NTSB CAROL · Event
Event CEN21LA303
Registry · N1175H
FAA Aircraft Registry record.
Make / Model
AERONCA 15AC
Year of manufacture
1948 · 73 years old at event
Engine
CONT MOTOR C145 SERIES (145 hp)
Seats / Engines
4 seats · 1 engine
ADS-B equipped
Yes — Mode-S A04943
Registrant of record
KRUMMREY STEVEN C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power for reasons that could not be determined based on the available information.
Factual narrative
On June 30, 2021, about 1800 eastern daylight time, an Aeronca 15AC airplane, N1175H, was substantially damaged when it was involved in an accident near Hastings, Michigan. The pilot receiving instruction and flight instructor were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The flight instructor reported that, about 45 minutes into a flight review, the engine lost power following a practice go-around. The pilot noted that the engine was “good and strong” during the initial portion of the go-around. About 400 ft above ground level, the engine “sputtered” and lost power. When the pilot leveled the wings, engine power was restored. The flight instructor took control of the airplane, and the engine subsequently lost power again, after which the flight instructor performed a forced landing to a grass area on airport property. During the landing, the airplane nosed over and came to rest inverted near the perimeter fence, resulting in substantial damage to the left-wing strut and rudder. The pilot reported that they departed on the flight with about 15 total gallons of fuel; 8 gallons in the left wing fuel tank and 7 gallons in the right wing fuel tank. The airplane was equipped with sight gauges at each wing root to indicate fuel quantity. The flight instructor recalled that, shortly before the loss of engine power, about 8 gallons and 2 gallons of fuel remained in the left and right fuel tanks, respectively. The mechanic who recovered the airplane reported that about 6 gallons remained in the left fuel tank and 2 gallons remained in the right fuel tank. The fuel caps were secure, and the accident site did not exhibit any evidence of a fuel spill. A postaccident examination and engine test run did not reveal any anomalies consistent with a preimpact failure or malfunction. Continuity of the airframe fuel system was confirmed. The pilot receiving instruction and flight instructor were conducting a flight review. About 45 minutes into the flight, the engine “sputtered” and lost power following a practice go-around. The flight instructor took control of the airplane and performed a forced landing, during which the airplane sustained substantial damage. The pilot reported that they departed on the flight with 8 gallons of fuel in the left-wing tank and 7 gallons of fuel in the right-wing tank. The flight instructor recalled that, shortly before the loss of engine power, the left and right tanks contained about 8 gallons and 2 gallons, respectively. The mechanic who recovered the airplane reported that about 6 gallons remained in the left fuel tank and 2 gallons in the right fuel tank. The fuel caps were secure, and the accident site did not exhibit any evidence of a fuel spill. A postaccident examination and engine test run did not reveal any anomalies consistent with a preimpact failure or malfunction. Continuity of the airframe fuel system was confirmed. The reason that fuel was being drawn predominantly from the right fuel tank could not be determined. The reason for the loss of engine power could not be determined based on the available information. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2021_CEN21LA303.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (go-around). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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 …
- NASA NTRS 2021 · Accepted Manuscript (Version with final changes)
Go-Around Criteria Refinement for Transport Category Aircraft
Presently, airline pilots are trained to go around if, when lower than 500 ft above the ground, they are outside of a handful of parameters such as airspeed, position, and rate of descent.
- NASA NTRS 2019 · Conference Paper
Validation of Proposed Go-Around Criteria Under Various Environmental Conditions
This paper evaluates the effects of environmental conditions on touchdown performance under varying approach states and validates proposed go-around criteria developed using data from a previously con…
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