|  Aerodynamics | Get the aerodynamics interface. | 
|  ClimbAtCruiseAirspeed | Select to define the climbing airspeed of the rotorcraft using the cruise airspeed of the current procedure. | 
|  ComputeDeltaAlt | The maximum change in altitude in a computed segment before the data is sampled again. | 
|  DefaultConfiguration | The aircraft's default configuration as saved in the catalog. | 
|  DefaultCruiseAltitude | The rotorcraft's default cruising altitude. | 
|  DescentRateFactor | The descent rate of the rotorcraft as a factor multiplied by the altitude change rate calculated at zero throttle. | 
|  IgnoreFPAForClimbDescentTransitions | Opt to ignore load factor limits when pushing over or pulling up. | 
|  MaxAltitude | The maximum altitude at which the rotorcraft is capable of operating. | 
|  MaxClimbAngle | The maximum pitch angle of the rotorcraft's flight path while climbing. | 
|  MaxDescentAngle | The maximum pitch angle of the rotorcraft's flight path while descending. | 
|  MaxLoadFactor | The maximum load factor that the aircraft can bear while maneuvering in formation. | 
|  MaxSafeAirspeed | The maximum cruising airspeed of the rotorcraft. | 
|  MaxSafeAirspeedType | The maximum safe airspeed type. | 
|  MaxSafeTranslationSpeed | The maximum translation speed of the rotorcraft. | 
|  MaxSafeTranslationSpeedType | The maximum safe translation speed type. | 
|  MaxTransitionPitchAngle | The maximum pitch angle of the flight path when transitioning between forward flight and hovering. | 
|  MinDescentRate | The minimum rate at which the aircraft will descend once established in a steady descent. | 
|  PitchRate | The pitch rate when transitioning between attitude modes or procedures. | 
|  Propulsion | Get the propulsion interface. | 
|  RollRate | The standard roll rate of the rotorcraft in a turn. | 
|  TFMaxFlightPathAngle | The maximum pitch angle of the flight path when the rotorcraft is engaged in terrain following flight. | 
|  TFTerrainWindow | The time interval over which terrain points are sampled when the rotorcraft is engaged in terrain following flight. | 
|  YawRate | The yaw rate when transitioning between attitude modes. | 
|  YawRateDot | The rate of change of the yaw rate. |