FTW95LA193
1995-05-07 · HOUSTON, Texas, United States · None · 1 aircraft · Status: Completed
Airport AXH
Current FAA registration · N18413
- Make / Model
- BEECH F33A
- Year of manufacture
- 1977 · 18 years old at event
- Engine
- CONT MOTOR IO 520 SERIES (285 hp)
- Seats / Engines
- 5 seats · 1 engine
- Last airworthiness date
- 19770913
- ADS-B equipped
- Yes — Mode-S A1521F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S INADEQUATE COMPENSATION FOR THE WIND CONDITIONS. A FACTOR WAS THE CROSSWIND.
Factual narrative
On May 7, 1995, at 1200 central daylight time, a Beech F33A, N18413, was substantially damaged following a loss of control while landing near Houston, Texas. The private pilot and his three passengers were not injured. Visual meteorological conditions prevailed for the personal cross country flight from Batesville, Texas. The pilot reported that, while he was flaring the airplane for landing on runway 09 at Houston Southwest Airport (AXH), he noticed he was drifting toward the left side of the runway. He further stated that full power was applied in an attempt to go around; however, the left wing tip contacted the ground. The airplane impacted at a 90 degree angle to the runway and slid through a grassy area and across a taxiway before coming to rest. Damage included separation of the nose landing gear and deformation of the engine support beam and firewall. At 1150 central daylight time, William P. Hobby Airport (HOU) located 15 miles to the northeast was reporting wind from 170 degrees varying in speed from 13 to 20 knots. Pilot reported wind was from 160 degrees at 15 knots, gusting to 20. According to the manufacturer, the maximum demonstrated crosswind component for a Beech F33A is 17 knots. WHILE FLARING FOR A CROSSWIND LANDING, THE PILOT ALLOWED THE AIRPLANE TO DRIFT LEFT OFF THE RUNWAY. FULL POWER WAS ADDED TO GO AROUND, BUT THE LEFT WING TIP CONTACTED THE GROUND AND THE AIRPLANE IMPACTED TERRAIN 90 DEGREES TO THE RUNWAY. WIND FROM 170 DEGREES VARYING IN SPEED FROM 13 TO 20 KNOTS WAS REPORTED AT 1150 CDT AT HOBBY AIRPORT 15 MILES NORTHEAST. THE PILOT REPORTED WIND WAS FROM 160 DEGREES AT 15 KNOTS, GUSTING TO 20. THE MAXIMUM DEMONSTRATED CROSSWIND COMPONENT FOR THE AIRPLANE WAS 17 KNOTS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW95LA193.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (loss of control). All research papers
- 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…
- 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.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …
- NTSB Aircraft Accident Reports 2022 · Accident report Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation) ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.