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Atlas / NTSB / CEN23LA249

NTSB CAROL · Event

Event CEN23LA249

2023-06-21 Mesquite, Texas, United States Airport · HQZ None 1 aircraft Status: Completed

Registry · N9354B

FAA Aircraft Registry record.

Make / Model

CESSNA 175

Year of manufacture

1958 · 65 years old at event

Engine

CONT MOTOR GO-300 SERIES (175 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19580326

ADS-B equipped

Yes — Mode-S ACFB22

Registrant of record

C2 AERO LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s inability to maintain directional control during the landing roll due to corroded brake caliper pins.

Factual narrative

On June 21, 2023, about 1447 central daylight time, a Cessna 175, N9354B, was substantially damaged when it was involved in an accident near Mesquite, Texas. The pilot and passenger were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, after touchdown on the runway the airplane veered to the left, exited the runway, and impacted a precision approach path indicator light. The right wing and fuselage sustained substantial damage. After the accident, a runway inspection revealed a continuous black tire mark from near the runway centerline, consistent with the position of the left main gear when landing. The tire mark terminated at the runway edge, where a tire impression began and continued to the wreckage location. During a postaccident examination, the left wheel brake caliper was wedged and unable to free float with corrosion present on the caliper pins. The pilot stated that following the last annual inspection, he took the airplane to Alaska to conduct back-country flying. This was the only time the airplane was stored outside. Normally, the airplane remained in a hangar in Texas and out of the elements. According to the pilot, after touchdown on the runway the airplane veered to the left, exited the runway, and impacted a precision approach path indicator light. The right wing and fuselage sustained substantial damage. After the accident, a runway inspection revealed a continuous black tire mark from near the runway centerline, consistent with the position of the left main gear when landing. The tire mark terminated at the runway edge, where a tire impression began and continued to the wreckage location. A postaccident examination of the left wheel brake revealed corroded caliper pins, which prevented the brake caliper from free floating as designed. This corrosion likely prevented the tire from rotating and resulted in the uncorrectable veer off the runway. 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-Landing gear brakes system-Fatigue/wear/corrosion

Verbatim from NTSB's published report. Source file NTSB_2023_CEN23LA249.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