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APEX TECHNICAL

FDB-0025 · ORIGINAL SOURCE VALUE

FMI-G-B8-000009

Registry: STAGEG_B8_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1__Failure_Modes. Original field names and values are displayed without translation or reinterpretation.

A
FMI-G-B8-000009
B
EFM-G-B7-000003
C
Progressive PP cell-wall buckling/crushing or core shear yielding
D
EFM-G-B7-000005
E
Progressive stiffness loss, matrix cracking, interface debond or accumulated core shear damage
F
Progressive core damage may lower cyclic stiffness and change failure location.
G
Flatwise compression or shear demand relative to the actual grade | Repeated loading under an uncalibrated spectrum
H
Progressive PP cell-wall buckling/crushing or core shear yielding interacting with Progressive stiffness loss, matrix cracking, interface debond or accumulated core shear damage
I
PP honeycomb core cell walls | Cyclic face / interface / core structural system
J
Progressive core damage may lower cyclic stiffness and change failure location. Potential consequence is a shift in stiffness, load capacity, damage location or fatigue retention; magnitude and probability are not established.
K
Future controlled evaluation: Load-displacement curve, residual thickness and damage location; Cycle history, stiffness retention, strain drift and damage progression; synchronize load-displacement records with DIC/acoustic-emission or sectioning where the approved protocol permits.
L
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
M
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
N
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
O
FAILURE_MODE_LOGIC
P
VERY_LOW
Q
NOT_OBSERVED
R
NOT_PERFORMED
S
AER-FC002-16-T700-PP-SHP
T
HYPOTHESIS_ONLY
U
NOT_EMPIRICAL
V
This is a mechanism-screening hypothesis for future observation planning, not an observed FC002 failure sequence or probability.

Identifiers mentioned in source fields

These are search links, not inferred engineering relationships.

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/STAGEG_B8_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1.xlsx
source_file_sha256
31a2907061ff3872f5527d842231a868f558ee78438db36e70cf8aeb2a3f4a03
source_locator
xlsx:sheet:10:Failure Modes:row:10
fields_sha256
a0942cd07691f580c3c9e09284ed89200483adcb52acdb35ee7eb8b3d650705c
source_version
FDB-0025