⚠ Fictional demo record. Not a real, current, or legally binding requirement.
AD-2026-004
“Wing Spar Fatigue Inspection”
Authority
EASA — European Union Aviation Safety Agency
Revision
0
Effective
2026-02-01
The AeroComply Loop for this Requirement
Description
Fictional demo AD requiring a one-time fatigue inspection of the wing spar on affected A320-200 aircraft beyond a specified cycle threshold.
Compliance time: Within 1,000 flight cycles
Impact — Affected Aircraft, Compliance Status & Action Required
This traces only real applicability assessment links already recorded in the dataset — aircraft this requirement has actually been evaluated against, not an inferred fleet match.
| Aircraft | System Result | Compliance Status | Action Required |
|---|---|---|---|
| N207ML | Applicable | Non-Compliant | Corrective action required |
| N118ML | Not Applicable | Compliant | None — compliant |
| N305ML | Applicable | Non-Compliant | Corrective action required |
Linked Maintenance Tasks
Maintenance events recorded with a direct relatedRequirementId link to this requirement.
AI Assistance — Coming in M4
Planned: explain this regulation in plain language, summarize evidence, retrieve relevant regulatory passages, and answer grounded questions.
The rules engine produces the compliance decision. AI explains and assists — it never makes or overrides the decision (see ADR-004).