This research tool has been used to visualize flight paths, test control algorithms, simulate an active airspace, or generate out-the-window visuals for in-house flight simulation software. Possible applications include active control of an XPlane simulation, flight visualization, recording states during a flight, or interacting with a mission over UDP. '''python All special chars like [Space][italic chars][,][/][*][-][#] etc. change with [_] char. For example:
L/D, ratio => L_D_ratio
L/D, etaP => L_D__etaP
wingn*, L cl* => wing_n_L_cl_
'''
X-Plane Data Set Output Table Official Website
Click to see X-Plane Data Set Output Table
| Field label | Descriptions of fields available in X‑Plane 10/11/12’s data output | Parameter Name in Library |
|---|---|---|
Frame rate |
||
| f-act, /sec | The actual frame rate being displayed by X-Plane. Unless your computer is bogged down, this will be the same as f-sim. | f_act_sec |
| f-sim, /sec | The frame rate the simulator is “pretending” to have in order to keep the flight model from failing. | f_sim_sec |
| frame, time | The time required to render one frame, in seconds. | frame_time |
| cpu, time | • | cpu_time |
| gpu, time | • | gpu_time |
| grnd, ratio | • | grnd_ratio |
| flit, ratio | • | flit_ratio |
Times |
||
| real, time | The number of seconds, in the real world, elapsed since the simulator was launched. | real_time |
| totl, time | The number of seconds elapsed since the simulator was launched minus time spent in a loading screen. | totl_time |
| missn, time | The time since the start of the “mission” (generally the time since the last time an aircraft or location was loaded). | missn_time |
| timer, time | The time elapsed on a timer for general use. | timer_time |
| zulu, time | “Zulu” time (Greenwich Mean Time, or GMT) in the simulator, in decimal hours (e.g., 3.5 for 3:30 a.m.). | zulu_time |
| local, time | Local time in the simulator, in decimal hours. | local_time |
| hobbs, time | The aircraft’s Hobbs time (a measurement of how long the aircraft’s systems have been run). | hobbs_time |
Simulator statistics (sim stats) |
||
| explo, DIM | • | explo_DIM |
| explo, USE | • | explo_USE |
| cratr, DIM | • | cratr_DIM |
| cratr, USE | • | cratr_USE |
| puffs, TOT | • | puffs_TOT |
| puffs, VIS | • | puffs_VIS |
| tris, vis | • | tris_vis |
| q, depth | • | q_depth |
Speeds |
||
| Vind, kias | The craft’s indicated airspeed, in knots indicated airspeed. | Vind_kias |
| Vind, keas | The craft’s indicated airspeed, in knots equivalent airspeed (the calibrated airspeed corrected for adiabatic compressible flow at the craft’s current altitude). | Vind_keas |
| Vtrue, ktas | The craft’s true airspeed (the speed of the craft relative to undisturbed air), in knots true airspeed. | Vtrue_ktas |
| Vtrue, ktgs | True airspeed, in knots true ground speed. | Vtrue_ktgs |
| Vind, mph | The craft’s indicated airspeed, in miles per hour. | Vind_mph |
| Vtrue, mphas | The craft’s true airspeed, in miles per hour airspeed. | Vtrue_mphas |
| Vtrue, mphgs | The craft’s true airspeed, in miles per hour ground speed. | Vtrue_mphgs |
Aircraft Mach speeds, vertical velocity, and g-loads (mach, VVI, G-load) |
||
| Mach, ratio | The aircraft’s current speed, as a ratio to Mach 1. | Mach_ratio |
| VVI, fpm | The aircraft’s current vertical velocity, in feet per minute. If everything is working as it should, this is normal to the local horizon under the aircraft. | VVI_fpm |
| Gload, norml | The g-load across the aircraft, relative to the aircraft body-axis, if all is working as it should. | Gload_norml |
| Gload, axial | The axial g-load on the aircraft. | Gload_axial |
| Gload, side | The side g-load on the aircraft. | Gload_side |
Atmosphere: weather |
||
