NTSB CAROL · Event
Event WPR22LA130
Registry · N101YY
FAA Aircraft Registry record.
Make / Model
PARADISE AIRCRAFT USA LLC P1
Engine
ROTAX 912ULS SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20150609
ADS-B equipped
Yes — Mode-S A00AA8
Registrant of record
EXECUTIVE AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power due to fuel exhaustion. Contributing to the accident was the pilot's inadequate preflight fuel inspection.
Factual narrative
The flight instructor reported that he had observed the student pilot use a dipstick to determine the fuel quantity. They then departed for a training flight with the belief that they had 10 gallons of fuel. They performed flight maneuvers for about 20 minutes then returned to the airport for pattern work. On the third takeoff, about 300 ft above ground level (agl), the engine experienced a total loss of power. The flight instructor initiated a forced landing to a road where the airplane struck a curb, which resulted in substantial damage to the right wing. After a debrief with the student, it was discovered by the flight instructor that the student may have inserted the fuel dipstick into the tank at an angle instead of vertically and got a higher level indication of fuel quantity. A postaccident examination of the wing tanks by the recovery agency, revealed less than a half-gallon of fuel remaining in the tanks. The pilot reported there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Aircraft-Fluids/misc hardware-Fluids-Fuel-Inadequate inspection
- — Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid level
- — Personnel issues-Task performance-Inspection-Preflight inspection-Instructor/check pilot
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-(general)-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2022_WPR22LA130.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 (fuel exhaustion). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- AOPA Air Safety Institute 2023 · Safety advisor
Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Helicopter Shaft Heating Parameters for Polyamide-11 Coating
In this study, the heating parameters required for polyamide-11 (P11) coating of the helicopter shaft were investigated. The torsion value created by the force applied to the middle of the helicopter'…
- NASA NTRS 2019 · Abstract
U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR)
A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other
Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …
Browse the full corpus — academia portal ↗