ATL04LA065
2004-01-11 · Allendale, South Carolina, United States · None · 1 aircraft · Status: Completed
Airport 88J
N800SL has since been reassigned. It is now registered to a different aircraft (PIPER PA-28-181, built 2024), which was not involved in this event.
Aircraft involved
Probable cause & findings
The failure of the hydraulic brake system accumulator due to a ruptured diaphragm. A factor was the ditch.
Factual narrative
On January 11, 2004, at 1410 eastern standard time, an Aero Commander 500, N800SL, registered to and operated by an airline transport pilot, collided with a ditch during an attempted takeoff at Allendale County Airport, Allendale, South Carolina. The personal flight was operated under the provision of Title 14 CFR Part 91 with no flight plan filed. Visual meteorological conditions prevailed at the time of the accident. The pilot and passenger were uninjured and the airplane sustained substantial damage. The flight was originating from Allendale County Airport, Allendale, South Carolina, on January 11, 2004 at 1400. According to the pilot, while on takeoff roll the airplane began to "track right", differential braking input was applied to line up the airplane with the runway center line. The pilot noticed that the brake pedal felt "soft" and aborted the takeoff. When brakes were applied to stop the airplane, they failed and the airplane veered off the left side of the runway into a ditch. Examination of the airplane revealed the outboard right wing was bent aft and curled upwards. The fuselage was buckled in the wing root area of left and right wing. No mechanical or flight control problems were reported by the pilot. Examination of the wheel brakes revealed that the hydraulic pucks were leaking, and the brake disc and linings were worn. Examination of the accumulator revealed the diaphragm was ruptured and the system would not maintain pressure. According to the pilot, while on takeoff roll the airplane began to "track right", differential braking input was applied to line up the airplane with the runway center line. When brakes were applied to stop the airplane, they failed and the airplane veered off the left side of the runway into a ditch. Examination of the wheel brakes revealed that the hydraulic pucks were leaking, and the brake disc and linings were worn. Examination of the accumulator revealed the diaphragm was ruptured and the system would not maintain pressure. No other flight control or mechanical problems were reported by the pilot. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_ATL04LA065.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. All research papers
- NTSB Aircraft Accident Reports 2016 · Accident report Loss of Control on Approach Atlas Air 5Y3591 N7500A
Multiple loss-of-control approach investigations. Series of approach-loss-of-control case studies bundled into one report — examines somatogravic illusion + mode-confusion contributors in turbulent en…
- Semantic Scholar 2011 · Article Characterization and Analysis of Traffic Alert and Collision Avoidance Resolution Advisories Resulting from 500' and 1,000' Vertical Separation FAA TCAS Monitoring in the U.S. National Airspace System
- arXiv 2026 · arXiv preprint nBMS, a Neuromorphic Battery Management System with a Silicon-Validated Spiking State-of-Charge Core for eVTOL Aircraft
State-of-charge (SoC) estimation for electric vertical take-off and landing (eVTOL) aircraft must run on the vehicle under hard energy and certification budgets, on a duty cycle unlike anything in the…
- arXiv 2025 · arXiv preprint Comparing the dynamics of idealized squall lines between NWP and LES models
Both Numerical Weather Prediction (NWP) models and Large-Eddy Simulation (LES) models are used to simulate convective systems, such as squall lines, but with different purposes.
- arXiv 2025 · arXiv preprint Toward Safe Integration of UAM in Terminal Airspace: UAM Route Feasibility Assessment using Probabilistic Aircraft Trajectory Prediction
Integrating Urban Air Mobility (UAM) into airspace managed by Air Traffic Control (ATC) poses significant challenges, particularly in congested terminal environments.
- Embry-Riddle Scholarly Commons 2025 · Journal article (IJAAA) Consumer Preferences and Willingness to Pay for Vertiport Design, Amenities, and Services
The rise of urban air mobility (UAM) and electric vertical takeoff and landing (eVTOL) aircraft necessitates the development of well-designed vertiports that align with consumer expectations.