NTSB CAROL · Event
Event LAX85LA082
Registry · N51FM
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22T
Year of manufacture
2020
Engine
CONT MOTOR TSIO-550-K (315 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20200821
ADS-B equipped
Yes — Mode-S A65F9F
Registrant of record
MEEKS AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PLT PLANNED TO FLY FROM SANTA ANA, CA. TO SCOTTSDALE, AZ. THE PLT REPORTED THAT THE ACFT HAD ENOUGH FUEL FOR 4 HRS OF FLYING TIME. THE ACFT'S FUEL GAGES ARE LOCATED ON THE WINGS & A FLASHLIGHT IS REQUIRED TO SEE THEM AT NIGHT. THE PLT STATED THAT HE WAS CARRYING AN OPERATIVE FLASHLIGHT, BUT HE DID NOT USE IT TO LOOK AT THE FUEL GAGES BECAUSE HE WAS CERTAIN HIS ACFT CONTAINED ENOUGH FUEL FOR THE FLT. AFTER FLYING FOR ABOUT 3.5 HOURS AND 12 MI FROM THE INTENDED DESTINATION, THE ENGINE SUDDENLY LOST ALL POWER. THE PLT ATTEMPTED TO MAKE A FORCED LANDING ON A ROAD.ON APPROACH THE ACFT COLLIDED WITH A TREE. THE POST-CRASH EXAM OF THE ACFT REVEALED ITS FUEL TANKS TO BE VIRTUALLY DRY. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_LAX85LA082.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. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2026 · arXiv preprint
Buffet Alleviation via Linear Stability Adjoint
Transonic buffet, self--sustained shock and shear--layer oscillations, imposes hard limits on the cruise envelope of modern transport aircraft, and avoiding it is a primary design driver.
- arXiv 2026 · arXiv preprint
Transonic Buffet Modeling via Invariant Manifolds
In transonic flow over aircraft wings, shock-boundary-layer interactions can give rise to transonic buffet, which degrades maneuverability through unsteady aerodynamic loads.
- arXiv 2025 · arXiv preprint
Aeroelastic Reduced-Order Model Differential Equations in Transonic Buffeting Flow
Numerical simulation of the transonic shock buffet phenomenon remains a formidable challenge due to its inherent nonlinear and unsteady characteristics.
- arXiv 2025 · arXiv preprint
Compact representation of transonic airfoil buffet flows with observable-augmented machine learning
Transonic buffet presents time-dependent aerodynamic characteristics associated with shock, turbulent boundary layer, and their interactions.
- arXiv 2023 · arXiv preprint
Experimental investigation on the turbulent wake flow in fully-established transonic buffet conditions
The transonic flight regime is often dominated by transonic buffet, a highly unsteady and complex shock-wave/boundary-layer interaction involving major parts of the flow field.
- Embry-Riddle Scholarly Commons 2017 · Journal article (IJAAA)
As Assessment of Airline Service Quality in a Category One Nation: Focus on Mallam Aminu Kano International Airport
To evaluate airline service quality from passengers’ in a Category One (CAT1) nation. The researchers used quantitative method to evaluate airline quality of service, from passengers’ perspective at M…
Browse the full corpus — academia portal ↗