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GAA16CA168

2016-03-26 · Jamestown, North Dakota, United States · None · 1 aircraft · Status: Completed

Airport JMS

Current FAA registration · N721RP

Make / Model
HUGHES HELICOPTERS INC HUGHES 369D
Year of manufacture
1981 · 35 years old at event
Engine
ROLLS-ROYC 250-C20B (420 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20110610
ADS-B equipped
Yes — Mode-S A9A8C8

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's excessive descent rate while flaring during a practice autorotation with a power recovery, which resulted in an impact with terrain.

Factual narrative

The pilot reported that he was performing a practice autorotation with a power recovery, and was the sole occupant in the helicopter. He reported that the power was introduced at 200 feet above ground level (AGL) and he entered the flare at too low of an altitude. The tail rotor system impacted the soft ground adjacent to the planned landing area. The helicopter sustained substantial damage to the tailboom, the tail rotor driveshaft assembly, and the tail rotor system. The pilot verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration has published Advisory Circular (AC) 61-140 Autorotation Training (2013). This AC discusses the flare portion for autorotation training and states in part: Every autorotational flare will be different depending on the existing wind conditions, airspeed, density altitude, and the aircraft gross weight. This AC also discusses common errors during autorotation training and states in part: Improper flare (too much or not enough). Flaring too low or too high (AGL). The pilot reported that he was performing a practice autorotation with a power recovery, and was the sole occupant in the helicopter. He reported that the power was introduced at 200 feet above ground level (AGL) and he entered the flare at too low of an altitude. The tail rotor system impacted the soft ground adjacent to the planned landing area. The helicopter sustained substantial damage to the tailboom, the tail rotor driveshaft assembly, and the tail rotor system. The pilot verified that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration has published Advisory Circular (AC) 61-140 Autorotation Training (2013). This AC discusses the flare portion for autorotation training and states in part: Every autorotational flare will be different depending on the existing wind conditions, airspeed, density altitude, and the aircraft gross weight. This AC also discusses common errors during autorotation training and states in part: Improper flare (too much or not enough). Flaring too low or too high (AGL). 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-Descent rate-Not attained/maintained - C

Verbatim from NTSB's published report. Source file NTSB_2016_GAA16CA168.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.