LAX06LA288

NTSB accident investigation · Hughes 369D · Somis, CA · September 6, 2006

Accident · FatalLimited investigationFinal report
Date
September 6, 2006, 13:55 local (20:55 UTC)
Place
Somis, CA
Injuries
2 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N812CEHughes 369D
Weather
Visual (VMC) · Day
Status
Completed · report March 31, 2008
Report
Approved by Office Director
Parties
Southern Calif. Edison Company, Federal Aviation Administration
FAA report
20060906020269A
Case key
64479

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

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Probable cause

The pilot's inadequate visual lookout, which resulted in a collision with wires.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

In flight collision with objectCruise
Object - wire,transmission
Visual lookout - inadequatePilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

The utility company pilot and a power line inspector departed for an aerial observation patrol flight of company power lines. A ground-based witness, who was located north of the accident site, reported observing the helicopter fly into the power lines. The witness did not indicate that the helicopter took any evasive action prior to the collision. The helicopter came to rest about 200 feet north of the two severed power lines. The impacted power lines had been suspended from towers that were about 1,763 feet apart and had an east-to-west orientation. The helicopter's northerly impact course appeared nearly perpendicular to the orientation of the power lines, which were about 150 feet above ground level at the point of impact.

Factual narrative

On September 6, 2006, at 1355 Pacific daylight time, a Hughes 369D, N812CE, collided with power lines while cruising about 3 miles north-northwest of Somis, California. The helicopter was owned and operated by the Southern California Edison Company (SCEC), Ontario, California, and it was substantially damaged upon impacting the ground. The commercial pilot and the power line inspector, both SCEC employees, were killed. The aerial observation flight was performed under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and a company flight plan was filed. The flight originated from Camarillo, California, at 1321.

A ground-based witness, who was located north of the accident site, reported observing the helicopter fly into the power lines. The witness did not indicate that the helicopter took any evasive action prior to the collision.

According to the Federal Aviation Administration (FAA) coordinator who responded to the accident site, the helicopter came to rest about 200 feet north of the severed power lines. SCEC representatives, who were participating in the Safety Board's investigation, reported that the impacted Edison Company power lines had been suspended from towers that were about 1,763 feet apart and had an east-to-west orientation. The helicopter's impact course appeared nearly perpendicular to the orientation of the power lines. SCEC personnel also reported that the impacted lines were located about 150 feet above ground level.

SCEC personnel also reported that the accident occurred during a routine patrol flight. An examination of the Edison Company aluminum conductor steel reinforced wires was performed. Three of the wires exhibited impact damage, and two wires were severed.

SCEC personnel submitted a report of the accident to the Safety Board investigator. In pertinent part, they stated the following:

"SCE is unaware of any exigent circumstances which may have affected [the pilot's] physical, mental or psychological health on the date of the accident."

An autopsy was performed by the County of Ventura Medical Examiner-Coroner, with specimens retained for toxicological analysis. No evidence of alcohol or screened drug substances was found during the toxicological tests.

Aircraft

Registration
N812CE
Reported as
Hughes 369D
Category
Helicopter
Serial number
720D
Airframe hours
8,065
Engine
Allison 250-C20, 450 horsepower, turbo shaft
Damage
Substantial damage
Flight
Aerial observation · Part 91
Operator
Southern California Edison Company
Registered owner
So. California Edison Company
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 1, 2006 · 96 hours before
Departed
CMA · Camarillo, CA
Flight plan
Company VFR

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
41
Injuries
Fatal
Certificates
Commercial, Flight instructor
Instrument ratings
Helicopter
Medical
Class 1, With waivers/limitations
Last flight review
August 1, 2006
Seat
Left
Flight hours
11,900 total · 24 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 61 °F
Altimeter
29.92 inHg
Observed at
CMA, 7 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.