N911R

Substantial
None

Eurocopter Deutschland BK117S/N: 7502

Accident Details

Date
Monday, August 20, 2007
NTSB Number
DFW07CA186
Location
Slaton, TX
Event ID
20070829X01263
Coordinates
33.489444, -101.650833
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's failure to maintain control of the hovering helicopter and the flight instructor's improper supervision of the flight.

Aircraft Information

Registration
N911R
Make
EUROCOPTER DEUTSCHLAND
Serial Number
7502
Model / ICAO
BK117

Registered Owner (Historical)

Name
MURPHY CHARLES R
Address
BOX 139
Status
Deregistered
City
LOMPOC
State / Zip Code
CA 93436
Country
United States

Analysis

The helicopter drifted backwards during a confined area operations training and the tail rotor blades struck tree branches while hovering over tall grass. The 11,330 hour flight instructor and the 16,800 hour pilot receiving instruction reported that they were both familiar with the training area being used, the flight was properly briefed, and they had both worked together as a crew in the past. The crew reported that the pilot performed a high recon of the landing area, noting the surface winds, approach and departure paths, and the conditions of the landing zone. The approach was planned to terminate at a hover. The grass at the landing zone is normally less than a foot long; however, due to the record rainfall this year, the grass was 3-to-4 feet tall. Both pilots underestimated the effects of prolonged hovering over tall grass. The tall-waving grass disoriented the pilot and allowed the helicopter to drift into the trees. The flight instructor was clearing the left side of the helicopter during the approach and hover, but was unable to react in time to take the flight controls to stop the drift. The flight crew immediately landed the helicopter in the confined area when they felt a vibration from the tail rotor. The helicopter was recovered to the operator's maintenance facility for damage assessment. Examination of the helicopter by the flight crew, the operator, and the FAA inspector, confirmed that both tail rotor blades were destroyed, the mounting bolts for the tail rotor 90 degree box were damaged or broken, and the tail fin gearbox mounting spar was also 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# DFW07CA186