ATL06CA004
2005-10-12 · Millington, Tennessee, United States · None · 1 aircraft · Status: Completed
Airport 2M8
Current FAA registration · N273PS
- Make / Model
- BEECH F33A
- Year of manufacture
- 1972 · 33 years old at event
- Engine
- CONT MOTOR IO 520 SERIES (285 hp)
- Seats / Engines
- 5 seats · 1 engine
- Last airworthiness date
- 19720512
- ADS-B equipped
- Yes — Mode-S A2B2F7
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper fuel management resulting in a total loss of engine power due to fuel starvation. A factor in the accident was the pilot's failure to maintain airspeed and misjudged distance to the forced landing area resulting in a stall and collision with the ground.
Factual narrative
"This report is based on information received by the NTSB. Additional details may be found in the NTSB's public docket for this case. For further information please contact the NTSB Office of Public Inquires." The pilot stated he crossed over the destination airport at mid field and entered a right downwind for landing to runway 36 when the engine lost power. Another airplane was on base leg for landing. The pilot elected to make a forced landing in the grass next to runway 36. He immediately switched the fuel tank from the left main fuel tank to the right fuel tank and attempted an engine restart without success. The pilot stated he misjudged his landing distance by about 150 feet and failed to maintain airspeed on final. The airplane stalled and collided with the ground on the nose gear. Examination of the airplane after the accident revealed the left fuel quantity indicator indicated empty. The fuel tank was not ruptured and no fuel was present in the fuel tank. The pilot's Operating Handbook states the airplane has three gallons of unusable fuel in each fuel tank. Three gallons of fuel was drained from the left main fuel tank. The fuel line was disconnected at the fuel flow divider, and the fuel line to the inlet side of the engine driven fuel pump was disconnected. No fuel was present. The nose section of the airplane was positioned in a brace and the airplane was tied down with a cargo strap. The engine was started and ran smoothly with the fuel selector selected on the right main fuel tank. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_ATL06CA004.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
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- Pilots of America Community ↗
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Related research
Matched on aircraft type or causal vocabulary (stall, fuel starvation). All research papers
- 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…