| SLprs, inHG | SLprs, in inches mercury. | SLprs_inHG |
| SLtmp, degC | SLtmp, in degrees Celsius. | SLtmp_degC |
| wind, speed | The wind speed around the aircraft, in knots. | wind_speed |
| wind, dir | The wind direction, in degrees clockwise deviation from north. Wind blowing from north to south has direction 0.0, while wind blowing from west to east has direction 270.0. | wind_dir |
| trb, locl | Amount of local turbulence. | trb_locl |
| prec, locl | Amount of local precipitation. | prec_locl |
| hail, locl | Amount of local hail. | hail_locl |
Atmosphere: aircraft |
||
| AMprs, inHG | AMprs, in inches mercury. | AMprs_inHG |
| AMtmp, degC | AMtmp, in degrees Celsius. | AMtmp_degC |
| LEtmp, degC | LEtmp, in degrees Celsius. | LEtmp_degC |
| dens, ratio | The aircraft’s density ratio. | dens_ratio |
| A, ktas | A, in knots true airspeed. | A_ktas |
| Q, psf | Q, dynamic pressure or velocity pressure, in pounds per square foot. | Q_psf |
| gravi, fts2 | Gravitational force, in feet per second squared. | gravi_fts2 |
System pressures |
||
| baro, inHG | Barometric pressure, in inches mercury. | baro_inHG |
| edens, part | • | edens_part |
| vacum, ratio | • | vacum_ratio |
| elec, ratio | • | elec_ratio |
| AHRS, ratio | Pressure in the attitude heading reference system (AHRS), as a ratio to normal. | AHRS_ratio |
Joystick aileron, elevator, and rudder input (joystick ail/elv/rud) |
||
| elev, yoke1 | The user’s elevator input, as a ratio to full upward deflection. For instance, a value of –1.000 indicated the user is commanding the aircraft’s nose down as fast as possible. | elev_yoke1 |
| ailrn, yoke1 | The user’s aileron input, as a ratio to full rightward deflection. For instance, a value of –1.000 indicated the user is commanding the aircraft to roll left as fast as possible. | ailrn_yoke1 |
| ruddr, yoke1 | The user’s rudder input, as a ratio to full rightward deflection. For instance, a value of –1.000 indicated the user is commanding the aircraft to yaw left as fast as possible. | ruddr_yoke1 |
Other flight controls |
||
| vect, rqst | The requested thrust vectoring. | vect_rqst |
| sweep, rqst | The requested wing sweep. | sweep_rqst |
| incid, rqst | The requested wing incidence. | incid_rqst |
| dihed, rqst | The requested wing dihedral. | dihed_rqst |
| retra, rqst | The requested wing retraction. | retra_rqst |
| water, jetts | Water jettisoned. | water_jetts |
Artificial stability inputs for aileron, elevator, and rudder (art stab ail/elv/rud) |
||
| elev, astab | The artificial stability system’s elevator input, as a ratio to full upward deflection. | elev_astab |
| ailrn, astab | The artificial stability system’s aileron input, as a ratio to full rightward deflection. | ailrn_astab |
| ruddr, astab | The artificial stability system’s aileron input, as a ratio to full rightward deflection. | ruddr_astab |
Flight control deflections for aileron, elevator, and rudder (flight con ail/elv/rud) |
||
| elev, surf | The proportion of the elevator deflected for upward pitch. If the elevators and flight inputs are in sync, this will match the combined yoke and artificial stability system input. | elev_surf |
| ailrn, surf | The proportion of the aileron deflected for rightward roll. If the elevators and flight inputs are in sync, this will match the combined yoke and artificial stability system input. | ailrn_surf |
| ruddr, surf | The proportion of the rudder deflected for rightward yaw. If the elevators and flight inputs are in sync, this will match the combined yoke and artificial stability system input. | ruddr_surf |
| nwhel, steer | The nosewheel’s direction, in degrees of deviation from pointing straight ahead. For instance, a value of –31.000 indicated the wheel is pointed left 31 degrees. | nwhel_steer |
