FDB-0025 · ORIGINAL SOURCE VALUE
FMI-G-B8-000004
Registry: failure_mode_interaction_registry. Original field names and values are displayed without translation or reinterpretation.
- affected_structural_layer
- PP honeycomb core geometry / cell architecture | Cyclic face / interface / core structural system
- confidence_level
- VERY_LOW
- configuration_id
- AER-FC002-16-T700-PP-SHP
- connected_prediction_ids
- PRED-G-B7-000004|PRED-G-B7-000005|PRED-G-B7-000009|PRED-G-B7-000010|PRED-G-B7-000012|PRED-G-B7-000013|PRED-G-B7-000014|PRED-G-B7-000015|PRED-G-B7-000016|PRED-G-B7-000017|PRED-G-B7-000018|PRED-G-B7-000019
- data_class
- HYPOTHESIS_ONLY
- empirical_status
- NOT_EMPIRICAL
- failure_interaction_id
- FMI-G-B8-000004
- failure_mode_a
- Core property or dimensional variability
- failure_mode_a_id
- EFM-G-B7-000001
- failure_mode_b
- Progressive stiffness loss, matrix cracking, interface debond or accumulated core shear damage
- failure_mode_b_id
- EFM-G-B7-000005
- future_physical_detection_method
- Future controlled evaluation: Density/dimension/conditioning plus compression response; Cycle history, stiffness retention, strain drift and damage progression; synchronize load-displacement records with DIC/acoustic-emission or sectioning where the approved protocol permits.
- initiation_driver
- Unconfirmed grade, cell size, thickness and environmental state | Repeated loading under an uncalibrated spectrum
- interaction_mechanism_hypothesis
- Core variability can change cyclic load sharing and accelerate stiffness-loss mechanisms.
- limitation
- This is a mechanism-screening hypothesis for future observation planning, not an observed FC002 failure sequence or probability.
- linked_prediction_ids
- PRED-G-B7-000004|PRED-G-B7-000005|PRED-G-B7-000009|PRED-G-B7-000010|PRED-G-B7-000012|PRED-G-B7-000013|PRED-G-B7-000014|PRED-G-B7-000015|PRED-G-B7-000016|PRED-G-B7-000017|PRED-G-B7-000018|PRED-G-B7-000019
- local_failure_mode
- Core property or dimensional variability interacting with Progressive stiffness loss, matrix cracking, interface debond or accumulated core shear damage
- observation_status
- NOT_OBSERVED
- physical_test_status
- NOT_PERFORMED
- potential_downstream_consequence
- Core variability can change cyclic load sharing and accelerate stiffness-loss mechanisms. Potential consequence is a shift in stiffness, load capacity, damage location or fatigue retention; magnitude and probability are not established.
- relationship_basis
- FAILURE_MODE_LOGIC
- trigger_parameter_keys
- face_architecture_factor|process_retention_factor|face_thickness_mm|core_thickness_mm|core_shear_strength_mpa|core_shear_modulus_mpa|fatigue_anchor_cycles|fatigue_exponent
Identifiers mentioned in source fields
These are search links, not inferred engineering relationships.
AER-FC002-16-T700-PP-SHPPRED-G-B7-000004PRED-G-B7-000005PRED-G-B7-000009PRED-G-B7-000010PRED-G-B7-000012PRED-G-B7-000013PRED-G-B7-000014PRED-G-B7-000015PRED-G-B7-000016PRED-G-B7-000017PRED-G-B7-000018PRED-G-B7-000019EFM-G-B7-000001EFM-G-B7-000005
Provenance
- archiveSha256
- ded5d3a55705d2387a6fec03fd5fd9c93d948acca3c3de8c66ed7a82fca45cc5
- virtual_path
- !/PICKLEBALL_DATABASE_APPROVED_FROZEN_BASELINES_THROUGH_STAGEG_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1_2026-09-15.zip!/stage_g_b8_cross_test_correlation_and_paddle_engineering_profile/approved_payload/STAGEG_B8_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1_2026-09-15.zip!/STAGEG_B8_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1/failure_mode_interaction_registry.csv
- source_file_sha256
- ed1a5fee67c947549382f06244d015d7c9757e7125f3edc7c0a71813ab8dcd76
- source_locator
- csv:row:4
- fields_sha256
- d9aeb33c99dcebd65634b600ec51dd15195687e1580cdcf317dc7e84c562d2ac
- source_version
- FDB-0025