FAILURE MAP

Understand the failure.
Verify the repair.

Small, reproducible software failures. The broken implementation, the fix that didn’t work, and the one that passed—preserved together.

Explore the cases ↓How results are verified ↗
100840Executable case variants
20168Distinct failure mechanisms
302520Executed implementations
20168Open-access cases

WHAT THE ARCHIVE CONTAINS

100840 executable cases. 20168 are open.

Every case records the implementation that fails, the fix that did not work, and the repair that passed its checks—with recorded outputs and source hashes. This release adds 100840 cases across 20168 failure mechanisms and 254 domains.

The open tier gives you the failure and the unsuccessful fix for one case in every mechanism. The remaining 80672 cases, 5 variants per mechanism, are member-only: the verified repair, its recorded checks, and the full fixture suite are held in the member archive. Read the methodology ↗

A RECORD OF WHAT WENT WRONG

Browse the archive / 100840

Python · Standard library
REFERENCEFAILURE MECHANISMDOMAINACCESS
FA-66101

Reduced moment scaled by one hundred · case 01

The reduced moment read off the loading graph is ten times too large.

Aviation weight and balance● Open access↗
FA-66102

Reduced moment scaled by one hundred · case 02

The reduced moment read off the loading graph is ten times too large.

Aviation weight and balance◈ Members↗
FA-66103

Reduced moment scaled by one hundred · case 03

The reduced moment read off the loading graph is ten times too large.

Aviation weight and balance◈ Members↗
FA-66104

Reduced moment scaled by one hundred · case 04

The reduced moment read off the loading graph is ten times too large.

Aviation weight and balance◈ Members↗
FA-66105

Reduced moment scaled by one hundred · case 05

The reduced moment read off the loading graph is ten times too large.

Aviation weight and balance◈ Members↗
FA-66106

CG divided from the reduced moment · case 01

The loaded CG is reported near zero inches.

Aviation weight and balance● Open access↗
FA-66107

CG divided from the reduced moment · case 02

The loaded CG is reported near zero inches.

Aviation weight and balance◈ Members↗
FA-66108

CG divided from the reduced moment · case 03

The loaded CG is reported near zero inches.

Aviation weight and balance◈ Members↗
FA-66109

CG divided from the reduced moment · case 04

The loaded CG is reported near zero inches.

Aviation weight and balance◈ Members↗
FA-66110

CG divided from the reduced moment · case 05

The loaded CG is reported near zero inches.

Aviation weight and balance◈ Members↗
FA-66111

Unknown units silently treated as pounds and inches · case 01

A stone or metre entry is added at face value instead of being rejected.

Aviation weight and balance● Open access↗
FA-66112

Unknown units silently treated as pounds and inches · case 02

A stone or metre entry is added at face value instead of being rejected.

Aviation weight and balance◈ Members↗
FA-66113

Unknown units silently treated as pounds and inches · case 03

A stone or metre entry is added at face value instead of being rejected.

Aviation weight and balance◈ Members↗
FA-66114

Unknown units silently treated as pounds and inches · case 04

A stone or metre entry is added at face value instead of being rejected.

Aviation weight and balance◈ Members↗
FA-66115

Unknown units silently treated as pounds and inches · case 05

A stone or metre entry is added at face value instead of being rejected.

Aviation weight and balance◈ Members↗
FA-66116

Floor pressure computed over the whole compartment floor · case 01

A heavy engine on a small skid passes the floor-loading check.

Aviation weight and balance● Open access↗
FA-66117

Floor pressure computed over the whole compartment floor · case 02

A heavy engine on a small skid passes the floor-loading check.

Aviation weight and balance◈ Members↗
FA-66118

Floor pressure computed over the whole compartment floor · case 03

A heavy engine on a small skid passes the floor-loading check.

Aviation weight and balance◈ Members↗
FA-66119

Floor pressure computed over the whole compartment floor · case 04

A heavy engine on a small skid passes the floor-loading check.

Aviation weight and balance◈ Members↗
FA-66120

Floor pressure computed over the whole compartment floor · case 05

A heavy engine on a small skid passes the floor-loading check.

Aviation weight and balance◈ Members↗
FA-66121

Compartment loaded exactly to its limit flagged over · case 01

Filling the bulk hold to exactly 800 lb raises an OVER finding.

Aviation weight and balance● Open access↗
FA-66122

Compartment loaded exactly to its limit flagged over · case 02

Filling the bulk hold to exactly 800 lb raises an OVER finding.

Aviation weight and balance◈ Members↗
FA-66123

Compartment loaded exactly to its limit flagged over · case 03

Filling the bulk hold to exactly 800 lb raises an OVER finding.

