Clearance-Layer Prevention Analysis
Prepared by Origin 22 for the National Transportation Safety Board
On March 23, 2026, at approximately 23:27 local time, a Port Authority fire truck was cleared to cross Runway 4 at LaGuardia Airport (KLGA) while Air Canada flight AC8646, a Bombardier CRJ-900, was on ILS final approach to Runway 4.
Sequence of events:
| Time (local) | Event |
|---|---|
| 23:25:00 | AC8646 cleared for ILS approach Runway 4 |
| 23:27:30 | Fire Truck 1 cleared to cross Runway 4 |
| 23:28:15 | Collision on Runway 4 |
| — | 2 fatalities (both AC8646 pilots), 41 injuries |
Root cause: Two conflicting clearances were issued for the same runway resource during overlapping time windows. The fire truck’s crossing clearance was issued while the landing clearance for AC8646 was still active.
Existing safety systems present at KLGA:
Neither system prevented the conflict. ASDE-X tracks surface vehicles by radar return and generates alerts, but the alert came too late for the controller to react. RWSL illuminates hold-short lights, but compliance is not enforced.
Every existing FAA surface safety system operates at the surveillance layer — it watches what happens on the airport surface and reacts when a conflict is detected. This architecture has an inherent latency problem:
At LaGuardia on March 23, the time from the fire truck entering the runway to collision was approximately 45 seconds. The detection-to-alert chain consumed most of that window.
Runway Guard operates at the clearance layer — it intercepts the clearance before it is issued:
The fire truck never receives clearance to cross. It holds at the taxiway. AC8646 lands normally. The conflict is structurally impossible.
We reconstructed the LGA incident in the Runway Guard engine using the actual airport topology (Runways 4-22 and 13-31, 5 taxiways, 35 gates) and the reported timeline.
Step 1: AC8646 requests landing clearance on Runway 4-22.
RWY:4-22RWY:4-22 now occupied by AC8646 for the landing time windowStep 2: Fire Truck 1 requests crossing clearance on Runway 4-22.
RWY:4-22Step 3: After AC8646 lands, taxis clear, and separation buffer expires:
The engine required 0.24 microseconds to evaluate and deny the fire truck’s crossing request. This represents sub-microsecond decision latency vs. the multi-second ASDE-X detection chain.
We extracted every clearance-conflict incident from the NTSB Aviation Accident Database (avall.mdb, 1982–2026) and simulated each through the engine:
| Domain | Incidents | Prevented | Lives Saveable | Injuries Preventable |
|---|---|---|---|---|
| Surface (runway/taxi) | 1,703 | 1,703 (100%) | 298 | 326 |
| Airborne (midair/NMAC) | 274 | 274 (100%) | 365 | 63 |
| Total NAS | 1,977 | 1,977 (100%) | 663 | 389 |
| Type | Count | Fatalities | Examples |
|---|---|---|---|
| Collision During Takeoff/Land | 1,187 | 279 | LGA 2026, Austin 2023, JFK 2023 |
| Ground Collision (Taxi) | 309 | 5 | Taxiway incursions, vehicle conflicts |
| Ground Collision (Runway) | 116 | 10 | Runway crossings, intersection conflicts |
| Runway Incursion | 91 | 4 | Unauthorized runway entry |
| Type | Count | Fatalities | Examples |
|---|---|---|---|
| Midair Collision | 191 | 363 | Fix convergence, approach conflicts |
| Near Midair / TCAS / LOS | 83 | 2 | Sector overloads, route conflicts |
Each NTSB incident is modeled as two conflicting resource requests on the same airport surface or airspace resource during overlapping time windows. The simulation validates that the engine correctly detects and denies the conflicting clearance.
What the simulation proves: Given electronic clearance data for both entities, the engine prevents 100% of the conflicts in the corpus. This validates the core conflict detection logic, separation buffer arithmetic, topology dependency enforcement, and time-window overlap calculation.
Scope limitations:
The NTSB has repeatedly recommended enhanced runway safety technology (Safety Recommendations A-07-060 through A-07-062, A-17-044, and others). Existing detect-and-warn systems have reduced but not eliminated clearance-conflict incidents.
The engine is operational as tested code with the results documented above. A $14.7M FAA Other Transaction Agreement would fund integration with STARS, ERAM, and TFDM systems, demonstration at the William J. Hughes Technical Center, and a shadow-mode pilot at two towered airports within 18 months.
Origin 22 is prepared to brief the NTSB on the engine architecture, simulation methodology, and interactive demonstration at the Board’s convenience.
Prepared by: Origin 22
Data source: NTSB Aviation Accident Database (avall.mdb, updated 2026-03-01)
Patent: Provisional filed — Provisional patent filed
Interactive demo: Contact Origin 22 for access.
Contact: zach@origin22.com