NTSB CAROL · Event
Event ANC24LA010
Registry · N172CN
FAA Aircraft Registry record.
Make / Model
CESSNA 172S
Year of manufacture
2020 · 3 years old at event
Engine
LYCOMING IO-360-L2A (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20200320
ADS-B equipped
Yes — Mode-S A120DA
Registrant of record
GALVIN FLIGHT SERVICES HAWAII LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The first pilot’s failure to maintain a stabilized approach, in gusty crosswind conditions, in an environment favoring wake turbulence.
Factual narrative
The first pilot, seated in the left seat, and the second pilot, seated in the right seat, both flight instructors, reported that the purpose of the flight was to accumulate additional flight time and practice various flight maneuvers. The first pilot reported that while she was performing a simulated, power-off, 180° landing to Runway 4L, adjacent to a large military airplane operating in the traffic pattern of a parallel runway, the accident airplane began a rapid descent while on short final. To arrest the rapid descent, the first pilot said she initiated a go-around by applying full engine power, but the rapid descend continued, and the airplane touched down hard before becoming airborne again. Airport wind conditions at the time of the accident were reported to be, 120°, at 10 knots, with peak gusts to 17 knots, which translates to a quartering, right tailwind. The second pilot reported that, prior to the accident sequence, as the approach to Runway 4L continued, the first pilot decided to lower the nose to gain airspeed and enter ground effect. The second pilot stated that, as the airplane passed through 75 to 50 ft above the runway, the airplane encountered an unusual sink rate, and he reacted by pulling back on the yoke as he yelled “flare” just before the airplane touched down hard. The second pilot reported that the airplane subsequently touched down hard, bounced back into the air, and the first pilot then initiated a go-around. After establishing a climb on the go-around, the first pilot transferred control to the second pilot, who subsequently performed a precautionary full-stop landing to check for damage. During the landing roll, the nose wheel deflated, and the airplane came to a stop on the runway, disabled. A post-flight inspection revealed that the airplane sustained substantial damage to the firewall and fuselage. The pilots reported that there were no pre-accident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot
- — Environmental issues-Conditions/weather/phenomena-Wind-Crosswind-Contributed to outcome
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Descent/approach/glide path-Not attained/maintained
Verbatim from NTSB's published report. Source file
NTSB_2023_ANC24LA010.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 (wake turbulence, go-around, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 2019 · Conference Paper
Aircraft wake turbulence minimization by aerodynamic means
The paper reviews NASA's efforts on wake vortex turbulence minimization by aerodynamic design or retrofit modifications to large transport aircraft.
- NASA NTRS 2019 · Conference Paper
Wake Turbulence Mitigation for Arrivals (WTMA)
The preliminary Wake Turbulence Mitigation for Arrivals (WTMA) concept of operations is described in this paper. The WTMA concept provides further detail to work initiated by the Wake Vortex Avoidance…
- NASA NTRS 2019 · Conference Paper
Aircraft wake turbulence avoidance
Aircraft wake turbulence /trailing vortex systems/ avoidance during flight, describing procedures for pilots and tower operators
- NASA NTRS 2019 · Conference Paper
Aircraft wake turbulence progress and plans
Aircraft wake turbulence and trailing vortices, investigating physical characteristics, hazard potential and avoidance techniques
Browse the full corpus — academia portal ↗