Datasets:
incident_id string | flight_id string | dataset_kind string | window_index int64 | window_seconds int64 | flight_phase string | fault_class string | flight_fault_class string | severity string | severity_ordinal int64 | severity_score float64 | active_mechanisms_json string | active_families_json string | scheduled_events_json string | fault_onset_window int64 | is_compound bool | domain_shift bool | source_type string | approved_mitigation string | approved_inspection string | physics_validation_status string | action_training_eligible bool | consequence_control float64 | consequence_power float64 | consequence_navigation float64 | consequence_altitude float64 | altitude_mean_m float64 | commanded_speed_mean_mps float64 | voltage_mean_v float64 | voltage_min_v float64 | voltage_slope_v_s float64 | current_mean_a float64 | motor_output_mean float64 | motor_output_std float64 | motor_imbalance float64 | accel_rms_g float64 | gyro_rms_dps float64 | attitude_error_mean_deg float64 | vibration_rms_g float64 | gps_satellites_mean int64 | gps_hdop_mean float64 | position_innovation_mean_m float64 | baro_altitude_std_m float64 | altitude_residual_mean_m float64 | vertical_speed_error_mean_mps float64 | wind_estimate_mean_mps float64 | qwen_source_evidence_json string | evidence_hash string | symptom_report string | report_generation_method string | report_validator_pass bool | report_retry_count int64 | report_source_run string | report_model string | report_model_revision string | prompt_version string |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
SYN5-7ADD0B85420F | FLT5-0003E1F7E4F1 | causal_benchmark | 0 | 5 | hover | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.129503 | 0 | 0.094741 | 0.05072 | 47.848338 | 0.009012 | 16.069825 | 15.952155 | -0.018984 | 10.963761 | 0.344191 | 0.025656 | 0.02446 | 1.089361 | 10.281036 | 1.129244 | 0.044031 | 19 | 0.745322 | 0.710557 | 0.212611 | 0.329678 | 0.169875 | 1.853065 | {"row_id": "SYN5-7ADD0B85420F", "phase": "hover", "state": "steady", "allowed_facts": ["satellite reception stayed strong", "vertical tracking stayed consistent"], "allowed_domains": ["altitude", "navigation"], "style_hint": "use concise technical wording"} | dd64ca380f1c034194e995d83ce2c7154799e176f9f1edab4d99c23d2a85456f | During hover, satellite reception was strong and vertical tracking was consistent throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-B6B0E0A18410 | FLT5-0003E1F7E4F1 | causal_benchmark | 1 | 5 | acceleration | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.169338 | 0 | 0.076743 | 0.071564 | 48.048466 | 7.884121 | 15.343126 | 15.213701 | -0.037829 | 27.740855 | 0.660557 | 0.040286 | 0.071122 | 1.342164 | 13.697935 | 0.916549 | 0.047531 | 18 | 0.746365 | 0.57557 | 0.300567 | 0.380098 | 0.206015 | 1.78948 | {"row_id": "SYN5-B6B0E0A18410", "phase": "acceleration", "state": "irregular", "allowed_facts": ["voltage sat lower than in the previous window"], "allowed_domains": ["power"], "style_hint": "use a compact flight-log style"} | a2c08565a9a2d2aa5f3e444a04311b5c894265aa75fcba57be351f2c0d02af58 | Voltage sat was lower than in the previous window during acceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-E4B208DEB209 | FLT5-0003E1F7E4F1 | causal_benchmark | 2 | 5 | circling | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.203565 | 0 | 0.081542 | 0.086872 | 47.727083 | 5.555973 | 15.358034 | 15.185469 | -0.014745 | 23.112163 | 0.567873 | 0.027059 | 0.033574 | 1.21359 | 19.338694 | 1.169986 | 0.039616 | 20 | 0.748047 | 0.611563 | 0.257277 | 0.413429 | 0.295364 | 1.307719 | {"row_id": "SYN5-E4B208DEB209", "phase": "circling", "state": "steady", "allowed_facts": ["the power draw stayed even", "voltage held its level"], "allowed_domains": ["power"], "style_hint": "begin with the strongest observation"} | 63c80c6b6b495facdd0ff82cbf8ba8b6219dad911388ebefdb3aa86099343fa9 | The power draw remained even and voltage held its level during circling. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-B9F0C1AFD928 | FLT5-0003E1F7E4F1 | causal_benchmark | 3 | 5 | circling | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.225373 | 0 | 0.076594 | 0.076614 | 47.670126 | 5.019276 | 15.688738 | 15.593418 | -0.022866 | 20.04552 | 0.54298 | 0.035561 | 0.043682 | 1.223753 | 21.410412 | 0.881439 | 0.056543 | 17 | 0.772007 | 0.574454 | 0.277503 | 0.497992 | 0.172581 | 2.325997 | {"row_id": "SYN5-B9F0C1AFD928", "phase": "circling", "state": "steady", "allowed_facts": ["the vertical profile stayed smooth", "the aircraft held a steady attitude"], "allowed_domains": ["altitude", "attitude"], "style_hint": "state the observation directly"} | 1522511e0eb01719e9deda2ded06d36b1fadf21d96301debb81aed7eab2b46b1 | The circling flight maintained a smooth vertical profile with the aircraft remaining in a steady attitude throughout the observation. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-5695AD92D6EA | FLT5-0003E1F7E4F1 | causal_benchmark | 4 | 5 | deceleration | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.147775 | 0 | 0.076501 | 0.068018 | 47.579633 | 3.490825 | 15.562719 | 15.5116 | -0.036373 | 18.999397 | 0.489415 | 0.0375 | 0.062065 | 1.245168 | 11.876038 | 0.84404 | 0.046501 | 17 | 0.868614 | 0.573759 | 0.285676 | 0.39371 | 0.200653 | 1.967628 | {"row_id": "SYN5-5695AD92D6EA", "phase": "deceleration", "state": "steady", "allowed_facts": ["vibration stayed low", "wind conditions stayed mild", "vertical tracking stayed consistent"], "allowed_domains": ["altitude", "motion", "wind"], "style_hint": "lead with aircraft behavior"} | fb621c41d5df8851ac6751d829dc1b2c1903da2cdc3bb3a0192980d15bc45300 | Vibration stayed low, wind conditions stayed mild, and vertical tracking was consistent during deceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-00F84A1AF5F6 | FLT5-000A0B7E04C2 | causal_benchmark | 0 | 5 | hover | environmental_disturbance | environmental_disturbance | low | 1 | 0.627632 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-C4B74EEC6306", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.6943836888951876}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.209211 | 0 | 0.090267 | 0.084752 | 25.746439 | 0.390619 | 16.276127 | 16.159686 | -0.029895 | 15.267423 | 0.425152 | 0.043301 | 0.050367 | 1.179913 | 12.597518 | 1.343672 | 0.071132 | 18 | 0.752138 | 0.677005 | 0.355957 | 0.410432 | 0.240286 | 5.023541 | {"row_id": "SYN5-00F84A1AF5F6", "phase": "hover", "state": "steady", "allowed_facts": ["altitude residual stayed small", "satellite coverage held steady", "altitude readings held steady"], "allowed_domains": ["altitude", "navigation"], "style_hint": "begin with the strongest observation"} | 9594ab6d073126b9798390aa363280f20846e795bfdf31e4c23058c7777b13b7 | Altitude residual was small, satellite coverage was steady, and altitude readings were steady during hover. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-1D3DCE2BD114 | FLT5-000A0B7E04C2 | causal_benchmark | 1 | 5 | waypoint | environmental_disturbance | environmental_disturbance | low | 1 | 0.568902 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-C4B74EEC6306", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.6943836888951876}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.189634 | 0.032386 | 0.070183 | 0.105435 | 25.679229 | 5.543948 | 15.675578 | 15.585393 | -0.04842 | 30.066663 | 0.632919 | 0.057671 | 0.064333 | 1.239207 | 14.202047 | 1.310638 | 0.064476 | 20 | 0.799683 | 0.526374 | 0.442828 | 0.356571 | 0.219589 | 6.242147 | {"row_id": "SYN5-1D3DCE2BD114", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["voltage continued falling from the previous window", "estimated wind increased"], "allowed_domains": ["power", "wind"], "style_hint": "state the observation directly"} | d525bf779c47327b56d900dd85d1f1a67d84e90e9600b272dee00b8381f1de24 | Voltage dropped below the previous window's level, and estimated wind increased during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-5170AA29F224 | FLT5-000A0B7E04C2 | causal_benchmark | 2 | 5 | circling | environmental_disturbance | environmental_disturbance | low | 1 | 0.743575 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-C4B74EEC6306", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.6943836888951876}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.247858 | 0 | 0.069353 | 0.109324 | 25.341035 | 5.502784 | 15.791666 | 15.675474 | -0.034703 | 26.811457 | 0.661299 | 0.058234 | 0.079535 | 1.369705 | 23.54654 | 1.426639 | 0.067422 | 17 | 0.91842 | 0.52015 | 0.45916 | 0.51127 | 0.250654 | 6.867542 | {"row_id": "SYN5-5170AA29F224", "phase": "circling", "state": "irregular", "allowed_facts": ["rotation rates stayed above their usual band", "acceleration readings drifted outside their usual band", "estimated wind picked up"], "allowed_domains": ["motion", "wind"], "style_hint": "use an as-clause"} | 6dd1b47e1b09eb3725bf5958c9cd10fbe8746462836708323094aa827dcd28aa | Rotation rates remained above their usual band, acceleration readings drifted outside their usual band, and estimated wind picked up during circling. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-0DE100D69351 | FLT5-000A0B7E04C2 | causal_benchmark | 3 | 5 | waypoint | environmental_disturbance | environmental_disturbance | low | 1 | 0.818661 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-C4B74EEC6306", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.6943836888951876}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.272887 | 0 | 0.076072 | 0.127959 | 25.46736 | 4.813769 | 15.35902 | 15.219914 | -0.030698 | 30.728294 | 0.667638 | 0.079261 | 0.114613 | 1.337135 | 18.008413 | 1.896946 | 0.077355 | 20 | 0.825309 | 0.570538 | 0.537427 | 0.643973 | 0.200626 | 8.936309 | {"row_id": "SYN5-0DE100D69351", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["estimated wind picked up"], "allowed_domains": ["wind"], "style_hint": "use a compact flight-log style"} | e6bfb9613c507320da71d73a47f2be90126fa0e0db8058e2422a6d4aeaafd8bc | During waypoint flight, estimated wind picked up noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-09DC78084324 | FLT5-000A0B7E04C2 | causal_benchmark | 4 | 5 | deceleration | environmental_disturbance | environmental_disturbance | low | 1 | 0.759769 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-C4B74EEC6306", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.6943836888951876}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.253256 | 0 | 0.082621 | 0.115792 | 25.484233 | 4.158415 | 15.854949 | 15.642217 | -0.021176 | 25.358613 | 0.636359 | 0.082485 | 0.106368 | 1.492856 | 19.488781 | 2.211239 | 0.084412 | 17 | 0.924511 | 0.619655 | 0.486328 | 0.57267 | 0.197445 | 10.685493 | {"row_id": "SYN5-09DC78084324", "phase": "deceleration", "state": "irregular", "allowed_facts": ["wind estimates ran higher through the window", "acceleration measurements varied unusually"], "allowed_domains": ["motion", "wind"], "style_hint": "use plain operator wording"} | c86520154bcf8b4bbdfefbc37d7cf95a659c64b8d649f25d1b131a982e137577 | During deceleration, wind estimates increased through the window while acceleration measurements varied unusually. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-CF754B6DF56D | FLT5-0034760BE01A | causal_benchmark | 0 | 5 | hover | gps_positioning | gps_positioning | low | 1 | 0.508372 | ["gps_visibility_loss"] | ["gps_positioning"] | [{"event_id": "EVT-9E5D7F88D636", "mechanism": "gps_visibility_loss", "start_window": 0, "strength": 0.9200192091840724}] | 0 | false | false | causal_synthetic_v5 | Switch to a non-GPS-dependent flight mode and avoid tight waypoint tracking. | Check antenna placement and shielding, and review the flight area for obstruction and multipath sources. | empirical_cases_unmapped_to_v5_equations | false | 0.169457 | 0 | 0.130625 | 0.060809 | 29.686245 | 0.261667 | 15.878492 | 15.701004 | -0.010064 | 17.178851 | 0.389742 | 0.025256 | 0.034672 | 1.103297 | 10.574185 | 1.291881 | 0.057616 | 14 | 1.076768 | 0.979686 | 0.205621 | 0.395256 | 0.201783 | 3.237911 | {"row_id": "SYN5-CF754B6DF56D", "phase": "hover", "state": "steady", "allowed_facts": ["altitude residual stayed small", "power delivery held steady", "the aircraft kept its orientation"], "allowed_domains": ["altitude", "attitude", "power"], "style_hint": "lead with the telemetry trend"} | 3fad27e700482e5de52099e1abc2f1edb24937d559f0e1ec67cd19db3179efe5 | During hover, altitude residual remained small, power delivery was steady, and the aircraft maintained its orientation. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-1C43506118AB | FLT5-0034760BE01A | causal_benchmark | 1 | 5 | waypoint | gps_positioning | gps_positioning | low | 1 | 0.617031 | ["gps_visibility_loss"] | ["gps_positioning"] | [{"event_id": "EVT-9E5D7F88D636", "mechanism": "gps_visibility_loss", "start_window": 0, "strength": 0.9200192091840724}] | 0 | false | false | causal_synthetic_v5 | Switch to a non-GPS-dependent flight mode and avoid tight waypoint tracking. | Check antenna placement and shielding, and review the flight area for obstruction and multipath sources. | empirical_cases_unmapped_to_v5_equations | false | 0.16562 | 0 | 0.205677 | 0.077901 | 29.556725 | 5.882702 | 15.623663 | 15.45485 | -0.009023 | 23.61666 | 0.595321 | 0.039418 | 0.06903 | 1.199026 | 12.214059 | 1.26251 | 0.056311 | 13 | 1.30653 | 1.542577 | 0.302565 | 0.506358 | 0.187126 | 2.695846 | {"row_id": "SYN5-1C43506118AB", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["position disagreement widened"], "allowed_domains": ["navigation"], "style_hint": "use plain operator wording"} | 83217789434b1187d3b75581f3f392fad8de5c4307e170dccc47bf8005f62472 | During waypoint flight, position disagreement widened noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-A4266D87243B | FLT5-0034760BE01A | causal_benchmark | 2 | 5 | circling | gps_positioning | gps_positioning | low | 1 | 0.856118 | ["gps_visibility_loss"] | ["gps_positioning"] | [{"event_id": "EVT-9E5D7F88D636", "mechanism": "gps_visibility_loss", "start_window": 0, "strength": 0.9200192091840724}] | 0 | false | false | causal_synthetic_v5 | Switch to a non-GPS-dependent flight mode and avoid tight waypoint tracking. | Check antenna placement and shielding, and review the flight area for obstruction and multipath sources. | empirical_cases_unmapped_to_v5_equations | false | 0.227522 | 0 | 0.285373 | 0.093654 | 29.43481 | 5.311003 | 15.539115 | 15.416623 | -0.018517 | 25.433454 | 0.5841 | 0.039824 | 0.071998 | 1.203591 | 21.614634 | 1.096773 | 0.061377 | 13 | 1.607486 | 2.140296 | 0.321017 | 0.608754 | 0.217042 | 2.411098 | {"row_id": "SYN5-A4266D87243B", "phase": "circling", "state": "irregular", "allowed_facts": ["position disagreement widened"], "allowed_domains": ["navigation"], "style_hint": "use chronological wording"} | caf3a3a9b4b15ca04fe66d05f68426d4f9d1319896509e4bdd8f976839b0c64c | Position disagreement widened during circling flight as it became more challenging to maintain consistent positions. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-8715F6DB6560 | FLT5-0034760BE01A | causal_benchmark | 3 | 5 | waypoint | gps_positioning | gps_positioning | medium | 2 | 1.202365 | ["gps_visibility_loss"] | ["gps_positioning"] | [{"event_id": "EVT-9E5D7F88D636", "mechanism": "gps_visibility_loss", "start_window": 0, "strength": 0.9200192091840724}] | 0 | false | false | causal_synthetic_v5 | Switch to a non-GPS-dependent flight mode and avoid tight waypoint tracking. | Check antenna placement and shielding, and review the flight area for obstruction and multipath sources. | empirical_cases_unmapped_to_v5_equations | false | 0.18125 | 0 | 0.400788 | 0.081252 | 29.672262 | 6.466632 | 15.523263 | 15.320793 | -0.037552 | 29.064292 | 0.628957 | 0.031898 | 0.057198 | 1.192446 | 12.464737 | 1.394865 | 0.061625 | 12 | 1.722457 | 3.005913 | 0.297433 | 0.528141 | 0.154816 | 3.10554 | {"row_id": "SYN5-8715F6DB6560", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["position disagreement increased from the previous window", "position disagreement widened"], "allowed_domains": ["navigation"], "style_hint": "state the observation directly"} | 943b784daa8bfe144d87ed3d504731c354c433e1df88537e6e3f0e857215dbd4 | Position disagreement increased from the previous waypoint flight, widening it across the observation window. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-8ECF505F50F8 | FLT5-0034760BE01A | causal_benchmark | 4 | 5 | deceleration | gps_positioning | gps_positioning | medium | 2 | 1.584227 | ["gps_visibility_loss"] | ["gps_positioning"] | [{"event_id": "EVT-9E5D7F88D636", "mechanism": "gps_visibility_loss", "start_window": 0, "strength": 0.9200192091840724}] | 0 | false | false | causal_synthetic_v5 | Switch to a non-GPS-dependent flight mode and avoid tight waypoint tracking. | Check antenna placement and shielding, and review the flight area for obstruction and multipath sources. | empirical_cases_unmapped_to_v5_equations | false | 0.16931 | 0 | 0.528076 | 0.088677 | 29.576154 | 3.693876 | 15.676948 | 15.509375 | -0.002777 | 21.617222 | 0.519051 | 0.025168 | 0.033982 | 1.281797 | 12.493085 | 0.922224 | 0.057565 | 9 | 2.195404 | 3.960568 | 0.254508 | 0.576401 | 0.191241 | 1.560031 | {"row_id": "SYN5-8ECF505F50F8", "phase": "deceleration", "state": "irregular", "allowed_facts": ["the position innovation widened through the window", "positioning precision slipped", "satellite availability decreased", "position innovation rose from the previous window"], "allowed_domains": ["navigation"], "style_hint... | e60ba13b8b762a9b7c1ab572996d76ed755e768831bc65b1d0f01f431f5d83de | Positioning precision slipped, satellite availability decreased, and position innovation rose from the previous window during deceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-FA857F86B34E | FLT5-0034794C532D | causal_benchmark | 0 | 5 | hover | barometer_altitude | barometer_altitude | low | 1 | 0.377827 | ["barometer_bias_drift"] | ["barometer_altitude"] | [{"event_id": "EVT-514B46FE7905", "mechanism": "barometer_bias_drift", "start_window": 0, "strength": 0.533800379652458}] | 0 | false | false | causal_synthetic_v5 | Treat reported altitude as unreliable and maintain a larger vertical safety margin. | Check the barometer port for blockage and airflow exposure, and verify altitude-sensor fusion settings. | empirical_cases_unmapped_to_v5_equations | false | 0.125942 | 0 | 0.095827 | 0.123675 | 28.326507 | 0.560159 | 15.617754 | 15.471927 | -0.032213 | 18.399303 | 0.454847 | 0.01866 | 0.022086 | 1.175435 | 9.902235 | 1.253017 | 0.04282 | 17 | 0.86188 | 0.718701 | 0.38506 | 0.803886 | 0.244169 | 2.544006 | {"row_id": "SYN5-FA857F86B34E", "phase": "hover", "state": "steady", "allowed_facts": ["voltage held its level", "motor loading held level"], "allowed_domains": ["motor", "power"], "style_hint": "use a compact flight-log style"} | a986bd43667aee44e080dba0adc37bb9faaa873a831bfbaed2844c60df1a2fb6 | Voltage held its level during hover while motor loading remained constant. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-8AA357BA4F8B | FLT5-0034794C532D | causal_benchmark | 1 | 5 | acceleration | barometer_altitude | barometer_altitude | medium | 2 | 1.276709 | ["barometer_bias_drift"] | ["barometer_altitude"] | [{"event_id": "EVT-514B46FE7905", "mechanism": "barometer_bias_drift", "start_window": 0, "strength": 0.533800379652458}] | 0 | false | false | causal_synthetic_v5 | Treat reported altitude as unreliable and maintain a larger vertical safety margin. | Check the barometer port for blockage and airflow exposure, and verify altitude-sensor fusion settings. | empirical_cases_unmapped_to_v5_equations | false | 0.154143 | 0.074529 | 0.088086 | 0.42557 | 28.384418 | 7.601427 | 15.017761 | 14.945463 | -0.045006 | 36.863234 | 0.734394 | 0.020482 | 0.029865 | 1.374374 | 14.643616 | 1.197585 | 0.043446 | 17 | 0.804103 | 0.660642 | 0.447057 | 2.766203 | 0.266999 | 3.188291 | {"row_id": "SYN5-8AA357BA4F8B", "phase": "acceleration", "state": "irregular", "allowed_facts": ["voltage slid below the previous window", "acceleration behaved unusually across the window", "altitude residual increased"], "allowed_domains": ["altitude", "motion", "power"], "style_hint": "lead with the telemetry trend"... | bdf5fe54a3b51ac89567fd8f483016b5590f8e3bec83395f9adc59d85258e731 | Voltage slid below the previous window, acceleration behaved unusually across the window, and altitude residual increased during acceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-27D20CCDCE24 | FLT5-0034794C532D | causal_benchmark | 2 | 5 | velocity | barometer_altitude | barometer_altitude | high | 3 | 2.389533 | ["barometer_bias_drift"] | ["barometer_altitude"] | [{"event_id": "EVT-514B46FE7905", "mechanism": "barometer_bias_drift", "start_window": 0, "strength": 0.533800379652458}] | 0 | false | false | causal_synthetic_v5 | Treat reported altitude as unreliable and maintain a larger vertical safety margin. | Check the barometer port for blockage and airflow exposure, and verify altitude-sensor fusion settings. | empirical_cases_unmapped_to_v5_equations | false | 0.227146 | 0.04331 | 0.089452 | 0.796511 | 28.678854 | 8.789643 | 15.083911 | 14.908918 | -0.031137 | 36.082753 | 0.753003 | 0.046866 | 0.095401 | 1.26494 | 13.980569 | 1.035119 | 0.060082 | 17 | 0.850696 | 0.670887 | 0.448106 | 5.177321 | 0.21798 | 3.287517 | {"row_id": "SYN5-27D20CCDCE24", "phase": "cruise", "state": "irregular", "allowed_facts": ["the altitude residual ran above its usual band"], "allowed_domains": ["altitude"], "style_hint": "lead