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pdm_rul_001
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD001
I am managing a fleet of aircraft engines and need to know which ones are running on fumes. Can you predict the remaining useful life for all test engines in the CMAPSS FD001 dataset? I need predictions for every unit, verification against the actual RUL values we have, and then tell me which 10 engines are most likely...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
{"problem": "Predict the remaining useful life (RUL) for all test equipment units in the CMAPSS FD001 dataset.", "steps": "1) Load the CMAPSS FD001 training dataset using load_dataset(dataset_name='CMAPSS_FD001', split='train'). 2) Load the corresponding test dataset using load_dataset(dataset_name='CMAPSS_FD001', spli...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 17.6, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_mae": 10.49, "sota_model": "CAELSTM", "sota_rmse": 14.44, "sota_source": "Nature Scientific Reports 2025 - Deep learning-based prognostic approach"}, "expected_m...
{"dependency_analysis": "Sequential dependencies: load_dataset(train) -> provides training data for model training; load_dataset(test) -> provides test units for prediction; load_ground_truth -> required for verification and metric calculation. train_rul_model -> produces model object that must be used in predict_rul c...
pdm_rul_002
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD002
We have got bearing vibration data from CWRU and I need to figure out which bearings are about to give out. Can you predict how much life each test bearing has left, check those predictions against the actual failure times we recorded, and then show me degradation curves for the 5 bearings most at risk? I need the accu...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "detect_degradation_trend", "calculate_rmse" ]
{"problem": "Predict RUL for bearing units in the CWRU dataset and analyze degradation trends.", "steps": "1) Load CWRU training data using load_dataset(dataset_name='CWRU', split='train'). 2) Load CWRU test data using load_dataset(dataset_name='CWRU', split='test'). 3) Load ground truth RUL values. 4) Train a bearing-...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 29.67, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "dataset_characteristics": "6 operating conditions, 1 fault mode (HPC degradation)"}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "Range [10, 25] ...
{"dependency_analysis": "Data loading -> model training -> prediction -> verification -> metric calculation -> visualization. The plot_degradation_trends tool requires both predictions and ground_truth, and operates on the top 5 risk units identified from predictions."}
The question text names CWRU, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_003
rotating_aero
RUL Prediction
Bearing
FEMTO
The FEMTO dataset has bearings running under three different operational scenarios, and I suspect the RUL predictions might vary by scenario. Can you predict remaining life for all test bearings, break down the accuracy (MAE, RMSE) for each of the three operational scenarios separately, and tell me which scenario gives...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "analyze_engine_signals", "calculate_rmse" ]
{"problem": "Predict RUL for bearings in FEMTO dataset across three operational scenarios and compare performance.", "steps": "1) Load FEMTO training data. 2) Load FEMTO test data. 3) Load ground truth RUL. 4) Identify three operational scenarios using identify_operational_scenarios(dataset='FEMTO'). 5) Train scenario-...
{"algorithm_reference": {"baseline_mae": 0.056, "baseline_model": "TCNMABG", "baseline_rmse": 0.082, "baseline_source": "MDPI Applied Sciences 2024", "metric_note": "FEMTO metrics in percentage of lifetime (0-1 scale)", "sota_model": "CNN-GRU-MHA", "sota_rmse": 0.0443, "sota_source": "MDPI 2024 - Transfer Learning for ...
{"complexity_level": "medium", "dependency_analysis": "Load data -> identify scenarios -> train separate models per scenario -> predict per scenario -> verify per scenario -> calculate metrics per scenario -> comparative analysis."}
FEMTO: the expected MAE/RMSE ranges do not state their unit (rul_percentage is 0-1); a constant 50% prediction lands just outside the MAE range.
pdm_rul_004
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD004
The XJTU dataset has bearings with five different fault types, and I want to see if our RUL predictions are more accurate for certain fault types. Can you predict remaining life for all test bearings, give me overall accuracy numbers, then break it down by fault type so I can see which fault types we predict best? This...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "classify_faults", "calculate_rmse" ]
{"problem": "Predict RUL for XJTU bearing dataset considering five different fault types.", "steps": "1) Load XJTU training and test data. 2) Load ground truth RUL. 3) Analyze fault types present using analyze_fault_types(dataset='XJTU'). 4) Train fault-type-specific RUL models. 5) Predict RUL for all test units. 6) Ve...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 31.84, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "dataset_characteristics": "6 operating conditions, 2 fault modes (HPC degradation + Fan degradation), most complex CMAPSS subset"}, "expected_mae_range": [10, 25], "...
{"dependency_analysis": "Data loading -> fault type analysis -> train fault-specific models -> predict -> verify -> calculate overall metrics -> calculate per-fault metrics -> comparative analysis."}
The question text names XJTU, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_005
rotating_aero
RUL Prediction
Bearing
FEMTO
The IMS dataset has very high-frequency vibration data, and I am worried that units showing anomalies might have different RUL prediction accuracy. Can you predict remaining life for all test bearings, detect any anomalies in the sensor data, and then compare prediction accuracy between units with anomalies versus norm...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "detect_degradation_trend", "calculate_rmse" ]
{"problem": "Predict RUL for IMS high-temporal-resolution bearing data with anomaly detection integration.", "steps": "1) Load IMS training data (high temporal resolution). 2) Load IMS test data. 3) Load ground truth RUL. 4) Perform anomaly detection on test data using detect_anomalies(dataset='IMS', method='isolation_...
{"algorithm_reference": {"baseline_model": "TCNMABG", "baseline_rmse": 0.082, "baseline_source": "MDPI Applied Sciences", "metric_note": "FEMTO metrics in percentage of lifetime (0-1 scale)", "sota_model": "TcLstmNet-CBAM", "sota_source": "Nature Scientific Reports 2025"}, "expected_mae_range": [10, 25], "expected_mae_...
{"dependency_analysis": "Load data -> anomaly detection -> model training -> prediction -> anomaly flagging -> verification -> overall metrics -> anomaly-stratified metrics."}
The question text names IMS, while the `source_dataset` field and ground truth refer to FEMTO; the ground-truth units could not be re-derived from files in the repository.
pdm_rul_006
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD001
The HUST dataset has bearings tested under different speeds and loads, which is great for seeing if our RUL predictions work across diverse conditions. Can you predict remaining life for all test bearings, give me overall accuracy, then break it down by speed/load combinations? I need to know if the model generalizes w...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "analyze_engine_signals", "calculate_rmse" ]
{"problem": "Predict RUL for HUST bearings under varying speeds and loads, analyzing generalization across operating conditions.", "steps": "1) Load HUST training data (collected under varying speeds and loads). 2) Load HUST test data. 3) Load ground truth RUL. 4) Analyze operating conditions using analyze_operating_co...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 17.6, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Self-attention+BiGRU+BiLSTM", "sota_rmse": 11.74, "sota_source": "ScienceDirect 2024 - Multiscale Deep Transfer Learning"}, "expected_mae_range": [10, 2...
{"dependency_analysis": "Load data -> analyze operating conditions -> train model -> predict -> verify -> overall metrics -> group by conditions -> per-condition metrics -> generalization assessment."}
The question text names HUST, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_007
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD002
The MFPT dataset was captured at a very high sampling rate (97.656KHz), so there is probably useful information in the frequency domain. Can you predict remaining life for all test bearings using both time and frequency domain features, verify the predictions, and tell me if adding frequency analysis improves accuracy ...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "analyze_engine_signals", "calculate_rmse" ]
{"problem": "Predict RUL for MFPT bearings using high-frequency vibration data (97.656KHz sampling rate) with frequency domain analysis.", "steps": "1) Load MFPT training data (high sampling rate). 2) Load MFPT test data. 3) Load ground truth RUL. 4) Perform frequency domain analysis using analyze_frequency_domain(data...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 29.67, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "dataset_characteristics": "6 operating conditions, frequency domain analysis applicable"}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "Range [10...
{"dependency_analysis": "Load data -> frequency domain analysis -> feature extraction -> train model with combined features -> predict -> verify -> calculate metrics -> compare feature contributions."}
The question text names MFPT, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_008
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD003
The Paderborn dataset has multiple sensor types-vibration, motor current, torque, and speed-and I want to know which ones actually help predict bearing failure. Can you predict remaining life using all sensors together, then test each sensor type individually to see which gives the best predictions? I need to know if w...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "analyze_engine_signals", "calculate_rmse" ]
{"problem": "Predict RUL for Paderborn bearings using multimodal sensor data (vibration, motor current, torque, speed).", "steps": "1) Load Paderborn training data (multimodal: vibration, current, torque, speed). 2) Load Paderborn test data. 3) Load ground truth RUL. 4) Analyze multimodal sensor contributions using ana...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 17.62, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Self-attention+BiGRU+BiLSTM", "sota_rmse": 13.5, "sota_source": "ScienceDirect 2024 - Multi-attention Mechanism"}, "expected_mae_range": [10, 25], "exp...
{"dependency_analysis": "Load multimodal data -> analyze sensor contributions -> train model with all sensors -> predict -> verify -> calculate metrics -> train separate models per sensor -> compare accuracy -> rank sensor importance."}
The question text names Paderborn, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_009
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD004
The Mendeley dataset has bearings running at speeds that constantly change between 600 and 1800 RPM, making the vibration signals non-stationary. Can you predict remaining life for all test bearings, accounting for these changing conditions, and show me how prediction accuracy varies across different speed ranges? I ne...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
{"problem": "Predict RUL for Mendeley bearings under non-stationary conditions (varying speed 600-1800RPM).", "steps": "1) Load Mendeley training data (non-stationary: speed 600-1800RPM). 2) Load Mendeley test data. 3) Load ground truth RUL. 4) Handle non-stationary signal characteristics using handle_non_stationary_da...
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 31.84, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Multi-attention Mechanism", "sota_rmse": 26.5, "sota_source": "ScienceDirect 2024"}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "R...
{"dependency_analysis": "Load non-stationary data -> apply non-stationary handling -> train adapted model -> predict -> verify -> calculate metrics -> analyze by speed range."}
pdm_rul_010
rotating_aero
RUL Prediction
Bearing
FEMTO
The Azure dataset is huge-over 876,000 samples-so I need RUL predictions that can actually run efficiently. Can you predict remaining life for all test units, verify the predictions, give me accuracy numbers, and also tell me how long it took and how much memory it used? I need to know if this is practical for producti...
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
{"problem": "Predict RUL for Azure dataset (876K+ samples) requiring efficient large-scale processing.", "steps": "1) Load Azure training data (876K+ samples, efficient loading required). 2) Load Azure test data. 3) Load ground truth RUL. 4) Handle large dataset efficiently using handle_large_dataset(dataset='Azure', m...
{"algorithm_reference": {"baseline_mae": 0.056, "baseline_model": "TCNMABG", "baseline_rmse": 0.082, "baseline_source": "MDPI 2024 - Temporal Convolutional Multi-Attention", "sota_model": "CNN-GRU-MHA", "sota_rmse": 0.0443, "sota_source": "MDPI 2024 - Transfer Learning for Bearing RUL"}, "expected_mae_range": [10, 25],...
{"dependency_analysis": "Load large dataset efficiently -> batch processing -> train with batches -> batch prediction -> verify -> calculate metrics -> performance benchmarking."}
FEMTO: the expected MAE/RMSE ranges do not state their unit (rul_percentage is 0-1); a constant 50% prediction lands just outside the MAE range.
pdm_fault_001
rotating_aero
Fault Classification
Bearing
CWRU
I have got CWRU bearing data with different fault types-inner race defects, outer race defects, and ball race defects. Can you classify which fault type each test bearing has, check those classifications against the actual fault labels, and give me accuracy numbers plus a breakdown of how well you classified each fault...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify bearing faults in CWRU dataset (inner race, outer race, ball race defects).", "steps": "1) Load CWRU training data. 2) Load CWRU test data. 3) Load ground truth fault labels. 4) Train fault classification model using train_fault_classifier(dataset='CWRU', fault_types=['inner_race', 'outer_race', '...
{"algorithm_reference": {"baseline_accuracy": 0.99, "baseline_model": "CNN-LSTM-GRU", "baseline_source": "MDPI 2024 - Hybrid Deep Learning for Bearing Fault Classification", "sota_accuracy": 1.0, "sota_model": "CNN-BLSTM", "sota_source": "Wiley 2021 - Bidirectional LSTM for Rotating Machinery Fault Diagnosis"}, "expect...
{"dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate overall accuracy -> generate confusion matrix -> calculate per-fault metrics."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_002
rotating_aero
Fault Classification
Bearing
XJTU
The XJTU dataset has five different fault types, and I suspect we might classify early-stage faults differently than late-stage ones. Can you classify all test bearings by fault type, give me overall and per-fault-type accuracy, and then break down accuracy by fault severity? I need to know if we catch faults better wh...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify five different fault types in XJTU dataset and analyze classification performance by fault severity.", "steps": "1) Load XJTU training data. 2) Load XJTU test data. 3) Load ground truth fault labels (5 fault types). 4) Analyze fault severity levels using analyze_fault_severity(dataset='XJTU'). 5) ...
{"algorithm_reference": {"baseline_accuracy": 0.92, "baseline_model": "CNN", "baseline_source": "XJTU-SY benchmark papers", "sota_accuracy": 0.97, "sota_model": "Transfer Learning CNN", "sota_source": "Domain adaptation for bearing fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_range_rat...
{"dependency_analysis": "Load data -> analyze severity -> train classifier -> classify -> verify -> overall accuracy -> per-fault accuracy -> severity-stratified analysis."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_003
rotating_aero
Fault Classification
Electric motor
ElectricMotorVibrations
We have both acoustic and vibration data for electric motors, and I want to know if using both helps classify faults better than using just one. Can you classify all test motor faults using the combined acoustic and vibration data, then test each modality separately to see which gives better accuracy? I need concrete n...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy", "analyze_engine_signals" ]
{"problem": "Classify motor faults using multimodal acoustic and vibrational data from Electric Motor Vibrations dataset.", "steps": "1) Load Electric Motor Vibrations training data (acoustic + vibrational). 2) Load test data. 3) Load ground truth fault labels. 4) Analyze multimodal signal contributions using analyze_m...
{"algorithm_reference": {"baseline_accuracy": 0.9, "baseline_model": "Single-modal CNN", "baseline_source": "Electric motor fault diagnosis benchmarks", "sota_accuracy": 0.97, "sota_model": "Multimodal Fusion CNN", "sota_source": "Acoustic-vibration fusion for motor diagnostics"}, "expected_accuracy_range": [0.85, 0.98...
{"dependency_analysis": "Load multimodal data -> analyze modalities -> train combined classifier -> classify -> verify -> calculate accuracy -> train separate classifiers per modality -> compare accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_004
rotating_aero
Fault Classification
Induction motor
RotorBrokenBar
We have induction motor data with broken rotor bars, and the severity ranges from 1 to 4 broken bars. Can you classify the severity level for each test motor, verify against the actual labels, and give me accuracy broken down by severity level? I also need a confusion matrix to see if the model confuses certain severit...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify broken rotor bar faults in induction motors with severity levels (1-4 broken bars).", "steps": "1) Load RotorBrokenBar training data. 2) Load test data. 3) Load ground truth labels (severity: 1-4 broken bars). 4) Analyze fault severity levels using analyze_fault_severity_levels(dataset='RotorBroke...
{"algorithm_reference": {"baseline_accuracy": 0.88, "baseline_model": "CNN", "baseline_source": "Rotor fault severity classification benchmarks", "sota_accuracy": 0.95, "sota_model": "Deep Residual Network", "sota_source": "Induction motor fault severity diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_a...
{"dependency_analysis": "Load data -> analyze severity levels -> train multi-class classifier -> classify -> verify -> overall accuracy -> per-severity accuracy -> confusion matrix generation."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_005
rotating_aero
Fault Classification
Gearbox
PlanetaryPdM
The planetary gearbox dataset has faults in different components-sun gear cracks, planet spalling, ring gear issues. Can you classify which component has the fault for each test gearbox, verify those classifications, and give me accuracy numbers overall and per component? This is for root cause analysis, so I need to k...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify and localize faults in planetary gearbox (sun gear crack, planet spalling, etc.) for root cause analysis.", "steps": "1) Load PlanetaryPdM training data. 2) Load test data. 3) Load ground truth fault labels (component-specific: sun gear, planet, etc.). 4) Localize fault components using localize_f...
{"algorithm_reference": {"baseline_accuracy": 0.89, "baseline_model": "CNN-1D", "baseline_source": "Planetary gearbox fault diagnosis benchmarks", "sota_accuracy": 0.96, "sota_model": "Attention-based CNN", "sota_source": "Component-level gearbox fault localization"}, "expected_accuracy_range": [0.85, 0.98], "expected_...
{"dependency_analysis": "Load data -> component localization -> train component-specific classifier -> classify and localize -> verify -> overall accuracy -> per-component accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_006
rotating_aero
Fault Classification
Bearing
Paderborn
The Paderborn dataset has both artificially induced and naturally occurring bearing faults. Can you classify the fault types for all test bearings, distinguish whether each fault was artificial or natural, and compare classification accuracy between the two? I need to know if our model works equally well on both types ...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify bearing faults in Paderborn dataset, distinguishing between artificially induced and naturally induced degradation.", "steps": "1) Load Paderborn training data (artificial + natural faults). 2) Load test data. 3) Load ground truth labels (fault type + induction method). 4) Distinguish artificial v...
{"algorithm_reference": {"baseline_accuracy": 0.91, "baseline_model": "CNN", "baseline_source": "Paderborn bearing fault benchmark", "sota_accuracy": 0.99, "sota_model": "FaultNet", "sota_source": "arXiv - Deep Learning for Bearing Fault Diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_range_rat...
{"dependency_analysis": "Load data -> distinguish induction methods -> train classifier -> classify -> verify -> overall accuracy -> separate accuracy for artificial vs. natural -> comparison analysis."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_007
rotating_aero
Fault Classification
Bearing
HUST
The HUST dataset has 5 different bearing types with 6 fault categories, all tested under varying speeds and loads. Can you classify the fault category for each test bearing, give me overall accuracy plus breakdowns by fault category and bearing type, and check if accuracy changes with operating conditions? I need a com...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy", "analyze_engine_signals" ]
{"problem": "Classify 6 fault categories across 5 bearing types in HUST dataset under varying speeds and loads.", "steps": "1) Load HUST training data (5 bearing types, 6 fault categories, varying conditions). 2) Load test data. 3) Load ground truth labels. 4) Analyze operating conditions using analyze_operating_condit...
{"algorithm_reference": {"baseline_accuracy": 0.88, "baseline_model": "CNN", "baseline_source": "HUST bearing fault benchmark", "sota_accuracy": 0.95, "sota_model": "Condition-aware Deep Network", "sota_source": "Multi-condition bearing fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_rang...
