GAA19CA185
2019-03-28 · Hermiston, Oregon, United States · Minor · 1 aircraft · Status: Completed
Airport HRI
Current FAA registration · N4250X
- Make / Model
- RANS S-2R
- Year of manufacture
- 1974 · 45 years old at event
- Engine
- P&W R1340 SERIES (600 hp)
- Seats / Engines
- 1 seats · 1 engine
- Last airworthiness date
- 19740808
- ADS-B equipped
- Yes — Mode-S A510A0
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's distraction due to a spray handle opening and his improper pitch trim setting during final approach, which resulted in an excessive pitchdown when he took his hand off the controls to close the handle.
Factual narrative
The pilot reported that, after completing an agricultural spraying flight, he returned to the airport. He added that, on final, he added flaps and became distracted by a spray handle that became open due to vibration. He took his hand off the control stick to close the spray handle, but because the airplane was improperly trimmed, the airplane pitched down severely. He pitched the nose up to about level, but the main landing gear struck the ground. The airplane bounced onto an irrigation system, the right main landing gear separated, and the airplane spun around before coming to rest. The airplane sustained substantial damage to both wings, fuselage, and empennage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that, after completing an agricultural application flight, he returned to the airport. He added that, on final, he added flaps and became distracted by a spray handle that became open due to vibration. He took his hand off the control stick to close the spray handle, but because the airplane was improperly trimmed, the airplane pitched down severely. He pitched the nose up to about level, but the main landing gear struck the ground. The airplane bounced and impacted an irrigation system, the right main landing gear separated, and the airplane spun around before coming to rest. The airplane sustained substantial damage to both wings, the fuselage, and the empennage. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Aircraft-Aircraft systems-Flight control system-Elevator tab control system-Incorrect use/operation - C
- C Personnel issues-Task performance-Use of equip/info-Use of equip/system-Pilot - C
- F Personnel issues-Psychological-Attention/monitoring-Attention-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2019_GAA19CA185.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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