NTSB CAROL · Event
Event ATL02LA149
Registry · N957T
FAA Aircraft Registry record.
Make / Model
PIPER PA-32R-301
Year of manufacture
2000 · 2 years old at event
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
7 seats · 1 engine
Last airworthiness date
20001011
ADS-B equipped
Yes — Mode-S AD5051
Registrant of record
SEVERN VALLEY AVIATION INC TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
Pilot in command failed to maintain directional control of the airplane during the landing roll that resulted in a ground loop and the overload failure of the right main landing gear.
Factual narrative
On August 1, 2002, at 1347 eastern daylight tine a Piper PA-32R-301, N957T, registered to B & B Contracting and operated by a private pilot, right main landing gear collapsed while taxiing after landing at Fort Lauderdale Executive Airport in Fort Lauderdale, Florida. The personal flight operated under the provisions of Title 14 CFR Part 91 with an instrument flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane was substantially damaged, and the private pilot and passenger were not injured. The flight departed Naples, Florida, at 1300 on August 1, 2001. According to the private pilot, as he applied braking action during rollout after landing the airplane began to veer left. Although the pilot added right rudder to correct the problem, he was not able to stop the airplane from veering to the left. The right main landing gear collapsed and the airplane spun around approximately 180 degrees, coming to rest on the runway surface with a heading of 130 degrees. Examination of the airplane revealed a significant amount of side load had occurred, and both the left and right main landing gear collapsed to the left as a result. The right wing was damaged when the landing gear collapsed. There were several tire marks on the runway that terminated at the point where the airplane rested. The pilot did not report a mechanical problem with the airplane prior to and during the accident sequence of events. The recorded winds were variable at three knots. According to the private pilot, as he applied braking action during rollout, the airplane began to veer left. Although he added right rudder to correct the problem, he was not able to stop the airplane from veering to the left. The right main landing gear collapsed and the airplane spun around approximately 180 degrees, coming to rest on the runway surface. Examination of the airplane revealed a significant amount of side load had occurred, and both the left and right main landing gears collapsed to the left. The right wing was damaged when the landing gear collapsed. There were several tire marks on the runway that terminated at the point where the airplane rested. The pilot did not report a mechanical problem with the airplane prior to and during the accident sequence of events. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_ATL02LA149.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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