ATL94LA149
1994-07-28 · MUSCLE SHOALS, Alabama, United States · None · 1 aircraft · Status: Completed
Airport MSL
Current FAA registration · N919JM
- Make / Model
- MILLER JOHN N SKYBOLT-180
- Seats / Engines
- 2 seats · 1 engine
- ADS-B equipped
- Yes — Mode-S ACB8EE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The fatigue failure of the main landing gear strut that resulted in a loss of control.
Factual narrative
On July 28, 1994 at 0917 central daylight time, a Miller Skybolt, N919JM was substantially damaged following a loss of control during landing at Muscle Shoals, Alabama. The commercial pilot was not injured in the accident. The aircraft was operated by the pilot, under the provisions of 14 CFR Part 91. Visual meteorological conditions existed at the time, and no flight plan had been filed for the personal flight. The flight departed Mobile, Alabama at 0730, and was enroute to Oshkosh, Wisconsin. The pilot stated that left main landing gear strut failed during landing, and he lost control of the aircraft. The aircraft ground looped causing substantial damage to the left wing and left wing strut. Examination of the left main landing gear revealed that the left landing gear strut had fractured, and the left gear had collapsed. The pilot reported that the fracture surface was visually examined in bright sunlight. He noted a "...change in [the] crystal structure of the steel: a 3/8 to 1/2 inch radial area with a larger nodular appearance with respect to the homogenous fine gray granular appearance of the rest of the surface. The outher 1/32 inch of the different area was quite black. We, therefore, surmised the presence of a previously unknown radial crack in the member, perhaps a manufacturing defect, present all along." THE PILOT STATED THAT AFTER TOUCHDOWN ON THE RUNWAY, THE AIRCRAFT VEERED OFF THE RUNWAY TO THE LEFT. EXAMINATION OF THE LEFT MAIN LANDING GEAR REVEALED THAT THE GEAR STRUT WAS FRACTURED, AND THE LEFT LANDING GEAR HAD COLLAPSED. FURTHER EXAMINATION OF THE FRACTURE SURFACE REVEALED A RADIAL AREA ABOUT 3/8 TO 1/2 INCH IN SIZE, THAT WAS QUITE DIFFERENT FROM THE HOMOGENOUS, FINE, GRAY GRANULAR APPEARANCE OF THE REMAINDER OF THE FRACTURE. THE OUTER 1/32 INCH OF THE DIFFERENT APPEARING AREA WAS DISCOLORED BLACK, WHICH REVEALED THE PRESENCE OF A PREVIOUSLY UNDETECTED FRACTURE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_ATL94LA149.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
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- 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.