N134SH

Substantial
None

HUGHES 500DS/N: 610969D

Accident Details

Date
Tuesday, August 6, 2013
NTSB Number
ANC13LA074
Location
Delta Junction, AK
Event ID
20130806X20950
Coordinates
64.046669, -145.695550
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power for undetermined reasons, which necessitated an emergency hovering autorotation, during which the helicopter impacted trees and terrain.

Aircraft Information

Registration
N134SH
Make
HUGHES
Serial Number
610969D
Engine Type
Turbo-shaft
Year Built
1981
Model / ICAO
500DH500
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
WELLS FARGO BANK NORTHWEST NA TRUSTEE
Address
MAC U1240-026
260 N CHARLES LINDBERGH DR
Status
Deregistered
City
SALT LAKE CITY
State / Zip Code
UT 84116-2812
Country
United States

Analysis

On August 5, 2013, about 1800 Alaska daylight time, a McDonnell Douglas/Hughes 500D helicopter, N134SH, was substantially damaged when it was involved in an accident near Delta Junction, Alaska. The pilot was not injured. The helicopter was being operated as a Title 14 Code of Federal Regulations Part 133 external load flight.

The pilot was transporting sections of water hose to a remote site via a 100-ft-long external load line attached to the helicopter’s belly-mounted cargo hook. The pilot reported that while the helicopter was hovering about 100 ft over the intended site and about 5 to 10 ft above trees while facing into a hill, the engine lost all power. He then initiated an emergency hovering autorotation and turned the helicopter left in an attempt to face it downhill. Subsequently, the helicopter settled into trees, during which the main rotor blades struck several of them, followed by it impacting terrain hard and then rolling onto its right side, which resulted in substantial damage to the main rotor drive system, tailboom, and fuselage.

During postaccident examination, about 60 lbs of fuel, 47 lbs of which were usable, were drained from the helicopter’s fuel cell. During an engine test-run, the engine produced fullrated power at various power settings. During a subsequent test-run, the electric fuel pump operated within its operating specifications. Examination of the fuel pump revealed that the motor commutator and brushes exhibited wear. Postaccident examination of the helicopter revealed no preaccident mechanical malfunctions or failures that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC13LA074