Aircraft

A named air-data computer.

A deployable air-driven electrical generator that is distinct from the aircraft's ram-air-turbine emergency generator.

A named pilot, copilot, or standby air-temperature sensor.

Stable root for the currently loaded aircraft. Child component objects are generation-bound and replaced atomically when the aircraft changes.

Aircraft-authored aerodynamic and static-pitch reference characteristics.

A provider-neutral airborne starting point for the user aircraft. USI applies all fields as one simulator operation.

Describes autopilot-channel access points captured for one loaded-aircraft graph. Unknown entries remain usable when a provider exposes a channel but cannot prove its physical installation.

Provides developer-friendly APU selections without exposing simulator switch enums, generator numbering, or pneumatic variable names.

Describes the named radio access points exposed for the currently loaded aircraft. Counts use the developer-facing one-based component names (for example, Com1). Installation states distinguish authoritative equipment discovery from a provider's addressable radio slots.

Load factors resolved along the aircraft's normal, axial, and lateral body axes, in multiples of standard gravity.

Provides developer-friendly occupant-facing state without exposing simulator-native switch or canopy names.

Stable IDs for the initial aircraft capability-discovery surface.

Aircraft-authored center-of-gravity limits relative to the aircraft reference point using signed aircraft axes and the selected length unit.

Current center-of-gravity position relative to the aircraft reference point in signed aircraft axes using the session's selected length unit.

Provider-authored classifications of the loaded aircraft. Multiple flags may be present because, for example, a cargo aircraft may also be an airliner or military aircraft.

A named aircraft clock. Time-of-day values reuse USI's normalized simulator clock; presentation state remains an aircraft-avionics fact.

The presentation selected on an aircraft clock.

Installation evidence captured for this component's aircraft graph.

Describes whether an aircraft component still belongs to the currently loaded aircraft graph.

Provider-neutral cause of the current aircraft crash state.

Describes a newly reported crash of the user aircraft.

Provides developer-friendly aircraft dynamics without exposing SimVars or DataRefs.

Configured component counts for the currently loaded aircraft's electrical system. These authoritative installed counts are distinct from the number of discoverable logical access points in a component collection.

Automated pilot-assistance state for the currently loaded aircraft.

Developer-facing flight-plan abstraction for the currently loaded aircraft. Native GPS and FMS implementations are reconciled here.

Exact force and moment decomposition reported by the provider's flight model. Sources remain separate so totals are not confused with causes.

Stable metadata for one loaded-aircraft fuel selector.

Loaded-aircraft fuel-selector topology, only returned when a count is established.

Side of an aircraft fuel system.

Stable metadata for one loaded-aircraft fuel tank.

Describes the fuel tanks observable for the loaded aircraft. Public tank numbers are stable, one-based identities and never expose a provider's native array slot or SimVar selector.

Provides developer-friendly identity and configuration values for the currently loaded user aircraft without exposing simulator-native names.

A provider-neutral identity snapshot for a loaded aircraft.

One typed value supplied when invoking an aircraft interaction.

The type of one argument accepted by an aircraft interaction.

Describes one observed aircraft-authored interaction change.

One typed position in an aircraft interaction's invocation schema.

A typed value published by an aircraft-authored interaction.

The value shape published by an aircraft-authored interaction.

Stable metadata for one authored landing-gear assembly.

Describes the landing-gear assemblies authored for the loaded aircraft. Public numbers are stable and one-based; provider array slots remain an implementation detail.

Aircraft-authored lateral center-of-gravity limits expressed as signed rightward distances relative to the aircraft reference point using the session's selected length unit.

Minimum and maximum load factors attained over the provider's current observation interval, in multiples of standard gravity.

Aircraft-authored longitudinal center-of-gravity limits expressed as percent mean aerodynamic chord.

Immutable, simulator-neutral snapshot of the aircraft's aerodynamic and three-axis translational/angular motion.

Provides developer-friendly aircraft oxygen state without exposing provider-native DataRefs or override mechanisms.

Stable metadata for one loaded-aircraft payload station.

Describes the payload-station graph configured by the loaded aircraft. Station numbers are one-based public identities and never expose a simulator's native array or SimVar index.

