NTSB CAROL · Event
Event DEN99LA078
Registry · N107BB
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22T
Year of manufacture
2016
Engine
CONT MOTOR TSIO-550-K (315 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20160129
ADS-B equipped
Yes — Mode-S A01ED0
Registrant of record
TER-BEAR LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of aircraft control for undetermined reasons. Factors were the sudden wind shift and wind gusts weather condition.
Factual narrative
On May 14, 1999, approximately 1330 mountain daylight time, a Bell/Mason RV-6, N107BB, was substantially damaged during a landing at Double Eagle II Airport, Albuquerque, New Mexico. The certificated commercial pilot, who was the sole occupant, received minor injuries. The airplane was being operated by the pilot under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the cross-country personal flight which originated from Ft. Worth, Texas, 3.5 hours before the accident. No flight plan had been filed. The airplane was on final approach for runway 22, at approximately 200 feet above ground level (agl), flying between 85 to 90 mph with full flaps. The pilot, a former military test pilot, said that the airplane suddenly yawed to the right approximately 35 to 45 degrees. He applied full power, raised the flaps, and executed a go-around. He said the airplane sideslipped to the left, then sideslipped to the right, and repeated this pattern for 3 to 4 cycles. The pilot said that "attempts to dampen the oscillation by leading the yaw were unsuccessful." He said that the sideslipping oscillations caused the airspeed to decrease to approximately 65 mph. During the 4th cycle of oscillations, the "aircraft made a rapid left roll to near inverted attitude," and he managed to continue to roll the airplane to the upright position. The airplane immediately impacted the ground "in a generally flat attitude with the left wing striking the ground first." He stated that the whole sequence extended for over a mile, or 30 to 45 seconds. The pilot said that he heard on the airport's Common Traffic Advisory Frequency that the wind was 260 degrees at 22 knots with gusts to 31 knots. A witness on the ground reported that moments before the accident, the wind had shifted around to the right approximately 90 degrees. A pilot flying a helicopter approximately 1 mile behind the accident airplane reported seeing the airplane "dutch roll" approximately 3 or 4 times with bank angles of approximately 35 to 40 degrees. The airplane appeared to "snap roll to the left," and stall/mush to the ground with the left wing tip impacting first. The airplane was on final approach for runway 22, and the wind was 260 degrees at 22 knots with gusts to 31 knots. A witness reported that moments before the accident, the wind shifted around to the right approximately 90 degrees. The pilot said the airplane suddenly yawed to the right 35 to 45 degrees, and he executed a go-around. A pilot flying a helicopter approximately 1 mile behind the accident airplane reported seeing the airplane 'dutch roll' approximately 3 or 4 times with bank angles of approximately 35 to 40 degrees. The airplane appeared to 'snap roll to the left,' and stall/mush to the ground with the left wing tip impacting first. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_DEN99LA078.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…
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