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Turbofan Engine Degradation Dataset Data: Dataset Structure and Field Coverage
Datadory delivers turbofan engine degradation dataset data covering comprehensive field definitions, entity mappings, and historical time series — structured for direct analytics and delivered on demand.
1,744 datasets. Pick your catch.
What do the FD001-FD004 subsets contain?
Four simulated fleets that differ on two axes: operating conditions (one versus six) and fault modes (one versus two - HPC degradation and fan degradation). Every row is one operational cycle of one engine unit across 26 whitespace-delimited columns: unit number, time in cycles, three operational settings (altitude, Mach number, throttle resolver angle) and 21 sensor channels such as fan inlet temperature, core speed, bypass duct pressure, fuel flow and oil temperature, with simulated sensor noise baked in.
Each subset arrives as three files: a training file of full run-to-failure trajectories, a test file truncated before failure, and a RUL file giving true remaining cycles for each test unit. That train/test split is what turns raw sensor text into a supervised benchmark - you predict cycles-to-failure and score against the RUL file.
train_FD001.txt alone carries 20,631 rows, which is why FD001 remains the standard starter configuration for a first remaining-useful-life model.
How do the four subsets compare?
The four configurations scale difficulty along condition diversity and fault complexity, and the unit counts below come straight from the readme tables shipped inside the archive. Pick FD001 or FD003 to validate a pipeline under constant conditions; move to FD002 and FD004 once your model must cope with six operating regimes.
When do you need the wider NASA prognostics repository instead?
Whenever the failure mode you care about is not a jet engine. The NASA Prognostics Data Set Repository lists 21 datasets ranging from about 12 MB (C-MAPSS v1) to about 15.8 GB (C-MAPSS v2) - tens of gigabytes in total - spanning lithium-ion battery aging, bearing vibration and FEMTO bearing accelerated degradation, CNC milling machine and milling tool wear, IGBT accelerated aging, capacitor electrical stress, MOSFET thermal overstress and fatigue crack growth in aluminium lap joints.
What pairs well with turbofan data when you move from lab to market?
A trained degradation model answers "when does this engine fail?"; the rest of this industry's pool answers the commercial questions around it.
The contrast between sensor archives and demand series runs through the head-to-head vs JMTBA Machine Tool Statistics (Japan) comparison: quality 8 sensor data versus quality 7 order statistics, answering different questions entirely.
| Subset | Train units | Test units | Operating conditions | Fault modes | Best used for |
|---|---|---|---|---|---|
| FD001 | 100 | 100 | ONE (sea level) | ONE (HPC degradation) | First remaining-useful-life pipeline; train_FD001 alone holds 20,631 rows |
| FD002 | 260 | 259 | SIX | ONE (HPC degradation) | Condition-robust models across six operating regimes |
| FD003 | 100 | 100 | ONE (sea level) | TWO (HPC and fan degradation) | Multi-fault modelling under constant conditions |
| FD004 | 248 | 249 | SIX | TWO (HPC and fan degradation) | The hardest configuration: six conditions and two fault modes |
Pick up where this leaves off
Every one of these ships with sample rows before you commit to anything.
Kaggle: NASA Turbofan Jet Engine (C-MAPSS)
NASA Prognostics Data Set Repository
NBER-CES Manufacturing Industry Database
Made-in-China.com
7 verified core fields · category placement · product_title …+6 more
JMTBA machine tool statistics Japan data
6 documented core fields · further breakdown fields on request · uchinaiju …+3 more
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Get a sampleQuestions worth asking
What is the difference between FD001 and FD002?
Operating conditions. FD001 runs 100 train and 100 test units under one sea-level condition with one fault mode (HPC degradation); FD002 runs 260 train and 259 test units across six operating conditions with the same single fault mode, which forces a model to separate condition effects from degradation effects.
Are there alternatives to C-MAPSS for predictive maintenance?
For engines, C-MAPSS remains the standard benchmark and the NASA repository adds C-MAPSS-2 plus the PHM08 Challenge data. For other components the same repository hosts battery aging, bearing vibration and FEMTO bearing degradation, CNC milling tool wear, IGBT and capacitor aging and aluminium fatigue crack growth - 21 run-to-failure datasets in all.