{"dependency_analysis": "Load data -> analyze conditions -> train classifier -> classify -> verify -> overall accuracy -> per-category accuracy -> per-bearing-type accuracy -> condition-stratified accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_008
rotating_aero
Fault Classification
Bearing
MFPT
The MFPT dataset has bearings with inner and outer race defects tested under different load conditions. Can you classify which type of defect each test bearing has, verify the classifications, and show me if accuracy changes with load? I need to know if we should account for load when classifying faults.
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy", "analyze_engine_signals" ]
{"problem": "Classify inner/outer race bearing defects in MFPT dataset under varying load conditions.", "steps": "1) Load MFPT training data (inner/outer race defects, varying loads). 2) Load test data. 3) Load ground truth labels. 4) Analyze load conditions using analyze_load_conditions(dataset='MFPT'). 5) Train fault...
{"algorithm_reference": {"baseline_accuracy": 0.94, "baseline_model": "CNN", "baseline_source": "MFPT bearing fault benchmark", "sota_accuracy": 0.98, "sota_model": "Load-aware CNN", "sota_source": "Variable-load bearing fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_range_rationale": "R...
{"dependency_analysis": "Load data -> analyze load conditions -> train classifier -> classify -> verify -> overall accuracy -> per-fault-type accuracy -> load-stratified accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_009
rotating_aero
Fault Classification
Bearing
Mendeley
The Mendeley dataset has bearings with changing speeds (600-1800 RPM), making the signals non-stationary. Can you classify the fault types for all test bearings, accounting for these changing conditions, and show me how accuracy varies across speed ranges? I need to know if non-stationary conditions hurt classification...
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
{"problem": "Classify bearing faults in Mendeley dataset under non-stationary conditions (speed 600-1800RPM).", "steps": "1) Load Mendeley training data (non-stationary). 2) Load test data. 3) Load ground truth labels. 4) Handle non-stationary classification using handle_non_stationary_classification(dataset='Mendeley'...
{"algorithm_reference": {"baseline_accuracy": 0.87, "baseline_model": "CNN", "baseline_source": "Non-stationary bearing fault classification", "sota_accuracy": 0.94, "sota_model": "Speed-Invariant CNN", "sota_source": "Adaptive feature extraction for variable-speed machinery"}, "expected_accuracy_range": [0.85, 0.98], ...
{"dependency_analysis": "Load non-stationary data -> apply non-stationary handling -> train adapted classifier -> classify -> verify -> overall accuracy -> speed-range-stratified accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_010
rotating_aero
Fault Classification
Gearbox
GearboxUoC
I have gearbox data from UoC and need to classify which components have faults. Can you classify the fault types for all test gearboxes, verify the classifications, and break down accuracy by gearbox component? I need to know which parts are hardest to diagnose.
[ "load_dataset", "load_ground_truth", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy", "analyze_engine_signals" ]
{"problem": "Classify gearbox faults in UoC dataset, analyzing classification performance across gearbox structural components.", "steps": "1) Load GearboxUoC training data. 2) Load test data. 3) Load ground truth fault labels. 4) Analyze gearbox structure using analyze_gearbox_structure(dataset='GearboxUoC'). 5) Train...
{"algorithm_reference": {"baseline_accuracy": 0.9, "baseline_model": "CNN", "baseline_source": "Gearbox fault diagnosis benchmarks", "sota_accuracy": 0.96, "sota_model": "Multi-scale CNN", "sota_source": "Structural component-aware gearbox fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_r...
{"dependency_analysis": "Load data -> analyze structure -> train classifier -> classify -> verify -> overall accuracy -> component-stratified accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_cost_benefit_001
rotating_aero
Cost-Benefit Analysis
Turbofan engine
CMAPSS_FD001
I am managing a fleet of aircraft engines and need to decide whether to do preventive maintenance or wait until failure. Can you predict remaining life for all test engines, calculate what it would cost to maintain them preventively versus letting them fail, and find the optimal maintenance threshold that minimizes tot...
[ "load_dataset", "predict_rul", "calculate_maintenance_cost", "calculate_failure_cost", "optimize_maintenance_schedule" ]
{"problem": "Perform cost-benefit analysis for CMAPSS FD001 engines comparing preventive maintenance vs. reactive maintenance strategies.", "steps": "1) Load CMAPSS FD001 test data. 2) Predict RUL for all test engines using predict_rul(dataset='CMAPSS_FD001'). 3) Calculate preventive maintenance cost using calculate_ma...
{"expected_cost_range": {"optimized": [3000, 40000], "preventive": [5000, 50000], "reactive": [50000, 500000]}, "expected_mae_range": [7, 18], "expected_mae_range_rationale": "MAE is calculated across ALL 100 test units in CMAPSS_FD001, not just the top 10 high-risk units. Ground truth statistics - Mean RUL: 75.5, Rang...
{"dependency_analysis": "Load data -> predict RUL -> calculate preventive cost -> calculate reactive cost -> optimize schedule -> compare strategies -> identify optimal threshold."}
Expected cost ranges depend on unit costs the question does not state; the MAE range is not meaningful for datasets without RUL labels.
pdm_cost_benefit_002
rotating_aero
Cost-Benefit Analysis
Bearing
CWRU
We have bearings with different fault types-inner race, outer race, and ball race defects-and each costs different amounts to fix. Can you classify the fault type for each test bearing, calculate maintenance and failure costs for each fault type, prioritize which bearings to fix first based on cost-benefit, and tell me...
[ "load_dataset", "classify_faults", "calculate_maintenance_cost", "optimize_maintenance_schedule", "calculate_failure_cost" ]
{"problem": "Perform cost-benefit analysis for CWRU bearings comparing maintenance costs by fault type (inner race, outer race, ball race).", "steps": "1) Load CWRU test data. 2) Classify faults for all test bearings using classify_faults(dataset='CWRU'). 3) Calculate fault-specific maintenance costs using calculate_fa...
{"expected_cost_range": {"optimized": [3000, 40000], "preventive": [5000, 50000], "reactive": [50000, 500000]}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in CWRU, not just the top 10 high-risk units. Range represents typical model performance for this datas...
{"dependency_analysis": "Load data -> classify faults -> calculate fault-specific costs -> calculate fault-specific failure costs -> optimize priority -> compare costs -> identify best ROI fault type."}
Expected cost ranges depend on unit costs the question does not state; the MAE range is not meaningful for datasets without RUL labels.
pdm_cost_benefit_003
rotating_aero
Cost-Benefit Analysis
Bearing
FEMTO
The FEMTO dataset has bearings running under three different operational scenarios, and maintenance costs vary by scenario. Can you predict remaining life for all test bearings in each scenario, calculate maintenance and failure costs per scenario, optimize the maintenance strategy for each scenario separately, and tel...
[ "load_dataset", "predict_rul", "analyze_engine_signals", "calculate_maintenance_cost", "optimize_maintenance_schedule" ]
{"problem": "Perform cost-benefit analysis for FEMTO bearings across three operational scenarios, optimizing maintenance strategy per scenario.", "steps": "1) Load FEMTO test data. 2) Identify three operational scenarios using identify_operational_scenarios(dataset='FEMTO'). 3) Predict RUL for all test units per scenar...
{"expected_cost_range": {"optimized": [3000, 40000], "preventive": [5000, 50000], "reactive": [50000, 500000]}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in FEMTO, not just the top 10 high-risk units. Range represents typical model performance for this data...
{"dependency_analysis": "Load data -> identify scenarios -> predict RUL per scenario -> calculate scenario costs -> optimize per scenario -> compare scenarios -> identify most critical scenario."}
Expected cost ranges depend on unit costs the question does not state; the MAE range is not meaningful for datasets without RUL labels.
pdm_cost_benefit_004
rotating_aero
Cost-Benefit Analysis
Bearing
XJTU
For the XJTU bearings, I need a comprehensive maintenance plan that considers both how much life is left and what type of fault is present, since different faults cost different amounts to fix. Can you predict remaining life and classify fault types for all test bearings, calculate combined maintenance and failure cost...
[ "load_dataset", "predict_rul", "classify_faults", "calculate_maintenance_cost", "optimize_maintenance_schedule" ]
{"problem": "Perform integrated cost-benefit analysis for XJTU bearings combining RUL prediction and fault classification for comprehensive maintenance optimization.", "steps": "1) Load XJTU test data. 2) Predict RUL for all test units. 3) Classify fault types for all test units. 4) Calculate combined maintenance costs...
{"expected_cost_range": {"optimized": [3000, 40000], "preventive": [5000, 50000], "reactive": [50000, 500000]}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in XJTU, not just the top 10 high-risk units. Range represents typical model performance for this datas...
{"dependency_analysis": "Load data -> predict RUL -> classify faults -> calculate combined costs -> optimize multi-objective -> generate prioritized list."}
Expected cost ranges depend on unit costs the question does not state; the MAE range is not meaningful for datasets without RUL labels.
pdm_cost_benefit_005
rotating_aero
Cost-Benefit Analysis
Industrial engine
Azure
We have a huge fleet (876K+ units) and I am wondering if we can save money by doing maintenance in bulk batches instead of individually. Can you predict remaining life for all test units, calculate what it costs to maintain them individually versus in bulk batches, optimize a fleet-wide maintenance schedule that takes ...
[ "load_dataset", "predict_rul", "calculate_maintenance_cost", "optimize_maintenance_schedule" ]
{"problem": "Perform fleet-wide cost-benefit analysis for Azure dataset (876K+ samples) optimizing bulk maintenance scheduling.", "steps": "1) Load Azure test data (large-scale). 2) Predict RUL for all test units. 3) Calculate bulk maintenance costs using calculate_bulk_maintenance_cost(units=all_units, base_cost=3000,...
{"expected_cost_range": {"optimized": [3000, 40000], "preventive": [5000, 50000], "reactive": [50000, 500000]}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in Azure, not just the top 10 high-risk units. Range represents typical model performance for this data...
{"dependency_analysis": "Load large dataset -> predict RUL -> calculate bulk costs -> calculate individual costs -> optimize fleet schedule -> analyze economies of scale -> identify optimal batch sizes."}
Expected cost ranges depend on unit costs the question does not state; the MAE range is not meaningful for datasets without RUL labels.
pdm_safety_001
rotating_aero
Safety/Policy Evaluation
Turbofan engine
CMAPSS_FD001
