MIA91LA087
1991-02-25 · VALKARIA, Florida, United States · Minor · 1 aircraft · Status: Completed
Airport X59
Current FAA registration · N609FT
- Make / Model
- PIPER PA-28-161
- Year of manufacture
- 1977 · 14 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19770624
- ADS-B equipped
- Yes — Mode-S A7E93D
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE FAILURE OF THE INSTRUCTOR PILOT TO SUPERVISE THE STUDENT PILOT'S ACTIONS, RESULTING IN A STALL AT A LOW ALTITUDE WHERE RECOVERY WAS NOT POSSIBLE.
Factual narrative
THE INSTRUCTOR PILOT INITIATED A SIMULATED ENGINE FAILURE AFTER TAKEOFF AT ABOUT 250 FT AGL. THE STUDENT INITIATED A STEEP TURN AND THE AIRPLANE STALLED. THE INSTRUCTOR ADDED THROTTLE AND ATTEMPTED TO RECOVER BUT THE AIRPLANE STRUCK THE TREES AND THE GROUND. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1991_MIA91LA087.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type or causal vocabulary (stall, engine failure). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
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- 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 Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- 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…