LAX85FA286

NTSB accident investigation · Bell 214B-1 · Squaw Valley, CA · June 20, 1985

Accident · FatalField investigationFinal report
Date
June 19, 1985, 17:15 local (Jun 20, 1985, 00:15 UTC)
Place
Squaw Valley, CA
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N214RMBell 214B-1
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850619074929A
Case key
24516

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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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.

Loss of engine power(total) - mech failure/malfHover
Turbine assembly,turbine wheel - disintegratedFactor
Turboshaft engine,gas generator turbine - failure,totalFactor
Maintenance,replacement - not identifiedManufacturerCause
Material inadequateManufacturerCause
Material defectManufacturerCause
In flight collision with terrain/waterDescent - emergency
Terrain condition - downhillFactor
Autorotation - attemptedPilot in commandFactor
Terrain condition - rough/unevenFactor
Altitude - inadequatePilot in commandFactor
Proper glidepath - not possiblePilot in command
Flare - not possiblePilot in commandFactor

Analysis

The helicopter was engaged in lowering a large pole to the ground when the eng failed catastrophically due to a total first turbine rotor disc failure. The plt turned the acft down the mountain but was unable to gain enough speed to autorotate. The acft impacted at an angle and burned. No parts of the first turbine rotor disc were recovered, therefore, a failure mode could not be determined. The disc had accumulated 2776 cycles at the time of the accident. Lycoming service bulletin no. 5508-0002 reports the service life limit for the disc is 2700 cycles. An eng teardown revealed nothing else wrong with the eng that could have contributed to its failure other than the first turbine rotor disc disintegration.

Aircraft

Registration
N214RM
Reported as
Bell 214B-1
Category
Helicopter
Serial number
28001
Airframe hours
8,455
Engine
Lycoming T5508D, 2,050 horsepower, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Business · Part 133
Registered owner
Rocky Mountain Helicoperts Inc
Airworthiness certificate
Standard, Utility
Last inspection
Continuous airworthiness · June 17, 1985 · 6 hours before
Departed
RLA · Squaw Valley, CA

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
34
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Right
Toxicology
Performed
Flight hours
12,247 total · 3,047 in this make and model · 250 in the last 90 days · 80 in the last 30 days · 9 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
310° at 7 knots
Visibility
40 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 52 °F
Altimeter
30.00 inHg
Observed at
TVL, 19 nm away

FAA reports on this event · 1

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