NTSB CAROL · Event
Event FTW03LA084
Registry · N1537R
FAA Aircraft Registry record.
Make / Model
COLUMBIA AIRCRAFT MFG LC41-550FG
Engine
CONT MOTOR TSIO-550-C (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20070816
ADS-B equipped
Yes — Mode-S A0D8B1
Registrant of record
B & R AERO LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed which resulted in a stall. Low altitude flight is a contributing factor.
Factual narrative
On January 14, 2003, at 1445 central standard time, an Air Tractor AT-401 agricultural airplane, N1537R, was substantially damaged following a loss of control while maneuvering near Alamo, Texas. The non-instrument rated commercial pilot, who was the sole occupant of the airplane, was seriously injured. The airplane was owned and operated by Moad Aviation, Inc., of Weslaco, Texas, under 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed throughout the area for the aerial application flight for which no flight plan was filed. The local flight originated (approximately 1400) from the Mid Valley Dusters Airport (43TX) near Alamo, Texas. The operator reported that the airplane had been flown on a local aerial application flight during the morning hours and was hangared after completion of the flight. He added that their normal procedures is to top-off the left wing prior to hangaring the airplane. The operator's standard fuel load for local flights was 63 gallons, which normally provides for a 2-hour range. The operator reported to the FAA inspector, who responded to the accident site, that the airplane was in the process of executing a turn to reverse direction, when the airplane stalled and impacted the ground in a nose low attitude. The inspector added that the evidence found at the accident site where consistent with an airplane impacting the ground in a nose low attitude, at a relatively slow airspeed. Examination of the wreckage by the FAA inspector and the operator, revealed that the main wreckage came to rest in an open field in an upright position approximately 75-feet from the initial point of impact. The Pratt & Whitney R-1340 radial engine was found separated from the airframe. The two-blade propeller assembly remained attached to the engine crankshaft. One propeller blade was found bent aft around the engine at about the midspan, while the other blade was slightly bent aft. Both wings sustained structural damage and both fuel cells were compromised during the accident sequence. The inspector added that he arrived at the accident site within an hour after the mishap and there was no evidence of fuel or fuel odors at the accident site. There was no fire. The memory card from the SATLOC system installed in the aircraft was recovered by the FAA inspector for further evaluation. The memory card was analyzed and found not to have any information pertaining to the accident flight. The card was returned to the operator upon completion of the investigation. Several attempts were made by the FAA inspector, as well as the NTSB Investigator-in-Charge to interview the 16,600-hour pilot after his release from the hospital following the accident. The pilot did not have any recollection of the accident or the circumstances prior to the mishap. During an aerial application flight, while the aircraft was in the process of executing a turn to reverse direction, the airplane stalled and impacted the ground in a nose low attitude. The evidence found at the accident site where consistent with an airplane impacting the ground in a nose low attitude, at a relatively slow airspeed. The main wreckage came to rest in an open field in an upright position, approximately 75-feet from the initial point of impact. The radial engine was found separated from the airframe. The two-bladed propeller assembly remained attached to the engine crankshaft. Both fuel cells were compromised during the accident sequence. An FAA inspector arrived at the accident site within an hour after the mishap and reported no evidence of fuel or fuel smell at the accident site. The memory card from the SATLOC system installed in the aircraft was recovered by the FAA inspector for further evaluation. The memory card was analyzed and found not to have any information pertaining to the accident flight. Several attempts were made by the FAA inspector, as well as the NTSB Investigator-in-Charge to interview the 16,600-hour pilot after his release from the hospital after the accident. The pilot reported that he did not have any recollection of the accident or the circumstances prior to the mishap. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2003_FTW03LA084.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, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