Wing sweep and thrust vectoring (wing sweep/thrust vect) |
||
| sweep, 1, deg | The craft’s wing sweep, in degrees back from normal. | sweep_1_deg |
| sweep, 2, deg | The craft’s wing sweep, in degrees back from normal. | sweep_2_deg |
| sweep, h, deg | The craft’s wing sweep, in degrees. | sweep_h_deg |
| vect, ratio | • | vect_ratio |
| sweep, ratio | The craft’s wing sweep, as a ratio to fully forward. | sweep_ratio |
| incid, ratio | The craft’s wing incidence, as a ratio to fully angled. | incid_ratio |
| dihed, ratio | The craft’s wing dihedral, as a ratio to fully angled. | dihed_ratio |
| retra, ratio | The craft’s wing retraction, as a ratio to fully retracted. | retra_ratio |
Trim, flaps, slats, and speedbrakes (trim/flap/slat/s-brakes) |
||
| trim, elev | Elevator trim. | trim_elev |
| trim, ailrn | Aileron trim. | trim_ailrn |
| trim, ruddr | Rudder trim. | trim_ruddr |
| flap, handl | • | flap_handl |
| flap, postn | Flap position. | flap_postn |
| slat, ratio | Slat position. | slat_ratio |
| sbrak, handl | sbrak_handl | |
| sbrak, postn | Speedbrake position. | sbrak_postn |
Landing gear and brakes (gear/brakes) |
||
| gear, 0/1 | Gear extended status. | gear_0_1 |
| wbrak, part | • | wbrak_part |
| lbrak, part | Left toe brake depression. | lbrak_part |
| rbrak, part | Right toe brake depression. | rbrak_part |
Angular moments |
||
| L, ftlb | Roll torque, in foot-pounds, about the long axis, which we call the z axis. | L_ftlb |
| M, ftlb | Pitch torque, in foot-pounds, about the lateral axis, which we call the x axis. | M_ftlb |
| N, ftlb | Yaw torque, in foot-pounds, about the vertical axis, which we call the y axis. | N_ftlb |
| Q, rad/s | Pitch rate, measured in body-axes (when all is working as it should). | Q_rad_s |
| P, rad/s | Roll rate, measured in body-axes (when all is working as it should). | P_rad_s |
| R, rad/s | Yaw rate, measured in body-axes (when all is working as it should). | R_rad_s |
Pitch, roll, headings |
||
| pitch, deg | The aircraft’s pitch, measured in body-axis Euler angles. | pitch_deg |
| roll, deg | The aircraft’s roll, measured in body-axis Euler angles. | roll_deg |
| hding, true | The aircraft’s true heading, measured in body-axis Euler angles. | hding_true |
| hding, mag | The aircraft’s magnetic heading, in degrees. | hding_mag |
Angle of attack, sideslip, and paths (AoA, side-slip, paths) |
||
| alpha, deg | The aircraft’s angle of attack, in degrees. | alpha_deg |
| beta, deg | The aircraft’s angle of sideslip, in degrees. | beta_deg |
| hpath, deg | • | hpath_deg |
| vpath, deg | • | vpath_deg |
| slip, deg | • | slip_deg |
Magnetic compass (mag compass) |
||
| mag, comp | • | mag_comp |
| mavar, deg | • | mavar_deg |
Latitude, longitude, and altitude (lat, lon, altitude) |
||
| lat, deg | The aircraft’s latitudinal location, in degrees. | lat_deg |
| lon, deg | The aircraft’s longitudinal location, in degrees. | long_deg |
| alt, ftmsl | The aircraft’s altitude, in feet above mean sea level. | alt_ftmsl |
| alt, ftagl | The aircraft’s altitude, in feet above ground level. | alt_ftagl |
| on, runwy | • | on_runwy |
| alt, ind | • | alt_ind |
| lat, south | • | lat_south |
| lon, west | • | lon_west |
Location, velocity, and distance traveled (loc, vel, dist traveled) |
||
| X, m | Relative to the inertial axes. | X_m |
| Y, m | Relative to the inertial axes. | Y_m |
| Z, m | Relative to the inertial axes. | Z_m |
| vX, m/s | Relative to the inertial axes. | vX_m_s |
| vY, m/s | Relative to the inertial axes. | vY_m_s |
| vZ, m/s | Relative to the inertial axes. | vZ_m_s |
| dist, ft | • | dist_ft |
| dist, nm | • | dist_nm |
Latitude for all aircraft (all planes: lat) |
||
| lat n, deg | Aircraft n’s latitudinal location (zero if craft n does not exist). | lat_n_deg |
