weight for which the stabilizer trim setting applies. WeightMeasure false false
value Stabilizer trim setting. Value false false

Referenced By

StabTable
{
  "changePerPctmacValue" : "number",
  "macPercent" : "number",
  "stabTable" : {
    "aircraftGroupConfiguration" : { },
    "flapsSettingValue" : "number",
    "macPercent" : "number",
    "maximumFlapsSettingValue" : "number",
    "maximumMacPercent" : "number",
    "maximumThrustRatingValue" : "number",
    "minimumFlapsSettingValue" : "number",
    "minimumMacPercent" : "number",
    "minimumThrustRatingValue" : "number",
    "remark" : [ { } ],
    "stab" : [ { } ],
    "stabText" : [ { } ],
    "tableName" : "string",
    "thrustRatingValue" : "number"
  },
  "towMeasure" : {
    "unitCode" : "string",
    "value" : "number"
  },
  "value" : { }
}