BFO93LA179
1993-09-19 · NORTH KINGSTOWN, Rhode Island, United States · None · 1 aircraft · Status: Completed
Airport OQU
Current FAA registration · N9931Q
- Make / Model
- CESSNA 172M
- Year of manufacture
- 1975 · 18 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19750904
- ADS-B equipped
- Yes — Mode-S ADE052
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT INADVERTENTLY ALLOWED THE AIRPLANE TO STALL AS HE WAS MANEUVERING TO AVOID BIRDS ON FINAL APPROACH.
Factual narrative
On September 19, 1993, about 0937 hours eastern daylight time, N9931Q, a Cessna 172, operated by the owner/pilot, impacted the ground after an uncontrolled descent following an approach to landing at the Quonset State Airport, North Kingstown, Rhode Island. The airplane was substantially damaged. The pilot and passenger were not injured. Visual meteorological conditions prevailed and a flight plan was filed. The personal flight departed from Marshfield, Massachusetts, about 0915 hours, and was conducted under 14 CFR 91. According to the pilot, the flight was on final approach to runway 5 when the pilot spotted a "large amount of sea gulls" flying in front of him near the runway threshold. The pilot stated that he banked right to avoid the birds, "which put the plane into stall mode and a rapid descent." He remembered hearing the stall warning horn. The nose gear hit the ground and the airplane veered to the right. The pilot attempted to go around, but the airplane "would not climb" and began to skid. The pilot stated that he then elected to perform a "controlled crash." According to an FAA aviation safety inspector, the airplane came to rest about 2,500 feet from the threshold of runway 5, and about 600 feet to the right of the runway 5 centerline. The propeller, firewall, nose gear, and the outboard sections of both wings were substantially damaged. The Quonset State Airport has another runway oriented along a magnetic bearing of 340 degrees. According to a ground witness, a certified flight instructor, the pilot of N9931Q never radioed for advisories for the active runway. The witness also stated that the winds were "fairly steady at 340 degrees at 12 to 15 miles per hour." The witness further stated: "I watched as the aircraft made a final approach to runway 5, flew through a flock of seagulls at approximately 100 feet above ground level, then failed to make a proper crosswind landing. After a hard landing, the aircraft drifted to the right. . . . the right wing contacted the ground and impact occurred." No mechanical malfunctions were reported. THE PILOT BEGAN AN APPROACH TO RUNWAY 5 WITH THE WIND FROM 340 DEGREES AT 15 KNOTS. THE OTHER RUNWAY AT THE AIRPORT WAS ORIENTED ALONG A MAGNETIC BEARING OF 340 DEGREES. THE PILOT DID NOT REQUEST AN AIRPORT ADVISORY BEFORE THE APPROACH. AS THE AIRPLANE CROSSED THE RUNWAY THRESHOLD, NUMEROUS SEAGULLS FLEW IN FRONT OF IT. THE PILOT STATED THAT HE BANKED RIGHT TO AVOID THE SEAGULLS, AND THE AIRPLANE STALLED. THE NOSE GEAR HIT THE GROUND, AND A GO-AROUND WAS ATTEMPTED. A GROUND WITNESS, A CERTIFIED FLIGHT INSTRUCTOR, STATED THAT THE AIRPLANE 'HIT HARD' AND DRIFTED TO THE RIGHT. THE RIGHT WING CONTACTED THE GROUND, AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. NO MECHANICAL MALFUNCTIONS WERE REPORTED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_BFO93LA179.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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 …
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…