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

Curtailment

A limitation to certified (manufacturer's) CG limits in order to account for certain operational assumptions and associated CG calculation inaccuracies.

Properties

Name Description Type Required Generic Enum Ignore
aftIndexValue Value of aft curtailment expressed in index units. If this field is entered, do not enter a %MAC/RC value. number false false
aftMacPercent Value of aft curtailment expressed as %MAC/RC. If this field is entered, do not enter an index value. number false false
curtailmentTable A Set of Curtailments. CurtailmentTable true false
forwardIndexValue Value of forward curtailment expressed in index units. If this field is entered, do not enter a %MAC/RC value. number false false
forwardMacPercent Value of forward curtailment expressed as %MAC/RC. If this field is entered, do not enter an index value. number false false
sumOfSquareInd Indicates that curtailment value is to be applied to the CG as a total value (false) or as a component of the quadratic sum (true). boolean false false
weightTypeCode Type of weight of CG limits to which the curtailment must be applied: Taxi (TA), Take Off (TO), Landing (LD) , Zero Fuel (ZF), In-flight (IN). WeightTypeCode false false

Referenced By

CurtailmentTable
{
  "aftIndexValue" : "number",
  "aftMacPercent" : "number",
  "curtailmentTable" : {
    "aircraftGroupConfiguration" : { },
    "conditionText" : "string",
    "curtailment" : [ { } ],
    "remark" : [ { } ],
    "tableName" : "string"
  },
  "forwardIndexValue" : "number",
  "forwardMacPercent" : "number",
  "sumOfSquareInd" : "boolean",
  "weightTypeCode" : {
    "weightTypeCodeEnum" : { }
  }
}