I am responsible for aircraft engine safety and need to identify which engines pose safety risks. Can you predict remaining life for all test engines, flag any with less than 20 cycles left as high risk, assess the safety risks (catastrophic failure, safety hazards, environmental impact), check if they comply with FAA ...
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
{"problem": "Assess safety risks and policy compliance for CMAPSS FD001 engines with low predicted RUL.", "steps": "1) Load CMAPSS FD001 test data. 2) Predict RUL for all test engines. 3) Identify engines with predicted RUL < 20 cycles (high risk). 4) Assess safety risk for high-risk engines using assess_safety_risk(un...
{"expected_mae_range": [7, 18], "expected_mae_range_rationale": "MAE is calculated across ALL 100 test units in CMAPSS_FD001, not just the top 10 high-risk units. Ground truth statistics - Mean RUL: 75.5, Range: 7-145. Expected MAE range represents typical model performance for this dataset.", "expected_output_format":...
{"dependency_analysis": "Load data -> predict RUL -> identify high-risk units -> assess safety risk -> check compliance -> generate recommendations -> classify risk levels."}
pdm_safety_002
rotating_aero
Safety/Policy Evaluation
Bearing
CWRU
Different bearing fault types have different safety implications. Can you classify the fault types for all test bearings, assess the safety impact of each fault type (vibration severity, failure probability, downtime risk), check compliance with ISO and ANSI vibration standards, and generate safety protocols for each f...
[ "load_dataset", "classify_faults", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
{"problem": "Assess safety impact of different bearing fault types (inner race, outer race, ball race) and generate safety protocols.", "steps": "1) Load CWRU test data. 2) Classify faults for all test bearings. 3) Assess safety impact by fault type using assess_fault_safety_impact(fault_types=['inner_race', 'outer_rac...
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in CWRU, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": ["low", "...
{"dependency_analysis": "Load data -> classify faults -> assess safety impact per fault type -> check standards -> generate protocols -> rank by criticality."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_003
rotating_aero
Safety/Policy Evaluation
Electric motor
ElectricMotorVibrations
Electric motor failures can be dangerous, especially with electrical hazards and fire risks. Can you classify the motor faults, assess safety risks (electrical hazards, fire risk, mechanical failure), check compliance with IEC and NEMA standards, and generate emergency shutdown protocols for high-risk motors? I need cl...
[ "load_dataset", "classify_faults", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
{"problem": "Assess safety risks for electric motor faults and generate emergency shutdown protocols.", "steps": "1) Load Electric Motor Vibrations test data. 2) Classify motor faults. 3) Assess motor safety risks using assess_motor_safety(faults=classifications, risk_factors=['electrical_hazard', 'fire_risk', 'mechani...
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in ElectricMotorVibrations, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk...
{"dependency_analysis": "Load data -> classify faults -> assess motor safety -> check electrical standards -> generate shutdown protocols -> classify risk levels."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_004
rotating_aero
Safety/Policy Evaluation
Induction motor
RotorBrokenBar
Broken rotor bars in induction motors get more dangerous as severity increases. Can you classify the severity level (1-4 broken bars) for each test motor, assess safety risks for each severity level, check compliance with IEEE and IEC motor standards, and generate maintenance policies that specify when to shut down imm...
[ "load_dataset", "classify_faults", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
{"problem": "Assess safety risks for broken rotor bar faults with severity levels (1-4 bars) and generate maintenance policies.", "steps": "1) Load RotorBrokenBar test data. 2) Classify fault severity (1-4 broken bars). 3) Assess safety by severity level using assess_severity_safety(severity_levels=[1,2,3,4], safety_me...
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in RotorBrokenBar, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels":...
{"dependency_analysis": "Load data -> classify severity -> assess safety per severity -> check standards -> generate policies -> define action thresholds."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_005
rotating_aero
Safety/Policy Evaluation
Gearbox
PlanetaryPdM
Planetary gearboxes have complex structures, and faults in different components have different safety implications. Can you classify the faults and identify which component (sun gear, planet, ring gear) is affected, assess safety risks for each component type, check compliance with AGMA and ISO gear standards, and gene...
[ "load_dataset", "classify_faults", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
{"problem": "Assess safety risks for planetary gearbox component-specific faults and generate component-targeted zsafety policies.", "steps": "1) Load PlanetaryPdM test data. 2) Classify faults and localize components (sun gear, planet gear, ring gear). 3) Assess gearbox safety by component using assess_gearbox_safety(...
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in PlanetaryPdM, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": [...
{"dependency_analysis": "Load data -> classify and localize faults -> assess safety per component -> check standards -> generate component policies -> rank by criticality."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_rul_011
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD001
Predict remaining useful life for IMS equipment and identify the 5 units most at risk.
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
Predict RUL for IMS dataset and identify top 5 risk units.
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 17.6, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_mae": 10.49, "sota_model": "CAELSTM", "sota_rmse": 14.44, "sota_source": "Nature Scientific Reports 2025 - Deep learning-based prognostic approach"}, "expected_m...
{"complexity": "Medium", "dependency_analysis": "Load data -> train model -> predict -> verify -> rank by risk."}
The question text names IMS, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_012
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD002
Predict remaining useful life for HUST equipment and identify the 5 units most at risk.
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
Predict RUL for HUST dataset and identify top 5 risk units.
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 29.67, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Multi-attention Mechanism", "sota_rmse": 23.5, "sota_source": "ScienceDirect 2024"}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "R...
{"complexity": "High", "dependency_analysis": "Load data -> train model -> predict -> verify -> rank by risk."}
The question text names HUST, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_013
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD003
Predict remaining useful life for MFPT equipment and identify the 5 units most at risk.
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
Predict RUL for MFPT dataset and identify top 5 risk units.
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 17.62, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Self-attention+BiGRU+BiLSTM", "sota_rmse": 13.5, "sota_source": "ScienceDirect 2024 - Multi-attention Mechanism"}, "expected_mae_range": [10, 25], "exp...
{"complexity": "Medium", "dependency_analysis": "Load data -> train model -> predict -> verify -> rank by risk."}
The question text names MFPT, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_014
rotating_aero
RUL Prediction
Turbofan engine
CMAPSS_FD004
Predict remaining useful life for Paderborn equipment and identify the 5 units most at risk.
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
Predict RUL for Paderborn dataset and identify top 5 risk units.
{"algorithm_reference": {"baseline_model": "BiLSTM", "baseline_rmse": 31.84, "baseline_source": "arXiv 2025 - Uncertainty-Aware Deep Learning Framework", "sota_model": "Multi-attention Mechanism", "sota_rmse": 26.5, "sota_source": "ScienceDirect 2024"}, "expected_mae_range": [10, 25], "expected_mae_range_rationale": "R...
{"complexity": "High", "dependency_analysis": "Load data -> train model -> predict -> verify -> rank by risk."}
The question text names Paderborn, but the ground truth is computed on the C-MAPSS subset in the `source_dataset` field. The field is correct; the question text is not. Fix planned for v1.1.
pdm_rul_015
rotating_aero
RUL Prediction
Bearing
FEMTO
Predict remaining useful life for Mendeley equipment and identify the 5 units most at risk.
[ "load_dataset", "load_ground_truth", "train_rul_model", "predict_rul", "verify_ground_truth", "calculate_mae", "calculate_rmse" ]
Predict RUL for Mendeley dataset and identify top 5 risk units.
{"algorithm_reference": {"baseline_mae": 0.056, "baseline_model": "TCNMABG", "baseline_rmse": 0.082, "baseline_source": "MDPI 2024 - Temporal Convolutional Multi-Attention", "sota_model": "TcLstmNet-CBAM", "sota_performance": "Best MAE on 11/14 bearings", "sota_source": "Nature Scientific Reports 2025"}, "expected_mae_...
{"complexity": "Medium", "dependency_analysis": "Load data -> train model -> predict -> verify -> rank by risk."}
FEMTO: the expected MAE/RMSE ranges do not state their unit (rul_percentage is 0-1); a constant 50% prediction lands just outside the MAE range.
pdm_fault_011
rotating_aero
Fault Classification
Bearing
Paderborn
Classify fault types for all test units in Paderborn dataset.
[ "load_dataset", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
Classify faults in Paderborn dataset.
{"algorithm_reference": {"baseline_accuracy": 0.92, "baseline_model": "CNN", "baseline_source": "Paderborn bearing fault benchmark", "sota_accuracy": 0.99, "sota_model": "FaultNet", "sota_source": "arXiv - Deep Learning for Bearing Fault Diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_range_rat...
{"complexity": "High", "dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_012
rotating_aero
Fault Classification
Bearing
HUST
Classify fault types for all test units in HUST dataset.
[ "load_dataset", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
Classify faults in HUST dataset.
{"algorithm_reference": {"baseline_accuracy": 0.88, "baseline_model": "CNN", "baseline_source": "HUST bearing fault benchmark", "sota_accuracy": 0.95, "sota_model": "Condition-aware Deep Network", "sota_source": "Multi-condition bearing fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_rang...
{"complexity": "High", "dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_013
rotating_aero
Fault Classification
Bearing
MFPT
Classify fault types for all test units in MFPT dataset.
[ "load_dataset", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
Classify faults in MFPT dataset.
{"algorithm_reference": {"baseline_accuracy": 0.94, "baseline_model": "CNN", "baseline_source": "MFPT bearing fault benchmark", "sota_accuracy": 0.98, "sota_model": "Load-aware CNN", "sota_source": "Variable-load bearing fault diagnosis"}, "expected_accuracy_range": [0.85, 0.98], "expected_accuracy_range_rationale": "R...
