N3183T

Substantial
Minor

ROBINSON HELICOPTER COMPANY R44 IIS/N: 11550

Accident Details

Date
Friday, January 2, 2015
NTSB Number
ERA15CA089
Location
Barranquitas, PR
Event ID
20150103X94415
Coordinates
18.209722, -66.293891
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

The pilot's failure to maintain control of the helicopter while landing which resulted in a tailrotor ground strike and collision with terrain.

Aircraft Information

Registration
N3183T
Make
ROBINSON HELICOPTER COMPANY
Serial Number
11550
Engine Type
Reciprocating
Year Built
2007
Model / ICAO
R44 IIR44
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
FLIGHT WORLD INC
Address
PO BOX 192343
NORTH RAMP LOT G-6
Status
Deregistered
City
SAN JUAN
State / Zip Code
PR 00919-2343
Country
United States

Analysis

After renting the helicopter from a flight school, the pilot took off and flew to a nearby town where he picked up two passengers. He then flew them to another town to attend a party. During the flights everything was normal. Upon arrival at their destination, the pilot began to circle and asked one of the passengers to call a friend who was on the ground on his cell phone, to check the landing area to make sure it was clear for him to land. After the pilot was told it was "clear for landing," he started a smooth descent "with all of the instruments in the green arc," to the landing area which was located on a dirt road on the ridge of a mountain. The landing was smooth and the pilot touched down lightly on the skids. While the helicopter had not fully set down and was still light on the skids, he began to check the "balance of the helicopter" before setting the collective to the full down position. When he moved the cyclic forward, the helicopter pitched forward. Then when he moved the cyclic aft to its previous position, the helicopter pitched aft and he heard a "big noise" and felt a vibration. He immediately "pulled" collective and rolled the throttle to the full throttle position to get the helicopter back into the air but, the helicopter started to spin clockwise and he could not stop the rotation, even with the application of full left pedal. He then leveled the helicopter while it was still spinning and tried to make it back to the landing site but, there was not enough power to keep it airborne. The left skid then contacted the ground and the helicopter rolled over on to its left side. Postaccident examination of the helicopter by a Federal Aviation Administration inspector revealed that the tail rotor assembly and tail boom were substantially damaged.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA15CA089