# Accident 20000725005559A: Cessna TU206G, Mccall, ID, July 25, 2000

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: July 25, 2000, 11:40 local time
- Place: Mccall, ID
- Damage: No damage
- Operating rules: Air taxi and commuter (Part 135)
- Operator: REAA
- Location: 45.0696° N, 115.9705° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=45.0696&lon=-115.9705&mi=10
- Aircraft: N206RA, a cancelled registration (https://openairdocs.org/deregistered/N206RA-2013-08-16) (OpenAirDocs)
- Registry model: Cessna TU206G (registry code 2073357, https://openairdocs.org/model/cessna-tu206g) (OpenAirDocs)
- Registry engine: Continental TSIO-520 series (registry code 17040, https://openairdocs.org/engine/continental-tsio-520-series) (OpenAirDocs)
- Reported make and model: CESSNA TU206G
- People aboard: 1
- Fatal injuries: 1
- NTSB investigation: [NTSB SEA00FA142](https://openairdocs.org/ntsb/SEA00FA142) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20000725005559A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) THE AIRCRAFT DEPARTED FROM A PRIVATE MOUNTAIN AIRSTRIP AT PISTOL CREEK, IDAHO, WHICH IS LOCATED 45 NAUTICAL MILES EAST OF MCCALL, IDAHO (MYL). WITNESSES STATED THAT THE AIRCRAFT LOST POWER AFTER TAKEOFF AND THE PILOT ATTEMPTED TO RETURN TO THE AIRSTRIP.  THE AIRCRAFT CRASHED IN THE TREES AND BURNED ADJACENT TO THE AIRSTRIP.

## The NTSB's investigation of this event (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA00FA142](https://openairdocs.org/ntsb/SEA00FA142), Jul 25, 2000: Cessna TU-206G (N206RA), Pistol Creek, ID, destroyed, 1 fatal. Probable cause: A loss of engine power due to the fracture of the #2 cylinder intake valve stem and the puncturing of the #2 piston dome by the intake valve head. Factors include no suitable landing site within the…

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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