complexType · extension complexBaseType · all
Mass breakdown
The <massBreakdown> is subdivided in <designMasses>, <fuel>, <payload> and <mOEM> (operating empty mass).
designMass
The design masses contain the overall values for mTOM and so forth. These should be listed as specified by the TLAR or found from initial sizing.
fuel and payload
The fuel and payload nodes should contain maximum values, i.e. full fuel tanks, all passengers on board and full cargo holding. These values may exceed the maximum allowable take-off mass as the actual loading of the aircraft should be specified in the weight and balance section of the aircraft.
mOEM
The operation empty mass structure is based on the Airbus Mass Standard brake down [AIRBUS MASS STANDARD 2008]. The operator’s mass empty (OME) is defined by the sum of the following component masses:
Each sub component has the following <massDescription> which include a:
The <massDescription> can be found at the <designMasses> direct under each item. At the <fuel>, <payload> and <mOEM> under massDescription in each item and sub item.
Concerning symmetry, a reference to a symmetric component (e.g. a wing) accounts for both components created by the symmetry, i.e. for the defined and the mirrored side, so their total mass has to be given. If the masses of the two sides differ, they are given separately, and the @symmetry attribute of the reference selects the side (def or symm, see stringUIDBaseType).
| Name | Type | Constraints | Use | Default | Description |
|---|---|---|---|---|---|
@externalDataDirectory | xsd:string | optional | Directory of the external file the element was read from, as URI | ||
@externalDataNodePath | xsd:string | optional | Path of the parent element in the merged dataset, at which the element was inserted from an external file | ||
@externalFileName | xsd:string | optional | Name of the external file the element was read from |
| Name | Type | Constraints | OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration. | Default | Description |
|---|---|---|---|---|---|
| allThe children below may appear in any order. Each may appear at most once. | |||||
designMasses | designMassesType | [1..1] required | Design masses of the aircraft | ||
payload | mPayloadType | [1..1] required | Payload mass | ||
fuel | mFuelType | [1..1] required | Fuel mass | ||
mOEM | oEMType | [1..1] required | Operating empty mass | ||
| Type | Name |
|---|---|
aircraftAnalysesType | massBreakdown |