CEN12CA269
2012-04-29 · Hugo, Oklahoma, United States · None · 1 aircraft · Status: Completed
Airport HHW
Aircraft involved
Probable cause & findings
The pilot’s inadequate collective control inputs while performing a hovering autorotation, which resulted in a hard landing. Contributing to the accident was the check airman's delayed remedial action.
Factual narrative
A check airman was giving the pilot in command a night vision goggle (NVG) annual check ride in the emergency medical service helicopter. After a satisfactory slope landing, the pilot in command repositioned the helicopter to a flat area and performed a hovering autorotation which resulted in a hard landing. The check airman then demonstrated a second hovering autorotation and the pilot in command performed a third hovering autorotation which was satisfactory. The check airman continued the annual check ride. After the flight, during a post flight inspection, substantial damage was discovered to the tail boom and the aft portion of the fuselage. The damage was consistent with a hard landing, presumably incurred during the first hovering autorotation in which the helicopter landed hard. In a statement provided to the NTSB, the check airman said that he should have guarded the collective more to limit the amount of control input during the practice autorotation maneuvers. A check airman was giving the pilot-in-command (PIC) an annual check ride with night vision goggles in the emergency medical service helicopter. After a satisfactory slope landing, the PIC repositioned the helicopter to a flat area and performed a hovering autorotation, which resulted in a hard landing. The check airman then demonstrated a second hovering autorotation, and the PIC performed another hovering autorotation that was satisfactory. The check airman continued the annual check ride. After the flight, during a post-flight examination, substantial damage was discovered to the tail boom and the aft portion of the fuselage. The damage was consistent with a hard landing, presumably incurred during the first hovering autorotation in which the helicopter landed hard. In a statement provided to the NTSB, the check airman said that he should have guarded the collective more to limit the amount of control input during the practice autorotation maneuvers. 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-Descent rate-Incorrect use/operation - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
- F Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12CA269.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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