NTSB CAROL · Event
Event ANC99LA062
Registry · N8883C
FAA Aircraft Registry record.
Make / Model
PIPER PA-22
Year of manufacture
1953 · 46 years old at event
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19560614
ADS-B equipped
Yes — Mode-S AC3E51
Registrant of record
BALL TRAVIS W
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The inadequate preflight by the pilot, who left the rudder gust lock installed, making directional control not possible.
Factual narrative
On May 15, 1999, at 1754 Alaska daylight time, a tailwheel equipped Piper PA-20 airplane, N8883C, sustained substantial damage when it departed the left edge of runway 19 at the Dillingham Airport, Dillingham, Alaska. The commercial pilot and sole passenger were not injured. The airplane was being operated under 14 CFR Part 91 as a personal flight by the pilot and his wife. The pilot originally intended to depart for the village of Ekuk, but was returning to park after taxiing for takeoff. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge (IIC) during a telephone interview on May 18, that during taxi, the airplane did not steer correctly, but he could not determine the reason. He told the IIC that he decided to return to parking. During the return taxi on runway 19, the airplane ground looped to the left, and the pilot was unable to control the turn with rudder input or wheel brakes. The tailwheel went off the left side of the runway onto uneven ground, damaging the tailwheel support structure and center empennage. The pilot told the IIC that after the accident, he discovered the external rudder gust lock still installed. Reported winds at the time of the accident were 210 degrees at 7 knots. Runway 19 measures 6,404 feet long by 150 feet wide. The pilot stated that during taxi for takeoff the tailwheel equipped airplane did not steer correctly. He said that he decided to return to parking. While returning to park, the airplane turned to the left 270 degrees, substantially damaging the empennage. Postaccident inspection revealed the rudder gust lock was still installed on the tail. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_ANC99LA062.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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