Loss of control Accident Eurocopter AS 350B3 Ecureuil N253HP,
ASN logo
ASN Wikibase Occurrence # 179504
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Wednesday 9 September 2015
Time:10:40
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Eurocopter AS 350B3 Ecureuil
Owner/operator:Private
Registration: N253HP
MSN: 7533
Year of manufacture:2013
Total airframe hrs:834 hours
Engine model:Turbomeca Arriel 2D
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Corner Canyon, UT -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Ambulance
Departure airport:Salt Lake City, UT (SLC)
Destination airport:Salt Lake City, UT (SLC)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that he and a tactical flight officer were conducting a high altitude rescue mission in "remote and nearly vertical" terrain with a public use helicopter, by doing a one-skid recovery. The purpose of this mission was to recover a fallen hiker.

A member of the three person ground recovery team had secured himself to a rescue rope that was anchored to the steep terrain above the plane-of-rotation of the main rotor system blades. Once the helicopter's right skid landed on a rock outcrop, the ground recovery team approached the helicopter to begin the loading process. During the approach to the helicopter, the rescue rope came in contact with a main rotor blade.

The pilot reported that the helicopter then, "rotated abruptly to the left and began to shake violently." The helicopter impacted terrain, the pilot regained control, and he then made an emergency landing at a lower altitude. He reported that upon applying power to land, the helicopter "began to shake violently again until touching down and reducing collective pitch." A postflight inspection revealed substantial damage to the main rotor system, the tail boom, and the empennage.

The pilot reported there were no pre-impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.
Probable Cause: The ground recovery team member's failure to secure a rescue rope during the helicopter loading process in steep terrain, resulting in the rope fouling the helicopter's main rotor system.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: GAA15CA258
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?omni=Home-N-Number&nNumberTxt=N253HP

Location

Revision history:

Date/timeContributorUpdates
12-Sep-2015 13:16 Raffles727 Added
12-Sep-2015 15:57 Geno Updated [Cn, Location]
05-Oct-2015 15:49 Aerossurance Updated [Time, Aircraft type, Operator, Source, Narrative]
20-Jan-2016 16:49 Aerossurance Updated [Total occupants, Source, Narrative]
06-May-2016 08:07 Medevac Updated [Source, Embed code]
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
17-Jan-2017 20:21 Aerossurance Updated [Time, Location, Source]
01-Dec-2017 15:26 ASN Update Bot Updated [Time, Operator, Other fatalities, Nature, Departure airport, Destination airport, Source, Embed code, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org