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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

September 6, 2006 · Hughes 369D · N812CE

Somis, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 6, 2006
Injury Outcomes
2 injuries (2 fatalities)
Location
Somis, CA
Aircraft
Hughes 369D
Tail Number
N812CE
Operator
Southern California Edison
Injuries
Fatal
Aircraft Damage
Substantial
NTSB Number
LAX06LA288

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.

NTSB Probable Cause

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

Full 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.

Flight

Event TypeAccident
Event Time13:55 PDT
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 369D
Tail NumberN812CE
Aircraft CategoryHeli
DamageSubstantial
OperatorSouthern California Edison
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20 · Turboshaft · 450
Seats4

People & Injuries

Injury Summary2 injuries (2 fatalities)
Fatal2
Serious0
Minor0
Uninjured0
Total2
Crew 1Age 41 · First Class · Fatal

Conditions

ConditionsVMC
LightDaylight
Wind250° @ 9 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter29.92 inHg
Observation Time20:55
Weather SourceWFAC

Appendix: Source Data