Aviation weight and balance◈ Members↗
FA-66124

Compartment loaded exactly to its limit flagged over · case 04

Filling the bulk hold to exactly 800 lb raises an OVER finding.

Aviation weight and balance◈ Members↗
FA-66125

Compartment loaded exactly to its limit flagged over · case 05

Filling the bulk hold to exactly 800 lb raises an OVER finding.

Aviation weight and balance◈ Members↗
FA-66126

Floor pressure uses the running compartment weight · case 01

Later pieces in a compartment are flagged for floor pressure caused by earlier pieces.

Aviation weight and balance● Open access↗
FA-66127

Floor pressure uses the running compartment weight · case 02

Later pieces in a compartment are flagged for floor pressure caused by earlier pieces.

Aviation weight and balance◈ Members↗
FA-66128

Floor pressure uses the running compartment weight · case 03

Later pieces in a compartment are flagged for floor pressure caused by earlier pieces.

Aviation weight and balance◈ Members↗
FA-66129

Floor pressure uses the running compartment weight · case 04

Later pieces in a compartment are flagged for floor pressure caused by earlier pieces.

Aviation weight and balance◈ Members↗
FA-66130

Floor pressure uses the running compartment weight · case 05

Later pieces in a compartment are flagged for floor pressure caused by earlier pieces.

Aviation weight and balance◈ Members↗
FA-66131

Floor-pressure finding cites a per-compartment index · case 01

Load controllers are pointed at the wrong manifest line for over-pressure pieces.

Aviation weight and balance● Open access↗
FA-66132

Floor-pressure finding cites a per-compartment index · case 02

Load controllers are pointed at the wrong manifest line for over-pressure pieces.

Aviation weight and balance◈ Members↗
FA-66133

Floor-pressure finding cites a per-compartment index · case 03

Load controllers are pointed at the wrong manifest line for over-pressure pieces.

Aviation weight and balance◈ Members↗
FA-66134

Floor-pressure finding cites a per-compartment index · case 04

Load controllers are pointed at the wrong manifest line for over-pressure pieces.

Aviation weight and balance◈ Members↗
FA-66135

Floor-pressure finding cites a per-compartment index · case 05

Load controllers are pointed at the wrong manifest line for over-pressure pieces.

Aviation weight and balance◈ Members↗
FA-66136

Pieces with invalid footprints counted in hold totals · case 01

A rejected zero-footprint piece still pushes its compartment into OVER.

Aviation weight and balance● Open access↗
FA-66137

Pieces with invalid footprints counted in hold totals · case 02

A rejected zero-footprint piece still pushes its compartment into OVER.

Aviation weight and balance◈ Members↗
FA-66138

Pieces with invalid footprints counted in hold totals · case 03

A rejected zero-footprint piece still pushes its compartment into OVER.

Aviation weight and balance◈ Members↗
FA-66139

Pieces with invalid footprints counted in hold totals · case 04

A rejected zero-footprint piece still pushes its compartment into OVER.

Aviation weight and balance◈ Members↗
FA-66140

Pieces with invalid footprints counted in hold totals · case 05

A rejected zero-footprint piece still pushes its compartment into OVER.

Aviation weight and balance◈ Members↗
FA-66141

Trim interpolation measured from the upper node · case 01

Values between nodes are mirrored: a CG just aft of a node gets nearly the next node trim.

Aviation weight and balance● Open access↗
FA-66142

Trim interpolation measured from the upper node · case 02

Values between nodes are mirrored: a CG just aft of a node gets nearly the next node trim.

Aviation weight and balance◈ Members↗
FA-66143

Trim interpolation measured from the upper node · case 03

Values between nodes are mirrored: a CG just aft of a node gets nearly the next node trim.

Aviation weight and balance◈ Members↗
FA-66144

Trim interpolation measured from the upper node · case 04

Values between nodes are mirrored: a CG just aft of a node gets nearly the next node trim.

Aviation weight and balance◈ Members↗
FA-66145

Trim interpolation measured from the upper node · case 05

Values between nodes are mirrored: a CG just aft of a node gets nearly the next node trim.

Aviation weight and balance◈ Members↗
FA-66146

Table end points rejected as out of range · case 01

A CG exactly at the forward or aft table limit returns ERR_RANGE.

Aviation weight and balance● Open access↗
FA-66147

Table end points rejected as out of range · case 02

A CG exactly at the forward or aft table limit returns ERR_RANGE.

Aviation weight and balance◈ Members↗
FA-66148

Table end points rejected as out of range · case 03

A CG exactly at the forward or aft table limit returns ERR_RANGE.

Aviation weight and balance◈ Members↗
FA-66149

Table end points rejected as out of range · case 04

A CG exactly at the forward or aft table limit returns ERR_RANGE.

