NTSB CAROL · Event
Event ANC98LA164
Registry · N8115V
FAA Aircraft Registry record.
Make / Model
GILL JAY L PC-2000
Year of manufacture
2001
Engine
ROTAX 582SER (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20070810
ADS-B equipped
Yes — Mode-S AB102E
Registrant of record
GILL JAY L
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The failure of the recently overhauled right brake seal resulting in a total loss of brake fluid, failure of the right brake system, and subsequent inability of the pilot to utilize the brake. A contributing factor was the soft terrain.
Factual narrative
On September 24, 1998, about 1240 Alaska daylight time, a Grumman S2F-1 airplane, N8115V, sustained substantial damage when it departed runway 21 during landing at the New Wasilla airport, Wasilla, Alaska. The solo airline transport pilot was not injured. The airplane was owned and operated by the pilot under 14 CFR Part 91 as a local, personal flight. The airplane was being operated under an FAA letter of authorization, leading to an experimental category airworthiness certificate. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge during a telephone interview on September 29, and wrote in his NTSB Pilot / Operator report, that during landing the right brake failed and the airplane began to drift to the left. The pilot said that soft earth on the left side of the runway compounded the left drift, and that differential power did not swing the nose of the airplane back to the right. The airplane departed the left side of the 3,700 feet long by 75 feet wide gravel runway, and the nose landing gear collapsed. Subsequent inspection of the airplane by an FAA Flight Standards District Office inspector revealed that the right brake seal failed, releasing the hydraulic fluid. A review of records showed that the right main landing gear had been overhauled, and the right brake seal replaced on June 8, 1998, at 7,363 airframe total hours, 15 hours prior to the accident. A review of work orders submitted by the overhaul facility listed the following repairs (in part): Remove R/H Wheel & Repair Leak 1.8 hours Overhaul Brakes 3.3 hours Install Tire & Set Brakes 0.8 hours Install R/H Brake 2.2 hours Install Brakes 4.3 hours During the landing roll, the right brake seal failed on the experimental category, ex-military airplane, releasing the hydraulic fluid and subsequently rendering the brake unusable. The airplane encountered soft earth as it began to drift left, and ultimately departed the left side of the 3,700 feet long by 75 feet wide gravel runway. The nose gear then collapsed. The right brake system had been overhauled and the right brake seal replaced 15 hours prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_ANC98LA164.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…
Browse the full corpus — academia portal ↗