NTSB CAROL · Event
Event FTW97LA150
Registry · N90485
FAA Aircraft Registry record.
Make / Model
WASHBURN RON FIRESTAR KXP
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20060411
ADS-B equipped
Yes — Mode-S AC8196
Registrant of record
ERICKSON JOSHUA J
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain alignment while landing on a stationary trailer. A factor was the pilot's lack of experience in trailer landing operations.
Factual narrative
On April 3, 1997, approximately 1830 central standard time, a Bell 47 helicopter, N90485, was substantially damaged following a loss of control while attempting to land on a stationary transport trailer, at Laredo International Airport, Laredo, Texas. The commercial rated pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the Title 14 CFR Part 91 personal flight. During an interview with the investigator-in-charge, the pilot stated that he was in the process of purchasing the helicopter from a business located at the airport. After a successful acceptance flight earlier that morning, the pilot landed the helicopter on the ramp, shut down, and finalized the deal. He had driven a trailer to the airport to transport the helicopter back to Louisiana after the purchase. The person that sold the helicopter to the pilot stated that he and the pilot discussed loading the helicopter onto the trailer utilizing a crane, but the pilot optioned to hover and land the aircraft on the trailer. Several witnesses observed the helicopter hovering over the trailer and attempting to land. They reported that as the helicopter touched down on the trailer, the right skid "slid off" the right side of the trailer. They subsequently observed the helicopter roll to the left and impact the ground, with the rotor blades striking the ground first. The pilot stated that he descended slowly down to the trailer platform, positioning the left skid as close to the left rail as possible. He further stated that upon touch down, the helicopter slid about 1 inch to the right, but the left skid looked square to the left rail. As he lowered the collective, he felt the helicopter drifting to the right skid and applied power and left lateral cyclic to arrest the drift. Subsequently, the craft banked sharply to the left and the rotor blades struck the ground. As the helicopter rolled to the left, the tail boom was severed. According to the pilot, this was the first time that he had landed on a trailer. A FAA inspector reported that the width of the trailer was about 4 inches wider than the helicopter's landing skids. The pilot was in the process of purchasing the helicopter from a business located at the airport. After a successful acceptance flight earlier that morning, the pilot landed the helicopter on the ramp, shut down, and finalized the deal. He had driven a trailer to the airport to transport the helicopter back to Louisiana after the purchase. The pilot stated that he descended slowly down to the trailer platform, positioning the left skid as close to the left rail as possible. Upon touch down, the helicopter slid about 1 inch to the right, but the left skid looked square to the left rail. As the pilot lowered the collective, he felt the helicopter drifting to the right skid and applied power and left lateral cyclic to arrest the drift. Subsequently, the craft banked sharply to the left and the rotor blades struck the ground. As the helicopter rolled to the left, the tail boom was severed. According to the pilot, this was the first time that he had landed on a stationary trailer. A FAA inspector reported that the width of the trailer was about 4 inches wider than the helicopter's landing skids. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_FTW97LA150.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Academic papers and agency reports matching this event's aircraft type or causal vocabulary (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.
- 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
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- 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.
- NASA NTRS 2021 · Conference Paper
Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.
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