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Aviation safety reports, made easier to study

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February 2, 2008 · Kidd Chris Harmon ROC · N96KR

Maricopa, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
February 2, 2008
Injury Outcomes
1 injury (1 fatality)
Location
Maricopa, CA
Aircraft
Kidd Chris Harmon ROC
Tail Number
N96KR
Operator
Kidd Chris
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
SEA08LA070

The pilot departed a location where visual meteorological conditions existed, and was attempting to fly to another location that was also reporting visual meteorological conditions. During the flight, the pilot entered an area of hilly terrain that was covered by a low overcast ceiling of variable height. While maneuvering through that area in winds that were reportedly gusting to 10 miles per hour, the airplane impacted the terrain. No evidence was found of any anomaly or malfunction of the airframe, flight controls, or engine.

NTSB Probable Cause

The pilot's failure to maintain an adequate terrain clearance altitude while maneuvering in mountainous, hilly terrain. Contributing to the accident were hilly terrain, a low ceiling and gusty winds.

Full Narrative

On February 2, 2008, about 1000 Pacific standard time, an experimental Kidd Harmon Rocket, N96KR, impacted the hilly terrain about 10 miles south of Maricopa, California. The private pilot, who was the sole occupant of the airplane, was killed, and the airplane, which was owned and operated by the pilot, was destroyed. The pilot of the 14 Code of Federal Regulations (CFR) part 91 personal pleasure flight departed a private airstrip near Taft, California, around 0930. According to a family member, he was en route to the area around New Cuyama, California. No flight plan had been filed. There was no report of an ELT activation. At the time the pilot departed Taft, there were visual meteorological conditions (VMC), with 10 miles visibly, in both Taft and New Cuyama. But witnesses who lived in the area reported that there were low ceilings of variable heights and winds gusting to about 10 miles per hour in the hills between the two locations. Reportedly, although the visibility below the clouds was good, the ceiling was touching the top of the hills in many places throughout the area. It is believed that the pilot attempted to follow State Highway 33 through the narrow valley that runs northeast to southwest through the aforementioned hills. While the pilot was maneuvering in that area, the airplane impacted the terrain while traveling in a northwesterly direction. According to the FAA Inspector who responded to the scene, the airplane hit "very hard" in a nose-down attitude, and traveled about 150 feet before coming to rest. The impact created a three-foot-deep crater, and tore the engine from the airframe. When the pilot did not show up at his destination on the day of his departure, his family reported him missing, and a search was initiated. The wreckage was eventually spotted from the air four days after the accident. The airplane was relocated to the facilities of Aircraft Recovery Services, where it underwent an FAA directed teardown inspection. That inspection did not reveal any evidence of a pre-impact anomaly or malfunction of the airframe, flight controls, or engine components. The FAA's Forensic Toxicology Research Team performed a toxicological examination on specimens taken from the pilot. That examination was negative for screened drugs and consumed ethanol. Due to the elapsed time between the accident and the discovery of the wreckage, the standard tests for carbon monoxide and cyanide were not performed. The Kern County Coroner performed an autopsy on the pilot, and the cause of death was determined to be from blunt force injuries, with the manner of death being listed as accidental.

Flight

Event TypeAccident
Event Time10:00 PST
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftKidd Chris Harmon ROC
Tail NumberN96KR
Aircraft CategoryAir
DamageDestroyed
OperatorKidd Chris
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540 · Reciprocating · 300
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 45 · Third Class · Fatal

Conditions

ConditionsVMC
LightDaylight
WindGusting 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point50 / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data