{"complexity": "High", "dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_014
rotating_aero
Fault Classification
Bearing
Mendeley
Classify fault types for all test units in Mendeley dataset.
[ "load_dataset", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
Classify faults in Mendeley dataset.
{"algorithm_reference": {"baseline_accuracy": 0.87, "baseline_model": "CNN", "baseline_source": "Non-stationary bearing fault classification", "sota_accuracy": 0.94, "sota_model": "Speed-Invariant CNN", "sota_source": "Adaptive feature extraction for variable-speed machinery"}, "expected_accuracy_range": [0.85, 0.98], ...
{"complexity": "High", "dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_fault_015
rotating_aero
Fault Classification
Electric motor
ElectricMotorVibrations
Classify fault types for all test units in ElectricMotorVibrations dataset.
[ "load_dataset", "train_fault_classifier", "classify_faults", "verify_classification", "calculate_accuracy" ]
Classify faults in ElectricMotorVibrations dataset.
{"algorithm_reference": {"baseline_accuracy": 0.9, "baseline_model": "Single-modal CNN", "baseline_source": "Electric motor fault diagnosis benchmarks", "sota_accuracy": 0.97, "sota_model": "Multimodal Fusion CNN", "sota_source": "Acoustic-vibration fusion for motor diagnostics"}, "expected_accuracy_range": [0.85, 0.98...
{"complexity": "High", "dependency_analysis": "Load data -> train classifier -> classify -> verify -> calculate accuracy."}
expected_fault_types holds a placeholder ("Fault_0") left by an earlier tool stub; the accuracy range [0.85, 0.98] is generic.
pdm_safety_006
rotating_aero
Safety/Policy Evaluation
Turbofan engine
CMAPSS_FD001
Identify safety risks and compliance issues for CMAPSS_FD001 equipment.
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
Assess safety risks for CMAPSS_FD001 equipment with low predicted RUL.
{"expected_mae_range": [7, 18], "expected_mae_range_rationale": "MAE is calculated across ALL 100 test units in CMAPSS_FD001, not just the top 10 high-risk units. Ground truth statistics - Mean RUL: 75.5, Range: 7-145. Expected MAE range represents typical model performance for this dataset.", "expected_output_format":...
{"complexity": "High", "dependency_analysis": "Load data -> predict RUL -> assess risk -> check compliance -> generate recommendations."}
pdm_safety_007
rotating_aero
Safety/Policy Evaluation
Bearing
CWRU
Identify safety risks and compliance issues for CWRU equipment.
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
Assess safety risks for CWRU equipment with low predicted RUL.
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in CWRU, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": ["low", "...
{"complexity": "High", "dependency_analysis": "Load data -> predict RUL -> assess risk -> check compliance -> generate recommendations."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_008
rotating_aero
Safety/Policy Evaluation
Bearing
FEMTO
Identify safety risks and compliance issues for FEMTO equipment.
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
Assess safety risks for FEMTO equipment with low predicted RUL.
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in FEMTO, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": ["low", ...
{"complexity": "High", "dependency_analysis": "Load data -> predict RUL -> assess risk -> check compliance -> generate recommendations."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_009
rotating_aero
Safety/Policy Evaluation
Bearing
XJTU
Identify safety risks and compliance issues for XJTU equipment.
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
Assess safety risks for XJTU equipment with low predicted RUL.
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in XJTU, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": ["low", "...
{"complexity": "High", "dependency_analysis": "Load data -> predict RUL -> assess risk -> check compliance -> generate recommendations."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
pdm_safety_010
rotating_aero
Safety/Policy Evaluation
Bearing
IMS
Identify safety risks and compliance issues for IMS equipment.
[ "load_dataset", "predict_rul", "assess_safety_risk", "check_compliance", "generate_safety_recommendations" ]
Assess safety risks for IMS equipment with low predicted RUL.
{"expected_mae_range": [10, 25], "expected_mae_range_rationale": "MAE is calculated across ALL test units in IMS, not just the top 10 high-risk units. Range represents typical model performance for this dataset based on historical benchmarks.", "expected_output_format": "json_report", "expected_risk_levels": ["low", "m...
{"complexity": "High", "dependency_analysis": "Load data -> predict RUL -> assess risk -> check compliance -> generate recommendations."}
Ground truth specifies only the allowed risk levels (and placeholder sample units); no unit-level answer can be checked.
engine_health_combined_001
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I need a complete health assessment for this aircraft engine based on the following sensor data from a single operational cycle. Analyze all major components and give me: (1) Health status for each component (Fan, LPC, HPC, HPT, LPT) - Healthy or Fault, (2) If there are timing issues, identify whether they're caused by...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Healthy", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": [], "overall_health_state": "Operating Normally", "rationale": "Ground truth from EngineMTQA engine 108410. Health state: Operatin...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "108410"}
Ground truth lists no faulty components, while its own root-cause note cites LPT efficiency and flow modifiers; pending SME adjudication.
engine_health_combined_002
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our maintenance team needs an urgent diagnostic report for this engine. Review the sensor readings below and determine: which components are functioning normally, which have faults, what's causing any timing anomalies, and the engine's overall operational status. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [Op...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Healthy", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": [], "overall_health_state": "Operating Normally", "rationale": "Ground truth from EngineMTQA engine 20119. Health state: Operating...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "20119"}
engine_health_combined_003
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Before this aircraft's next flight, I need you to analyze the engine telemetry and provide a full component-by-component health assessment. Check Fan, LPC, HPC, HPT, and LPT systems, identify any efficiency or flow issues, and classify the overall engine condition. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Healthy", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": [], "overall_health_state": "Operating Normally", "rationale": "Ground truth from EngineMTQA engine 8389. Health state: Operating ...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "8389"}
engine_health_combined_004
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
This engine flagged an alert during the last flight. Analyze the sensor data and tell me: (1) Which specific components show signs of malfunction? (2) Are the timing problems related to efficiency degradation or flow restrictions? (3) Should we ground this aircraft for maintenance? ENGINE SIGNAL DATA SUMMARY (1 operat...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Fault", "HPC": "Fault", "HPT": "Fault", "LPC": "Fault", "LPT": "Fault"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["Fan", "LPC", "HPC", "HPT", "LPT"], "overall_health_state": "Abnormal Degradation", "rationale": "Ground truth from EngineMTQA engine 60739...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "60739"}
engine_health_combined_005
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I need a complete health assessment for this aircraft engine based on the following sensor data from a single operational cycle. Analyze all major components and give me: (1) Health status for each component (Fan, LPC, HPC, HPT, LPT) - Healthy or Fault, (2) If there are timing issues, identify whether they're caused by...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT"], "overall_health_state": "Abnormal Degradation", "rationale": "Ground truth from EngineMTQA engine 78384. Health state: Abno...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "78384"}
engine_health_combined_006
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our maintenance team needs an urgent diagnostic report for this engine. Review the sensor readings below and determine: which components are functioning normally, which have faults, what's causing any timing anomalies, and the engine's overall operational status. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [Op...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Fault", "HPT": "Healthy", "LPC": "Fault", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["LPC", "HPC"], "overall_health_state": "Abnormal Degradation", "rationale": "Ground truth from EngineMTQA engine 46790. Health state:...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "46790"}
engine_health_combined_007
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Before this aircraft's next flight, I need you to analyze the engine telemetry and provide a full component-by-component health assessment. Check Fan, LPC, HPC, HPT, and LPT systems, identify any efficiency or flow issues, and classify the overall engine condition. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Fault"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT", "LPT"], "overall_health_state": "Abnormal Degradation", "rationale": "Ground truth from EngineMTQA engine 24953. Health state:...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "24953"}
engine_health_combined_008
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
This engine flagged an alert during the last flight. Analyze the sensor data and tell me: (1) Which specific components show signs of malfunction? (2) Are the timing problems related to efficiency degradation or flow restrictions? (3) Should we ground this aircraft for maintenance? ENGINE SIGNAL DATA SUMMARY (1 operat...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Fault"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT", "LPT"], "overall_health_state": "Imminent Failure", "rationale": "Ground truth from EngineMTQA engine 20495. Health state: Imm...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "20495"}
Question text is identical to engine_health_combined_012; all checkable ground-truth fields agree (benign duplicate).
engine_health_combined_009
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I need a complete health assessment for this aircraft engine based on the following sensor data from a single operational cycle. Analyze all major components and give me: (1) Health status for each component (Fan, LPC, HPC, HPT, LPT) - Healthy or Fault, (2) If there are timing issues, identify whether they're caused by...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT"], "overall_health_state": "Imminent Failure", "rationale": "Ground truth from EngineMTQA engine 77593. Health state: Imminent...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "77593"}
engine_health_combined_010
