# NTSB investigations: Bombardier CL-600-2C11

NTSB aviation accident and incident investigations since 1962: the probable cause, findings, aircraft, crew, weather and docket of each, linked to the FAA registry and the FAA’s own reports.

## Latest cases

- [NTSB ENG26LA011](https://openairdocs.org/ntsb/ENG26LA011.md): Bombardier CL-600-2C11 · Hibbing, MN · Incident · No injuries · Class 4 · Limited · Final report · Nov 23, 2025 · N707EV · No damage
  > The elevator control restriction was caused by the failure of an elevator autopilot servo control cable which failed due to cyclic fatigue. The slack in the cable wrapped around the servo mount in such a way that it interfered with the rotation of the servo…
- [NTSB ENG25LA009](https://openairdocs.org/ntsb/ENG25LA009.md): Bombardier CL-600-2C11 · Dulles, VA · Incident · No injuries · Class 4 · Limited · Final report · Nov 20, 2024 · N501GJ · No damage
  > The elevator control restriction was caused by the failure of the elevator autopilot servo control cable, which failed due to cyclic fatigue. The slack in the broken cable wrapped around the elevator autopilot servo mount in such a way that it was bound…
- [NTSB DCA21LA024](https://openairdocs.org/ntsb/DCA21LA024.md): Bombardier CL600 2C10 · Phoenix, AZ · Accident · Serious injuries · Class 4 · Limited · Final report · Nov 14, 2020 · N778SK · No damage
  > The flight attendant’s use of improper procedures when opening the main cabin door.
- [NTSB DCA17LA182](https://openairdocs.org/ntsb/DCA17LA182.md): Bombardier CL 600 2C10 · Denver, CO · Accident · No injuries · Class 3 · Limited · Final report · Jul 2, 2017 · N796SK · Substantial damage
  > The fuel supply tube fitting pulling out of the left engine’s operability bleed valve (OBV) during the landing rollout, allowing fuel to leak and contact hot engine cases, which ignited a fire that caused thermal damage to the engine pylon. Contributing to…
- [NTSB ENG12IA004](https://openairdocs.org/ntsb/ENG12IA004.md): Bombardier CL600 2C10 · Atlanta, GA · Incident · No injuries · Incident investigation · Final report · Oct 23, 2011 · N751EV · No damage
  > The Start Operability Bleed Valve (OBV) fuel return adapter-fitting fractured and separated in cyclic fatigue, which allowed fuel to spill onto a hot engine case that ignited the undercowl fire. The OBV fuel adapter-fitting was dropped and the damage reduced…

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT c."ntsbNumber", c."eventDate", c."eventType", c."eventCity", c."eventStateOrRegion", a.n_number, a."aircraftMake", a."aircraftModel", c."highestInjuryLevel", c."totalFatal", c."completionStatus", c.report_url
FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c."mKey" AND a.position = 1
WHERE c."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('1390021'))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESC
```

This list as a web page: https://openairdocs.org/ntsb?model=1390021

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