N5905X

Destroyed
Fatal

Brantly Helicopter B-2 S/N: 41

Accident Details

Date
Saturday, October 22, 1994
NTSB Number
FTW95FA020
Location
ARTESIA, NM
Event ID
20001206X02428
Coordinates
32.839656, -104.429084
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

THE PILOT'S IMPAIRMENT OF JUDGMENT AND PERFORMANCE DUE TO DRUGS, AND HIS FAILURE TO MAINTAIN CLEARANCE FROM A POWERLINE.

Aircraft Information

Registration
N5905X
Make
BRANTLY HELICOPTER
Serial Number
41
Engine Type
Reciprocating
Model / ICAO
B-2 BRB2
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
CANION JAMES L
Address
PO BOX 292
Status
Deregistered
City
CARLSBAD
State / Zip Code
NM 88221
Country
United States

Analysis

HISTORY OF FLIGHT

On October 22, 1994, approximately 1030 mountain daylight time, N5905X, a Brantly B-2, was destroyed when it collided with a power line and impacted terrain while maneuvering at Artesia, New Mexico. The commercial pilot was fatally injured. Visual meteorological conditions prevailed.

A witness saw the helicopter approach a parking lot behind his residence and thought it was going to land. The helicopter suddenly pulled up and collided with a 69,000 volt power line. The witness saw parts separate from the helicopter as it spun to the ground. There was post-impact fire.

PERSONNEL INFORMATION

The pilot's logbook contained entries from July 18, 1980, to November 30, 1991. In the memorandum section of the logbook was an entry indicating the pilot had received a biennial flight review on April 4, 1993, in a Cessna 150 (0.6 hours) and in a Brantly B2B (2.0 hours). The pilot held an advanced ground instructor certificate.

WRECKAGE AND IMPACT INFORMATION

The wreckage, confined to a vacant lot, was scattered for 375 feet and aligned on a magnetic heading of 180 degrees. Across the street was a spliced power line. To the south was a splinted pole. Paint and antiskid material was scuffed off the top of the left skid in a "chatter" fashion. The leading edge of two main rotor blades, outboard of the lead-lag hinge, bore the same type of damage. Fire damage was confined to the cockpit and engine areas.

MEDICAL AND PATHOLOGICAL INFORMATION

Autopsy and toxicological protocols (4681-1094-5E) were performed by the Office of the Medical Investigator in Albuquerque, New Mexico. A toxicological screen was also performed by FAA's Civil Aeromedical Institute (CAMI). According to the Medical Investigator's report, cannabinoids (marijuana) was detected in the urine, and 5.9% saturation of carbon monoxide was detected femoral blood. According to CAMI's report, 0.003 ug/ml tetrahydrocannabinol (marijuana) was detected in blood; 0.012 ug/ml tetrahydrocannabinol carboxylic acid (marijuana metabolite) was detected in blood, and 0.169 ug/ml tetrahydrocannabinol was detected in urine. According to a CAMI spokesman, these levels indicate the pilot was exposed to the drug within the previous 2 hours. Cocaine and benzoylecgonine (cocaine metabolite) was also detected in the blood. The CAMI spokesperson also reported that the pilot's peripheral vision would have been affected by the combination of these drugs.

ADDITIONAL INFORMATION

The wreckage was released to the owner's representative on October 23, 1994.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95FA020