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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

August 12, 1992 · Hughes 369D · N58425

Maxwell, CA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
August 12, 1992
Injury Outcomes
1 injury (1 fatality)
Location
Maxwell, CA
Aircraft
Hughes 369D
Tail Number
N58425
Operator
Colorado Helicopters
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
LAX92GA347

The helicopter collided with a powerline transmission tower while towing cable attached by means of a cargo hook. The helicopter was moving laterally toward the tower when it hit the tower with the M/R blades. The blade tip weight separated and penetrated the tail boom in two places, damaging the T/R drive shaft. The helicopter spun twice to the right in a slow descent tethered by the steel cable. During the second turn, parts of the T/R separated. Witnesses did not observe the cable being jettisoned. The pilot was newly hired, and did not have any prior Class C external load experience. He had received training by the company chief pilot, who then left the company 3 days after the pilot was hired, leaving the pilot to work alone. The FAA office holding the operator's certificate had been notified of the chief pilot's departure. The office did not, nor was it required to, notify the local FAA district office of the operator's external load operations within that office's geographic responsibility.

NTSB Probable Cause

THE FAILURE OF THE PILOT TO MAINTAIN AN ADEQUATE VISUAL OUTLOOK, AND FAILURE OF THE COMPANY TO PROVIDE ADEQUATE TRAINING. CONTRIBUTING TO THE ACCIDENT WAS: INADEQUATE COMPANY SUPERVISION DURING THE OPERATION, AND INADEQUATE SURVEILLANCE BY THE FAA WHICH FAILED TO DETECT THE INADEQUATE TRAINING OF THE PILOT.

Full Narrative

THE HELICOPTER COLLIDED WITH A POWERLINE TRANSMISSION TOWER WHILE TOWING CABLE ATTACHED BY MEANS OF A CARGO HOOK. THE HELICOPTER WAS MOVING LATERALLY TOWARD THE TOWER WHEN IT HIT THE TOWER WITH THE M/R BLADES. THE BLADE TIP WEIGHT SEPARATED AND PENETRATED THE TAIL BOOM IN TWO PLACES, DAMAGING THE T/R DRIVE SHAFT. THE HELICOPTER SPUN TWICE TO THE RIGHT IN A SLOW DESCENT TETHERED BY THE STEEL CABLE. DURING THE SECOND TURN, PARTS OF THE T/R SEPARATED. WITNESSES DID NOT OBSERVE THE CABLE BEING JETTISONED. THE PILOT WAS NEWLY HIRED, AND DID NOT HAVE ANY PRIOR CLASS C EXTERNAL LOAD EXPERIENCE. HE HAD RECEIVED TRAINING BY THE COMPANY CHIEF PILOT, WHO THEN LEFT THE COMPANY 3 DAYS AFTER THE PILOT WAS HIRED, LEAVING THE PILOT TO WORK ALONE. THE FAA OFFICE HOLDING THE OPERATOR'S CERTIFICATE HAD BEEN NOTIFIED OF THE CHIEF PILOT'S DEPARTURE. THE OFFICE DID NOT, NOR WAS IT REQUIRED TO, NOTIFY THE LOCAL FAA DISTRICT OFFICE OF THE OPERATOR'S EXTERNAL LOAD OPERATIONS WITHIN THAT OFFICE'S GEOGRAPHIC RESPONSIBILITY.

Flight

Event TypeAccident
Event Time16:10 PDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftHughes 369D
Tail NumberN58425
Aircraft CategoryHeli
DamageDestroyed
OperatorColorado Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats2

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 30 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility25 sm
CeilingNone
Temperature / Dew Point10 C / 0 C
Altimeter0
Weather SourceWIT

Appendix: Source Data