NTSB CAROL · Event
Event GAA18CA391
Registry · N6508K
FAA Aircraft Registry record.
Make / Model
CESSNA 172P
Year of manufacture
1980 · 38 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19800910
ADS-B equipped
Yes — Mode-S A89034
Registrant of record
TROY OAKLAND PILOTS FLYING CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s failure to maintain a proper landing flare, which resulted in a hard, porpoised landing during an aborted go-around.
Factual narrative
The solo student pilot reported that during landing, the airplane slowed, and the stall warning sounded as the main landing gear contacted the runway. He added that, it appeared that the airplane had landed, but he then observed the nose drop below the horizon. He added power to go around, but the nose wheel impacted the runway and the airplane pitched "rearward". Subsequently, the airplane porpoised, the nose landing gear strut collapsed, and he aborted the go around. The student taxied the airplane to park without further incident. The flight instructor reported that, he witnessed that the airplane on approach was a little flat but did not appear to be unstable. The student then pitched the airplane for the numbers, the airplane floated down the runway, and touched down in a flat attitude. Subsequently, the airplane bounced 2 to 3 ft in the air, porpoised, and the student was then able to taxi from the runway. The flight instructor added that, the student was too late on his flare and all of the energy came down on the nose wheel. The airplane sustained substantial damage to the fuselage. The student pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation system at the accident airport reported that, about the time of the accident, the wind was from 250° at 7 knots. The student pilot landed on runway 27. The solo student pilot reported that, during landing, the airplane slowed, and the stall warning sounded as the main landing gear contacted the runway. He added that it appeared that the airplane had landed, but he then observed the nose drop below the horizon. He added power to go around, but the nosewheel impacted the runway, and the airplane pitched "rearward." Subsequently, the airplane porpoised, the nose landing gear strut collapsed, and he aborted the go-around. The student taxied the airplane to park without further incident. The flight instructor reported that he witnessed that the airplane on approach was a little flat but did not appear to be unstable. The student then pitched the airplane for the numbers, the airplane floated down the runway, and it then touched down in a flat attitude. Subsequently, the airplane bounced 2 to 3 ft, porpoised, and the student was then able to taxi from the runway. The flight instructor added that the student was too late on the flare and that all of the energy came down on the nosewheel. The airplane sustained substantial damage to the fuselage. The student reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation system at the airport reported that, about the time of the accident, the wind was from 250° at 7 knots. The student pilot landed the airplane on runway 27. 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-Landing flare-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Student/instructed pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA391.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 (stall, 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 2019 · Conference Paper
Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM)
Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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 …
- 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…
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
Browse the full corpus — academia portal ↗