NTSB CAROL · Event
Event CEN24LA329
Registry · N1652T
FAA Aircraft Registry record.
Make / Model
CESSNA 414
Year of manufacture
1973 · 51 years old at event
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
7 seats · 2 engines
Last airworthiness date
19810612
ADS-B equipped
Yes — Mode-S A106F1
Registrant of record
BAS PART SALES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A loss of brake fluid for reasons that could not be determined, which resulted in a loss of braking effectiveness during landing.
Factual narrative
On July 4, 2024, about 1030 mountain daylight time, a Cessna 414 airplane, N1652T, was substantially damaged when it was involved in an accident at Lake County Airport (LXV), Leadville, Colorado. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that the airplane’s brake system operated normally during the startup, taxi, and takeoff. The initial landing approach at the destination terminated in a go-around due to another airplane back-taxiing on the runway. The second approach was normal, and the airplane touched down about 1,500 ft from the runway threshold. He attempted to apply the brakes after touchdown; however, there was no pressure on the brake pedals and no braking was available. There was also no pressure available on the co-pilot’s brake pedals. The airplane rolled the length of the runway. The pilot attempted to turn onto the perpendicular taxiway at the end of the runway, but the airplane departed the pavement, and the nose landing gear collapsed. The nose landing gear trunnion and wheel well structure sustained substantial damage during the accident sequence. An examination of the brake system revealed that the left brake master cylinder was nearly empty and no pressure from the brake pedal to the wheel caliper was available. The right brake master cylinder contained about 1/4-inch of fluid. Pressure to the wheel caliper was obtained with about three-quarter deflection of the brake pedal. The brake lines and calipers did not exhibit any evidence of leakage, and free movement of the caliper pistons was observed. Both the left and right brake linings exhibited minimal remaining thickness with signs of overheating. Airplane maintenance records noted that the landing gear was worked on during the most recent annual inspection, which was completed about two months before the accident. The pilot reported that the airplane had flown about 40 hours since the inspection. The mechanic who conducted the annual inspection reported that the brakes were inspected and no anomalies were observed at that time. The pilot reported that the airplane’s brake system operated normally during the startup, taxi, and takeoff; however, while landing at the destination airport, he attempted to apply the brakes; however, there was no pressure on the brake pedals and no braking was available. There was also no pressure available on the co-pilot’s brake pedals. The airplane rolled the length of the runway. The pilot attempted to turn onto the perpendicular taxiway at the end of the runway, but the airplane departed the pavement and the nose landing gear collapsed. The nose landing gear trunnion and wheel well structure sustained substantial damage during the accident sequence. An examination of the brake system revealed that the left brake master cylinder was nearly empty and no pressure from the brake pedal to the wheel caliper was available. The right brake master cylinder contained about 1/4-inch of fluid remaining. Pressure to the wheel caliper was obtained with about three-quarter deflection of the brake pedal. The brake lines and calipers did not exhibit any evidence of leakage, and free movement of the caliper pistons was observed. Both the left and right brake linings exhibited minimal remaining thickness with signs of overheating. Airplane maintenance records noted that the landing gear was worked on during the most recent annual inspection, which was completed about two months before the accident. The pilot reported that the airplane had flown about 40 hours since the inspection. The mechanic who conducted the annual inspection reported that the brakes were inspected and no anomalies were observed at that time. Although the runway excursion was a result of the loss of brake fluid, the exact reason for the loss of brake fluid during the flight could not be determined. 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).
- — Aircraft-Aircraft systems-Landing gear system-Brake-Damaged/degraded
- — Aircraft-Fluids/misc hardware-Fluids-(general)-Fluid level
Verbatim from NTSB's published report. Source file
NTSB_2024_CEN24LA329.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 (runway excursion, go-around, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Semantic Scholar 2025 · Article (Applied Sciences)
Decision-Making Framework for Aviation Safety in Predictive Maintenance Strategies
The implementation of predictive maintenance (PM) in aviation presents unique challenges due to strict safety requirements, complex operational environments, and regulatory constraints.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- Embry-Riddle Scholarly Commons 2024 · Journal article (JAAER)
Low-Resource Automatic Speech Recognition Domain Adaptation – A Case-Study in Aviation Maintenance
With timeliness and efficiency being critical in the aviation maintenance industry, the need has been growing for smart technological solutions that optimize and streamline the different underlying ta…
Browse the full corpus — academia portal ↗