NTSB CAROL · Event
Event ERA10CA352
Registry · N801RG
FAA Aircraft Registry record.
Make / Model
VAN'S AIRCRAFT RV-8
Year of manufacture
2007 · 3 years old at event
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20070901
ADS-B equipped
Yes — Mode-S AAE712
Registrant of record
SWEDE AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during the landing rollout.
Factual narrative
The pilot/owner of the tail-wheeled airplane stated that he was conducting touch-and-go landings at the conclusion of a 30-minute local pleasure flight. The first two landings were "normal," and the third touchdown was "smooth." As the pilot lowered the tailwheel, the airplane veered to the left. The pilot corrected, and the airplane made "an abrupt swerve to the right." The left main landing gear collapsed, and the airplane came to rest upright in grass off the right edge of the runway. The left wing sustained substantial damage, and closer inspection of the airplane revealed that the left undercarriage outboard attachment bracket had fractured. Examination of the bracket at the NTSB Materials Laboratory indicated that the fracture was the result of overstress. In a subsequent interview, the pilot stated that he typically wore a parachute while flying, but was not wearing one during the accident flight. He stated that the absence of the parachute placed him further from the controls than he was accustomed, and that he was unable to move the rudder pedals through their full range of motion. The pilot stated that there were no deficiencies in the performance or handling of the airplane. The pilot/owner of the tailwheel-equipped airplane stated that he was conducting touch-and-go landings at the conclusion of a 30-minute local pleasure flight. he noted that the first two landings were normal, and the third touchdown was "smooth." As the pilot lowered the tailwheel, the airplane veered to the left. The pilot corrected, and the airplane made "an abrupt swerve to the right." The left main landing gear collapsed and the airplane came to rest upright in grass off the right edge of the runway. The left wing sustained substantial damage, and closer inspection of the airplane revealed that the left undercarriage outboard attachment bracket had fractured. Examination of the bracket at the NTSB Materials Laboratory indicated that the fracture was the result of overstress. In a subsequent interview, the pilot stated that he typically wore a parachute while flying, but was not wearing one during the accident flight. He stated that the absence of the parachute placed him further from the controls than he was accustomed, and that he was unable to move the rudder pedals through their full range of motion. The pilot stated that there were no deficiencies in the performance or handling of the airplane. 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).
- 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
- — Personnel issues-Action/decision-Action-Incomplete action-Pilot
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA10CA352.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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