ERA12CA403
2012-06-09 · Selinsgrove, Pennsylvania, United States · None · 1 aircraft · Status: Completed
Airport SEG
Current FAA registration · N2052K
- Make / Model
- LUSCOMBE 8E
- Year of manufacture
- 1947 · 65 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19551026
- ADS-B equipped
- Yes — Mode-S A1A73E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airplane control during the takeoff.
Factual narrative
The pilot reported that the airplane suddenly veered to the left during the takeoff roll and he was unable to stop before it departed the left side of the runway. A witness at the airport observed the airplane airborne over the grass area between the runway and taxiway, when the right wing struck the ground. The airplane then bounced on the right and left main landing gears, before coming to rest on the grass. The airplane's right wing was substantially damaged. Post accident examination of the airplane by a Federal Aviation Administration inspector did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation. The pilot reported that the airplane suddenly veered to the left during the takeoff roll and that he was unable to stop the airplane before it departed the left side of the runway. A witness at the airport observed the airplane airborne over the grass area between the runway and taxiway, and the right wing struck the ground. The airplane then bounced on the right and left main landing gears before coming to rest on the grass. The airplane's right wing was substantially damaged. Postaccident examination of the airplane did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2012_ERA12CA403.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
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.