NTSB CAROL · Event
Event WPR10CA405
Registry · N992WS
FAA Aircraft Registry record.
Make / Model
HONDA AIRCRAFT CO LLC HA-420
Year of manufacture
2017
TCDS
A00018AT · HONDA AIRCRAFT COMPANY LLC
Engine
GE HONDA HF-120
Seats / Engines
8 seats · 2 engines
Last airworthiness date
20170929
ADS-B equipped
Yes — Mode-S ADDC16
Registrant of record
RE WDC INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's delay in making the decision to abort the takeoff. Contributing to the accident was the condition of the takeoff surface, and the high density altitude.
Factual narrative
The pilot of the turbocharged airplane was executing a takeoff from a 1,900 foot long grass/turf back country airstrip. The surface of the airstrip was rough, with occasional holes and soft spots, and areas of vegetation. The density altitude calculated by the pilot was 5,495 feet. Although he had determined that the airplane should be able to successfully complete the takeoff, during the later part of the takeoff roll the pilot became uncomfortable with the airplane's rate of acceleration, and he therefore elected to abort the takeoff. After making the decision to abort the takeoff, the pilot was unable to stop the airplane before it went off the end of the runway, rolled down a bank, and nosed over onto its back, whereupon it sustained substantial damage to both its wings and its fuselage. According to the pilot, there was no indication of any engine or flight control anomalies. In the Operator Safety Recommendation section of the NTSB form 6120.1, the pilot stated, "A decision to abort earlier may have prevented the roll off the end of the runway." The pilot of the turbocharged airplane was executing a takeoff from a 1,900-foot-long grass/turf back country airstrip. The surface of the airstrip was rough, with occasional holes and soft spots, and areas of vegetation. The density altitude calculated by the pilot was 5,495 feet. Although he had determined that the airplane should be able to successfully complete the takeoff, during the latter part of the takeoff roll the pilot became uncomfortable with the airplane's rate of acceleration, and he therefore elected to abort the takeoff. After making the decision to abort the takeoff, the pilot was unable to stop the airplane before it went off the end of the runway, rolled down a bank, and nosed over onto its back, whereupon it sustained substantial damage to both its wings and its fuselage. According to the pilot, there was no indication of any engine or flight control anomalies. In the Operator Safety Recommendation section of the NTSB form 6120.1, the pilot stated, "A decision to abort earlier may have prevented the roll off the end of the runway." 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-Action/decision-Action-Delayed action-Pilot - C
- — Environmental issues-Physical environment-Terrain-Rough terrain-Contributed to outcome
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surfa-Soft-Contributed to outcome
- — Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-High density altitude-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2010_WPR10CA405.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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