Provides aircraft performance limits in stable aviation units without exposing simulator-native configuration names.

Provides actual cabin pressurization telemetry in stable aviation units.

Broad simulator-neutral classification of the user aircraft's primary propulsion system. Provider-specific engine subtypes are intentionally normalized into stable categories.

Normalized operating condition of an aircraft radio.

Body-axis position using the developer's selected length unit.

A position relative to the aircraft authoring origin, expressed in feet along developer-facing forward, rightward, and upward body axes.

Describes a provider-reported user-aircraft relocation.

Identifies why the simulator repositioned the user aircraft.

Aircraft rotational inertia divided by aircraft mass, expressed about the conventional roll, pitch, and yaw axes using the selected area unit.

Aircraft rotational inertia about its conventional axes, including the provider's documented cross-coupled term, using the session's selected moment-of-inertia unit.

Kind of flight sensor protected by a named heater.

Flight-deck position served by a named sensor.

Provides developer-friendly state for the currently loaded user aircraft without exposing simulator-native names or scalar encodings.

Normalized contamination condition of the surface beneath the aircraft.

One active physical contact between the aircraft and a surface. Provider slot numbers are intentionally omitted from this observation model.

Normalized physical surface beneath the user aircraft.

Preference-aware physical measurements for the principal aircraft systems. Unit-bearing numeric operations remain available for deterministic algorithms.

Provider-neutral aircraft systems display.

Aircraft-system page selected on a multifunction systems display.

Side of the aircraft tailplane represented by a component.

Normalized operating mode for an aircraft transponder.

Provides vacuum-system measurements in stable aviation units.

Provides developer-friendly aircraft warning state without exposing simulator-native annunciator names.

Stable identity for one configured water-ballast tank.

Loaded-aircraft water-ballast tank topology.

Provides aircraft weight and balance measurements in stable aviation units.

Flight-deck window protected by a named electric heater.

Side of the aircraft wing represented by a component.

One stable structural region of the loaded aircraft. Native section counts and failure encodings are intentionally hidden.

Aircraft-installed airshow-smoke equipment. Provider variables, events, and toggle commands remain below this absolute-state contract.

The aircraft's alternate static-air source for pressure-sensitive flight instruments.

Aircraft exposure to ambient smoke in the simulated world. This is separate from smoke emitted by the aircraft and from camera-local smoke density.

A named pilot, copilot, or standby angle-of-attack sensor.

A named area-navigation system, including inertial or long-range navigation equipment when that is the provider's installed source.

A named attitude and heading reference system.

Aircraft-wide audio-panel and intercom behavior. Individual receiver audio selections and volumes remain on their named radio components.

Aircraft-wide automatic power reserve. Installation evidence and current status are separate; discovering this logical component does not prove it is installed.

Aircraft-wide automatic thrust-reverser selection.

One discoverable autopilot computer/channel in the currently loaded aircraft. Public numbering is one-based; native channel identities remain below USI.

A discoverable left- or right-side pump that transfers fuel from auxiliary tanks to feeder tanks.

Provider-neutral avionics equipment-cooling system.

Common health behavior for a named integrated-avionics hardware unit.

A named bleed-air distribution duct on the aircraft.

A named valve that isolates part of the aircraft bleed-air ducting.

A named cabin door or exit. Its logical number is stable developer-facing identity, not proof that the loaded aircraft physically installs the entry.

A named cabin-pressure pack on the aircraft pneumatic system.

Aircraft carrier-launch equipment. Exact provider capabilities remain on this single domain object even where no truthful cross-provider equivalent exists.

A short-duration named aircraft chronometer.

A named pilot or copilot instrument-lighting control whose selected brightness is independent from panel floodlights and achieved light output.

A named cockpit-panel light whose selected brightness is independent from the aircraft-wide cockpit spotlight switch and actual lighting output.

Shared developer-facing behavior for a named cockpit timer.

Aircraft contrail-generation conditions. This does not claim that a visual effect is installed or currently visible.

Provider-neutral aircraft communications datalink.

