ERA11CA441
2011-08-05 · Sylacauga, Alabama, United States · None · 1 aircraft · Status: Completed
Airport SCD
Aircraft involved
Probable cause & findings
A stuck exhaust-valve on the number one cylinder which resulted in a loss of engine power.
Factual narrative
The student pilot and his flight instructor took off from their home airport and proceeded to an outlying airport to practice landings and takeoffs. After the student demonstrated a touch and go landing, as the airplane climbed through approximately 150 feet above ground level the engine lost power. The flight instructor then took control of the airplane, and attempted to trouble shoot the loss of power while executing a turn to the right as the forested area off the end of the runway precluded landing straight ahead. The airplane then descended below the tops of the trees and the flight instructor attempted to follow an S-turn in a road and land in an area free from obstructions. Midway through the turn however, the airspeed began to degrade and the airplane began to stall. The flight instructor then reduced angle of attack to keep from stalling and losing control and allowed the left wing to come in contact with a tree. The airplane then yawed to the left, the right wing then contacted trees, and the airplane impacted the ground. Post accident examination by a Federal Aviation Administration inspector revealed that the exhaust valve for the No.1 cylinder was stuck in the open position which was consistent with the engine's loss of power. The student demonstrated a touch-and-go landing and as the airplane climbed through approximately 150 feet above ground level, the engine lost power. The certified flight instructor (CFI) took control of the airplane and attempted to troubleshoot the loss of power while executing a turn to the right, as the forested area off the end of the runway precluded landing straight ahead. The airplane descended below the tops of the trees, and the CFI attempted to follow an S-turn in a road and land in an area free from obstructions. Midway through the turn, the airspeed began to degrade, and the airplane began to stall. The CFI reduced the angle of attack to keep from stalling and losing control and allowed the left wing to come in contact with a tree. The airplane yawed to the left, the right wing contacted trees, and the airplane impacted the ground. A postaccident examination revealed that the exhaust valve for the No.1 cylinder was stuck in the open position which was consistent with the engine's loss of power. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft power plant-Engine (reciprocating)-Recip eng cyl section-Malfunction - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA11CA441.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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 …
- 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.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…