# Accident 19930914034379A: Piper PA34200, St Louis, MO, September 14, 1993

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: September 14, 1993, 19:30 local time
- Place: St Louis, MO
- Airport: Weiss Airport
- Damage: Substantial damage
- Phase of flight: Go Round (Aborted VFR)
- Operating rules: General operating rules (Part 91)
- Location: 38.5290° N, 90.4494° W: From the FAA, an estimate near the named town, within about 3 miles
- Nearby events: https://openairdocs.org/map.md?lat=38.5290&lon=-90.4494&mi=10
- Aircraft: N3084T, a cancelled registration (https://openairdocs.org/deregistered/N3084T-2012-09-05) (OpenAirDocs)
- Registry model: Piper PA-34-200 (registry code 7103405, https://openairdocs.org/model/piper-pa-34-200) (OpenAirDocs)
- Registry engine: Lycoming I0360 series (registry code 41515, https://openairdocs.org/engine/lycoming-i0360-series) (OpenAirDocs)
- Reported make and model: PIPER PA34200
- Reported engine: LYC IO360C1E6
- People aboard: 3
- Fatal injuries: 0
- Pilot flight hours: 2,188 total, 5 in this make and model, 12 in the last 90 days
- NTSB investigation: [NTSB CHI93LA361](https://openairdocs.org/ntsb/CHI93LA361) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/19930914034379A

## Narrative

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

WIND GUST RAISED A WING TRYING TO ALIGN WITH RUNWAY. BEGAN GO AROUND LOST CONTROL. ROLLED. STRUCK 4 PARKED AIRCRAFT

## 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 CHI93LA361](https://openairdocs.org/ntsb/CHI93LA361), Sep 15, 1993: Piper PA-34-200 (N3084T), Fenton, MO, substantial damage. Probable cause: FAILURE OF THE PILOT TO MAINTAIN LATERAL (ROLL) AND DIRECTIONAL CONTROL OF THE AIRPLANE, WHEN ONE ENGINE HESITATED TO RESPOND TO APPLICATION OF POWER DURING AN ATTEMPTED GO-AROUND. FACTORS RELATED TO…

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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