# NTSB investigations: Cessna 208B, 2005

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 SEA06LA031](https://openairdocs.org/ntsb/SEA06LA031.md): Cessna 208B · Portland, OR · Accident · Minor injuries · Limited investigation · Final report · Dec 24, 2005 · N753FE · Substantial damage
  > A partial loss of engine power for an undetermined reason during the initial takeoff climb resulting in an in-flight collision with objects.
- [NTSB ANC06CA012](https://openairdocs.org/ntsb/ANC06CA012.md): Cessna 208 · Brevig Mission, AK · Accident · No injuries · Data collection · Final report · Dec 19, 2005 · N303GV · Substantial damage
  > The pilot's inadequate compensation for crosswind conditions, which resulted in the left wing striking the ground while taxiing. A factor in the accident was a crosswind.
- [NTSB ANC06CA011](https://openairdocs.org/ntsb/ANC06CA011.md): Cessna 208B · Newtok, AK · Accident · No injuries · Data collection · Final report · Dec 13, 2005 · N454SF · Substantial damage
  > The pilot's inadequate compensation for gusting crosswind conditions, which resulted in the airplane exiting the runway, encountering snow, and the nose gear collapsing. Factors associated with the accident were the gusting wind and the icy runway.
- [NTSB DFW06LA010](https://openairdocs.org/ntsb/DFW06LA010.md): Cessna 208 · Round Rock, TX · Accident · Minor injuries · Limited investigation · Final report · Oct 19, 2005 · N978FE · Substantial damage
  > The loss of engine power due to the failure of the engine-driven fuel pump. A contributing factor was the inadequate inspection of the engine driven fuel pump.
- [NTSB LAX05LA244](https://openairdocs.org/ntsb/LAX05LA244.md): Cessna 208B · Globe, AZ · Accident · Minor injuries · Limited investigation · Final report · Jul 22, 2005 · N717BT · Substantial damage
  > The fatigue failure of the compressor turbine stator vane, the liberation of vane material into the compressor turbine, and the total loss of engine power. Also causal was the operator's failure to inspect the compressor turbine vane during fuel nozzle checks.
- [NTSB DFW05IA150](https://openairdocs.org/ntsb/DFW05IA150.md): Cessna 208B · Clarendon, TX · Incident · No injuries · Incident investigation · Final report · Jun 7, 2005 · N9505B · No damage
  > The loss of total engine power due to damage of the compressor stator vanes caused by a foreign object. A contributing factor was an in-flight ingestion of bird(s).

## 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 year(c."eventDate") = 2005
  AND c."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('2073701', '2073700', '2073705'))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESC
```

This list as a web page: https://openairdocs.org/ntsb?model=2073701&year=2005

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