LAX92FA054

NTSB accident investigation · Aerospatiale SA 316B · Bridgeport, CA · November 28, 1991

Accident · FatalField investigationFinal report
Date
November 27, 1991, 23:21 local (Nov 28, 1991, 07:21 UTC)
Place
Bridgeport, CA
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N146RMAerospatiale SA 316B
Weather
Visual (VMC) · Night/dark
Status
Completed · report January 27, 1993
Report
Approved by Office Director
FAA report
19911127053719A
Case key
27392

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

Failure of the helicopter's tail rotor drive shaft and drive shaft bearing due to undetermined reason(s).

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.

Airframe/component/system failure/malfunctionCruise
Rotor drive system,tail rotor drive shaft bearing - failure,totalCause
Rotor drive system,tail rotor drive shaft - failure,totalCause
Reason for occurrence undeterminedCause
Loss of control - in flightCruise
Light condition - dark night
Aircraft control - not possiblePilot in command
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - mountainous/hilly

Analysis

The aeromedical evacuation (ems-medevac) flt was made at ngt ovr mtn trrn. The plt interrupted his normal psn rprt & broadcast 'mayday' 3 times, giving his psn to a company dispatcher. He did not state the nature of the emergency. No further comm was recorded. Witnesses in a southbound auto saw the helicopter flying toward them from the south. They stated the helicopter's fuselage started rotating counter-clockwise. It then veered to the west, went out of sight, and crashed. All maj components, except about 33 inches of the tail rotor drive shaft & its #5 brg, were located. The tail boom was found in 3 sections. Rotational & longitudinal scoring damage was noted on the tail boom in the vcnty of the #3 & #5 brg supports. A lab rprt stated that the rotational dmg occurred before the gross deformation of the tail boom & subsequent in-flt breakup of the helicopter.

Aircraft

Registration
N146RM
Reported as
Aerospatiale SA 316B
Category
Helicopter
Serial number
1614
Airframe hours
7,525
Engine
Turbomeca ARTOUSTE IIIB, 858 horsepower, turbo shaft
Damage
Destroyed
Flight
Part 135
Operator
Rocky Mountain Helicopters
Registered owner
Rocky Mountain Helicopters
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · October 25, 1991 · 53 hours before
Departed
Q18 · Bridgeport, CA
Destination
NONE · Reno, NV
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
44
Certificate
Airline transport
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
11,095 total · 2,163 in this make and model · 11,095 as pilot in command · 76 in the last 90 days · 28 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Visibility
3 statute miles
Temperature
12 °F

FAA reports on this event · 1

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