NTSB CAROL · Event
Event ANC16CA069
Registry · N743R
FAA Aircraft Registry record.
Make / Model
PIPER PA-18-150
Year of manufacture
1981 · 35 years old at event
Engine
LYCOMING O-320-B2B (160 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20141003
ADS-B equipped
Yes — Mode-S A9FF26
Registrant of record
KISKADDON LUKE M
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airplane control during the landing roll, which resulted in a nose-over.
Factual narrative
The pilot reported he was conducting stop-and-go-landings in a tailwheel-equipped airplane to a dry, gravel runway. During the third landing, he reported all three wheels from the landing gear were in contact with the runway and he slowed with normal braking application. He reported that he abruptly felt the tail of the airplane lift, the propeller impacted terrain, and the airplane nosed over. The airplane sustained substantial damage to the fuselage, the right wing struts, and the rudder. During a telephone conversation with the National Transportation Safety Board investigator-in-charge, the pilot stated that he was unsure if a tail wind or his braking application caused the airplane to nose over. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot wore a surplus U.S. Navy Flight Deck Crewman's helmet for the flight in addition to utilizing a four-point restraint system. He reported that if he was not wearing a helmet, the injuries sustained to his face, head, and brain would have been serious or fatal. The closest weather reporting facility was the Wasilla Airport, Wasilla, Alaska, about 20 miles southeast of the accident site. At 1556, an Aviation Routine Weather Report (METAR) was reporting in part: wind, calm. In the weather section of the National Transportation Safety Board Accident/Incident Reporting Form 6120.1, the pilot reported the wind direction was variable and the wind speed was light and variable at the accident site. The Federal Aviation Administration (FAA) has published the Airplane Flying Handbook FAA-H-8083-3A (2004). This handbook discusses braking application procedures for tailwheel-equipped airplanes and states in part: Some models of tailwheel airplanes are equipped with heel brakes rather than toe brakes. In either configuration the brakes are used primarily to stop the airplane at a desired point, to slow the airplane, or as an aid in making a sharp controlled turn. Whenever used, they must be applied smoothly, evenly, and cautiously at all times. The FAA and the Medallion Foundation has published the Alaska Flight Review Guide (2014). This guide discusses aviation life support equipment and states in part: Considering the type of aircraft and mission, a helmet may help survive an accident. The U.S. military and European community has established standards for flying helmets. Emphasize the importance of choosing a helmet which meets an appropriate standard for the type of operation, and which is kept in good repair. Fatal and serious injury data suggests that helmets are most useful in tandem seat aircraft. A three-point harness is the minimum installation recommended for both front and back seats. The four and five point harnesses are a great improvement to the security of the user due to the geometry of the belts installation. Any properly installed and worn shoulder harness is an improvement over no shoulder harness at all. The pilot reported he was conducting stop-and-go-landings in a tailwheel-equipped airplane to a dry, gravel runway. During the third landing, he reported all three wheels from the landing gear were in contact with the runway and he slowed with normal braking application. He reported that he abruptly felt the tail of the airplane lift, the propeller impacted terrain, and the airplane nosed over. The airplane sustained substantial damage to the fuselage, the right wing struts, and the rudder. During a telephone conversation with the National Transportation Safety Board investigator-in-charge, the pilot stated that he was unsure if a tail wind or his braking application caused the airplane to nose over. The pilot reported there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot wore a surplus U.S. Navy Flight Deck Crewman's helmet for the flight in addition to utilizing a four-point restraint system. He reported that if he was not wearing a helmet, the injuries sustained to his face, head, and brain would have been serious or fatal. The closest weather reporting facility was the Wasilla Airport, Wasilla, Alaska, about 20 miles southeast of the accident site. At 1556, an Aviation Routine Weather Report (METAR) was reporting in part: wind, calm. In the weather section of the National Transportation Safety Board Accident/Incident Reporting Form 6120.1, the pilot reported the wind direction was variable and the wind speed was light and variable at the accident site. The Federal Aviation Administration (FAA) has published the Airplane Flying Handbook FAA-H-8083-3A (2004). This handbook discusses braking application procedures for tailwheel-equipped airplanes and states in part: Some models of tailwheel airplanes are equipped with heel brakes rather than toe brakes. In either configuration the brakes are used primarily to stop the airplane at a desired point, to slow the airplane, or as an aid in making a sharp controlled turn. Whenever used, they must be applied smoothly, evenly, and cautiously at all times. The FAA and the Medallion Foundation has published the Alaska Flight Review Guide (2014). This guide discusses aviation life support equipment and states in part: Considering the type of aircraft and mission, a helmet may help survive an accident. The U.S. military and European community has established standards for flying helmets. Emphasize the importance of choosing a helmet which meets an appropriate standard for the type of operation, and which is kept in good repair. Fatal and serious injury data suggests that helmets are most useful in tandem seat aircraft. A three-point harness is the minimum installation recommended for both front and back seats. The four and five point harnesses are a great improvement to the security of the user due to the geometry of the belts installation. Any properly installed and worn shoulder harness is an improvement over no shoulder harness at all. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2016_ANC16CA069.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). 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 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…
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