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CEN20CA284

2020-07-14 · Spring, Texas, United States · None · 1 aircraft · Status: Completed

Airport DWH

Current FAA registration · N1332Z

Make / Model
BEECH 95-55
Year of manufacture
1961 · 59 years old at event
Engine
CONT MOTOR I0-470 SERIES (260 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19610615
ADS-B equipped
Yes — Mode-S A0890C

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

Excessive wear of the left brake liners which reduced brake effectiveness resulting in a runway excursion.

Factual narrative

The cabin entry door popped open during the takeoff roll. The pilot immediately rejected the takeoff; however, the airplane did not slow down. As the pilot attempted to exit onto a taxiway at the end of the runway, the airplane departed the pavement and came to rest in a ditch causing substantial damage to the forward fuselage, and damage to nose gear and propellers. During a postaccident inspection, a Federal Aviation Administration inspector determined that the left main landing gear brake disc was discolored consistent with overheating. The brake liners were worn at or beyond service limits. The right main landing gear brake disc and liners remained within service limits; although, the disc was warped. No other anomalies were observed. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft systems-Landing gear system-Brake-Fatigue/wear/corrosion - C
  • — Personnel issues-Task performance-Maintenance-(general)-Maintenance personnel

Verbatim from NTSB's published report. Source file NTSB_2020_CEN20CA284.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (runway excursion). All research papers