ANC84LA111
1984-07-04 · SELDOVIA, Alaska, United States · None · 1 aircraft · Status: Completed
Airport SOV
Current FAA registration · N1795K
- Make / Model
- LUSCOMBE 8E
- Year of manufacture
- 1946 · 38 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19570723
- ADS-B equipped
- Yes — Mode-S A13DAD
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT NOSED OVER DURING LANDING ON A 2600 FT GRAVEL RWY NESTLED IN THE HILLS WITH VARIABLE WINDS. THE PLT HAD TEMPORARILY TRADED ACFT FOR THIS TRIP AND HAD NOT FLOWN THIS TYPE OF ACFT FOR THE PRECEDING 90 DAY PERIOD. HE NORMALLY FLEW HIS CESSNA 185. HE WAS FAMILIAR WITH THIS ARPT AND HAD MADE ONE GO-AROUND BEFORE THE ACCIDENT BECAUSE OF BEING HIGHAND FAST. THE 2ND APPROACH WAS FLOWN, ACCORDING TO THE PLT, AT 60 MPH AND HE CROSSED THE THRESHOLD AT ABOUT 30 FT AGL. THE TOUCHDOWN WAS ABOUT MIDFIELD AND IN ATTEMPTING TO BRAKE, THE PLT SAID, THE TAIL KEPT COMING UP. HE THOUGHT A GUST OFTAILWIND HAD ACTED ON THE FLAPS AND UP ELEVATOR TO PUSH THE TAIL OF THE ACFT UP. HE SAID HE SHOULD HAVE HAD MORE CONCERN ABOUT THE POSSIBILITY OF VARYING WINDS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1984_ANC84LA111.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 (go-around). All research papers
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- Semantic Scholar 2022 · Article (Journal of Safety Research) Go-around accidents and general aviation safety.
INTRODUCTION Changes in General Aviation (GA) accident rates, specifically in the go-around phase, are examined by comparing the number of accidents, the proportion of fatal accidents, and the proport…
- Semantic Scholar 2021 · Article (Aerospace) Classification and Analysis of Go-Arounds in Commercial Aviation Using ADS-B Data
Go-arounds are a necessary aspect of commercial aviation and are conducted after a landing attempt has been aborted. It is necessary to conduct go-arounds in the safest possible manner, as go-arounds …