Longitude for all aircraft (all planes: lon) |
||
| lon n, deg | Aircraft n’s longitudinal location (zero if craft n does not exist). | lon_n_deg |
Altitude for all aircraft (all planes: alt) |
||
| alt n, ftmsl | Aircraft n’s altitude location (zero if craft n does not exist). | alt_n_ftmsl |
Commanded throttle (throttle command) |
||
| thron, part | Aircraft n’s commanded throttle. | thro_n_part |
Actual throttle (throttle actual) |
||
| thron, part | Aircraft n’s actual throttle. | thro_n_part |
Engine or propeller mode (feather-norm-beta-revers) |
||
| moden, 0123 | Engine n’s current “mode,” where 0 corresponds to feathered, 1 corresponds to normal, 2 to beta, and 3 to reverse thrust. | mode_n_0123 |
Propeller setting (prop setting) |
||
| propn, set | Aircraft n’s propeller setting. | prop_n_set |
Mixture setting |
||
| mixtn, ratio | Aircraft n’s mixture setting. | mixt_n_ratio |
Carburetor heat setting (carb heat setting) |
||
| heatn, ratio | Aircraft n’s carburetor heat setting. | heat_n_ratio |
Cowl flap setting |
||
| cowln, set | Aircraft n’s cowl flap setting. | cowl_n_set |
Magneto settings |
||
| magnn, set | Aircraft n’s magneto setting. | magn_n_set |
Starter timeout |
||
| starn, sec | Aircraft n’s starter timeout. | star_n_sec |
Engine power |
||
| power, n, hp | Engine n’s power, in horsepower. | power_n_hp |
Engine thrust |
||
| thrst, n, lb | The thrust, in pounds, generated by engine n. | thrst_n_lb |
Engine torque |
||
| trq n, ftlb | The torque, in foot-pounds, generated by engine n. | trq_n_ftlb |
Engine RPM |
||
| rpm n, engin | The current RPM of engine n. | rpm_n_engin |
Propeller RPM (prop RPM) |
||
| rpm n, prop | The current RPM of propeller n. | rpm_n_prop |
Propeller pitch (prop pitch) |
||
| ptchn, deg | The current pitch of propeller n. | ptch_n_deg |
Slipstream/propwash/jetwash (propwash/jetwash) |
||
| pwash, kt | • | pwash_kt |
N1 |
||
| N1 n, pcnt | The current N1 for engine n. | N1_n_pcnt |
N2 |
||
| N2 n, pcnt | The current N2 for engine n. | N2_n_pcnt |
Manifold pressure (MP) |
||
| MP n, inhg | The current manifold pressure for engine n, in inches mercury. | MP_n_inhg |
Engine pressure ratio (EPR) |
||
| EPR n, part | The current engine pressure ratio for engine n. | EPR_n_aprt |
Fuel flow (FF) |
||
| FF n, lb/h | The current fuel flow for engine n, in pounds per hour. | FF_n_lb_h |
Interstage turbine temperature (ITT) |
||
| ITT n, deg | The current interstage turbine temperature for engine n. | ITT_n_deg |
Exhaust gas temperature (EGT) |
||
| EGT n, deg | The current exhaust gas temperature for engine n. | EGT_n_deg |
Cylinder head temperature (CHT) |
||
| CHT n, deg | The current cylinder head temperature for engine n. | CHT_n_deg |
Oil pressure |
||
| OILPn, psi | The current oil pressure for engine n, in pounds per square inch. | OILP_n_psi |
Oil temperature (Oil temp) |
||
| OILTn, deg | The current oil temperature for engine n. | OILT_n_deg |
Fuel pressure |
||
| FUEPn, psi | The current fuel pressure for engine n, in pounds per square inch. | FUEP_n_psi |
Generator amperage |
||
| genrn, amp | The current generator amperage for generator n. | genr_n_amp |
Battery amperage |
||
| battn, amp | The current batter amperage for battery n. | batt_n_amp |
Battery voltage |
||
| battn, volt | The current battery voltage for battery n. | batt_n_volt |
Fuel pump on/off |
||
| pumpn, 0/1 | Fuel pump n’s status. | pump_n_0_1 |
Idle speed lo/hi |
||
| idlen 0/1 | Engine n’s idle speed. | idle_n_0_1 |
Battery on/off |
||
| battn, 0/1 | Battery n’s status. | batt_n_0_1 |
Generator on/off |
||
| genrn, 0/1 | Generator n’s status. | genr_n_0_1 |
Inverter on/off |
||
| invrn, 0/1 | Inverter n’s status. | invr_n_0_1 |
FADEC on/off |
||
| fadec, 0/1 | The FADEC’s status. | fadec_0_1 |
