CHI97LA115
1997-04-27 · DULUTH, Minnesota, United States · Serious · 1 aircraft · Status: Completed
Airport DLH
Aircraft involved
Probable cause & findings
the loss of engine power for undetermined reasons and the pilot's failure to maintain aircraft control.
Factual narrative
On April 27, 1997, at 1218 central daylight time, a Cessna 182P, N7355Q, operated by a private pilot collided with the terrain during a go-around on runway 03 at the Duluth International Airport, Duluth, Minnesota. The pilot reported that he initiated the go-around and he was unable to obtain an increase in engine power upon advancing the throttle. The 14 CFR Part 91 flight was operating in visual meteorological conditions without a flight plan. The pilot and one passenger received minor injuries. An additional passenger received serious injuries. The flight originated from Buffalo, Minnesota, at 1130 cdt. The pilot reported that while on final approach for runway 03, he applied full flaps in increments of 10 degrees along with the carburetor heat. He reported the airplane was "sinking faster than I felt that I should be, so I decided to go-around." The pilot reported he added power, but "full power never came on!" According to the pilot, the right wing stalled and contacted the terrain followed by the nose of the airplane. A review of a maintenance work order for N7355Q, dated 4/24/97, indicated that a pilot reported a power loss on takeoff. The work order states the mechanic ran the engine up to full rpm and after 5 seconds the rpm dropped to 1,900. The write up continued to state that the engine cowl was removed and the fuel system was checked for contaminates and proper fuel flow. The fuel line at the carburetor was disconnected and fuel flow was checked on all fuel selector settings. Checked ok. The gascolator was removed and checked for contaminants - none found. The carburetor/cowling inlet was checked for obstructions and found a boot loose. A bracket was fabricated and installed and was a new air filter assembly. The engine was then run-up and test flow without any discrepancies noted. The engine was removed from the airplane after the accident and it was transported to Bulduc Aviation, Anoka, Minnesota, for an engine test run. The test run was overseen by an inspector from the Federal Aviation Administration, Flight Standards District Office, Minneapolis, Minnesota. The inspector reported that the engine started without "hesitation" and it operated normally when cycled throughout its operating range. See attached Inspector's Statement for details. The pilot reported that he was unable to obtain an increase in engine power upon advancing the throttle while attempting a go-around. He stated that during the go-around, the right wing stalled and contacted the ground followed by the nose of the airplane. A postaccident engine test run failed to reveal any discrepancies in the engine's operation. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_CHI97LA115.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 (stall, go-around, maintenance). All research papers
- Embry-Riddle Scholarly Commons 2023 · Conference paper The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA) From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- Semantic Scholar 2026 · Article (Reliability Engineering & System Safety) Understanding human error in military aviation maintenance: The role of Performance shaping factors, cognitive workload and error orientation
- 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.
- Semantic Scholar 2025 · Article (Applied Sciences) Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.