The aircraft's dedicated distance-measuring-equipment receiver. This is distinct from DME observations supplied by a paired NAV receiver.

Split drag-rudder (yaw-brake) surfaces, kept distinct from the centerline rudder and from roll spoilers even when an aircraft coordinates them.

A long-duration named aircraft elapsed-time counter.

A named provider-neutral electric gyro system.

A named electrically driven aircraft hydraulic pump.

A controllable connection between aircraft electrical buses.

One discoverable semantic electrical circuit. Provider circuit names, indexes, buses, and breaker representations remain below this object.

A named aircraft electrical inverter.

Named electrical power-line access point; connection is not evidence of voltage or load.

Named electrical relay access point. Installation is Unknown without topology evidence; coil power, attached-line connection and breaker state are separate.

The cockpit electrical voltmeter, distinct from direct battery, bus or generator measurements.

A role-aware provider-neutral electronic flight-instrument system.

The aircraft's primary and optional secondary pitch-control surfaces.

The aircraft's combined pitch-and-roll elevon surface system.

The aircraft's deployable emergency electrical generator, when installed.

A named engine and airframe interface unit.

Aircraft-wide oil and radiator cooling-flap controls, separate from each engine's cowl flap. Logical discovery does not confirm physical installation.

A named engine-driven aircraft hydraulic pump.

Aircraft-wide engine-starting selections.

Simulator-rendered exhaust presentation for the loaded aircraft. This is distinct from engine operating state and from ambient-smoke exposure.

Jettisonable external fuel-tank equipment. Provider tank identities and release commands remain below this simulator-neutral aircraft component.

Common identity and health behavior for a flight-deck sensor.

The aircraft's primary and optional secondary roll-control surfaces. Provider wing indexes and native angular units remain below this simulator-neutral component.

Authored force-feedback behavior for the aircraft's physical controls.

A named routing junction in a component fuel network.

Named fuel-line access point. Logical discovery does not establish physical installation or associate a line number with an engine, tank or pump.

One common named fuel-pump type for every supported simulator.

The aircraft's cockpit fuel-quantity presentation. Indicated values may differ from the physical contents reported by named components because the aircraft can apply gauge and display behavior.

One discoverable fuel selector on the loaded aircraft.

One discoverable fuel tank on the loaded aircraft.

A logical aggregation of every fuel tank on one side of an aircraft. This does not assert tank count, identity, or physical topology.

A named conditional trigger in a component fuel network.

One common named fuel-valve type. Network numbering and engine association are explicit roles, never inferred from one another.

Named generator access point. Its number identifies an electrical source, not an engine association; discovery does not establish installation.

Named satellite-navigation receiver guidance. The component represents the same aviation concept whether its provider is a GPS, integrated FMS, or another area-navigation implementation.

Provider-neutral effectiveness state of applied ground deicing.

An external ground source supplying pneumatic air to the aircraft.

The loaded aircraft's Hobbs meter, distinct from simulator uptime, current-flight elapsed time, and per-engine elapsed-time counters.

A named hydraulic pressure accumulator.

A named hydraulic actuator.

A logical hydraulic-system access point. Its number identifies a provider target and does not, by itself, prove installation in the loaded aircraft.

Common lifecycle and validation for named hydraulic components.

A named hydraulic power-transfer unit.

A named pump in a component-based hydraulic network.

A named valve in a component-based hydraulic network.

Simulator-neutral access to automated pilot assistance for the loaded aircraft. Provider AI names and enum ordering remain below this contract.

The flight plan being flown by the user aircraft, independent of the simulator or installed navigator that owns the native plan.

Simulator-managed services requested for the currently loaded aircraft. Successful requests confirm acceptance, not arrival or completed servicing.

Discovers advanced interactions published by the currently loaded aircraft. Normal aircraft systems should be accessed through their typed USI components.

Simulator-neutral state and controls for the lifting envelope of a lighter-than-air aircraft.

Provider-neutral aircraft armament, targeting, and defensive-aids access. Native station indexes, DataRefs, and momentary commands remain below this contract.

Provider-neutral aircraft ice-detection equipment.

A named pneumatic source selected to supply air-driven instruments.

