Dataset Viewer
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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
End of preview. Expand in Data Studio

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

  1. A mechanistic simulator produces telemetry from sampled aircraft, battery, sensor and environment state. Fault events change those latent parameters, never the telemetry directly.
  2. Labels are read from the event log afterwards, so the fault class never builds the telemetry.
  3. Facts are derived from the telemetry against fixed thresholds.
  4. Qwen/Qwen2.5-0.5B-Instruct rewrites those facts as an operator report, using a system prompt, few-shot examples, a JSON output format and explicit constraints.
  5. 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

Why model outputs were rejected

Model-written share per fault class

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

How each class is described by its text

Reports in TF-IDF space, coloured by class

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

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

Words per report

Top content words and Zipf plot

Top content words and Zipf plot

Word cloud

Word cloud

Signal families mentioned together

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

Telemetry correlations

Similarity between fault signatures

Similarity between fault signatures

Persistence of fault evidence across windows

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_mitigation and approved_inspection are 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 generator
  • 02_dataset_and_eda.ipynb - this analysis
  • manifest.json - seed, model revision, row counts and SHA-256 of each file
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