Igniter on/off |
||
| ignin, 0/1 | Igniter n’s status. | igni_n_0_1 |
Fuel weights |
||
| fuel, n lb | Fuel tank n’s weight, in pounds. | fuel_n_lb |
Payload weights and center of gravity (payload weights and CG) |
||
| empty, lb | The aircraft’s empty weight, in pounds. | empty_lb |
| payld, lb | The aircraft’s payload weight, in pounds. | payld_lb |
| fuel, totlb | The total weight of the aircraft’s fuel, in pounds. | fuel_totlb |
| jetti, lb | The aircraft’s jettisonable weight, in pounds. | jetti_lb |
| curnt, lb | The aircraft’s current weight, in pounds. | curnt_lb |
| maxim, lb | The aircraft’s maximum weight, in pounds. | maxim_lb |
| cg, ftref | The aircraft’s center of gravity, measured in feet behind the reference point. | cg_ftref |
Aerodynamic forces, in wind axes (aero forces) |
||
| lift, lb | The lift acting on the aircraft, in pounds. | lift_lb |
| drag, lb | The drag acting on the aircraft, in pounds. | drag_lb |
| side, lb | The side forces acting on the aircraft, in pounds. | side_lb |
Engine forces |
||
| norml, lb | • | norml_lb |
| axial, lb | • | axial_lb |
| side, lb | • | side_lb |
Landing gear vertical force (landing gear vert force) |
||
| gear, lb | • | gear_lb |
Landing gear deployment |
||
| gear, rat | • | gear_rat |
Lift-to-drag ratio and coefficients (lift over drag coeffs) |
||
| L/D, ratio | The aircraft’s lift-to-drag ratio. | L_D_ratio |
| cl, total | • | cl_total |
| cd, total | • | cd_total |
| L/D, *etaP | • | L_D__etaP |
Propeller efficiency (prop efficiency) |
||
| Peffn, ratio | Propeller n’s efficiency ratio. | Peff_n_ratio |
Aileron deflections (defs: ailerons) |
||
| Lailn,n,deg | The deflection of left aileron n, in degrees. | Lailn_n_deg |
| Railn, n, deg | The deflection of right aileron n, in degrees. | Railn_n_deg |
Roll spoiler deflection (defs: roll spoilers) |
||
| Lsplr,n, deg | The deflection of left spoiler n, in degrees. | Lsplr_n_deg |
| Rsplr, n, deg | The deflection of right spoiler n, in degrees. | Rsplr_n_deg |
Elevator deflections (defs: elevators) |
||
| elevn, deg | The deflection of elevator n, in degrees. | elev_n_deg |
Rudder deflection (defs: rudders) |
||
| rudrn, deg | The deflection of rudder n, in degrees. | rudr_n_deg |
Yaw brake deflections (defs: yaw brakes) |
||
| Lyawb, deg | The deflection of the left yaw brake, in degrees. | Lyawb_deg |
| Ryawb, deg | The deflection of the right yaw brake, in degrees. | Ryawb_deg |
Control forces |
||
| pitch, lb | The pitch forces acting on the controls in the pilot’s hands. | pitch_lb |
| roll, lb | The roll forces acting on the controls in the pilot’s hands. | roll_lb |
| hdng, lb | The heading forces acting on the controls in the pilot’s hands. | hdng_lb |
| l-brk, lb | The left brake forces acting on the controls at the pilot’s feet. | l_brk_lb |
| r-brk, lb | The right brake forces acting on the controls at the pilot’s feet. | r_brk_lb |
Total vertical thrust vectors (total vert thrust vects) |
||
| vertn, tvect | • | vert_n_tvect |
Total lateral thrust vectors (total lat thrust vects) |
||
| latrn, tvect | • | latr_n_tvect |
Pitch cyclic disc tilts |
||
| pitch, cycli | • | pitch_cycli |
Roll cyclic disc tilts |
||
| roll, cycli | • | roll_cycli |
Pitch cyclic flapping |
||
| pitch, flap | pitch_flap | |
Roll cyclic flapping |
||
| roll, flap | roll_flap | |
Ground effect (lift) from wings (grnd effect lift, wings) |
||
| wingn, L cl* | wing_n_L_cl_ | |
| wingn, R cl* | • | wing_n_R_cl_ |
Ground effect (drag) from wings (grnd effect drag, wings) |
||
| wingn, Lcdi* | • | wing_n_Lcdi_ |
| wingn, Rcdi* | • | wing_n_Rcdi_ |
Ground effect (wash) from wings (grnd effect wash, wings) |
||
| wingn, wash* | • | wing_n_wash_ |
Ground effect (lift) from stabilizers (grnd effect lift, stabs) |