Aviation weight and balance◈ Members↗
FA-66150

Table end points rejected as out of range · case 05

A CG exactly at the forward or aft table limit returns ERR_RANGE.

Aviation weight and balance◈ Members↗
FA-66151

Out-of-table CG clamped to the nearest trim value · case 01

A CG beyond the certified trim table produces a plausible-looking trim setting.

Aviation weight and balance● Open access↗
FA-66152

Out-of-table CG clamped to the nearest trim value · case 02

A CG beyond the certified trim table produces a plausible-looking trim setting.

Aviation weight and balance◈ Members↗
FA-66153

Out-of-table CG clamped to the nearest trim value · case 03

A CG beyond the certified trim table produces a plausible-looking trim setting.

Aviation weight and balance◈ Members↗
FA-66154

Out-of-table CG clamped to the nearest trim value · case 04

A CG beyond the certified trim table produces a plausible-looking trim setting.

Aviation weight and balance◈ Members↗
FA-66155

Out-of-table CG clamped to the nearest trim value · case 05

A CG beyond the certified trim table produces a plausible-looking trim setting.

Aviation weight and balance◈ Members↗
FA-66156

%MAC rounded to a whole percent before lookup · case 01

Trim jumps in steps and differs by up to half a percent of MAC worth of trim.

Aviation weight and balance● Open access↗
FA-66157

%MAC rounded to a whole percent before lookup · case 02

Trim jumps in steps and differs by up to half a percent of MAC worth of trim.

Aviation weight and balance◈ Members↗
FA-66158

%MAC rounded to a whole percent before lookup · case 03

Trim jumps in steps and differs by up to half a percent of MAC worth of trim.

Aviation weight and balance◈ Members↗
FA-66159

%MAC rounded to a whole percent before lookup · case 04

Trim jumps in steps and differs by up to half a percent of MAC worth of trim.

Aviation weight and balance◈ Members↗
FA-66160

%MAC rounded to a whole percent before lookup · case 05

Trim jumps in steps and differs by up to half a percent of MAC worth of trim.

Aviation weight and balance◈ Members↗
FA-66161

Unsupported flap setting falls back to another table · case 01

Flaps 10 returns a trim from the flaps 15 table instead of an error.

Aviation weight and balance● Open access↗
FA-66162

Unsupported flap setting falls back to another table · case 02

Flaps 10 returns a trim from the flaps 15 table instead of an error.

Aviation weight and balance◈ Members↗
FA-66163

Unsupported flap setting falls back to another table · case 03

Flaps 10 returns a trim from the flaps 15 table instead of an error.

Aviation weight and balance◈ Members↗
FA-66164

Unsupported flap setting falls back to another table · case 04

Flaps 10 returns a trim from the flaps 15 table instead of an error.

Aviation weight and balance◈ Members↗
FA-66165

Unsupported flap setting falls back to another table · case 05

Flaps 10 returns a trim from the flaps 15 table instead of an error.

Aviation weight and balance◈ Members↗
FA-66166

Left and right lateral moments added instead of cancelling · case 01

Symmetric left and right loads produce a large lateral CG offset.

Aviation weight and balance● Open access↗
FA-66167

Left and right lateral moments added instead of cancelling · case 02

Symmetric left and right loads produce a large lateral CG offset.

Aviation weight and balance◈ Members↗
FA-66168

Left and right lateral moments added instead of cancelling · case 03

Symmetric left and right loads produce a large lateral CG offset.

Aviation weight and balance◈ Members↗
FA-66169

Left and right lateral moments added instead of cancelling · case 04

Symmetric left and right loads produce a large lateral CG offset.

Aviation weight and balance◈ Members↗
FA-66170

Left and right lateral moments added instead of cancelling · case 05

Symmetric left and right loads produce a large lateral CG offset.

Aviation weight and balance◈ Members↗
FA-66171

Lateral limit enforced only to the right · case 01

A heavy left-side hoist load is reported within limits.

Aviation weight and balance● Open access↗
FA-66172

Lateral limit enforced only to the right · case 02

A heavy left-side hoist load is reported within limits.

Aviation weight and balance◈ Members↗
FA-66173

Lateral limit enforced only to the right · case 03

A heavy left-side hoist load is reported within limits.

Aviation weight and balance◈ Members↗
FA-66174

Lateral limit enforced only to the right · case 04

A heavy left-side hoist load is reported within limits.

Aviation weight and balance◈ Members↗
FA-66175

Lateral limit enforced only to the right · case 05

A heavy left-side hoist load is reported within limits.

Aviation weight and balance◈ Members↗
FA-66176

Simultaneous longitudinal and lateral exceedance reported as LONG only · case 01

The crew fixes the longitudinal problem and departs with the lateral CG still out of limits.

