GAA18CA159

NTSB accident investigation · Hughes 269 · Jacksonville, FL · March 10, 2018

Accident · No injuriesData collectionFinal report
Date
March 10, 2018, 14:30 local (19:30 UTC)
Place
Jacksonville, FL
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N9020MHughes 269
Defining event
Autorotation: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report September 10, 2018
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20180310001899A
Case key
96858

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

On this page

Probable cause

The pilot’s failure to maintain rotor rpm during a practice autorotation, which resulted in ground contact and a dynamic rollover.

Findings · 3

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.

Use of equip/info: use of equip/systemPersonnel issues › Task performance · PilotHughes 269A: 2 casesAll aircraft: 1,391 casesProbable cause
Performance/control parameters: prop/rotor parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedHughes 269A: 7 casesAll aircraft: 182 casesProbable cause
Terrain: mountainous/hilly terrainEnvironmental issues › Physical environment · Contributed to outcomeHughes 269A: 1 caseAll aircraft: 329 cases

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 helicopter pilot reported that he entered a practice autorotation and intended to terminate the maneuver to a hover. During the flare phase of the maneuver, he allowed the rotor rpm to decay. He increased collective and subsequently added power with throttle. The nose of the helicopter yawed to the right and simultaneously the fuselage rolled to the left. He applied left pedal, but the left skid struck rising terrain and the helicopter entered dynamic rollover. The helicopter sustained substantial damage to the main rotor drive system and the tail rotor drive system. The pilot reported that there were no mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Factual narrative

The helicopter pilot reported that he entered a practice autorotation and intended to terminate the maneuver to a hover. During the flare phase of the maneuver, he allowed the rotor RPM to decay. He increased collective and subsequently added power with throttle. The nose of the helicopter yawed to the right and simultaneously the fuselage rolled to the left. He applied left pedal, but the left skid struck rising terrain and the helicopter entered dynamic rollover. The helicopter sustained substantial damage to the main rotor drive system and the tail rotor drive system. The pilot reported that there were no mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Aircraft

Registration
N9020M
Reported as
Hughes 269 (A)
Category
Helicopter
Serial number
64-18188
Built
1964
Airframe hours
4,093.8
Engine
Lycoming HIO-360-B1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Skypro Industries Inc
Registered owner
Skypro Industries Inc
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 4, 2017
Departed
CRG · Jacksonville, FL
Destination
CRG · Jacksonville, FL
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
60
Injuries
None
Certificates
Flight instructor, Commercial, Airline transport
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
November 15, 2017
Seat
Right
Restraint
4-point
Flight hours
12,958 total · 301 in this make and model · 88 in the last 90 days · 31 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
140° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 43 °F
Altimeter
30.03 inHg
Observed at
KCRG, 3 nm away

Docket · 2

The files NTSB released with the investigation on July 5, 2018, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.5 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.

Other investigations on N9020M · 1

Matched to the same aircraft by N-number and date.