||
| hstab, L cl* | • | hstab_L_cl_ |
| hstab, R cl* | • | hstab_R_cl_ |
| vstb1, cl* | • | vstb1_cl_ |
Ground effect (drag) from stabilizers (grnd effect drag, stabs) |
||
| hstab, Lcdi* | • | hstab_Lcdi_ |
| hstab, Rcdi* | • | hstab_Rcd |
| vstbn, cdi* | • | vstb_n_cdi_ |
Ground effect (wash) from stabilizers (grnd effect wash, stabs) |
||
| hstab, wash* | • | hstab_wash_ |
| vstbn, wash* | • | vstb_n_wash_ |
Ground effect (lift) from propellers (grnd effect lift, props) |
||
| propn, cl* | prop_n_cl_ | |
Ground effect (drag) from propellers (grnd effect drag, props) |
||
| propn, cdi* | prop_n_cdi_ | |
Wing lift |
||
| wingn, lift | The lift generated by wing n. | wing_n_lift |
Wing drag |
||
| wingn, drag | The drag generated by wing n. | wing_n_drag |
Stabilizer lift (stab lift) |
||
| hstab, lift | The lift generated by the horizontal stabilizer. | hstab_lift |
| vstbn, lift | The lift generated by the vertical stabilizer. | vstb_n_lift |
Stabilizer drag (stab drag) |
||
| hstab, drag | The drag generated by the horizontal stabilizer. | hstab_drag |
| vstbn, drag | The drag generated by the vertical stabilizer. | vstb_n_drag |
COM 1/2 frequency |
||
| COM n, freq | The current frequency of the COM n radio. | COM_n_freq |
| COM n, stby | The standby frequency of the COM n radio. | COM_n_stby |
| COM, xmt | The transmit status of the COM n. | COM_xmt |
NAV 1/2 frequency |
||
| NAV n, freq | The current frequency of the NAV n radio. | NAV_n_freq |
| NAV n, stby | The standby frequency of the NAV n radio. | NAV_n_stby |
| NAV n, type | • | NAV_n_type |
NAV 1/2 OBS |
||
| NAV n, OBS | • | NAV_n_OBS |
| NAV n, s-crs | • | NAV_n_s_crs |
| NAV n, flag | • | NAV_n_flag |
| NAV n deflections | ||
| NAV n, n-typ | • | NAV_n_n_typ |
| NAV n, to-fr | • | NAV_n_to_fr |
| NAV n, m-crs | • | NAV_n_m_crs |
| NAV n, r-brg | • | NAV_n_r_brg |
| NAV n, dme-d | • | NAV_n_dme_d |
| NAV n, h-def | • | NAV_n_h_def |
| NAV n, v-def | • | NAV_n_v_def |
ADF 1/2 status |
||
| ADF n, freq | • | ADF_n_freq |
| ADF n, card | • | ADF_n_card |
| ADF n, r-brg | • | ADF_n_r_brg |
| ADF n, n-typ | • | ADF_n_n_typ |
DME status |
||
| DME, nav01 | • | DME_nav01 |
| DME, mode | • | DME_mode |
| DME, found | • | DME_found |
| DME, dist | • | DME_dist |
| DME, speed | • | DME_speed |
| DME, time | • | DME_time |
| DME, n-typ | • | DME_n_type |
| DME–3, freq | • | DME_3_freq |
GPS status |
||
| GPS, mode | • | GPS_mode |
| GPS, index | • | GPS_index |
| dist, nm | • | dist_nm |
| OBS, mag | • | OBS_mag |
| crs, mag | • | crs_mag |
| rel, brng | • | rel_brng |
| hdef, dots | • | hdef_dots |
| vdef, dots | • | vdef_dots |
Transponder status (XPNDR status) |
||
| trans, mode | • | trans_mode |
| trans, sett | • | trans_sett |
| trans, ID | • | trans_ID |
| trans, inter | • | trans_inter |
Marker status |
||
| OM, morse | Signal from outer marker (OM) | OM_morse |
| MM, morse | Signal from middle marker (MM) | MM_morse |
| IM, morse | Signal from inner marker (IM) | IM_morse |
| audio, activ | • | audio_activ |
Switches 1: electrical |
||
| avio, 0/1 | The status of the AVIO switch. | avio_0_1 |
| nav, lite | The status of the navigation light switch. | nav_lite |
| beacn, lite | The status of the beacon switch. | beacn_lite |
| strob, lite | The status of the strobe light switch. | strob_lite |
| land, lite | The status of the landing light switch. | land_lite |
| taxi, lite | The status of the taxi light switch. | taxi_lite |
Switches 2: EFIS |
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| ECAM, mode | The ECAM mode. | ECAM_mode |
| EFIS, sel n | • | EFIS_sel_n |
| HSI, sel n | • | HSI_sel_n |
| HSI, arc | • | HSI_arc |
| map, r-sel | • | map_r_sel |
| map, range | • | map_range |
