Skip to content

ERA12CA434

2012-07-07 · Bayport, New York, United States · Minor · 1 aircraft · Status: Completed

Airport 23N

Current FAA registration · N3993P

Make / Model
JONES PETER M BOEING/JONES 75
Year of manufacture
1984 · 28 years old at event
Engine
CONT MOTOR W670 SERIES (250 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19841031
ADS-B equipped
Yes — Mode-S A4A707

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The airplane’s encounter with a wind shift to a tailwind during takeoff, which resulted in the pilot’s decision to abort the takeoff and the airplane’s subsequent runway overrun.

Factual narrative

The pilot reported he conducted 6 previous uneventful flights utilizing both runway 18 and 36 for takeoff due variable winds. He elected to depart from runway 18 on the accident flight because the windsock indicated a primarily southwesterly wind. The pilot stated that the takeoff roll was normal; however, shortly after liftoff the airplane encountered a tailwind which resulted in a degradation of performance. The airplane began to sink and lose airspeed, and the pilot elected to abort the takeoff. The airplane touched back down onto the runway, and subsequently nosed-over, which resulted in substantial damage to the vertical stabilizer. The pilot, pilot-rated passenger and several witnesses reported a wind shift around the time of the accident. A weather report from a nearby airport revealed a 20 degree shift in wind direction and a 7 knot increase in winds with a 24 knot gust from the northwest during the hour that the accident took place. Postaccident inspection of the airplane revealed that there were no mechanical anomalies that would have precluded normal operation. The pilot reported that he had conducted six previous uneventful flights on the day of the accident utilizing both runways 18 and 36 for takeoff due to variable winds. He elected to depart from runway 18 on the accident flight, because the windsock indicated a primarily southwesterly wind. The pilot stated that the takeoff roll was normal; however, shortly after liftoff, the airplane encountered a tailwind, which resulted in a degradation of performance. The airplane began to sink and lose airspeed, and the pilot aborted the takeoff. The airplane touched back down onto the runway, and the pilot applied the brakes in an effort to stop the airplane on the remaining runway. The airplane nosed over, which resulted in substantial damage to the vertical stabilizer. The pilot, pilot-rated passenger, and several witnesses reported a wind shift around the time of the accident. Weather reports from a nearby airport revealed that, during the period from about 1 hour 40 minutes before to about 20 minutes after the accident, there was a 40 degree shift in wind direction and an increase in wind speed from 9 knots to 18 knots, gusting to 24 knots. Postaccident examination of the airplane revealed no mechanical anomalies that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Environmental issues-Conditions/weather/phenomena-Wind-Sudden wind shift-Effect on operation - C
  • — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Climb rate-Attain/maintain not possible

Verbatim from NTSB's published report. Source file NTSB_2012_ERA12CA434.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.