NTSB CAROL · Event
Event MIA01LA112
Registry · N74SM
FAA Aircraft Registry record.
Make / Model
CESSNA 182Q
Year of manufacture
1979 · 22 years old at event
Engine
CONT MOTOR O-470 SERIES (230 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19790822
ADS-B equipped
Yes — Mode-S A9F1CD
Registrant of record
YELLOW AIRPLANE LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to flare on landing resulting in a hard landing.
Factual narrative
On April 6, 2001, at about 1815 eastern standard time, a Cessna 182Q, N74SM, registered to the Civil Air Patrol Inc., operating as a 14 CFR Part 91 positioning flight collided with the runway on landing at Lakeland-Linder Regional Airport, Lakeland, Florida. Visual meteorological conditions prevailed and a VFR flight plan was filed. The airplane sustained substantial damage, and the private pilot reported no injuries. The flight originated from North Perry Airport, Hollywood, Florida, about 1 hour 55 minutes before the accident. The pilot stated she made a normal landing and was holding back pressure on the yoke. During the landing rollout she felt a shudder after the nose wheel touched down on the runway. She assumed she had blown a tire. She informed the control tower that she had blown a tire and rolled to a stop on the side of the runway. After exiting the airplane she observed that the nose wheel was flat and both propeller tips were curled aft. The pilot stated during her preflight inspection the nose gear plate would not stay closed, it was difficult to obtain a fuel sample, and the fuel selector identification plate was installed backwards. Examination of the airplane by the NTSB and the FAA revealed the nose wheel had collided with the runway first on landing. The front of the nose wheel pants was scuffed and scratched, the right front side of the pant was scratched and broken. The nose wheel tire was flat and had a scuff mark running across the width of the tire. The engine cowling was removed and both sides of the engine firewall was bent inward. The left side of the forward fuselage located next to the firewall had a diagonal crease running from the firewall outboard to the lower left wing strut. There was no damage noted to either main landing gear or the bottom of the fuselage. The pilot stated she made a normal landing. During the landing rollout she felt a shudder after the nose wheel touched down on the runway. Examination of the airplane by the NTSB and FAA revealed the nose wheel had collided with the runway first. The front of the nose wheel pants was scuffed and scratched, the right front side of the pant was scratched and broken. The nose wheel tire was flat and had a scuff mark running across the width of the tire. The engine cowling was removed and both sides of the engine firewall was bent inward. The left side of the forward fuselage located next to the firewall had a diagonal crease running from the firewall to the lower left wing strut. There was no damage noted to either main landing gear or the bottom of the fuselage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_MIA01LA112.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 (stall). 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 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 …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- 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.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