with the telemetry trend"} | c7db8e4f5f2e4af1b40f2adaf470ee47d6738e095d8eab34dc0a153425a9e358 | During cruise, the altitude residual ran above its usual band noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-A67A301A45E4 | FLT5-0034794C532D | causal_benchmark | 3 | 5 | waypoint | barometer_altitude | barometer_altitude | high | 3 | 3 | ["barometer_bias_drift"] | ["barometer_altitude"] | [{"event_id": "EVT-514B46FE7905", "mechanism": "barometer_bias_drift", "start_window": 0, "strength": 0.533800379652458}] | 0 | false | false | causal_synthetic_v5 | Treat reported altitude as unreliable and maintain a larger vertical safety margin. | Check the barometer port for blockage and airflow exposure, and verify altitude-sensor fusion settings. | empirical_cases_unmapped_to_v5_equations | false | 0.157254 | 0.01818 | 0.095392 | 1.291812 | 28.739596 | 5.804599 | 15.183924 | 15.098323 | -0.044727 | 30.177744 | 0.654376 | 0.022139 | 0.030921 | 1.210683 | 11.974679 | 1.076128 | 0.053467 | 18 | 0.802591 | 0.71544 | 0.411082 | 8.396776 | 0.244555 | 3.433109 | {"row_id": "SYN5-A67A301A45E4", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["the altitude residual ran above its usual band"], "allowed_domains": ["altitude"], "style_hint": "put the phase at the end"} | 8b5014c60c7c25ebc867a8f9896324b0a570bf98d7f8d660eb2ec09d9680dc14 | The altitude residual ran above its usual band during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-3794B65D30A4 | FLT5-0034794C532D | causal_benchmark | 4 | 5 | deceleration | barometer_altitude | barometer_altitude | high | 3 | 3 | ["barometer_bias_drift"] | ["barometer_altitude"] | [{"event_id": "EVT-514B46FE7905", "mechanism": "barometer_bias_drift", "start_window": 0, "strength": 0.533800379652458}] | 0 | false | false | causal_synthetic_v5 | Treat reported altitude as unreliable and maintain a larger vertical safety margin. | Check the barometer port for blockage and airflow exposure, and verify altitude-sensor fusion settings. | empirical_cases_unmapped_to_v5_equations | false | 0.128966 | 0 | 0.086628 | 1.892481 | 28.544137 | 4.611065 | 15.078945 | 14.970573 | -0.036456 | 30.717162 | 0.616692 | 0.025535 | 0.038422 | 1.2955 | 12.251784 | 1.059624 | 0.041521 | 19 | 0.807446 | 0.649708 | 0.407791 | 12.301126 | 0.2037 | 3.409398 | {"row_id": "SYN5-3794B65D30A4", "phase": "deceleration", "state": "irregular", "allowed_facts": ["the altitude residual ran above its usual band"], "allowed_domains": ["altitude"], "style_hint": "use concise technical wording"} | 49b36e0710e322aa3003df1e93d84bdd7d6c9231e4b0111d79a85299596fafbf | The altitude residual ran above its usual band during deceleration. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-2BC02186E952 | FLT5-00516990A651 | causal_benchmark | 0 | 5 | hover | low_voltage | low_voltage | low | 1 | 0.458625 | ["battery_resistance_growth"] | ["low_voltage"] | [{"event_id": "EVT-09B477792CDF", "mechanism": "battery_resistance_growth", "start_window": 0, "strength": 0.2661179017081604}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.152875 | 0 | 0.071918 | 0.072535 | 18.323637 | 0.29518 | 15.626378 | 15.539725 | -0.021668 | 15.089307 | 0.401825 | 0.022287 | 0.032963 | 1.184558 | 14.523111 | 1.438114 | 0.049927 | 18 | 0.880405 | 0.539384 | 0.304645 | 0.302664 | 0.214783 | 3.44551 | {"row_id": "SYN5-2BC02186E952", "phase": "hover", "state": "steady", "allowed_facts": ["satellite reception stayed strong", "rotation rates remained gentle", "motor outputs tracked one another"], "allowed_domains": ["motion", "motor", "navigation"], "style_hint": "use chronological wording"} | d3f0a0215209954268007410db6e8399ffd9b75912130efc57f902057c5c7918 | During hover, satellite reception remained strong, rotation rates were gentle, and motor outputs tracked each other throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-4532D6C38AA9 | FLT5-00516990A651 | causal_benchmark | 1 | 5 | acceleration | low_voltage | low_voltage | low | 1 | 0.523146 | ["battery_resistance_growth"] | ["low_voltage"] | [{"event_id": "EVT-09B477792CDF", "mechanism": "battery_resistance_growth", "start_window": 0, "strength": 0.2661179017081604}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.174382 | 0 | 0.078983 | 0.10049 | 18.204639 | 8.05012 | 15.083412 | 14.947587 | -0.019034 | 32.479284 | 0.736198 | 0.029772 | 0.049968 | 1.413954 | 16.566299 | 0.959976 | 0.055254 | 17 | 0.843514 | 0.59237 | 0.422059 | 0.504113 | 0.194395 | 3.729905 | {"row_id": "SYN5-4532D6C38AA9", "phase": "acceleration", "state": "irregular", "allowed_facts": ["acceleration measurements varied unusually", "voltage sat lower than in the previous window"], "allowed_domains": ["motion", "power"], "style_hint": "use a while-clause"} | 3bee0c2abeb378203e306224149839a1915c210ff228e92e30d924d13ded8112 | Voltage sat was lower than in the previous window during acceleration measurements, varying unusually. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-578D44E343A0 | FLT5-00516990A651 | causal_benchmark | 2 | 5 | velocity | low_voltage | low_voltage | low | 1 | 0.586495 | ["battery_resistance_growth"] | ["low_voltage"] | [{"event_id": "EVT-09B477792CDF", "mechanism": "battery_resistance_growth", "start_window": 0, "strength": 0.2661179017081604}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.195498 | 0 | 0.074063 | 0.103303 | 18.278359 | 9.581614 | 14.778222 | 14.653095 | -0.015783 | 34.221536 | 0.779547 | 0.037902 | 0.067229 | 1.233696 | 15.577082 | 1.047556 | 0.066469 | 19 | 0.958105 | 0.555475 | 0.433872 | 0.581342 | 0.180083 | 3.27683 | {"row_id": "SYN5-578D44E343A0", "phase": "cruise", "state": "steady", "allowed_facts": ["motor outputs remained balanced", "motor loading held level"], "allowed_domains": ["motor"], "style_hint": "use a while-clause"} | 65ee7d3c83b717979d995b0ce2e85481995cee82faec0c270310dfd911bf29e7 | During cruise, motor outputs remained balanced while motor loading held level throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-1914887709C9 | FLT5-00516990A651 | causal_benchmark | 3 | 5 | waypoint | low_voltage | low_voltage | low | 1 | 0.597008 | ["battery_resistance_growth"] | ["low_voltage"] | [{"event_id": "EVT-09B477792CDF", "mechanism": "battery_resistance_growth", "start_window": 0, "strength": 0.2661179017081604}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.199003 | 0 | 0.109667 | 0.106258 | 18.538661 | 6.275204 | 14.806204 | 14.680627 | -0.026988 | 30.800667 | 0.631541 | 0.026376 | 0.038117 | 1.213533 | 13.802489 | 0.920477 | 0.067661 | 18 | 0.792771 | 0.822504 | 0.446282 | 0.515223 | 0.172859 | 3.599574 | {"row_id": "SYN5-1914887709C9", "phase": "waypoint flight", "state": "steady", "allowed_facts": ["the aircraft held a steady attitude", "altitude tracking remained stable"], "allowed_domains": ["altitude", "attitude"], "style_hint": "lead with the telemetry trend"} | 9da3c692965d1db8e6f7b40d1b34dbfa94a74368b60662a41d5b65583b66ca9c | The aircraft held a steady attitude and altitude tracking remained stable during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-B2796B517BA3 | FLT5-00516990A651 | causal_benchmark | 4 | 5 | deceleration | low_voltage | low_voltage | low | 1 | 0.455268 | ["battery_resistance_growth"] | ["low_voltage"] | [{"event_id": "EVT-09B477792CDF", "mechanism": "battery_resistance_growth", "start_window": 0, "strength": 0.2661179017081604}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.151756 | 0 | 0.064484 | 0.082494 | 18.632634 | 3.423011 | 15.010554 | 14.976644 | -0.008729 | 22.607102 | 0.548636 | 0.026151 | 0.03334 | 1.30847 | 14.416824 | 1.227018 | 0.051505 | 16 | 0.927825 | 0.483626 | 0.346475 | 0.497535 | 0.176129 | 3.784638 | {"row_id": "SYN5-B2796B517BA3", "phase": "deceleration", "state": "steady", "allowed_facts": ["wind conditions stayed mild", "aircraft orientation held steady", "the position solution stayed firm"], "allowed_domains": ["attitude", "navigation", "wind"], "style_hint": "use a compact flight-log style"} | 7434d6cf2992d0af62656a414853363d67975a7b842ef28d13ea29683cae6234 | During deceleration, wind conditions remained mild, the aircraft's orientation was steady, and the position solution remained firm. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-896713A258EE | FLT5-00AD49C2644E | causal_benchmark | 0 | 5 | hover | environmental_disturbance | environmental_disturbance | low | 1 | 0.551201 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-69FBAEF02EC7", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.5782602616773894}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.183734 | 0 | 0.061325 | 0.1073 | 37.796551 | 0.496396 | 15.686793 | 15.629122 | -0.018651 | 19.961687 | 0.427136 | 0.043699 | 0.072963 | 1.211521 | 11.195035 | 1.485879 | 0.062469 | 19 | 0.766596 | 0.459937 | 0.450661 | 0.508446 | 0.203768 | 5.154194 | {"row_id": "SYN5-896713A258EE", "phase": "hover", "state": "steady", "allowed_facts": ["power delivery held steady", "vibration stayed within its usual band"], "allowed_domains": ["motion", "power"], "style_hint": "use plain operator wording"} | e0a42849b5146bed30c7a2d8b369ae3e2d3b7862de45aa0ccda58dce2fc5b315 | Power delivery was steady during hover while vibration stayed within its usual band. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-2CE3A0C82BAA | FLT5-00AD49C2644E | causal_benchmark | 1 | 5 | acceleration | environmental_disturbance | environmental_disturbance | low | 1 | 0.637618 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-69FBAEF02EC7", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.5782602616773894}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.212539 | 0 | 0.061752 | 0.115537 | 37.928574 | 6.587082 | 15.368988 | 15.195276 | -0.016972 | 28.534689 | 0.688152 | 0.055273 | 0.064056 | 1.510107 | 20.191231 | 1.821135 | 0.065863 | 17 | 0.803049 | 0.463139 | 0.485257 | 0.427788 | 0.241839 | 8.369866 | {"row_id": "SYN5-2CE3A0C82BAA", "phase": "acceleration", "state": "irregular", "allowed_facts": ["estimated wind ran above its usual band", "acceleration measurements wandered from their usual range"], "allowed_domains": ["motion", "wind"], "style_hint": "lead with aircraft behavior"} | 7bb8ff59f57c6f4f3ac193d40e654e93002dd7369bf84e319982e28cf7238597 | During acceleration, estimated wind ran above its usual band while acceleration measurements wandered from their usual range throughout the observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-53FD6AEFC6D2 | FLT5-00AD49C2644E | causal_benchmark | 2 | 5 | waypoint | environmental_disturbance | environmental_disturbance | low | 1 | 0.480056 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-69FBAEF02EC7", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.5782602616773894}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.160019 | 0 | 0.070496 | 0.114404 | 37.697887 | 5.984083 | 15.352527 | 15.21051 | -0.008721 | 25.416464 | 0.634998 | 0.036141 | 0.053755 | 1.195333 | 14.760362 | 1.368288 | 0.054406 | 19 | 0.806512 | 0.528718 | 0.480498 | 0.470981 | 0.198455 | 6.16233 | {"row_id": "SYN5-53FD6AEFC6D2", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["the wind estimate climbed through the window"], "allowed_domains": ["wind"], "style_hint": "begin with the strongest observation"} | 0f3e7c233a2c7d9e5a582c3a6981819f4ca863523f8ac4f4dc4cb33a693ea1cf | The wind estimate climbed through the window during waypoint flight. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-688C6850532C | FLT5-00AD49C2644E | causal_benchmark | 3 | 5 | circling | environmental_disturbance | environmental_disturbance | low | 1 | 0.900713 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-69FBAEF02EC7", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.5782602616773894}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.300238 | 0 | 0.080358 | 0.12066 | 37.537988 | 4.980793 | 15.350265 | 15.120786 | -0.022682 | 27.169796 | 0.69375 | 0.073711 | 0.094437 | 1.416727 | 28.522578 | 2.211435 | 0.083808 | 20 | 0.823037 | 0.602683 | 0.506771 | 0.496814 | 0.179291 | 10.42568 | {"row_id": "SYN5-688C6850532C", "phase": "circling", "state": "irregular", "allowed_facts": ["estimated wind picked up", "measured rotation rates were elevated", "acceleration readings sat outside their everyday band"], "allowed_domains": ["motion", "wind"], "style_hint": "begin with the strongest observation"} | 41c076a31ca9c1444103c02e2fbc5c56f5f3863506bf918f347f66afe10eca12 | Estimated wind picked up, measured rotation rates were elevated, and acceleration readings sat outside their everyday band during circling. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-FF537223E9C1 | FLT5-00AD49C2644E | causal_benchmark | 4 | 5 | deceleration | environmental_disturbance | environmental_disturbance | low | 1 | 0.596246 | ["wind_gust_event"] | ["environmental_disturbance"] | [{"event_id": "EVT-69FBAEF02EC7", "mechanism": "wind_gust_event", "start_window": 0, "strength": 0.5782602616773894}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.198749 | 0 | 0.064335 | 0.117626 | 37.120051 | 3.380578 | 15.460219 | 15.206234 | -0.032222 | 24.687659 | 0.604846 | 0.057202 | 0.07814 | 1.434449 | 18.334312 | 1.898146 | 0.067575 | 20 | 0.89866 | 0.482515 | 0.494029 | 0.465625 | 0.224472 | 9.908356 | {"row_id": "SYN5-FF537223E9C1", "phase": "deceleration", "state": "irregular", "allowed_facts": ["estimated wind ran above its usual band", "acceleration measurements varied unusually"], "allowed_domains": ["motion", "wind"], "style_hint": "lead with aircraft behavior"} | 83273fcc9cccf4f2bea5f5300e6a686e01a62bfd4929b76298634395ad19ab69 | The aircraft decelerated unexpectedly, with estimated wind speeds above its usual band and varying acceleration measurements. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-EE8C9D6DADAD | FLT5-00B471557224 | causal_benchmark | 0 | 5 | hover | imu | imu | low | 1 | 0.387695 | ["imu_gyro_bias"] | ["imu"] | [{"event_id": "EVT-25B0CEB40077", "mechanism": "imu_gyro_bias", "start_window": 0, "strength": 0.3850070912581666}] | 0 | false | false | causal_synthetic_v5 | Avoid rapid attitude changes and prefer stable flight modes until the estimate settles. | Recalibrate the IMU on a level surface and inspect vibration isolation of the flight controller. | selected_direct_anchor_only | false | 0.129232 | 0 | 0.127047 | 0.092172 | 45.929759 | 0.396915 | 15.63173 | 15.460217 | -0.017886 | 20.279444 | 0.447251 | 0.025759 | 0.029671 | 1.148259 | 10.641559 | 1.517691 | 0.043939 | 16 | 1.131911 | 0.952854 | 0.38712 | 0.439132 | 0.195017 | 4.925321 | {"row_id": "SYN5-EE8C9D6DADAD", "phase": "hover", "state": "steady", "allowed_facts": ["the vertical profile stayed smooth", "voltage remained steady", "motor outputs remained balanced"], "allowed_domains": ["altitude", "motor", "power"], "style_hint": "use a compact flight-log style"} | c9e9c7a9d8743706d9e50fdba540fd95f7c0f68636335f5cd12cf41645ec061a | The vertical profile was smooth, voltage was steady, and motor outputs were balanced during hover. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-4668804F2197 | FLT5-00B471557224 | causal_benchmark | 1 | 5 | acceleration | imu | imu | low | 1 | 0.545735 | ["imu_gyro_bias"] | ["imu"] | [{"event_id": "EVT-25B0CEB40077", "mechanism": "imu_gyro_bias", "start_window": 0, "strength": 0.3850070912581666}] | 0 | false | false | causal_synthetic_v5 | Avoid rapid attitude changes and prefer stable flight modes until the estimate settles. | Recalibrate the IMU on a level surface and inspect vibration isolation of the flight controller. | selected_direct_anchor_only | false | 0.181912 | 0 | 0.13187 | 0.107458 | 46.11085 | 7.247024 | 15.310248 | 15.198818 | -0.02881 | 31.562509 | 0.712854 | 0.033474 | 0.05806 | 1.395638 | 17.281606 | 1.778818 | 0.042555 | 16 | 1.010548 | 0.989024 | 0.451325 | 0.568908 | 0.206494 | 3.880341 | {"row_id": "SYN5-4668804F2197", "phase": "acceleration", "state": "irregular", "allowed_facts": ["acceleration behaved unusually across the window"], "allowed_domains": ["motion"], "style_hint": "use a compact flight-log style"} | d842b5f92e6b70579c3b7b39b45b8632858d9b3d73c6994454fcc0d412bfb19c | During acceleration, acceleration behaved unusually across the window noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-7485224E77F1 | FLT5-00B471557224 | causal_benchmark | 2 | 5 | velocity | imu | imu | low | 1 | 0.537525 | ["imu_gyro_bias"] | ["imu"] | [{"event_id": "EVT-25B0CEB40077", "mechanism": "imu_gyro_bias", "start_window": 0, "strength": 0.3850070912581666}] | 0 | false | false | causal_synthetic_v5 | Avoid rapid attitude changes and prefer stable flight modes until the estimate settles. | Recalibrate the IMU on a level surface and inspect vibration isolation of the flight controller. | selected_direct_anchor_only | false | 0.179175 | 0 | 0.139749 | 0.109283 | 46.146873 | 8.190325 | 15.043714 | 14.960291 | -0.03844 | 34.450072 | 0.713896 | 0.027282 | 0.0399 | 1.246309 | 17.02162 | 1.626606 | 0.040867 | 17 | 1.072285 | 1.048121 | 0.458988 | 0.597031 | 0.181682 | 4.17142 | {"row_id": "SYN5-7485224E77F1", "phase": "cruise", "state": "steady", "allowed_facts": ["vibration stayed within its usual band", "estimated wind held light through the window", "rotation rates remained gentle"], "allowed_domains": ["motion", "wind"], "style_hint": "use concise technical wording"} | 5940c96dcdb0955fc04b6680f05ce69e318626bf147cc91d436d08c86a8ce477 | Vibration stayed within its usual band, estimated wind held light through the window, and rotation rates remained gentle during cruise. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-B09101972C91 | FLT5-00B471557224 | causal_benchmark | 3 | 5 | waypoint | imu | imu | low | 1 | 0.629097 | ["imu_gyro_bias"] | ["imu"] | [{"event_id": "EVT-25B0CEB40077", "mechanism": "imu_gyro_bias", "start_window": 0, "strength": 0.3850070912581666}] | 0 | false | false | causal_synthetic_v5 | Avoid rapid attitude changes and prefer stable flight modes until the estimate settles. | Recalibrate the IMU on a level surface and inspect vibration isolation of the flight controller. | selected_direct_anchor_only | false | 0.209699 | 0 | 0.129891 | 0.122167 | 46.289133 | 6.786447 | 15.228967 | 15.093816 | -0.023727 | 31.853407 | 0.695292 | 0.034226 | 0.051425 | 1.198433 | 17.329734 | 2.516387 | 0.046595 | 16 | 1.07969 | 0.974186 | 0.513101 | 0.70001 | 0.246148 | 3.063427 | {"row_id": "SYN5-B09101972C91", "phase": "waypoint flight", "state": "steady", "allowed_facts": ["motor outputs remained balanced", "estimated wind held light through the window"], "allowed_domains": ["motor", "wind"], "style_hint": "state the observation directly"} | fd2578762d3c1a55a531f8dca614e0f096a9f250d36c628c2cd210b6efbec9a8 | Motor outputs remained balanced and estimated wind held light through the window during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-2E9055EE17EE | FLT5-00B471557224 | causal_benchmark | 4 | 5 | deceleration | imu | imu | low | 1 | 0.67835 | ["imu_gyro_bias"] | ["imu"] | [{"event_id": "EVT-25B0CEB40077", "mechanism": "imu_gyro_bias", "start_window": 0, "strength": 0.3850070912581666}] | 0 | false | false | causal_synthetic_v5 | Avoid rapid attitude changes and prefer stable flight modes until the estimate settles. | Recalibrate the IMU on a level surface and inspect vibration isolation of the flight controller. | selected_direct_anchor_only | false | 0.226117 | 0 | 0.13731 | 0.103496 | 46.272211 | 3.805095 | 15.505005 | 15.495005 | -0.02488 | 26.962431 | 0.589468 | 0.031375 | 0.052058 | 1.309793 | 20.149727 | 2.713399 | 0.046313 | 17 | 1.032933 | 1.029822 | 0.434682 | 0.563566 | 0.212403 | 4.530784 | {"row_id": "SYN5-2E9055EE17EE", "phase": "deceleration", "state": "steady", "allowed_facts": ["altitude residual stayed small", "vertical tracking stayed consistent"], "allowed_domains": ["altitude"], "style_hint": "use concise technical wording"} | a5f1420f283a487ba46a41d70077db0daba0905b79254132368f11d4ddf8474e | The aircraft experienced deceleration with small altitude residuals and consistent vertical tracking throughout the observation. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-6145DAD5026F | FLT5-00DBAD84EA33 | causal_benchmark | 0 | 5 | hover | motor_propeller | motor_propeller | low | 1 | 0.537607 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-A38A4DBEB54A", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.6859527509775085}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.179202 | 0 | 0.08051 | 0.071124 | 23.283456 | 0.596142 | 16.234169 | 16.050293 | -0.029623 | 16.903489 | 0.402105 | 0.032712 | 0.044198 | 1.097863 | 11.706341 | 0.941187 | 0.060929 | 19 | 0.717851 | 0.603822 | 0.29872 | 0.44058 | 0.221895 | 3.104331 | {"row_id": "SYN5-6145DAD5026F", "phase": "hover", "state": "steady", "allowed_facts": ["estimated wind remained moderate", "aircraft orientation held steady", "satellite coverage held steady"], "allowed_domains": ["attitude", "navigation", "wind"], "style_hint": "begin with the strongest observation"} | 69eff3574baa1b419cbd1a57b75ec5717a020f26bf83881270fd2b12bdacda81 | The aircraft's orientation was steady, and satellite coverage was strong during the hover phase. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-C613C8A4D0C9 | FLT5-00DBAD84EA33 | causal_benchmark | 1 | 5 | waypoint | motor_propeller | motor_propeller | low | 1 | 0.481755 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-A38A4DBEB54A", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.6859527509775085}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.160585 | 0.005078 | 0.063316 | 0.0775 | 23.503564 | 5.629252 | 15.568253 | 15.375559 | -0.04132 | 28.168473 | 0.612724 | 0.039405 | 0.067006 | 1.158883 | 12.218904 | 1.291972 | 0.054599 | 17 | 0.732224 | 0.474867 | 0.3255 | 0.431576 | 0.17336 | 3.117594 | {"row_id": "SYN5-C613C8A4D0C9", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["voltage fell from the previous window"], "allowed_domains": ["power"], "style_hint": "lead with aircraft behavior"} | 6bcc12a954da30168fe0cc320bf95bae5894537176320a8413b1d556317c5ab9 | During waypoint flight, voltage fell from the previous window noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-535571EF58B4 | FLT5-00DBAD84EA33 | causal_benchmark | 2 | 5 | circling | motor_propeller | motor_propeller | medium | 2 | 1.274843 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-A38A4DBEB54A", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.6859527509775085}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.424948 | 0 | 0.061891 | 0.072465 | 23.306328 | 4.910341 | 15.559395 | 15.386531 | -0.031202 | 29.281391 | 0.611293 | 0.083059 | 0.178478 | 1.268658 | 20.957883 | 1.596169 | 0.070735 | 16 | 0.74234 | 0.464181 | 0.304354 | 0.454394 | 0.221361 | 3.149392 | {"row_id": "SYN5-535571EF58B4", "phase": "circling", "state": "irregular", "allowed_facts": ["the motors ran at uneven output"], "allowed_domains": ["motor"], "style_hint": "state the observation directly"} | 88733d8945c25d3dc4c01dd8c611edf8bb18d1843d71ad21412d07fc67736869 | During circling, the motors ran at uneven output noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-F20AEBDB4DDB | FLT5-00DBAD84EA33 | causal_benchmark | 3 | 5 | waypoint | motor_propeller | motor_propeller | medium | 2 | 1.414426 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-A38A4DBEB54A", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.6859527509775085}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.471475 | 0.056944 | 0.058519 | 0.080185 | 23.33012 | 6.065208 | 15.487957 | 15.372401 | -0.054805 | 31.782147 | 0.664818 | 0.090565 | 0.19802 | 1.122108 | 14.513865 | 1.562943 | 0.084749 | 19 | 0.718142 | 0.438891 | 0.336778 | 0.36333 | 0.194141 | 3.174226 | {"row_id": "SYN5-F20AEBDB4DDB", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["motor outputs became uneven"], "allowed_domains": ["motor"], "style_hint": "use chronological wording"} | 4f409c38ee950c0c51a5913e1911d88feb532b97dd58376b80f37174f4716d95 | During waypoint flight, motor outputs became uneven noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-7290A42E00ED | FLT5-00DBAD84EA33 | causal_benchmark | 4 | 5 | deceleration | motor_propeller | motor_propeller | medium | 2 | 1.67383 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-A38A4DBEB54A", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.6859527509775085}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.557943 | 0 | 0.078508 | 0.074878 | 23.166167 | 4.670969 | 15.486929 | 15.32987 | -0.031551 | 28.717229 | 0.622451 | 0.108226 | 0.234336 | 1.264904 | 13.526309 | 1.160851 | 0.080189 | 16 | 0.897974 | 0.58881 | 0.314487 | 0.369261 | 0.174121 | 2.639916 | {"row_id": "SYN5-7290A42E00ED", "phase": "deceleration", "state": "irregular", "allowed_facts": ["motor-output variation was elevated", "one motor ran harder than the others"], "allowed_domains": ["motor"], "style_hint": "use a compact flight-log style"} | d11995834fba1f8ab3f511d644ad968556bf6dcb9707c4fe0358c41090af5eda | During deceleration, motor-output variation was elevated, with one motor running harder than the others. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-900D1F20FBCC | FLT5-00E4D0D7C35B | causal_benchmark | 0 | 5 | hover | environmental_disturbance | environmental_disturbance | low | 1 | 0.42172 | ["turbulence_burst"] | ["environmental_disturbance"] | [{"event_id": "EVT-F32FDA6920E0", "mechanism": "turbulence_burst", "start_window": 0, "strength": 0.34932294262165936}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.140573 | 0 | 0.105069 | 0.09454 | 39.312382 | 0.935272 | 15.571273 | 15.519249 | -0.019526 | 16.060442 | 0.407312 | 0.027211 | 0.040723 | 1.111464 | 10.91089 | 1.087875 | 0.047795 | 19 | 0.986968 | 0.788021 | 0.361161 | 0.614509 | 0.267787 | 1.116103 | {"row_id": "SYN5-900D1F20FBCC", "phase": "hover", "state": "steady", "allowed_facts": ["satellite reception stayed strong", "motor outputs remained balanced"], "allowed_domains": ["motor", "navigation"], "style_hint": "put the phase at the end"} | c92d966f12f45037a03b152d01042f72a04905e17f42788b5395b6577051de24 | During hover, satellite reception was strong while motor outputs were maintained at their balanced levels. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-9ECA38B7EB5B | FLT5-00E4D0D7C35B | causal_benchmark | 1 | 5 | acceleration | environmental_disturbance | environmental_disturbance | low | 1 | 0.502927 | ["turbulence_burst"] | ["environmental_disturbance"] | [{"event_id": "EVT-F32FDA6920E0", "mechanism": "turbulence_burst", "start_window": 0, "strength": 0.34932294262165936}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.167642 | 0 | 0.110218 | 0.108765 | 39.453001 | 7.929558 | 14.986377 | 14.926101 | -0.020004 | 31.569698 | 0.679905 | 0.041693 | 0.07041 | 1.337831 | 13.576085 | 1.033706 | 0.056644 | 18 | 0.902673 | 0.826632 | 0.438267 | 0.706975 | 0.235742 | 1.066554 | {"row_id": "SYN5-9ECA38B7EB5B", "phase": "acceleration", "state": "irregular", "allowed_facts": ["voltage fell from the previous window"], "allowed_domains": ["power"], "style_hint": "begin with the flight phase"} | bd5c8c0498076e8527eac83e2884d053f719878385e53b38624e004c4c3448d1 | During acceleration, voltage fell from the previous window noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-14376C442962 | FLT5-00E4D0D7C35B | causal_benchmark | 2 | 5 | waypoint | environmental_disturbance | environmental_disturbance | low | 1 | 0.559853 | ["turbulence_burst"] | ["environmental_disturbance"] | [{"event_id": "EVT-F32FDA6920E0", "mechanism": "turbulence_burst", "start_window": 0, "strength": 0.34932294262165936}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.186618 | 0 | 0.119179 | 0.09675 | 39.507215 | 5.350796 | 15.306317 | 15.111324 | -0.018981 | 23.61295 | 0.548548 | 0.043091 | 0.065636 | 1.17038 | 12.395055 | 1.877073 | 0.06345 | 18 | 0.970145 | 0.893843 | 0.40635 | 0.601828 | 0.300073 | 1.647073 | {"row_id": "SYN5-14376C442962", "phase": "waypoint flight", "state": "steady", "allowed_facts": ["vibration stayed within its usual band", "navigation indicators remained consistent"], "allowed_domains": ["motion", "navigation"], "style_hint": "use an as-clause"} | 56ef72ef5b6041de6079c01964b7151ca3a0ee03365411b8a9fd5e8465200044 | Vibration stayed within its usual band and navigation indicators remained consistent during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-B6B367F569E3 | FLT5-00E4D0D7C35B | causal_benchmark | 3 | 5 | circling | environmental_disturbance | environmental_disturbance | low | 1 | 0.635361 | ["turbulence_burst"] | ["environmental_disturbance"] | [{"event_id": "EVT-F32FDA6920E0", "mechanism": "turbulence_burst", "start_window": 0, "strength": 0.34932294262165936}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.211787 | 0 | 0.102574 | 0.100146 | 39.221726 | 5.018056 | 15.305139 | 15.106156 | -0.022418 | 25.733662 | 0.554344 | 0.031903 | 0.034147 | 1.200789 | 20.119776 | 1.323265 | 0.053816 | 18 | 0.879892 | 0.769301 | 0.420615 | 0.607665 | 0.298449 | 2.148708 | {"row_id": "SYN5-B6B367F569E3", "phase": "circling", "state": "steady", "allowed_facts": ["altitude tracking remained stable", "the position solution stayed firm", "rotation rates remained gentle"], "allowed_domains": ["altitude", "motion", "navigation"], "style_hint": "use plain operator wording"} | 08146405f3ce6ed809cebea958fec73df511b18cc13ff2a617b33dcc92a0b2a1 | Circling, altitude tracking remained stable, position solution remained firm, and rotation rates were gentle. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-4D5B4388DCE4 | FLT5-00E4D0D7C35B | causal_benchmark | 4 | 5 | deceleration | environmental_disturbance | environmental_disturbance | low | 1 | 0.550857 | ["turbulence_burst"] | ["environmental_disturbance"] | [{"event_id": "EVT-F32FDA6920E0", "mechanism": "turbulence_burst", "start_window": 0, "strength": 0.34932294262165936}] | 0 | false | false | causal_synthetic_v5 | Reduce airspeed, increase attitude margins and consider postponing the mission window. | No airframe defect implied; review wind and turbulence conditions for the flight window. | no_direct_fault_anchor_in_current_project | false | 0.183619 | 0 | 0.117797 | 0.0953 | 39.027393 | 3.711768 | 15.334336 | 15.209449 | -0.013981 | 24.325065 | 0.533997 | 0.052917 | 0.070861 | 1.267028 | 13.705463 | 1.331259 | 0.06243 | 18 | 0.939107 | 0.883476 | 0.400261 | 0.564241 | 0.243758 | 2.532084 | {"row_id": "SYN5-4D5B4388DCE4", "phase": "deceleration", "state": "steady", "allowed_facts": ["position innovation stayed small", "vertical tracking stayed consistent"], "allowed_domains": ["altitude", "navigation"], "style_hint": "begin with the strongest observation"} | 4cb4c9ba04e4ed6cb8919f74f258619a4a74eb38bc7b70fed813612a86e5a931 | During deceleration, vertical tracking remained consistent while position innovation was small. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-551963689614 | FLT5-0125D1B26C2E | causal_benchmark | 0 | 5 | hover | motor_propeller | motor_propeller | low | 1 | 0.696783 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-BA86BAC8A0CA", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.8456626483635479}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.232261 | 0 | 0.12943 | 0.083243 | 36.407215 | 0.685251 | 15.434064 | 15.315334 | -0.014134 | 17.112259 | 0.388301 | 0.046803 | 0.09755 | 1.072956 | 9.547952 | 0.857756 | 0.056264 | 18 | 0.820953 | 0.970725 | 0.349622 | 0.474643 | 0.199214 | 1.419887 | {"row_id": "SYN5-551963689614", "phase": "hover", "state": "steady", "allowed_facts": ["voltage remained steady", "motor loading held level"], "allowed_domains": ["motor", "power"], "style_hint": "use a while-clause"} | 94d922a22c38130b47610547cdde2834c9c33f3f4abd21d0a39a1275becb3beb | During hover, voltage remained steady while motor loading was held at a level throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-85B4535F97F4 | FLT5-0125D1B26C2E | causal_benchmark | 1 | 5 | waypoint | motor_propeller | motor_propeller | medium | 2 | 1.243744 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-BA86BAC8A0CA", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.8456626483635479}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.414581 | 0 | 0.109929 | 0.090311 | 36.648195 | 5.58272 | 14.972807 | 14.836827 | -0.032758 | 25.179281 | 0.576913 | 0.075453 | 0.174124 | 1.124637 | 12.744719 | 0.805662 | 0.068736 | 18 | 0.831571 | 0.824469 | 0.379306 | 0.509532 | 0.19111 | 0.467437 | {"row_id": "SYN5-85B4535F97F4", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["voltage dropped below the previous window", "motor output imbalance grew"], "allowed_domains": ["motor", "power"], "style_hint": "use a compact flight-log style"} | e46a7760bab2cbe750deeff24d38e1785a0f2f7bba35131d3dd129e369fb5e28 | Voltage dropped below the previous window and motor output imbalance grew during waypoint flight across the window. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-E9ED98D251FB | FLT5-0125D1B26C2E | causal_benchmark | 2 | 5 | circling | motor_propeller | motor_propeller | medium | 2 | 1.364119 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-BA86BAC8A0CA", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.8456626483635479}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.454706 | 0 | 0.118025 | 0.086405 | 36.37384 | 4.43494 | 14.952638 | 14.82808 | -0.032784 | 26.793649 | 0.566866 | 0.088389 | 0.190977 | 1.215512 | 20.665809 | 0.916773 | 0.073685 | 17 | 0.83218 | 0.885186 | 0.362899 | 0.391713 | 0.244066 | 1.553374 | {"row_id": "SYN5-E9ED98D251FB", "phase": "circling", "state": "irregular", "allowed_facts": ["one motor ran harder than the others"], "allowed_domains": ["motor"], "style_hint": "use plain operator wording"} | ee84a265ea3c2dcf2b260a29d73afae3896f246eb0244d947d65d4a4584e68fc | One motor ran harder than the others during circling maneuver. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-1F2334E76C4A | FLT5-0125D1B26C2E | causal_benchmark | 3 | 5 | waypoint | motor_propeller | motor_propeller | high | 3 | 2.191136 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-BA86BAC8A0CA", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.8456626483635479}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.730379 | 0 | 0.096125 | 0.102454 | 36.332205 | 6.448902 | 14.749514 | 14.665353 | -0.032936 | 30.74379 | 0.653518 | 0.130003 | 0.306759 | 1.101579 | 14.661771 | 1.286262 | 0.095896 | 18 | 0.91218 | 0.720938 | 0.430308 | 0.444226 | 0.243338 | 1.224258 | {"row_id": "SYN5-1F2334E76C4A", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["spread across motor outputs widened", "one motor ran harder than the others"], "allowed_domains": ["motor"], "style_hint": "use plain operator wording"} | 60e9d3bb255b727c8fab487bf0f37e786ff2b159c3f62fda31cb71ed2d808531 | The spread across motor outputs widened, with one motor running harder than the others, during waypoint flight. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-92D34F9EA8CA | FLT5-0125D1B26C2E | causal_benchmark | 4 | 5 | deceleration | motor_propeller | motor_propeller | high | 3 | 2.491533 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-BA86BAC8A0CA", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.8456626483635479}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.830511 | 0 | 0.093112 | 0.087788 | 36.25903 | 4.239735 | 14.676201 | 14.523422 | -0.015713 | 29.617115 | 0.59191 | 0.149112 | 0.348815 | 1.21079 | 14.422153 | 1.589836 | 0.099314 | 17 | 0.883763 | 0.69834 | 0.368711 | 0.380644 | 0.203387 | 0.874243 | {"row_id": "SYN5-92D34F9EA8CA", "phase": "deceleration", "state": "irregular", "allowed_facts": ["one motor ran harder than the others", "motor-output variation was elevated"], "allowed_domains": ["motor"], "style_hint": "state the observation directly"} | 5ef44b240b5f13de544c816cd168c97a81f70ad6aad16bf0d99de11b0d5f86e0 | One motor ran harder than the others, and motor-output variation was elevated during deceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-303C87CF5EA0 | FLT5-013A39711250 | causal_benchmark | 0 | 5 | hover | low_voltage | low_voltage | low | 1 | 0.414945 | ["battery_soc_depletion"] | ["low_voltage"] | [{"event_id": "EVT-EAD54B70504E", "mechanism": "battery_soc_depletion", "start_window": 0, "strength": 0.7976407705831466}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.138315 | 0 | 0.12551 | 0.08267 | 27.980571 | 0.344608 | 15.59879 | 15.522811 | -0.000195 | 16.564182 | 0.355677 | 0.017516 | 0.030099 | 1.12348 | 7.730996 | 1.113934 | 0.047027 | 17 | 1.027491 | 0.941327 | 0.347215 | 0.410625 | 0.182818 | 1.881365 | {"row_id": "SYN5-303C87CF5EA0", "phase": "hover", "state": "steady", "allowed_facts": ["voltage remained steady", "motor outputs tracked one another"], "allowed_domains": ["motor", "power"], "style_hint": "use chronological wording"} | dc25ad64a5cdde5b61c33f744a2f189d36f82595174af27e19fd421ffc9ef68e | During hover, voltage remained steady and motor outputs tracked each other as the aircraft continued to move. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-7527D7A49257 | FLT5-013A39711250 | causal_benchmark | 1 | 5 | acceleration | low_voltage | low_voltage | low | 1 | 0.589864 | ["battery_soc_depletion"] | ["low_voltage"] | [{"event_id": "EVT-EAD54B70504E", "mechanism": "battery_soc_depletion", "start_window": 0, "strength": 0.7976407705831466}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.196621 | 0 | 0.105531 | 0.106033 | 28.113888 | 7.766566 | 15.048967 | 14.965664 | -0.029873 | 27.033288 | 0.650708 | 0.036897 | 0.082581 | 1.375247 | 13.318941 | 0.901426 | 0.059454 | 17 | 1.04131 | 0.791483 | 0.44534 | 0.511941 | 0.193028 | 2.021183 | {"row_id": "SYN5-7527D7A49257", "phase": "acceleration", "state": "irregular", "allowed_facts": ["acceleration readings sat outside their everyday band", "voltage slid below the previous window"], "allowed_domains": ["motion", "power"], "style_hint": "use a while-clause"} | b45c3f9a152ab56fa4fe7cf44861a3d7d5ad8bcf47159798becbc96143a31afe | Acceleration readings sat outside their everyday band and voltage slid below the previous window during acceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-562F496AF571 | FLT5-013A39711250 | causal_benchmark | 2 | 5 | velocity | low_voltage | low_voltage | low | 1 | 0.547957 | ["battery_soc_depletion"] | ["low_voltage"] | [{"event_id": "EVT-EAD54B70504E", "mechanism": "battery_soc_depletion", "start_window": 0, "strength": 0.7976407705831466}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.182652 | 0 | 0.124305 | 0.099287 | 28.500638 | 9.110702 | 14.59883 | 14.465715 | -0.017127 | 25.142773 | 0.664093 | 0.03491 | 0.076714 | 1.149956 | 10.525489 | 0.993296 | 0.054508 | 15 | 1.077134 | 0.932289 | 0.417006 | 0.454375 | 0.16917 | 1.907651 | {"row_id": "SYN5-562F496AF571", "phase": "cruise", "state": "irregular", "allowed_facts": ["voltage sat lower than in the previous window"], "allowed_domains": ["power"], "style_hint": "use an as-clause"} | f1c2c517870f12ffb6de0facf69d9eb464ca5e096216b1e7e2175c5f01c34e92 | Voltage sat was lower than in the previous window during cruise. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-A9B0B8163EAA | FLT5-013A39711250 | causal_benchmark | 3 | 5 | circling | low_voltage | low_voltage | low | 1 | 0.634677 | ["battery_soc_depletion"] | ["low_voltage"] | [{"event_id": "EVT-EAD54B70504E", "mechanism": "battery_soc_depletion", "start_window": 0, "strength": 0.7976407705831466}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.211559 | 0.005481 | 0.112551 | 0.100133 | 28.361623 | 4.420125 | 14.169394 | 14.086845 | -0.024339 | 19.741034 | 0.520856 | 0.030082 | 0.06369 | 1.205018 | 20.098118 | 1.037982 | 0.053146 | 18 | 1.124817 | 0.84413 | 0.388526 | 0.650865 | 0.218148 | 1.421399 | {"row_id": "SYN5-A9B0B8163EAA", "phase": "circling", "state": "irregular", "allowed_facts": ["voltage stayed beneath its usual average"], "allowed_domains": ["power"], "style_hint": "use a while-clause"} | eda173beae8e4de70595f1e395405a30a393cdd2f8faea9fe568991718723639 | Voltage stayed below its usual average during circling operation, lasting for several minutes. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-074A2D6D8EFF | FLT5-013A39711250 | causal_benchmark | 4 | 5 | deceleration | low_voltage | low_voltage | medium | 2 | 1.146535 | ["battery_soc_depletion"] | ["low_voltage"] | [{"event_id": "EVT-EAD54B70504E", "mechanism": "battery_soc_depletion", "start_window": 0, "strength": 0.7976407705831466}] | 0 | false | false | causal_synthetic_v5 | Shorten the remaining mission and plan an early recovery while power reserve remains. | Check pack voltage under load, per-cell balance, connector resistance and battery cycle history. | no_direct_fault_anchor_in_current_project | false | 0.178384 | 0.382178 | 0.104857 | 0.086742 | 28.171352 | 4.337044 | 13.218619 | 13.182772 | -0.037558 | 22.558487 | 0.527799 | 0.032537 | 0.073159 | 1.26093 | 11.496608 | 1.084067 | 0.060651 | 16 | 1.170877 | 0.78643 | 0.364317 | 0.491071 | 0.266731 | 1.422485 | {"row_id": "SYN5-074A2D6D8EFF", "phase": "deceleration", "state": "irregular", "allowed_facts": ["voltage dropped below the previous window", "average voltage was unusually low", "voltage bottomed out below its usual floor"], "allowed_domains": ["power"], "style_hint": "use an as-clause"} | 62fb7869f5efa77464a6298084a1bc9922f12ade9cda14d63bee9e7f8ed60257 | Voltage dropped below the previous window, average voltage was unusually low, and voltage bottomed out below its usual floor during deceleration. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-E36EB91AD8EA | FLT5-0148B127D4BE | causal_benchmark | 0 | 5 | hover | motor_propeller | motor_propeller | low | 1 | 0.52721 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-B5E79894DCA1", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.4308597240473051}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.175737 | 0 | 0.139953 | 0.070544 | 42.129183 | 0.390204 | 15.755023 | 15.631359 | -0.016597 | 19.05036 | 0.383388 | 0.030692 | 0.037932 | 1.187457 | 9.567379 | 1.064003 | 0.05975 | 16 | 1.171093 | 1.049648 | 0.296285 | 0.35524 | 0.146932 | 5.214166 | {"row_id": "SYN5-E36EB91AD8EA", "phase": "hover", "state": "steady", "allowed_facts": ["voltage remained steady", "attitude error stayed small"], "allowed_domains": ["attitude", "power"], "style_hint": "use a while-clause"} | 99331b5cc8637eaf6a6beeb291a377221987664d73f5e6cd656d8d6f55e6ca2f | During hover, voltage remained steady while attitude error remained small over the observation window. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-01EA003ECEC9 | FLT5-0148B127D4BE | causal_benchmark | 1 | 5 | acceleration | motor_propeller | motor_propeller | low | 1 | 0.578419 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-B5E79894DCA1", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.4308597240473051}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.192806 | 0 | 0.149406 | 0.093957 | 42.544425 | 7.272488 | 15.568598 | 15.536106 | -0.0131 | 27.192059 | 0.672767 | 0.043038 | 0.071924 | 1.421779 | 15.942061 | 1.917083 | 0.065554 | 17 | 1.095154 | 1.120542 | 0.394617 | 0.420982 | 0.195143 | 4.600577 | {"row_id": "SYN5-01EA003ECEC9", "phase": "acceleration", "state": "irregular", "allowed_facts": ["acceleration measurements wandered from their usual range"], "allowed_domains": ["motion"], "style_hint": "use a while-clause"} | c73f903ea572cd9e7f2bfe4a201a63f9e279441d771d0dba3f3805d43f6afa56 | Accelerations measured ranged widely during acceleration test while maintaining stability. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-1EC230E0E241 | FLT5-0148B127D4BE | causal_benchmark | 2 | 5 | waypoint | motor_propeller | motor_propeller | low | 1 | 0.717259 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-B5E79894DCA1", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.4308597240473051}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.239086 | 0 | 0.153065 | 0.079919 | 42.264426 | 5.3474 | 15.573971 | 15.483464 | -0.027426 | 25.61097 | 0.576376 | 0.058609 | 0.100416 | 1.27831 | 12.5494 | 1.476789 | 0.076613 | 17 | 1.102708 | 1.147987 | 0.335662 | 0.429269 | 0.219236 | 4.674923 | {"row_id": "SYN5-1EC230E0E241", "phase": "waypoint flight", "state": "steady", "allowed_facts": ["motor loading held level", "vertical tracking stayed consistent", "aircraft orientation held steady"], "allowed_domains": ["altitude", "attitude", "motor"], "style_hint": "put the phase at the end"} | 927e65907ca33298c6af95e4cf5110a18bb86663bd3b74501c05b7b1292de990 | During waypoint flight, motor loading was held level, vertical tracking remained consistent, and aircraft orientation was steady. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-E57CE0E093A3 | FLT5-0148B127D4BE | causal_benchmark | 3 | 5 | circling | motor_propeller | motor_propeller | low | 1 | 1.02603 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-B5E79894DCA1", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.4308597240473051}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.34201 | 0 | 0.15855 | 0.079867 | 42.256003 | 4.930469 | 15.74054 | 15.621722 | -0.022564 | 23.598453 | 0.601502 | 0.076034 | 0.143644 | 1.323046 | 21.048604 | 1.244106 | 0.073207 | 18 | 1.071593 | 1.189127 | 0.33544 | 0.43702 | 0.17683 | 4.891591 | {"row_id": "SYN5-E57CE0E093A3", "phase": "circling", "state": "irregular", "allowed_facts": ["motor output imbalance grew"], "allowed_domains": ["motor"], "style_hint": "use a while-clause"} | 2b4e85df3c114d2bca060aba2d97c3d812546779c66c90d2d35a9e982a71b386 | During circling, motor output imbalance grew noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-04493E9E2589 | FLT5-0148B127D4BE | causal_benchmark | 4 | 5 | deceleration | motor_propeller | motor_propeller | medium | 2 | 1.282966 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-B5E79894DCA1", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.4308597240473051}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.427655 | 0 | 0.138705 | 0.090246 | 42.237598 | 3.783355 | 15.5204 | 15.325487 | -0.015946 | 23.457053 | 0.561228 | 0.080981 | 0.179615 | 1.353176 | 13.483604 | 1.62248 | 0.092722 | 16 | 1.052725 | 1.040291 | 0.379035 | 0.450969 | 0.196607 | 4.315717 | {"row_id": "SYN5-04493E9E2589", "phase": "deceleration", "state": "irregular", "allowed_facts": ["acceleration readings drifted outside their usual band", "one motor ran harder than the others"], "allowed_domains": ["motion", "motor"], "style_hint": "use concise technical wording"} | 5c8bc584a85f5db94e0a469d86627ca63e02be84efff248f0603612d43f1d210 | Accelerated readings drifted outside their usual band, one motor ran harder than the others during deceleration. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-9B0F5370DAB8 | FLT5-0172DF34B622 | causal_benchmark | 0 | 5 | hover | motor_propeller | motor_propeller | low | 1 | 0.423553 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-48A7DC4EFFF6", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.41850290629141945}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.141184 | 0 | 0.125458 | 0.06632 | 30.233857 | 0.267521 | 15.441684 | 15.313692 | -0.017665 | 13.820236 | 0.348069 | 0.025492 | 0.038914 | 1.097117 | 8.516986 | 1.143179 | 0.048003 | 16 | 1.011302 | 0.940936 | 0.278543 | 0.342859 | 0.164061 | 2.141729 | {"row_id": "SYN5-9B0F5370DAB8", "phase": "hover", "state": "steady", "allowed_facts": ["aircraft orientation held steady", "wind conditions stayed mild", "satellite reception stayed strong"], "allowed_domains": ["attitude", "navigation", "wind"], "style_hint": "begin with the strongest observation"} | 7ce87497d8b5eb46c2a70c20ab89fde9683e5e9590c6e32c208117fc433b7fae | The aircraft orientation was steady, wind conditions were mild, and satellite reception was strong during the hover phase. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-CC3E3DBDB16B | FLT5-0172DF34B622 | causal_benchmark | 1 | 5 | acceleration | motor_propeller | motor_propeller | low | 1 | 0.510062 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-48A7DC4EFFF6", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.41850290629141945}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.170021 | 0 | 0.096431 | 0.090311 | 30.523399 | 8.785739 | 14.629001 | 14.456543 | -0.026895 | 28.246065 | 0.70235 | 0.03925 | 0.067286 | 1.367432 | 16.151974 | 0.778323 | 0.04928 | 17 | 0.916979 | 0.723236 | 0.379306 | 0.478783 | 0.253873 | 1.841633 | {"row_id": "SYN5-CC3E3DBDB16B", "phase": "acceleration", "state": "irregular", "allowed_facts": ["voltage continued falling from the previous window", "acceleration measurements wandered from their usual range"], "allowed_domains": ["motion", "power"], "style_hint": "begin with the strongest observation"} | f0706cb323c626d5970abd79b336350abbadce4627b367d895f4fd927988cec5 | The voltage dropped from the previous window and the acceleration measurements drifted outside their usual range. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-847C1BBED865 | FLT5-0172DF34B622 | causal_benchmark | 2 | 5 | velocity | motor_propeller | motor_propeller | low | 1 | 0.860068 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-48A7DC4EFFF6", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.41850290629141945}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.286689 | 0 | 0.091657 | 0.084486 | 30.586808 | 9.131316 | 14.600552 | 14.528782 | -0.003068 | 26.817006 | 0.705863 | 0.059562 | 0.12041 | 1.13924 | 12.789703 | 1.304856 | 0.059626 | 17 | 0.9452 | 0.687428 | 0.354842 | 0.465688 | 0.212652 | 1.655762 | {"row_id": "SYN5-847C1BBED865", "phase": "cruise", "state": "steady", "allowed_facts": ["estimated wind held light through the window", "altitude tracking remained stable", "motor outputs remained balanced"], "allowed_domains": ["altitude", "motor", "wind"], "style_hint": "begin with the flight phase"} | 3c114dcc2d60645007c89773c44d230524f9cfb90a605b18903a626430112ae6 | During cruise, estimated wind held light through the window, altitude tracking remained stable, and motor outputs remained balanced. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-45CF96B7EA72 | FLT5-0172DF34B622 | causal_benchmark | 3 | 5 | waypoint | motor_propeller | motor_propeller | low | 1 | 0.973937 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-48A7DC4EFFF6", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.41850290629141945}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.324646 | 0 | 0.110244 | 0.077367 | 30.733974 | 6.605904 | 14.700099 | 14.533627 | -0.011944 | 26.739317 | 0.611942 | 0.066056 | 0.136351 | 1.180724 | 12.756259 | 1.015819 | 0.074139 | 18 | 0.990449 | 0.826829 | 0.324943 | 0.471478 | 0.20582 | 1.802908 | {"row_id": "SYN5-45CF96B7EA72", "phase": "waypoint flight", "state": "irregular", "allowed_facts": ["motor output imbalance grew"], "allowed_domains": ["motor"], "style_hint": "state the observation directly"} | 7b87ff4f0129e4eec1a682cebcaaf1dc791328007288a9fd6e72cad6b40cc6ec | During waypoint flight, motor output imbalance grew noticeably throughout the full observation window. | canonical_grounded_fallback | true | 3 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-26FD6F4B2880 | FLT5-0172DF34B622 | causal_benchmark | 4 | 5 | deceleration | motor_propeller | motor_propeller | medium | 2 | 1.106587 | ["motor_efficiency_loss"] | ["motor_propeller"] | [{"event_id": "EVT-48A7DC4EFFF6", "mechanism": "motor_efficiency_loss", "start_window": 0, "strength": 0.41850290629141945}] | 0 | false | false | causal_synthetic_v5 | Reduce aggressive manoeuvring and return to a controlled hover before continuing. | Inspect propellers for chips, cracks and imbalance, and check motor mounts and bearing play. | selected_direct_anchor_only | false | 0.368862 | 0 | 0.097255 | 0.07365 | 30.628645 | 4.584639 | 14.927645 | 14.799299 | -0.028088 | 23.861971 | 0.55623 | 0.068075 | 0.154922 | 1.271671 | 12.148767 | 1.082977 | 0.069442 | 19 | 1.014367 | 0.729409 | 0.309332 | 0.466388 | 0.194526 | 2.242879 | {"row_id": "SYN5-26FD6F4B2880", "phase": "deceleration", "state": "irregular", "allowed_facts": ["the motors ran at uneven output"], "allowed_domains": ["motor"], "style_hint": "use chronological wording"} | e63f83ea698f9b9d18f8582c79e19902f5a3ff8f3c314a82705a937a3623250b | During deceleration, the motors ran at uneven output, which was noted in the chronological order. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-8DC5C0238997 | FLT5-019231BFE388 | causal_benchmark | 0 | 5 | waypoint | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.133679 | 0 | 0.080129 | 0.070239 | 31.791013 | 6.198054 | 15.757811 | 15.577408 | -0.023501 | 25.587795 | 0.580379 | 0.024583 | 0.032984 | 1.149566 | 11.112058 | 0.707108 | 0.045451 | 16 | 0.837418 | 0.600965 | 0.269204 | 0.360954 | 0.238813 | 1.146006 | {"row_id": "SYN5-8DC5C0238997", "phase": "waypoint flight", "state": "steady", "allowed_facts": ["satellite reception stayed strong", "motor outputs remained balanced"], "allowed_domains": ["motor", "navigation"], "style_hint": "use plain operator wording"} | 835c1ae55ac99e033de4c8ea248a086212b1aa7a244518833752dc9e6a4105d0 | Satellite reception was strong while motor outputs remained balanced during waypoint flight. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-4D9D7E67E991 | FLT5-019231BFE388 | causal_benchmark | 1 | 5 | velocity | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.163259 | 0 | 0.103474 | 0.070279 | 31.624031 | 8.85952 | 15.684527 | 15.518251 | -0.030403 | 29.173725 | 0.678189 | 0.037021 | 0.068569 | 1.12625 | 10.97685 | 0.874971 | 0.052332 | 17 | 1.009164 | 0.776058 | 0.29517 | 0.373656 | 0.156176 | 0.301904 | {"row_id": "SYN5-4D9D7E67E991", "phase": "cruise", "state": "steady", "allowed_facts": ["aircraft orientation held steady", "motor output stayed even across the window"], "allowed_domains": ["attitude", "motor"], "style_hint": "use concise technical wording"} | 6358180efec610074a3e13b8a5e8235ded44784358e08682d9d4090a152a8d14 | During cruise, the aircraft maintained steady orientation and motor output remained consistent across the observation window. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-17B3E358508D | FLT5-019231BFE388 | causal_benchmark | 2 | 5 | circling | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.182103 | 0.045907 | 0.098372 | 0.057551 | 31.547412 | 4.719658 | 15.911169 | 15.722822 | -0.051936 | 23.337514 | 0.542331 | 0.024265 | 0.031253 | 1.190806 | 17.299761 | 1.295931 | 0.045907 | 16 | 0.879206 | 0.737791 | 0.241712 | 0.330176 | 0.150817 | 1.067969 | {"row_id": "SYN5-17B3E358508D", "phase": "circling", "state": "steady", "allowed_facts": ["satellite coverage held steady", "the position solution stayed firm", "rotation rates remained gentle"], "allowed_domains": ["motion", "navigation"], "style_hint": "use a while-clause"} | 326c051e82528b822ebbcf8b51ac02d1c5b9d0a6a1463e74a35ada669a0284e9 | Circling, satellite coverage remained steady, position solution remained firm, and rotation rates were gentle throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-5740C28B0870 | FLT5-019231BFE388 | causal_benchmark | 3 | 5 | velocity | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.146702 | 0 | 0.081559 | 0.072135 | 31.890263 | 9.053079 | 15.5028 | 15.388739 | -0.024462 | 32.24915 | 0.677337 | 0.035029 | 0.055189 | 1.19366 | 11.594141 | 0.624561 | 0.049879 | 18 | 0.841958 | 0.611691 | 0.270891 | 0.310088 | 0.245259 | 0.631518 | {"row_id": "SYN5-5740C28B0870", "phase": "cruise", "state": "steady", "allowed_facts": ["power delivery held steady", "vertical tracking stayed consistent", "estimated wind held light through the window"], "allowed_domains": ["altitude", "power", "wind"], "style_hint": "begin with the strongest observation"} | 92bfeffd7f0aa71ad4adfc343519bc1373b4f98c194e05e4179f3fd9f21aba90 | Power delivery remained steady, vertical tracking was consistent, and estimated wind was light through the window during cruise. | qwen_validated | true | 1 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
SYN5-51616ED31C71 | FLT5-019231BFE388 | causal_benchmark | 4 | 5 | deceleration | normal | normal | none | 0 | 0 | [] | [] | [] | -1 | false | false | causal_synthetic_v5 | No corrective action required; continue the mission profile as planned. | Routine post-flight log review only. | real_informed_baseline_context_only | false | 0.153727 | 0.039042 | 0.083416 | 0.057742 | 31.626459 | 3.925622 | 15.939279 | 15.782524 | -0.050151 | 22.058392 | 0.515484 | 0.037937 | 0.064565 | 1.195709 | 10.178642 | 1.040253 | 0.050336 | 18 | 0.924427 | 0.625618 | 0.20342 | 0.249989 | 0.196322 | 1.240649 | {"row_id": "SYN5-51616ED31C71", "phase": "deceleration", "state": "steady", "allowed_facts": ["voltage remained steady", "attitude tracking stayed close to target"], "allowed_domains": ["attitude", "power"], "style_hint": "use a compact flight-log style"} | a48c7747362fb2d45702429b843dc38100bfa8843e1cbc0480cd3551f2b40277 | During deceleration, voltage remained steady and attitude tracking remained close to target throughout the observation period. | qwen_validated | true | 0 | v5_production_v6 | Qwen/Qwen2.5-0.5B-Instruct | 7ae557604adf67be50417f59c2c2f167def9a775 | v5_observable_evidence_only_production_v1 |
UAV Fault Symptom Reports
A synthetic dataset of UAV flight telemetry paired with operator-style symptom reports written by a language model. Each row is one five-second window of a flight: 20 telemetry channels, the fault class, a severity derived from simulated consequences, and a one-sentence report.
| split | rows | flights | model-written reports | unique reports |
|---|---|---|---|---|
| benchmark | 10,500 | 2,100 | 82.0% | 79.7% |
| challenge | 3,500 | 700 | 88.1% | 91.0% |
benchmark is balanced across seven classes (six fault families plus normal). challenge is harder: mostly normal flights, random fault onset, and some flights with two faults.
How it was generated
- A mechanistic simulator produces telemetry from sampled aircraft, battery, sensor and environment state. Fault events change those latent parameters, never the telemetry directly.
- Labels are read from the event log afterwards, so the fault class never builds the telemetry.
- Facts are derived from the telemetry against fixed thresholds.
Qwen/Qwen2.5-0.5B-Instructrewrites those facts as an operator report, using a system prompt, few-shot examples, a JSON output format and explicit constraints.- Every report is validated: length, no numbers, no diagnosis, no actions, no inferred causes, no signals the model was not given, no chat-style text. Failures are retried twice, then replaced by a templated sentence built from the same facts.
The model never sees the fault class, the severity or the recommended action.
Exploratory data analysis
Instruction-following failures
82.0% of reports were written by the model and accepted. The rest failed validation three times. Rejection reasons across all attempts:
| reason | rejections | share_of_attempts |
|---|---|---|
| Too short / too long | 21821 | 0.275 |
| Other | 5936 | 0.075 |
| Inferred a cause | 5704 | 0.072 |
| Linked observations causally | 4094 | 0.052 |
| Changed what an observation said | 1131 | 0.014 |
| Mentioned a signal it was not given | 914 | 0.012 |
| Ignored the given signals | 824 | 0.01 |
| Invented a number | 309 | 0.004 |
Why model outputs were rejected
Model-written share per fault class
Hallucination
Accepted reports naming a signal they were not given: 0. Reports linking observations causally: 0. Reports changing what an observation says: 0. Earlier runs did contain both: at their worst, 869 reports in one run linked observations causally and 264 changed what an observation said. The validator was extended in response and every failing report was regenerated. 48.2% of accepted reports add no content word beyond their facts.
Inconsistency between text and label
Each report describes one five-second window, and never sees the label. 36.4% of fault windows show no threshold crossing and are described as steady; 15.8% of normal windows cross one during ordinary manoeuvres and are described as irregular. These rows are where the text alone cannot identify the fault.
How each class is described by its text
Reports in TF-IDF space, coloured by class
Duplication, and how the EDA changed the generation
The first full run had 42.8% duplicate reports. The cause was the input: the evidence builder drew from a small fixed pool of facts, which capped how many different reports were possible. Widening the evidence phrasings brought duplicates down to 20.3%. Counting reports that differ only in word order or function words as the same, the near-duplicate rate is 24.5%.
The same review found up to 69 benchmark rows per run whose minimum voltage exceeded their mean voltage, which is impossible. The simulator was corrected; only the affected rows changed.
Every generation run
Read by hand
70 model-written reports, ten per fault class, were read by the team against the facts each was given. This was done on run three, and the rules were tightened in response to what it found, so the counts below describe the run that was reviewed: 36 faithful, 25 uncertain, 7 changed the meaning of a fact, 2 invented a cause. Those three failure modes do not occur in this dataset.
Two habits were recorded rather than treated as errors: a one-sentence report sometimes omits one of several given facts, and sometimes generalises beyond the specific signals it was given.
The cost of stricter rules
Duplicate reports stand at 20.3%. Forbidding a report from inventing a cause, swapping a signal name or adding an intensity word leaves less room to paraphrase the same facts, so reports resemble each other more. Accuracy was preferred over variety, and both are measured here.
Text statistics
Words per report
Top content words and Zipf plot
Word cloud
Signal families mentioned together
Telemetry
Severity is scored per window, so it can escalate within a flight: 43.6% of flights change severity across their five windows, and 92.5% of those only escalate.
Telemetry correlations
Similarity between fault signatures
Persistence of fault evidence across windows
Flagged issues
| issue | type | rows affected | share of rows | handling |
|---|---|---|---|---|
| Model failed its instructions and fell back to a template | instruction following | 1885 | 0.18 | Kept, labelled canonical_grounded_fallback; the sentence states the same facts |
| Accepted report names a signal it was not given | hallucination | 0 | 0 | Blocked by the validator before acceptance |
| Report links observations causally | hallucination | 0 | 0 | Blocked by the validator; up to 869 such reports in an earlier run were regenerated |
| Report changes what an observation says | hallucination | 0 | 0 | Blocked by the validator; up to 264 such reports in an earlier run were regenerated |
| Minimum voltage above mean voltage | telemetry consistency | 0 | 0 | Simulator fixed; up to 69 benchmark rows per run were affected before the fix |
| Fault window described as steady operation | inconsistency (text vs. label) | 2785 | 0.265 | Intended: the fault was not visible in that window. Flagged for the recommendation step |
| Normal window described as irregular | inconsistency (text vs. label) | 201 | 0.019 | Intended: ordinary manoeuvres cross thresholds. Flagged for the recommendation step |
| Exact duplicate report text | duplication | 2128 | 0.203 | Reduced from the first run by widening the evidence (Part F) |
| Near-duplicate report text (differs only in word order or function words) | duplication | 2574 | 0.245 | Flagged; each row still carries its own telemetry, but the text adds little on its own |
| Reports judged unfaithful when read by hand | manual review | 9 | 0.001 | Of 70 reports read from v5_production_v3; the rules were tightened in response and these patterns no longer occur |
| Chat residue in a report | instruction following | 0 | 0 | Blocked by the validator |
Limitations
- The simulator is a transparent mechanistic prototype, not a validated flight-dynamics model.
- Severity is a declared academic rubric, not a certified safety scale.
approved_mitigationandapproved_inspectionare fixed academic placeholders, one per fault family; they are not maintenance procedures.- A report describes one five-second window and never sees the label, so it may omit one of several given facts or describe a fault window as steady when nothing crossed a threshold.
Files
01_synthetic_data_generation.ipynb- the generator02_dataset_and_eda.ipynb- this analysismanifest.json- seed, model revision, row counts and SHA-256 of each file
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