NTSB CAROL · Event
Event LAX83FA310
Registry · N300JT
FAA Aircraft Registry record.
Make / Model
PIPER PA-34-200T
Year of manufacture
1978 · 5 years old at event
Engine
CONT MOTOR TSIO-360 SER (225 hp)
Seats / Engines
7 seats · 2 engines
Last airworthiness date
20020110
ADS-B equipped
Yes — Mode-S A3202C
Registrant of record
MENTOR CAPITAL LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
DURING ARRIVAL, A DESCENT WAS BEGUN FROM 8000 TO 7000 FT MSL AT 0151 HST. AT 0155 HST, THE AIRCREW WAS CLEARED FOR A VISUAL APCH FROM 7000 FT MSL & A RAPID DESCENT WAS STARTED WITH 20 DEG OF FLAPS & APRX 25 INCHES MAP (MANIFOLD PRESSURE). THE ACFT WAS MANEUVERED TO INTERCEPT THE ILS LOCALIZER & GLIDE SLOPE AS A REFERENCE. AFTER INTERCEPTING THE GLIDE SLOPE AT ABOUT 3000 FT, THE PILOT-IN-COMMAND (PIC) CALLED FOR 2250 RPM & GEAR EXTENSION. WHILE DESCENDING THRU APRX 2000 FT, HE NOTICED THE ACFT SLOWING DOWN & DESCENDING BELOW THE GLIDE SLOPE, SO HE CALLED FOR A POWER INCREASE TO 27 INCHES MAP. AT ABOUT THAT TIME, THE AIRCREW NOTED THAT THE ENGS WERE NOT RESPONDING & HAD LOST POWER. SUBSEQUENTLY, A FORCED LANDING WAS MADE IN A SUGAR CANE FIELD WITH THE GEAR IN A TRANSIENT POSITION. THE FUEL SELECTORS WERE FOUND POSITIONED TO FUEL TANKS CONTAINING FUEL, BUT THE POSITIONING DURING THE DESCENT WAS NOT VERIFIED. THE TEMP &DEW POINT WERE 72 & 65 DEG. THIS WOULD HAVE BEEN BARELY WITHIN THE ENVELOPE FOR CARB ICE ON ICING PROBABILITY CHARTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_LAX83FA310.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 (icing). 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 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