NTSB CAROL · Event
Event MIA95LA129
Aircraft involved
Probable cause & findings
The failure of the tail wheel landing gear system for undetermined reasons. This resulted in an on-ground loss of control on landing rollout, ground loop, and collapse of the right main landing gear.
Factual narrative
On April 26, 1995, about 1912 eastern daylight time, a Pitts S-2B, N711BT, registered to Everglades Aerobatic, operating as a 14 CFR Part 91 instructional flight, ground looped on landing at Naples Municipal Airport and crashed. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The certified flight instructor/commercial pilot, and the rated student pilot (airline transport pilot) were not injured. The flight originated from Naples, Florida, about 50 minutes before the accident. the accident was initially reported to the NTSB as an incident, and was up-graded to an accident on May 10, 1995. The flight instructor stated he thought the rated student pilot allowed the airplane to roll too much to the right before exiting the runway. The student pilot applied left rudder, however, he thought the student pilot applied too much left rudder, and he applied right rudder. The airplane continued to the left 180 degrees. The right main landing gear collapsed, and the airplane came to a full stop. Examination of the airplane by the Director of Maintenance for Sun Aircraft Services USA, Inc., revealed the right spring on the tail wheel to be hanging free, the attachment clip was missing, and was not located. The flight instructor stated while taxiing to his hangar on a previous flight on April 12, 1995, the tail wheel steering did not feel right. Subsequent examination of the tail wheel assembly revealed the right spring was loose and the attachment clip had vibrated off. The airplane was taken to Naples Air Center, Inc., for repair. The tail wheel spring and attachment clips were worn and required replacement. Mr. Alfred A. Bennett, Naples Air Center, Inc., stated in a letter dated May 22, 1995, that it would be virtually impossible for a new attachment clip to vibrate loose from its installation and fall off during normal operation because of the tension required to open the clip. Possibly during a ground loop the stress in the opposing direction and the severe side load encountered may be enough to open or break the clip. Examination of photographs submitted with the NTSB Pilot/Operator Aircraft Accident Report of the tail wheel assembly revealed no evidence of distortion on the chain attached to the tail wheel spring. The airplane veered to the left on landing rollout. The right main landing gear collapsed, and the airplane came to a full stop. Examination of the airplane revealed the right hand spring on the tail wheel to be hanging free, the attachment clip was missing, and was not located. There was no evidence of distortion on the chain attached to the tail wheel spring. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_MIA95LA129.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, loss of control, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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- Semantic Scholar 2016 · Article (Interacción)
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- NTSB Aircraft Accident Reports 2002 · Accident report
Loss of Control and Impact with Pacific Ocean — Alaska 261
Alaska Airlines Flight 261 (MD-83) Pacific Ocean, January 31, 2000 — 88 fatalities. Definitive investigation of the Alaska 261 pitch-runaway-and-loss-of-control crash.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
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