CHI84LA397
1984-09-21 · ALEXANDRIA, Minnesota, United States · None · 1 aircraft · Status: Completed
Airport AXN
Current FAA registration · N2930B
- Make / Model
- BEECH D35
- Year of manufacture
- 1953 · 31 years old at event
- Engine
- CONT MOTOR E225 SERIES (225 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19550823
- ADS-B equipped
- Yes — Mode-S A302F9
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT WAS STARTED WITH THE THROTTLE OPEN AFTER REFUELING.THE PLT SAID THE ACFT COLLIDED WITH A GAS HOSE BEFORE HE COULD GET THE THROTTLE REDUCED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_CHI84LA397.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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External sources are reported, not agency: signal that something happened, not fact about what happened.
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Related research
Matched on aircraft type. All research papers
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- NASA NTRS 2019 · Other A Flight Investigation of Exhaust-Heat De-Icing, Special Report
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- Semantic Scholar 2019 · Article (Aerospace Medicine and Human Performance) Speech Analysis for Fatigue and Sleepiness Detection of a Pilot.
BACKGROUND: Mental fatigue and sleepiness are well recognized determinants of human-error related accidents and incidents in aviation.
- Semantic Scholar 2018 · Article (Sustainability) A Hybrid HFACS-BN Model for Analysis of Mongolian Aviation Professionals’ Awareness of Human Factors Related to Aviation Safety
Safety is crucial to ensure the sustainability of aviation growth. To better clarify the influences of human factors on aviation accident risks, this study developed a hybrid HFACS-BN model (HFACS: Hu…
- Embry-Riddle Scholarly Commons 2014 · Journal article (IJAAA) Aerodynamic Optimization of Box Wing – A Case Study
The optimization of a possible medium range box wing commercial airliner is presented in three stages. Preliminary research is used to determine various parameters for a potential box wing model, and …