CEN11CA661
2011-09-10 · Huntington, Indiana, United States · None · 1 aircraft · Status: Completed
Airport HHG
Current FAA registration · N71212
- Make / Model
- LUSCOMBE 8A
- Year of manufacture
- 1946 · 65 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560106
- ADS-B equipped
- Yes — Mode-S A98611
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The failure of the right main landing gear strut due to internal corrosion.
Factual narrative
The pilot reported that he heard a "pop noise" during his three-point landing. The airplane's nose veered right and the right wing dropped. The right main landing gear collapsed. The right wing sustained substantial damage when it contacted the runway. A post accident examination of the separated landing gear strut revealed that the interior of the strut exhibited a rust color consistent with oxidation. The separation was consistent with overload. The pilot reported that he had completed a normal landing, and during the landing roll, he heard a "pop noise." He said that the nose veered right, and he applied left rudder, but the right wing dropped and the right main landing gear collapsed. The airplane sustained substantial damage. A postaccident examination of the separated landing gear strut revealed that the interior of the strut exhibited a rust color consistent with oxidation. The separation was consistent with overload. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft systems-Landing gear system-Main landing gear attach sec-Fatigue/wear/corrosion - C
Verbatim from NTSB's published report. Source file
NTSB_2011_CEN11CA661.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- Embry-Riddle Scholarly Commons 2020 · Conference paper Concurrent Sessions: Session 8A - Technology in Aviation
- arXiv 2020 · arXiv preprint Continuation Method with the Trusty Time-stepping Scheme for Linearly Constrained Optimization with Noisy Data
The nonlinear optimization problem with linear constraints has many applications in engineering fields such as the visual-inertial navigation and localization of an unmanned aerial vehicle maintaining…