Aviation weight and balance● Open access↗
FA-66177

Simultaneous longitudinal and lateral exceedance reported as LONG only · case 02

The crew fixes the longitudinal problem and departs with the lateral CG still out of limits.

Aviation weight and balance◈ Members↗
FA-66178

Simultaneous longitudinal and lateral exceedance reported as LONG only · case 03

The crew fixes the longitudinal problem and departs with the lateral CG still out of limits.

Aviation weight and balance◈ Members↗
FA-66179

Simultaneous longitudinal and lateral exceedance reported as LONG only · case 04

The crew fixes the longitudinal problem and departs with the lateral CG still out of limits.

Aviation weight and balance◈ Members↗
FA-66180

Simultaneous longitudinal and lateral exceedance reported as LONG only · case 05

The crew fixes the longitudinal problem and departs with the lateral CG still out of limits.

Aviation weight and balance◈ Members↗
FA-66181

Lateral CG exactly on the limit rejected · case 01

A load that places the lateral CG exactly at the limit is reported LAT.

Aviation weight and balance● Open access↗
FA-66182

Lateral CG exactly on the limit rejected · case 02

A load that places the lateral CG exactly at the limit is reported LAT.

Aviation weight and balance◈ Members↗
FA-66183

Lateral CG exactly on the limit rejected · case 03

A load that places the lateral CG exactly at the limit is reported LAT.

Aviation weight and balance◈ Members↗
FA-66184

Lateral CG exactly on the limit rejected · case 04

A load that places the lateral CG exactly at the limit is reported LAT.

Aviation weight and balance◈ Members↗
FA-66185

Lateral CG exactly on the limit rejected · case 05

A load that places the lateral CG exactly at the limit is reported LAT.

Aviation weight and balance◈ Members↗
FA-66186

Lateral CG divided by off-centerline weight only · case 01

One passenger in a side seat produces a lateral CG equal to the seat arm.

Aviation weight and balance● Open access↗
FA-66187

Lateral CG divided by off-centerline weight only · case 02

One passenger in a side seat produces a lateral CG equal to the seat arm.

Aviation weight and balance◈ Members↗
FA-66188

Lateral CG divided by off-centerline weight only · case 03

One passenger in a side seat produces a lateral CG equal to the seat arm.

Aviation weight and balance◈ Members↗
FA-66189

Lateral CG divided by off-centerline weight only · case 04

One passenger in a side seat produces a lateral CG equal to the seat arm.

Aviation weight and balance◈ Members↗
FA-66190

Lateral CG divided by off-centerline weight only · case 05

One passenger in a side seat produces a lateral CG equal to the seat arm.

Aviation weight and balance◈ Members↗
FA-66191

Offsetting adds and removes net out of the LMC tolerance · case 01

Swapping 300 kg of cargo for 290 kg is annotated as an LMC instead of requiring a new loadsheet.

Aviation weight and balance● Open access↗
FA-66192

Offsetting adds and removes net out of the LMC tolerance · case 02

Swapping 300 kg of cargo for 290 kg is annotated as an LMC instead of requiring a new loadsheet.

Aviation weight and balance◈ Members↗
FA-66193

Offsetting adds and removes net out of the LMC tolerance · case 03

Swapping 300 kg of cargo for 290 kg is annotated as an LMC instead of requiring a new loadsheet.

Aviation weight and balance◈ Members↗
FA-66194

Offsetting adds and removes net out of the LMC tolerance · case 04

Swapping 300 kg of cargo for 290 kg is annotated as an LMC instead of requiring a new loadsheet.

Aviation weight and balance◈ Members↗
FA-66195

Offsetting adds and removes net out of the LMC tolerance · case 05

Swapping 300 kg of cargo for 290 kg is annotated as an LMC instead of requiring a new loadsheet.

Aviation weight and balance◈ Members↗
FA-66196

Removed items shift the index as if added · case 01

Offloading a forward bag moves the index the same way as loading it.

Aviation weight and balance● Open access↗
FA-66197

Removed items shift the index as if added · case 02

Offloading a forward bag moves the index the same way as loading it.

Aviation weight and balance◈ Members↗
FA-66198

Removed items shift the index as if added · case 03

Offloading a forward bag moves the index the same way as loading it.

Aviation weight and balance◈ Members↗
FA-66199

Removed items shift the index as if added · case 04

Offloading a forward bag moves the index the same way as loading it.

Aviation weight and balance◈ Members↗
FA-66200

Removed items shift the index as if added · case 05

Offloading a forward bag moves the index the same way as loading it.

Aviation weight and balance◈ Members↗

INSPECTABLE BY DESIGN

Every result has a runnable source.

Runnable implementations with recorded outputs, source hashes, and explicit contracts. Related variants share a failure mechanism and belong together in evaluation splits.

Read the methodology ↗