NTSB CAROL · Event
Event FTW04LA071
Registry · N234DD
FAA Aircraft Registry record.
Make / Model
BELLANCA 17-30A
Year of manufacture
1973 · 31 years old at event
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19730117
ADS-B equipped
Yes — Mode-S A217AB
Registrant of record
NUNEZ CHRISTIAN
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons and the pilot's misjudgment of altitude and distance during the forced landing which resulted in a collision with trees and transmission wires.
Factual narrative
On February 8, 2004, approximately 1415 central standard time, a Beech BE-23 single-engine airplane, N234DD, was substantially damaged during a forced landing shortly after take off from Mena Intermountain Municipal Airport (M39), near Mena, Arkansas. The airline transport rated pilot/owner, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 ferry flight destined for the Ellington Airport (EFD), near Houston, Texas. The 5,625-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), that he purchased the aircraft used and since it was out of annual, he had the owner inspect the aircraft and obtain a ferry permit. The pilot added that on the day of the flight, he preformed an "extensive" pre-flight of the aircraft, topped off the fuel tanks, did an engine run-up, and took off from runway 17 without incident. While climbing out, the pilot reported that the engine lost power, and he made an immediate turn towards the runway. The pilot stated that the aircraft landed short of the runway in some small trees and brush. A Federal Aviation Administration (FAA) inspector performed an on-scene examination of the airplane. According to the inspector, after takeoff from runway 17 (a 6,000-foot-long and 100-foot-wide asphalt runway), the pilot made a left downwind departure and climbed to an altitude of 2,000 feet above ground level (agl), when the engine lost power. The pilot attempted to re-start the engine, but was unsuccessful. He turned left and aligned the airplane with the runway while descending. The pilot flew along the length of the runway, but never landed. As the airplane approached the end of the runway, he aligned the airplane with a taxiway, but decided to turn and land in an open clearing, where it struck trees and power lines. Examination of the airplane revealed that the tail section was partially separated, and both wings exhibited extensive leading edge damage. Both fuel tanks were ruptured, and all fuel screens were absent of debris. The engine was run on the airframe with the original bent propeller still installed. Since the airplane's fuel tanks were ruptured, an alternate fuel source was rigged to provide fuel to the engine. The engine started immediately, but only ran for five minutes. Another propeller was installed, and the engine was started. It ran continuously at various power settings without interruption. No mechanical deficiencies were noted. The airplane had just been recently purchased, was out of annual inspection, and was being ferried to Houston, where it was scheduled to undergo an annual inspection. The FAA issued the ferry permit based on the belief that the airplane had undergone an annual inspection over a year ago. Further examination revealed that the airplane had not received an annual inspection since 1988. Weather at M39 at the time of the accident was reported as wind from 180 degrees at 7 knots, visibility 10 statute miles, and clear skies. The reason for the loss of engine power could not be determined. After takeoff from runway 17 (a 6,000-foot-long and 100-foot-wide asphalt runway), the 5,625-hour air transport pilot made a left downwind departure and climbed to an altitude of 2,000 feet above ground level (agl), when the engine lost power. The pilot attempted to re-start the engine, but was unsuccessful. He turned left and aligned the airplane with the runway while descending. The pilot flew along the length of the runway, but never landed. As the airplane approached the end of the runway, he aligned the airplane with a taxiway, but decided to turn and land in an open clearing, where it struck trees and power lines. The engine was run on the airframe with the original bent propeller still installed for five minutes. After installation of a new propeller, and the engine was started, it ran continuously at various power settings without interruption. No mechanical deficiencies were noted. The airplane was out of annual inspection, and was being ferried to Houston, Texas where it was scheduled to undergo an annual inspection. The FAA issued the ferry permit based on the belief that the airplane had undergone an annual inspection over a year ago. Further examination revealed that the airplane had not received an annual inspection since 1988. The reason for the loss of engine power could not be determined. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_FTW04LA071.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…
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