NTSB CAROL · Event
Event MIA07CA078
Registry · N555X
FAA Aircraft Registry record.
Make / Model
GOODYEAR ROBERT J HUMMEL BIRD
Year of manufacture
2005 · 2 years old at event
Engine
ROTAX SEE BOMBADIER
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20060114
ADS-B equipped
Yes — Mode-S A7140B
Registrant of record
GOODYEAR ROBERT J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed during a go-around.
Factual narrative
The pilot stated that he had completed several laps around the ultralight traffic pattern at Lakeland Linder Airport, when he decided to land. He entered left traffic, and while on left downwind for a landing on the ultralight runway 27, at and altitude of 400 feet AGL, he noticed another aircraft about 1,500 feet ahead of him and at a slightly lower altitude. He further stated that while turning to left base, he noticed that his airspeed was 70 mph, his altitude was 400 feet, and the airplane in front of him had slowed down considerably. When turning final, he was at an altitude of 300 ft. AGL, his airspeed was 65 MPH, and he was closing on the aircraft that was ahead him. At this point the pilot said he reduced his airspeed to just below 60 MPH. When he slowed down he noticed that the aircraft ahead of him started to increase altitude, and he was still closing on that aircraft, so the pilot said he decided to go around on the inside. He made a pretty hard bank to the left, felt the left crosswind get under his wing. His airspeed was just below 55 MPH, and he was at an altitude of 195 feet AGL, when his aircraft stalled. The pilot that as he made corrections in an attempt to recover, his aircraft abruptly turned right, causing his head to strike the canopy, and he lost consciousness. According to the pilot, that was the last thing he remembered until he awakened in the hospital the next day. The pilot said that prior to the accident there were no mechanical failures or malfunctions to his aircraft or any of its systems. The pilot said that while turning final to land on runway 27, he was at an altitude of 300 ft. AGL, an airspeed of 65 MPH, and he was closing in on the aircraft that was ahead of him. At this point he said he reduced his airspeed to just below 60 MPH, and when he slowed down he noticed that the aircraft ahead of him started to increase altitude. He was still closing on that aircraft and decided to go around on the inside. He made a hard bank to the left, and was at an altitude of 195 feet AGL, when his aircraft stalled. He said he made corrections in an attempt to recover, and his aircraft abruptly turned right, causing his head to strike the canopy, and he lost consciousness. The pilot said that prior to the accident there were no mechanical failures or malfunctions to his aircraft or any of its systems. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_MIA07CA078.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
Browse the full corpus — academia portal ↗