Switches 3: Autopilot, flight director, and head-up display (switches 3: AP/f-dir/HUD) |
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| ap, src | • | ap_src |
| fdir, mode | • | fdir_mode |
| fdir, ptch | • | fdir_ptch |
| fdir, roll | • | fdir_roll |
| HUD, power | • | HUD_power |
| HUD, brite | • | HUD_brite |
Switches 4: anti-ice |
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| deice, all | • | deice_all |
| deice, inlet | • | deice_inlet |
| deice, prop | • | deice_prop |
| deice, windo | • | deice_windo |
| deice-n, pitot | • | deice_n_pitot |
| deice, AOA | • | deice_AOA |
| deice, wing | • | deice_wing |
Switches 5: anti-ice/fuel |
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| alt, airn | • | alt_air_n |
| auto, ignit | • | auto_ignit |
| manul, ignit | • | manul_ignit |
| l-eng, tank | • | l_eng_tank |
| r-eng, tank | • | r_eng_tank |
Switches 6: clutch and artificial stability (switches 6: clutch/astab) |
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| prero, engag | • | prero_engag |
| clutc, ratio | • | clutc_ratio |
| art, ptch | • | art_ptch |
| art, roll | • | art_roll |
| yaw, damp | • | yaw_damp |
| auto, brake | • | auto_brake |
Switches 7: miscellaneous (switches 7: misc) |
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| tot, energ | • | tot_energ |
| radal, feet | • | radal_feet |
| prop, sync | • | prop_sync |
| fethr, mode | • | fethr_mode |
| puffr, power | • | puffr_power |
| water, scoop | • | water_scoop |
| arrst, hook | • | arrst_hook |
| chute, deply | • | chute_deply |
Annunciators: general |
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| mast, cau | • | mast_cau |
| mast, war | • | mast_war |
| mast, accp | • | mast_accp |
| auto, disco | • | auto_disco |
| low, vacum | • | low_vacum |
| low, volt | • | low_volt |
| fuel, quant | • | fuel_quant |
| hyd, press | • | hyd_press |
Annunciators: general |
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| yawda, on | • | yawda_on |
| sbrk, on | • | sbrk_on |
| GPWS, warn | • | GPWS_warn |
| ice, warn | • | ice_warn |
| pitot, off | • | pitot_off |
| cabin, althi | • | cabin_althi |
| afthr, arm | • | afthr_arm |
| ospd, time | • | ospd_time |
Annunciators: engine |
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| fuel, press | • | fuel_press |
| oil, press | • | oil_press |
| oil, temp | • | oil_temp |
| inver, warn | • | inver_warn |
| gener, warn | • | gener_warn |
| chip, detec | • | chip_detec |
| engin, fire | • | engin_fire |
| ignit, 0/1 | • | ignit_0_1 |
Armed autopilot functions (autopilot arms) |
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| nav, arm | • | nav_arm |
| alt, arm | • | alt_arm |
| app, arm | • | app_arm |
| vnav, enab | • | vnav_enab |
| vnav, arm | • | vnav_arm |
| vnav, time | • | vnav_time |
| gp, enabl | • | gp_enabl |
| app, typ | • | app_typ |
Autopilot modes |
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| auto, throt | • | auto_throt |
| mode, hding | • | mode_hding |
| mode, alt | • | mode_alt |
| bac, 0/1 | • | bac_0_1 |
| app, | • | app_ |
| sync, butn | • | sync_butn |
Autopilot values |
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| set, speed | The desired speed setting for the autopilot. | set_speed |
| set, hding | The desired heading setting for the autopilot. | set_hding |
| set, vvi | The desired vertical velocity setting for the autopilot. | set_vvi |
| dial, alt | • | dial_alt |
| vnav, alt | • | vnav_alt |
| use, alt | • | use_alt |
| sync, roll | • | sync_roll |
| sync, pitch | • | sync_pitch |
Weapon status |
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| hdng, delta | • | hdng_delta |
| pitch, delta | • | pitch_delta |
| R, d/sec | • | R_d_sec |
| Q, d/sec | • | Q_d_sec |
| rudd, ratio | • | rudd_ratio |
| elev, ratio | • | elev_ratio |
