# Accident 19910213018409A: Piper PA32R301, Plant City, FL, February 13, 1991

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: February 13, 1991, 14:45 local time
- Place: Plant City, FL
- Airport: Plant City Municipal Airport
- Damage: Substantial damage
- Phase of flight: Roll-Out (Fixed Wing)
- Operating rules: General operating rules (Part 91)
- Location: 27.0806° N, 82.1303° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=27.0806&lon=-82.1303&mi=10
- Aircraft: N95T, registered now (https://openairdocs.org/aircraft/N95T) (OpenAirDocs)
- Registry model: Piper PA-32R-301 (registry code 7103218, https://openairdocs.org/model/piper-pa-32r-301) (OpenAirDocs)
- Registry engine: Lycoming 0-540 series (registry code 41532, https://openairdocs.org/engine/lycoming-0-540-series) (OpenAirDocs)
- Reported make and model: PIPER PA32R301
- Reported engine: LYC IO540K1G5
- People aboard: 1
- Fatal injuries: 0
- Pilot flight hours: 820 total, 32 in the last 90 days
- NTSB investigation: [NTSB MIA91LA081](https://openairdocs.org/ntsb/MIA91LA081) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19910213018409A

## Narrative

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

DRIFTED OFF DOWNWIND SIDE RUNWAY LANDING IN GUSTY CROSSWIND. OVER CORRECTED CAUSING SIDE LOAD. FOLDED RIGHT GEAR.

## 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 MIA91LA081](https://openairdocs.org/ntsb/MIA91LA081), Feb 13, 1991: Piper PA-32R-301 (N95T), Plant City, FL, substantial damage. Probable cause: FAILURE OF THE PILOT TO MAINTAIN PROPER ALIGNMENT DURING THE LANDING ROLL, EXCESSIVE RUDDER INPUT, AND LOSS OF DIRECTIONAL CONTROL RESULTING IN THE COLLAPSE OF THE RIGHT MAIN LANDING GEAR.

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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