A named integrated avionics processing unit.

A named integrated navigator containing satellite-navigation and radio- tuning functions while preserving their independent health state.

Aircraft jettisonable or slung-load equipment. Multi-station payload and future sling topology remain separate named component concerns.

One discoverable landing-gear assembly on the loaded aircraft.

A named landing-guidance receiver with distinct lateral and vertical channels.

Aircraft equipment that carries and releases liquid, including water-bomber refill and drop controls where the provider exposes those exact semantics.

A named magnetic-field sensor used by integrated avionics.

The aircraft's marker-beacon receiver. Provider-specific light and enum representations are normalized below this component.

A named multifunction display hardware unit.

One named bearing pointer on a role-aware electronic flight display.

A named integrated navigation/communication equipment unit. This is distinct from the independently usable NAV and COM receiver objects.

Provider-neutral aircraft-installed camera equipment.

One discoverable payload station on the loaded aircraft.

A named piston-cylinder access point. Installation is explicit, not inferred from readable temperature.

A graph snapshot of named cylinder access points, with installed count when known.

A named temperature-controlled area of the aircraft.

A named fan in the aircraft pneumatic network.

Common lifecycle and validation for indexed pneumatic components.

A named junction in the aircraft pneumatic distribution network.

A named line in the aircraft pneumatic distribution network.

A named valve in the aircraft pneumatic network.

A named primary flight display hardware unit.

A named radio-altimeter receiver.

A role-aware radio-magnetic indicator. Native selector values and provider-specific pointer switches remain below this component.

Aircraft-wide maneuvering reaction-control propulsion.

Aircraft-wide emergency recovery parachute equipment.

The loaded aircraft's logical ground-refueling connection point. Availability does not imply that simulator refueling service is active.

Aircraft-wide rocket-assisted takeoff equipment. The same named component is present for every simulator; unsupported providers return typed results.

A named rotor access point, independent of engine numbering. Installation may be Unknown; readable telemetry is not evidence of physically installed equipment.

Aircraft-wide rotor-brake selection and configured strength.

A named rotor-driven aircraft hydraulic pump.

Aircraft-wide rotor pre-rotation equipment.

Provider-neutral helicopter or gyrocopter rotor-drive clutch.

Aircraft-wide rotorcraft facts, separate from individual engine and rotor indexing.

The aircraft's primary and optional secondary directional-control surfaces.

A named satellite-based augmentation receiver.

A named heater protecting one aircraft flight sensor.

Provides simulator-neutral access to roll spoilers (spoilerons), kept distinct from the speed-brake surfaces that may share physical panels.

A named pilot, copilot, or standby static-pressure sensor.

Provider-neutral tail-rotor transmission equipment.

Provider-neutral ice-protection equipment for one tailplane.

Aircraft-wide thrust-vectoring selection and achieved position.

A named TKS fluid pump. Numbering preserves the authoritative aircraft channels without inventing primary or backup roles.

Provider-neutral aircraft-wide TKS fluid supply and pump state.

Aircraft towing and winch equipment. Provider-specific observations remain available on this single simulator-neutral component without changing its identity or requiring provider branches.

A named source of aircraft instrument-vacuum pressure.

An aircraft's movable nose and protective visor system.

Aircraft water-ballast equipment. Releasable water carried by a water- bomber remains a separate control system.

One named water-ballast tank on the loaded aircraft.

Provider-neutral onboard weather-radar equipment.

Weather-radar presentation controls and indications for one electronic flight display.

A named pilot or copilot cockpit wind indication. This remains distinct from the simulator environment's actual local wind observation.

A named heater protecting one flight-deck window.

A named non-wiper rain-repellent system serving one flight-deck windshield.

A named wiper serving one flight-deck windshield.

Aircraft-wide summaries of actual aerodynamic condensation around the loaded aircraft's wings. Native aerodynamic-wing slots remain internal.

Fixed wing planform and variable airframe geometry. Requested and achieved variable-geometry positions remain distinct.

Provider-neutral ice-protection equipment for one wing.

A physical yaw-string indication, distinct from aerodynamic sideslip and an instrument's slip/skid ball.