NTSB CAROL · Event
Event MIA99LA052
Registry · N5836P
FAA Aircraft Registry record.
Make / Model
PIPER PA-24-250
Year of manufacture
1959 · 39 years old at event
Engine
LYCOMING 0-540 SERIES (250 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19590409
ADS-B equipped
Yes — Mode-S A78445
Registrant of record
SHORT FINAL LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The delay by the pilot-in-command (CFI) to take control of the airplane and inadvertent stall/mush resulting in the uncontrolled descent and impact with the runway.
Factual narrative
On December 19, 1998, about 1714 eastern standard time, a Piper PA-24-250, N5836P, registered to Cross Winds Aviation, Inc., experienced an in-flight loss of control during takeoff from the St. Petersburg-Clearwater International Airport, Clearwater, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed for the 14 CFR Part 91 instructional flight. The airplane was substantially damaged and the certified flight instructor (CFI), private-rated student, and one passenger were not injured. The flight was originating at the time of the occurrence. The purpose of the flight was for the student to practice soft field takeoffs because he had failed the soft field takeoff procedure during his commercial checkride 3 days earlier. The CFI stated that the student had the tendency while practicing soft field takeoffs previously to not apply enough right rudder after the nose wheel left the ground resulting in the airplane drifting to the left. The airplane was taxied to the runway and after being cleared for takeoff, power was applied and the student initiated a soft field takeoff procedure. After the nose landing gear came off the runway, the airplane began drifting to the left and the CFI advised the student to apply "a lot more right rudder!" The CFI stated that the student applied "way too much" right rudder and while flying in ground effect, the airplane was flying in a cross control condition with right rudder and left aileron inputs applied. The CFI advised the student to remove the right rudder input and he corrected with left rudder and removed the left aileron input. The CFI reported that while in a cross controlled power-on stalled condition, the left wingtip contacted the runway, followed by the right wing. The airplane then traveled off the runway onto grass and came to rest with the right main landing gear collapsed. The CFI stated that he should have taken corrective action sooner. Examination of the right main landing gear assembly by an FAA airworthiness inspector revealed that the threaded portion of the rod end for the extension/retract rod was bent and broken. The student had failed the soft field takeoff procedure during a commercial checkride 3 days earlier and was flying with his flight instructor for additional training. The instructor stated that the student had the tendency to allow the airplane to drift to the left after the nose wheel came off the ground. The flight departed and with the student performing a soft field takeoff, the airplane began drifting to the left. The instructor advised the student to apply 'a lot more right rudder!' and the student applied 'way too much' right rudder. While flying in a cross controlled condition, the instructor attempted to regain control but the airplane stalled and the left wing of the airplane contacted the runway, followed by the right wing. The airplane then traveled off the runway onto grass and came to rest with the right main landing gear collapsed. The instructor stated that he should have taken corrective action sooner. Examination of the airplane revealed a bent and broken threaded portion of a rod end for the retract/extension rod. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_MIA99LA052.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). 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.
- 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 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.
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
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