NTSB CAROL · Event
Event FTW98LA103
Aircraft involved
Probable cause & findings
The pilot's flight into known adverse weather conditions which resulted in an inadvertent stall due to airframe ice. A factor was the icing conditions.
Factual narrative
On January 8, 1998, at 1145 central standard time, a Cessna 340A, twin engine airplane, N26956, was substantially damaged following a loss of control during landing on runway 17L at the Wiley Post Airport, Bethany, Oklahoma. The aircraft was operated by Sierra Aviation, Inc., of Bethany, under Title 14 CFR Part 91. The commercial pilot, sole occupant, was not injured. Instrument meteorological conditions prevailed for the repositioning flight and an IFR flight plan was filed. The flight departed Tradewind Airport, Amarillo, Texas, at 0915. During a telephone interview, conducted by the investigator-in-charge, the pilot reported that he transported a passenger to Amarillo during a morning flight under Title 14 CFR Part 135. Before the departure at Amarillo, the pilot obtained a weather briefing which included a "chance of icing in clouds and precipitation" with freezing temperatures existing from the cloud tops (4,000 to 5,000 feet msl) to the ground. During the en route phase of the return flight, the skies were clear above 5,000 feet msl. When the flight arrived in the Oklahoma Approach Control Airspace, the flight received radar vectors for the ILS approach. During the approach descent, the aircraft encountered moderate rime and mixed icing in the clouds. At about the outer marker, the pilot cycled the deicing boots and then extended the gear and flaps. The pilot recalled that the tip tanks and the unheated portion of the windshield had ice accumulations. The approach airspeed was blue line plus 10 knots with a power setting at 23 inches of manifold pressure. The aircraft was over the runway at 25 feet agl for the landing flare/touchdown when the pilot reduced the manifold pressure approximately 2 inches. The airplane "dropped" to the runway. The pilot stated that he had encounter icing conditions several months back on a flight into Denver, Colorado. The FAA inspector and the director of maintenance for the operator examined the airplane and found structural damage at the right gear attachment bracket and the right wing. The wing and fuselage were twisted and buckled. The right and left engines were canted downward 7 1/2 degrees and 5 degrees, respectively. The pilot obtained a standard weather briefing for the round trip flight from the Wiley Post Airport to the Tradewind Airport, Amarillo, Texas. A review of the weather briefing tapes by the IIC revealed that the pilot received the airmet for moderate rime or mixed icing across Oklahoma from 6,000 feet to FL 180. A pilot report from the crew of a Boeing 737 departing the Oklahoma City area reported moderate mixed icing below 3,500 feet msl during the initial departure climb. At the time that N26956 departed the Wiley Post Airport, 1 mile visibility with freezing rain and mist was being reported at the airport. During the return flight, the pilot filed an IFR flight plan for the descent into the Oklahoma City area. The weather briefer verified that the pilot was aware of the airmet for moderate icing from the freezing level to FL 180. The briefer informed the pilot that the freezing level was at the surface. Weather briefings received by the pilot included an airmet for moderate rime and mixed icing conditions from the freezing level at the surface to FL 180. During the ILS approach descent, the aircraft encountered moderate rime and mixed icing in the clouds. The pilot cycled the deicing boots and extended the gear and flaps. The tip tanks and the unheated portion of the windshield accumulated ice. The approach airspeed was blue line plus 10 knots with a power setting at 23 inches of manifold pressure. The aircraft was over the runway at 25 feet agl for the landing flare/touchdown when the pilot reduced the manifold pressure approximately 2 inches. The airplane 'dropped' to the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_FTW98LA103.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, 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.
- NTSB Aircraft Accident Reports 2022 · Accident report
Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Embry-Riddle Scholarly Commons 2023 · Faculty research project
Reconfigurable Guidance and Control Systems for Emerging On-Orbit Servicing, Assembly, and Manufacturing (OSAM) Space Vehicles
Dynamic response to emergent situations is a necessity in the on-orbit servicing, assembly, and manufacturing (OSAM) field, because traditional on-orbit guidance and control (G&C) cannot respond effic…
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- Embry-Riddle Scholarly Commons 2023 · Conference paper
The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- NASA NTRS 2019 · Conference Paper
Simulation Modeling Requirements for Loss-of-Control Accident Prevention of Turboprop Transport Aircraft
In-flight loss of control remains the leading contributor to aviation accident fatalities, with stall upsets being the leading causal factor. The February 12, 2009.
Browse the full corpus — academia portal ↗