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our maintenance team needs an urgent diagnostic report for this engine. Review the sensor readings below and determine: which components are functioning normally, which have faults, what's causing any timing anomalies, and the engine's overall operational status. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [Op...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Healthy", "LPC": "Fault", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["LPC"], "overall_health_state": "Imminent Failure", "rationale": "Ground truth from EngineMTQA engine 107977. Health state: Imminen...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "107977"}
engine_health_combined_011
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Before this aircraft's next flight, I need you to analyze the engine telemetry and provide a full component-by-component health assessment. Check Fan, LPC, HPC, HPT, and LPT systems, identify any efficiency or flow issues, and classify the overall engine condition. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT"], "overall_health_state": "Imminent Failure", "rationale": "Ground truth from EngineMTQA engine 3966. Health state: Imminent ...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "3966"}
engine_health_combined_012
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
This engine flagged an alert during the last flight. Analyze the sensor data and tell me: (1) Which specific components show signs of malfunction? (2) Are the timing problems related to efficiency degradation or flow restrictions? (3) Should we ground this aircraft for maintenance? ENGINE SIGNAL DATA SUMMARY (1 operat...
[ "analyze_engine_signals", "assess_component_health", "diagnose_timing_issues" ]
1. Parse embedded sensor data summary. 2. Analyze each component's sensor readings for anomalies. 3. Determine health status (Healthy/Fault) for Fan, LPC, HPC, HPT, LPT. 4. Identify root cause of timing issues (efficiency vs flow modifier). 5. Classify overall health state (Operating Normally/Abnormal Degradation/Immin...
{"component_health": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Fault"}, "expected_answer_type": "structured_health_assessment", "faulty_components": ["HPT", "LPT"], "overall_health_state": "Imminent Failure", "rationale": "Ground truth from EngineMTQA engine 9788. Health state: Immi...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "comprehensive_component_assessment", "source_engine_id": "9788"}
Question text is identical to engine_health_combined_008; all checkable ground-truth fields agree (benign duplicate).
engine_health_combined_013
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I've collected engine telemetry across 10 operational cycles and need a trend analysis. Based on this data: (1) What is the qualitative condition of the engine (Good/Moderate/Poor/Bad/Extremely Poor)? (2) What's the estimated probability range of engine failure? (3) What maintenance actions should we take? ENGINE SIGN...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "10%-30%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["106656", "106678", "106703", "106716", "106741", "106779", "106797", "106828", "106851", "106874"]}
Question text is identical to engine_health_combined_017, but the two ground truths disagree on qualitative_condition.
engine_health_combined_014
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our predictive maintenance system flagged this engine for review. Analyze the 10-cycle trend data and provide: overall condition assessment, failure probability estimate, and your recommended maintenance strategy. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters] - Altitude: stable at 35,...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "10%-30%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["10240", "10254", "10272", "10287", "10306", "10333", "10357", "10373", "10398", "10422"]}
Same signal summary as engine_health_combined_013/017, which carry different ground truths (Good vs Moderate Condition).
engine_health_combined_015
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
This engine is due for its scheduled inspection. Based on the multi-cycle signal data, assess whether the condition has degraded, estimate failure risk, and recommend whether to proceed with routine maintenance or escalate to urgent repairs. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters]...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "10%-30%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["39611", "39628", "39665", "39699", "39715", "39735", "39768", "39789", "39821", "39848"]}
Same signal summary as engine_health_combined_013/017, which carry different ground truths (Good vs Moderate Condition).
engine_health_combined_016
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Fleet management needs a health trend report for this engine unit. Analyze the 10-cycle data and provide: (1) Current condition classification, (2) Failure probability range for the next 50 cycles, (3) Specific maintenance recommendations. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters] ...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "10%-30%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["39612", "39628", "39665", "39700", "39716", "39734", "39768", "39790", "39820", "39848"]}
Same signal summary as engine_health_combined_013/017, which carry different ground truths (Good vs Moderate Condition).
engine_health_combined_017
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I've collected engine telemetry across 10 operational cycles and need a trend analysis. Based on this data: (1) What is the qualitative condition of the engine (Good/Moderate/Poor/Bad/Extremely Poor)? (2) What's the estimated probability range of engine failure? (3) What maintenance actions should we take? ENGINE SIGN...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "10%-30%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["89747", "89763", "89781", "89802", "89810", "89833", "89851", "89860", "89870", "89891"]}
Question text is identical to engine_health_combined_013, but the two ground truths disagree on qualitative_condition.
engine_health_combined_018
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our predictive maintenance system flagged this engine for review. Analyze the 10-cycle trend data and provide: overall condition assessment, failure probability estimate, and your recommended maintenance strategy. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters] - Altitude: stable at 35,...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "30%-50%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["100319", "100335", "100349", "100366", "100376", "100388", "100402", "100421", "100435", "100451"]}
Scenarios 018-020 share one signal summary but differ in failure_probability_range (30%-50% vs 70%-100%).
engine_health_combined_019
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
This engine is due for its scheduled inspection. Based on the multi-cycle signal data, assess whether the condition has degraded, estimate failure risk, and recommend whether to proceed with routine maintenance or escalate to urgent repairs. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters]...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "70%-100%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitat...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["74131", "74165", "74189", "74213", "74231", "74257", "74275", "74308", "74334", "74363"]}
Scenarios 018-020 share one signal summary but differ in failure_probability_range (30%-50% vs 70%-100%).
engine_health_combined_020
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Fleet management needs a health trend report for this engine unit. Analyze the 10-cycle data and provide: (1) Current condition classification, (2) Failure probability range for the next 50 cycles, (3) Specific maintenance recommendations. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters] ...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "70%-100%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitat...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["20473", "20490", "20502", "20514", "20534", "20543", "20555", "20574", "20584", "20603"]}
Scenarios 018-020 share one signal summary but differ in failure_probability_range (30%-50% vs 70%-100%).
engine_health_combined_021
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
I've collected engine telemetry across 10 operational cycles and need a trend analysis. Based on this data: (1) What is the qualitative condition of the engine (Good/Moderate/Poor/Bad/Extremely Poor)? (2) What's the estimated probability range of engine failure? (3) What maintenance actions should we take? ENGINE SIGN...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "50%-70%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["112649", "112680", "112706", "112724", "112748", "112773", "112805", "112827", "112850", "112878"]}
engine_health_combined_022
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Our predictive maintenance system flagged this engine for review. Analyze the 10-cycle trend data and provide: overall condition assessment, failure probability estimate, and your recommended maintenance strategy. ENGINE SIGNAL DATA SUMMARY (10 operational cycles): [Operational Parameters] - Altitude: fluctuating b...
[ "analyze_engine_signals", "detect_degradation_trend", "assess_component_health", "optimize_maintenance_schedule" ]
1. Parse 10-cycle sensor trend data. 2. Analyze degradation patterns across cycles. 3. Classify qualitative condition. 4. Estimate failure probability based on trend severity. 5. Generate maintenance recommendations appropriate to condition.
{"condition_options": ["Good Condition", "Moderate Condition", "Poor Condition", "Bad Condition", "Extremely Poor Condition"], "expected_answer_type": "trend_analysis_with_recommendations", "failure_probability_range": "50%-70%", "probability_options": ["1%-10%", "10%-30%", "30%-50%", "50%-70%", "70%-100%"], "qualitati...
{"complexity": "High", "is_closed_ended": false, "scenario_type": "multi_cycle_trend_analysis", "source_engine_ids": ["16461", "16484", "16499", "16518", "16546", "16556", "16575", "16601", "16616", "16631"]}
engine_health_combined_023
rotating_aero
Health Analysis
Aero-engine
EngineMTQA
Emergency diagnostic request: An engine fault indicator lit up during cruise. Review the telemetry and determine which components have failed, the nature of the timing issue, and the severity of the situation. ENGINE SIGNAL DATA SUMMARY (1 operational cycles): [Operational Parameters] - Altitude: fluctuating betwee...
[ "analyze_engine_signals", "diagnose_timing_issues" ]
1. Parse sensor data for anomaly indicators. 2. Identify which components show fault signatures. 3. Analyze timing patterns to determine efficiency vs flow issues. 4. Pinpoint the affected subsystem. 5. Assess overall severity.
{"component_health_detail": {"Fan": "Healthy", "HPC": "Healthy", "HPT": "Fault", "LPC": "Healthy", "LPT": "Healthy"}, "expected_answer_type": "fault_diagnosis", "faulty_components": ["HPT"], "healthy_components": ["Fan", "LPC", "HPC", "LPT"], "overall_health_state": "Imminent Failure", "rationale": "Fault diagnosis fro...
{"complexity": "High", "is_closed_ended": true, "scenario_type": "fault_diagnosis", "source_engine_id": "2364"}
End of preview. Expand in Data Studio

PHMForge

Canonical copy: ibm-research/PHMForge. This repository is a mirror; cite and download from the IBM Research copy.

PHMForge is a benchmark for LLM agents on industrial Prognostics and Health Management (PHM). It has 99 scenarios across eight asset classes. To solve one, an agent has to find and call MCP-served tools that wrap PHM algorithms, then return an answer that is checked against a deterministic ground truth.

  • Paper: PHMForge: Evaluating LLM Agents on Industrial Prognostics through MCP-Native, Algorithm-Grounded Tools, NeurIPS 2026 Evaluations & Datasets Track (poster). Link to be added.
  • Code: the MCP server implementations and evaluation harness are not part of this release.
  • AssetOpsBench: PHMForge is a companion benchmark to AssetOpsBench. 45 of its scenarios also ship in the AssetOpsBench PHM release (see Relation to the AssetOpsBench PHM release).
  • License: CC BY 4.0 for the scenario files. The underlying sensor datasets keep their own licenses (see Source datasets).

Harbor tasks

The harbor/ folder packages all 99 scenarios as 123 Harbor tasks: the 24 lithium-ion scenarios in two phrasings, plus the other 75. Each task carries the question, the public data it needs, and a separate verifier. See harbor/README.md.

Dataset structure

There is one test split. The configs are:

Config Scenarios Content
all (default) 99 everything
rotating_aero 75 turbofans, aero-engines, bearings, motors, gearboxes, industrial engine
lithium_ion 24 NASA PCoE lithium-ion cells (BESS extension)

Per task category: Health Analysis 39, RUL Prediction 20, Fault Classification 20, Safety/Policy Evaluation 13, Cost-Benefit Analysis 7.

