FTW00LA226
2000-08-05 · SHAWNEE, Oklahoma, United States · None · 1 aircraft · Status: Completed
Airport SNL
Current FAA registration · N182DG
- Make / Model
- CESSNA 182M
- Year of manufacture
- 1969 · 31 years old at event
- Engine
- CONT MOTOR O-470 SERIES (230 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19690814
- ADS-B equipped
- Yes — Mode-S A1486C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control of the airplane during the landing flare/touchdown. A factor was the gusty wind condition.
Factual narrative
On August 5, 2000, at 1200 central daylight time, a Cessna 182M airplane, N182DG, was substantially damaged when it impacted the runway following a loss of control at the Shawnee Municipal Airport, near Shawnee, Oklahoma. The airplane was registered to and operated by Basin Aviation Inc., of Midland, Texas. The instrument rated private pilot and her two passengers were not injured. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 personal flight, for which an IFR flight plan was filed. The cross-country flight originated from the Midland Airpark, near Midland, Texas, and was destined for Shawnee, Oklahoma. During a telephone interview conducted by the NTSB Investigator-In-Charge, the pilot reported that she was cleared for the ILS 17 approach at the Shawnee Municipal Airport. While she was on final approach, the Unicom operator reported the winds from 170 degrees at 19 knots. The airplane was 5 feet agl when a "wind gust from the west lifted the right wing," and the airplane "stalled and bounced." She advanced the throttle, regained control of the airplane, and executed the second touchdown without further incident. She stated that the wind, at the time of the accident, was from the southwest and gusty. She added that she had received a DUAT's weather briefing before the flight, and the winds were forecast to be from the south between 17 and 22 knots. At 1153, the weather observation facility at the Will Rogers World Airport, Oklahoma, City, Oklahoma, (located 30 miles east of the accident site) reported the winds from 200 degrees at 15 knots. At 1253 the winds were reported from 200 degrees at 17 knots, gusting to 22 knots. The FAA inspector reported that the engine firewall was wrinkled and the propeller blades were bent. Multiple attempts by the NTSB to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), were not responded to by the pilot. The flight was cleared for the ILS approach to runway 17. When the flight was on the final approach leg, the Unicom operator reported the winds from 170 degrees at 19 knots. According to the pilot, as the airplane was in the landing flare/touchdown, at 5 feet agl, a 'gust of wind from the west lifted the right wing,' and subsequently, the airplane 'stalled and bounced.' The pilot applied power, regained control of the airplane, and landed the airplane without further incident. The pilot reported that the wind was gusty from the southwest at the time of the accident. At 1253, a weather observation facility (located 30 miles east of the accident site) reported the wind from 200 degrees at 17 knots, gusting to 22 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_FTW00LA226.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, loss of control). All research papers
- Semantic Scholar 2016 · Article (Interacción) Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …