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ERA12CA079

2011-11-19 · Lyman, Mississippi, United States · None · 1 aircraft · Status: Completed

Airport MS82

Current FAA registration · N75Q

Make / Model
BEECH C-45G
Year of manufacture
1951 · 60 years old at event
Engine
P&W R-985 SERIES (450 hp)
Seats / Engines
10 seats · 2 engines
Last airworthiness date
19630822
ADS-B equipped
Yes — Mode-S AA190E

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The collapse of the right main landing gear during landing due to an encounter with soft terrain.

Factual narrative

The pilot stated that he and the passengers had just completed a local sightseeing flight and were returning back to the private airport from whence they departed. The approach was unremarkable. On landing the main gear wheels touched down onto the turf runway at an indicated speed of 90 mph. Upon the airplane settling, it encountered a soft spot on the turf runway. The right propeller made contact with the ground. The airplane then slid forward on its nose and ground looped toward the right incurring substantial damage to the wing and fuselage before coming to a stop 180 degrees from the direction of landing. An examination of the right main gear torque knee link by the responding Federal Aviation Administration inspector revealed the link fractured in overload; permitting the lower right gear, wheel assembly, to twist. The pilot did not report any mechanical failures or malfunctions to the airplane or any of its systems prior to the accident. The pilot stated that, during landing, the main landing gear wheels touched down on the turf runway at an indicated speed of 90 mph. During the landing roll, the right main landing gear encountered a soft spot on the runway and collapsed. The right propeller contacted the ground, the airplane slid forward on its nose, and ground looped toward the right, incurring substantial damage to the wing and fuselage, before coming to a stop opposite the direction of landing. The pilot attributed the collapse of the right main landing gear to the failure of the right main gear torque knee link. An examination of the right main gear torque knee link revealed that the link fractured in overload, which allowed the lower portion of the right landing gear, including the wheel assembly, to twist and separate. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Environmental issues-Operating environment-Airport facilities/design-Runway/landing area condition-Effect on equipment - C
  • C Environmental issues-Physical environment-Runway/land/takeoff/taxi surfa-Soft-Effect on equipment - C
  • — Aircraft-Aircraft systems-Landing gear system-Main gear strut/axle/truck-Capability exceeded

Verbatim from NTSB's published report. Source file NTSB_2011_ERA12CA079.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.