Per asset class: aero-engine 30, lithium-ion cell 24, bearing 22, turbofan 14, electric motor 3, gearbox 3, induction motor 2, industrial engine 1.

Fields

Field Type Description
id string Scenario ID (e.g. pdm_rul_001, engine_health_combined_005, bess_rul_003)
subset string rotating_aero or lithium_ion
task_category string One of the five task categories
asset_class string Asset class
source_dataset string Public dataset the ground truth is computed on (e.g. CMAPSS_FD001, NASA_PCoE_B0005)
question string Scenario query. For lithium_ion this is the protocol-style ("explicit") form.
question_operator_style string lithium_ion only: the operator-style ("fuzzy") form of the same question
required_tools list[string] Tools in the reference workflow
procedure string Reference procedure
ground_truth string (JSON) Ground truth and validation tolerances (e.g. expected_mae_range, labels, required fields)
metadata string (JSON) Remaining original fields (e.g. dependency analysis, difficulty, failure modes)
known_issue string Empty, or a description of a documented problem with the scenario (see Known issues)
from datasets import load_dataset
ds = load_dataset("yushengli/PHMForge", "all", split="test")
import json; gt = json.loads(ds[0]["ground_truth"])

Datasheet

Motivation

LLM agents are starting to call industrial asset-management tools through the Model Context Protocol (MCP). PHMForge measures whether an agent can select, sequence and compose algorithm-grounded tools for PHM tasks, rather than whether it can produce a plausible text answer. It was created by the PHMForge team (Columbia University, IBM Research, Georgia Tech).

Composition

  • What one item is: a scenario. It has a natural-language query, the reference tool workflow, and a ground truth with validation tolerances.
  • Data volume: the scenarios point to public sensor datasets but do not include them.
  • Personal information: none; there are no human subjects.
  • Agent outputs: the dataset contains none.

Collection process

  • 75 rotating-equipment and aero-engine scenarios: written by the consortium's subject-matter experts in six expansion stages (paper, Appendix D).
  • 24 lithium-ion scenarios: added in Stage 6.
  • Ground truth: derived from the source datasets with documented scripts, or cited to the source.
  • LLM use: the paper states that no LLM was used in scenario generation, query formulation or ground-truth derivation.

Quality assessment

  • Human rating: two SMEs independently rated a stratified sample of 30 of the 75 rotating-equipment/aero-engine scenarios on realism, difficulty calibration and ground-truth correctness (1–4 scale). Ordinal Krippendorff's α was 0.86, 0.58 and 0.73 respectively, and 0.75 pooled (paper, Table 2).

  • The 24 lithium-ion scenarios are not covered by that sample. As a supplementary check:

    • the checkable ground truths were recomputed from the processed NASA PCoE data;
    • two LLM-originated rating columns were produced under the same rubric, then reviewed and revised by an author. The paper reports their post-review agreement (Table 2, Appendix E.6).

    These are not independent human ratings or an inter-annotator agreement between experts. The issues found are listed under Known issues.

Known issues

61 of the 99 scenarios carry a non-empty known_issue field. They fall into two groups.

Errors to be fixed in v1.1:

  • Dataset named in the question text (10 RUL scenarios). In nine of them the question names a bearing dataset, while the ground truth is computed on the C-MAPSS subset in source_dataset. The field is correct and the question text is not. A tenth (pdm_rul_005) names IMS for FEMTO data.
  • Contradictions (9 aero-engine Health scenarios). Scenarios with the same signal summary have different ground truths (013–017 and 018–020), and engine_health_combined_001 has an internally inconsistent ground truth.
  • Lithium-ion ground truth or specification errors (9 scenarios). These were found by the recomputation check (paper, Appendix E.6). None of them is an RUL Prediction scenario.

Generic ground truth (33 scenarios):

  • Fault Classification: a generic accuracy range plus a placeholder field.
  • Cost-Benefit: cost ranges that depend on unstated unit costs.
  • Safety/Policy: only the allowed risk levels are specified.
  • FEMTO RUL: ranges without a unit.

These scenarios can be scored only on what the ground truth specifies.

Scoring: the results in the paper scored all scenarios as released.

See RELEASE_NOTES.md for the per-scenario list. Until v1.1, report results both with and without the flagged scenarios.

Relation to the AssetOpsBench PHM release

  • The 45 RUL, Fault, Safety and Cost-Benefit scenarios are identical (same IDs and text) to the prognostics_and_health_management config of ibm-research/AssetOpsBench (code: github.com/IBM/AssetOpsBench).
  • The 30 aero-engine Health scenarios differ.
    • Here they are the engine_health_combined_* formulations, which the paper's automated harness evaluated (Table 3).
    • AssetOpsBench lists the original EngineMTQA formulations (enginemtqa_train_qa_*).
    • Both are derived from EngineMTQA. The ID correspondence between the two formulations will be added in a later release.

Recommended uses

  • Evaluating tool-using agents on PHM workflows: tool selection, ordering, parameterization, and answer correctness against the deterministic ground truth.
  • Not recommended:
    • Treating a high score as evidence that an agent is ready for unsupervised safety-critical operation.
    • Drawing per-class conclusions for the four smallest asset classes (n ≤ 3 each).

Distribution and maintenance

  • Distribution: through Hugging Face under CC BY 4.0.
  • Versioning: versioned increments under the living-benchmark expansion plan (paper, Appendix D.3). Issues and corrections go through the code repository's issue tracker.

Source datasets

The scenarios are built on these public datasets. If you use them, cite the original sources; their licenses and terms of use apply to the sensor data, including the processed subsets in harbor/.

Dataset Asset Original reference Accessed via
C-MAPSS FD001–FD004 Turbofan Saxena et al., PHM 2008, doi:10.1109/PHM.2008.4711414 NASA Prognostics Data Repository
NASA PCoE Li-ion (B0005–B0018) Li-ion cell Saha & Goebel, Battery Data Set, NASA Ames, 2007 NASA Prognostics Data Repository
EngineMTQA Aero-engine Wang et al., ITFormer, ICML 2025, PMLR 267 Hugging Face
Azure Predictive Maintenance Industrial engine Microsoft Azure AI Gallery, Kaggle mirror PDMBench
CWRU Bearing Case Western Reserve University Bearing Data Center PDMBench
FEMTO / PRONOSTIA Bearing Nectoux et al., IEEE PHM 2012 PDMBench
IMS Bearing Qiu et al., J. Sound Vib. 2006, doi:10.1016/j.jsv.2005.03.007 PDMBench
XJTU-SY Bearing Wang et al., IEEE Trans. Reliab. 2020, doi:10.1109/TR.2018.2882682 PDMBench
HUST Bearing Thuan & Hong, BMC Res. Notes 2023, doi:10.1186/s13104-023-06400-4 PDMBench
MFPT Bearing Bechhoefer, MFPT fault data sets, 2013 PDMBench
Paderborn Bearing Lessmeier et al., PHME 2016, doi:10.36001/phme.2016.v3i1.1577 PDMBench
Rotor Broken Bar Induction motor Treml et al., IEEE DataPort 2020, doi:10.21227/fmnm-bn95 PDMBench
UoC Gearbox Gearbox Cao et al., IEEE Access 2018, doi:10.1109/ACCESS.2018.2837621 PDMBench
Mendeley bearing Bearing original source not confirmed PDMBench
Electric Motor Vibrations Electric motor original source not confirmed PDMBench
Planetary PdM Planetary gearbox original source not confirmed PDMBench

PDMBench: Zhang et al., OpenReview; processed files in submission096 on Hugging Face (CC BY 4.0).

Citation

@inproceedings{li2026phmforge,
  title     = {{PHMForge}: Evaluating {LLM} Agents on Industrial Prognostics through
               {MCP}-Native, Algorithm-Grounded Tools},
  author    = {Li, Yusheng and Feng, Tianjun and Chen, Yunfeng and Tsai, Chun-Yi and Sun, Yihan and
               Patel, Dhaval and El Maghraoui, Kaoutar and Lin, Shuxin and Das, Ayan},
  booktitle = {Advances in Neural Information Processing Systems (Evaluations and Datasets Track)},
  year      = {2026}
}
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