NTSB CAROL · Event
Event BFO92IA017
Registry · N923HA
FAA Aircraft Registry record.
Make / Model
CESSNA AIRCRAFT CO 525B
Year of manufacture
2008
TCDS
A1W1 · TEXTRON AVIATION INC
Engine
WILLIAMS FJ44-3A
Seats / Engines
8 seats · 2 engines
Last airworthiness date
20200928
ADS-B equipped
Yes — Mode-S ACC9FF
Registrant of record
TVPX AIRCRAFT SOLUTIONS INC TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
IMPROPER INSTALLATION OF THE LOW FUEL PRESSURE WARNING SWITCH SNUBBER ON THE #1 ENGINE, RESULTING IN FATIGUE FAILURE OF THE SNUBBER, A FUEL LEAK (SPRAY), AND SUBSEQUENT EXPLOSION/FIRE DAMAGE. A FACTOR RELATED TO THE INCIDENT WAS: INADEQUATE DESIGN OF THE FIREWALL, WHICH ALLOWED FUEL VAPORS TO MIGRATE TO THE HOT SECTION OF THE ENGINE.
Factual narrative
AS THE GEAR & FLAPS WERE RETRACTED AFTER TAKEOFF, THE #1 ENGINE LOW FUEL PRESSURE WARNING LIGHT ILLUMINATED. AT ABOUT 400' AGL, A "LOUD BANG" WAS HEARD FOLLOWED BY A #1 ENGINE FIRE WARNING INDICATION. THE ENGINE WAS SHUT DOWN & BOTH FIRE EXTINGUISHING BOTTLES WERE DISCHARGED. THE FLIGHTCREW EXTENDED THE LANDING GEAR BY USING THE ALTERNATE SYSTEM & MADE A NO-FLAP EMERGENCY LANDING. THEY USED EMERGENCY BRAKES, BUT DIRECTIONAL CONTROL WAS LOST & THE AIRCRAFT EXITED THE SIDE OF THE RUNWAY & STOPPED WITH THE FIRE EXTINGUISHED. AN EXAM OF THE #1 ENGINE AREA REVEALED A FAILED LOW FUEL PRESSURE WARNING SWITCH SNUBBER & FIRE DAMAGE TO THE ENGINE, NACELLE & WHEELWELL. THERE WAS EVIDENCE THAT DURING INSTALLATION, THE LOW FUEL PRESSURE WARNING SWITCH SNUBBER WAS TORSIONALLY DEFORMED, THEN FATIGUE & SUBSEQUENT FAILURE OCCURRED. GAPS IN THE FIREWALL ALLOWED LEAKING FUEL (SPRAY) TO ENTER THE HOT SECTION & IGNITE. THIS RESULTED IN AN EXPLOSION & FIRE. FIRE PROPAGATION RESULTED IN BURNED WIRES TO THE #1 STANDBY HYDRAULIC PUMP & A RUPTERED #2 SYSTEM HYDRAULIC LINE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_BFO92IA017.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). 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 …
- 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…
- 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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