# Incident 20120727018409I: Cessna 210B, Fort Worth, TX, July 27, 2012

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: July 27, 2012, 17:08 local time
- Place: Fort Worth, TX
- Damage: Minor damage
- Phase of flight: Takeoff: Climb Out
- Operating rules: General operating rules (Part 91)
- Location: 32.7254° N, 97.3208° W: Placed by OpenAirDocs: center of Fort Worth, TX, within about 11 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=32.7254&lon=-97.3208&mi=10
- Aircraft: N9571X, registered now (https://openairdocs.org/aircraft/N9571X) (OpenAirDocs)
- Registry model: Cessna 210B (registry code 2073410, https://openairdocs.org/model/cessna-210b) (OpenAirDocs)
- Registry engine: Continental IO-470 series (registry code 17044, https://openairdocs.org/engine/continental-io-470-series) (OpenAirDocs)
- Reported make and model: CESSNA 210B
- Reported engine: CONT MOTOR IO-470 SER
- People aboard: 4
- Fatal injuries: 0
- Other injuries: 0
- Pilot certificates: Private pilot
- Pilot flight hours: 730 total, 496 in this make and model, 10 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20120727018409I

## Narrative

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

ON FRIDAY, JULY 27, 2012 AT APPROXIMATELY 5:08PM CST, CESSNA 210B, N9571X, LANDED ON THE IH35 SOUTH BOUND ACCESS ROAD APPROXIMATELY 4 MILES WEST OF THE FORT WORTH SPINKS AIRPORT (FWS), TEXAS.THE AIRCRAFT LANDED GEAR UP AND FLAPS UP SHORTLY AFTER DEPARTURE OF SPINKS AIRPORT.  THE PILOT REPORTED THAT THE ENGINE STARTED RUNNING VERY "ROUGH" SHORTLY AFTER TAKE OFF AND THEN COMPLETELY STOPPED.  THE PILOT REPORTED THAT HE CHANGED FUEL TANKS FROM RIGHT TO LEFT JUST PRIOR TO STOPPAGE.  THE PILOT WAS ENROUTE TO HOUSTON, TX WITH HIS WIFE, BROTHER AND SISTER-IN-LAW.  NO INJURIES WERE REPORTED.  THE PILOT REPORTED THAT HE DID NOT HAVE TIME TO PUMP THE GEAR OR FLAPS DOWN PRIOR TO LANDING.  MINOR DAMAGE TO THE UNDER CARRIAGE AND ONE PROP.  PHOTOS OF THE #2 CYLINDER AND SPARK PLUG WAS SENT TO CONTINENTAL ENGINES CORP FOR CONSULTATION.  CONSENSUS WITH THE CONTINENTAL INVESTIGATOR, FAA INSPECTOR AND OWNER (A&P MECHANIC) WAS THAT DETENATION WAS THE CAUSE FOR THE #2 CYLINDER TO FAIL.  THE INVESTIGATION FAILED TO IDENTIFY THE EXACT REASON WHY DETENATION OCCURED.

## Other reports on N9571X (1)

Matched to the same aircraft by N-number and date.

- [Accident 19770429009929A](https://openairdocs.org/incident/19770429009929A), Apr 29, 1977: Cessna 210B (N9571X), Fenton, MO, Substantial damage. Main gear observed in intermediate position on final. Left gear collapsed into wheel-well on ldg

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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