NTSB CAROL · Event
Event CEN16LA231
Registry · N377H
FAA Aircraft Registry record.
Make / Model
CESSNA 182Q
Seats / Engines
4 seats · 1 engine
ADS-B equipped
Yes — Mode-S A44E7B
Registrant of record
CHUPP JEFFREY L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain a proper airspeed during the landing approach, which resulted in an improper flare and hard landing.
Factual narrative
On June 21, 2016, about 1947 central daylight time, a Cessna 182Q airplane, N377H, sustained substantial damage during a hard landing on runway 27 at the Anoka County-Blaine Airport (ANE), Blaine, Minnesota. The pilot and passenger were not injured. The airplane sustained damage to the forward fuselage and firewall. The airplane was registered to a private individual and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was not on a flight plan. The local flight originated about 10 minutes prior to the accident. The pilot reported that while in the traffic pattern, she applied carburetor heat and extended the flaps to 10 degrees. At this point her passenger informed her that the engine manifold pressure had reduced to 4 inches of manifold air pressure (MAP). She added throttle and the it recovered to 14-15 MAP. She stated that she was concerned about having an engine failure and kept the airspeed at 80 knots until she was sure she had the runway made. She then throttled back. The airspeed reduced to 60 knots and as the airplane crossed the end of the runway she "lost all airspeed". She stated that a short time later the airplane was 8-10 ft in the air and a hard landing was made. The private pilot was conducting a local personal flight. The pilot reported that, while in the traffic pattern, she applied carburetor heat and extended the flaps to 10 degrees. At this point, the passenger informed her that the engine manifold air pressure had reduced to 4 inches. She added throttle, and the manifold air pressure recovered to between 14 and 15 inches. The pilot stated that she was concerned about having an engine failure and kept the airspeed at 80 knots until she was sure the airplane could reach the runway. She added that she then throttled back and that the airspeed reduced to 60 knots and, as the airplane crossed the end of the runway, she "lost all airspeed." She stated that, shortly after, the airplane descended to 8 to 10 ft above the ground and then landed hard. Based on the available information, the airplane's engine responded to the pilot's control inputs. It is likely that the pilot's concern about the engine led to her failure to maintain a proper approach airspeed during the landing, which resulted in a hard landing. 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).
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- — Personnel issues-Psychological-Attention/monitoring-Attention-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2016_CEN16LA231.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 (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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