| V, kts | • | V_kts |
| dis, ft | • | dist_ft |
Pressurization status |
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| alt, set | • | alt_set |
| vvi, set | • | vvi_set |
| alt, act | • | alt_act |
| vvi, act | • | vvi_act |
| test, time | • | test_time |
| diff, psi | • | diff_psi |
| dump, all | • | dump_all |
| bleed, src | • | bleed_src |
Auxiliary power unit and ground power unit status (APU/GPU status) |
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| APU, eqipd | • | APU_eqipd |
| APU, swtch | • | APU_swtch |
| APU, runng | • | APU_runng |
| APU, N1 | • | APU_N1 |
| APU, genrt | • | APU_genrt |
| GPU, power | • | GPU_power |
Radar status |
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| targ, selct | The status of the target selection. | targ_selct |
Hydraulic status |
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| hydr, pumpn | The status of hydraulic pump n. | hydr_pump_n |
| hydr, qtyn | The hydraulic fluid in pump n. | hydr_qty_n |
| hydr, presn | The pressure of hydraulic pump n. | hydr_pres_n |
Electrical and solar power status (elec & solar status) |
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| busn, amp | Bus n’s amperage. | bus_n_amp |
| busn, volt | Bus n’s voltage. | bus_n_volt |
| engin, in W | • | engin_in_W |
| solar, out W | • | solar_out_W |
| batt, w-hr | • | batt_w_hr |
| Cross, tie | • | Cross_tie |
Icing status 1 |
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| inlet, ice | • | inlet_ice |
| prop, ice | • | prop_ice |
| pitot, ice | • | pitot_ice |
| statc, ice | • | statc_ice |
Icing status 2 |
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| aoa, ice | • | aoa_ice |
| lwing, ice | • | lwing_ice |
| rwing, ice | • | rwing_ice |
| windo, ice | • | windo_ice |
Warning status |
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| warn, time | • | warn_time |
| caut, time | • | caut_time |
| warn, work | • | warn_work |
| caut, work | • | caut_work |
| gear, work | • | gear_work |
| gear, warn | • | gear_warn |
| stall, warn | • | stall_warn |
| VRS, ratio | • | VRS_ratio |
Flight plan legs (flite-plan legs) |
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| leg, # | • | leg__ |
| leg, type | • | leg_type |
| leg, lat | • | leg_lat |
| leg, lon | • | leg_lon |
Hardware options |
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| pedal, nobrk | • | pedal_nobrk |
| pedal, wibrk | • | pedal_wibrk |
| yoke, PFC | • | yoke_PFC |
| pedal, PFC | • | pedal_PFC |
| throt, PFC | • | throt_PFC |
| cecon, PFC | • | cecon_PFC |
| switc, PFC | • | switc_PFC |
| btogg, PFC | • | btogg_PFC |
Camera location |
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| camra, lon | The camera’s longitudinal location. | camra_lon |
| camra, lat | The camera’s latitudinal location. | camra_lat |
| camra, ele | The camera’s elevation. | camra_ele |
| camra, hdg | The camera’s heading. | camra_hdg |
| camra, pitch | The camera’s pitch. | camra_pitch |
| camra, roll | The camera’s roll. | camra_roll |
| camra, clou | The camera’s cloud cover. | camra_clou |
Ground location |
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| cntr, X | • | cntr_X |
| cntr, Y | • | cntr_Y |
| cntr, Z | • | cntr_Z |
| slope, X | • | slope_X |
| slope, Z | • | slope_Z |
Climb statistics (climb stats) |
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| h-spd, kt | • | h_spd_kt |
| v-spd, fpm | • | v_spd_fpm |
| mult, VxVVI | • | mult_VxVVI |
Cruise statistics (cruise stats) |
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| ff, pph | • | ff_pph |
| ff, gph | • | ff_gph |
| speed, mph | • | speed_mph |
| eta, smpg | • | eta_smpg |
| eta, nm/lb | • | eta_nm_lb |
| range, sm | • | range_sm |
| endur, hours | • | endur_hours |
| mult, VxMPG | • | mult_VxMPG |