GAA16CA168

NTSB accident investigation · Hughes 369 · Jamestown, ND · March 26, 2016

Accident · No injuriesData collectionFinal report
Date
March 26, 2016, 15:30 local (20:30 UTC)
Place
Jamestown, ND
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N721RPHughes 369
Defining event
Autorotation: Controlled flight into terr/obj (CFIT)
Weather
Visual (VMC) · Day
Status
Completed · report June 15, 2016
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA Fargo FSDO
FAA report
20160326004249A
Case key
92917

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: descent rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedHughes Helicopters HUGHES 369D: 5 casesAll aircraft: 242 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

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).

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).

Aircraft

Registration
N721RP
Reported as
Hughes 369 (D)
Category
Helicopter
Serial number
310981D
Built
1981
Airframe hours
18,500.4
Engine
Rolls-Royce 250-C20B, 420 horsepower, turbo shaft
Damage
Substantial damage
Flight
Ferry · Part 91
Operator
Haverfield International Inc
Registered owner
Haverfield International Inc
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · March 21, 2016
Departed
JMS · Jamestown, ND
Destination
JMS · Jamestown, ND
Airport
JMS · Jamestown Rgnl, runway 04, 5,750 × 75 ft, asphalt
Equipment
None

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
24
Injuries
None
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
June 20, 2015
Seat
Left
Restraint
3-point
Flight hours
3,100 total · 1,500 in this make and model · 3,000 as pilot in command · 200 in the last 90 days · 70 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
36 °F, dew point 12 °F
Altimeter
30.12 inHg
Observed at
KJMS, 1 nm away

Docket · 2

The files NTSB released with the investigation on May 31, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.5 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.