# NTSB LAX92LA134: Bell 206BIII, N59613, Glenbrook, NV, March 2, 1992

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: March 2, 1992, 10:29 local (18:29 UTC)
- Place: Glenbrook, NV
- Coordinates: 39.050334, -119.920829 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=39.0503&lon=-119.9208&mi=10
- Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 5 uninjured
- Status: Completed, report June 11, 1993
- Report: Approved by Office Director
- NTSB case key (mKey): 27571
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=LAX92LA134
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/27571/pdf
- Page: https://openairdocs.org/ntsb/LAX92LA134

## Probable cause

FAILURE OF THE PILOT-IN-COMMAND TO FOLLOW THE HELICOPTER'S PERFORMANCE DATA WHILE TRANSLATING OUT OF TRANSLATIONAL LIFT TO AND OUT OF GROUND EFFECT.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Loss of control - in flight, hover
  - performance data - not followed, pilot in command (cause)
- In flight collision with terrain/water, descent - uncontrolled
  - terrain condition - water

## Analysis

THE HELICOPTER BEGAN AN UNCOMMANDED RIGHT TURN WHILE FLYING OUT OF GROUND EFFECT AT ABOUT 20 KNOTS FORWARD AIRSPEED WITH A DENSITY ALTITUDE OF 6,875 FT.  THE PILOT REPORTED THE WINDS TO BE FROM THE HELICOPTER'S THE RIGHT FRONT WHEN IT STARTED THE UNCOMMANDED RIGHT TURN.  THE PILOT ATTEMPTED TO ARREST THE RIGHT TURN BUT WITHOUT SUCCESS.  THE HELICOPTER DESCENDED UNCONTROLLED UNTIL IT CRASHED INTO THE LAKE.  THERE WERE NO REPORTS OF ANY PREEXISTING MECHANICAL FAILURES OR MALFUNCTIONS THAT MAY HAVE CONTRIBUTED TO THE LOSS OF CONTROL.  THE PILOTS OPERATING HANDBOOK (POH) WARNS PILOTS TO EXERCISE CAUTION WHEN OPERATING AT LOW AIRSPEEDS AT HIGH ALTITUDES. THE POH INDICATES THAT TAILROTOR CONTROL MAY BE MARGINAL WHEN THE RELATIVE WIND IS IN THE CRITICAL WIND AZIMUTH AREA WHICH BEGINS AT THE RIGHT FRONT OF THE HELICOPTER.  THE PILOT FAILED TO EVALUATE THE HELICOPTER'S PERFORMANCE DATA BEFORE DEPARTING.

## Aircraft

- Registration: [N59613](https://openairdocs.org/deregistered/N59613-1994-01-28), registration cancelled 1994-01-28, S/N 1502 (OpenAirDocs)
- Reported make and model: BELL 206BIII
- Registry model: [Bell 206B](https://openairdocs.org/model/bell-206b) (registry code 1181511) (OpenAirDocs)
- Category: Helicopter
- Serial number: 1502
- Airframe hours: 7356
- Engines: ALLISON 250C20B 420 horsepower turbo shaft
- Damage: Substantial damage
- Flight: Aerial observation, Part 91
- Operator: Smith Helicopter, Inc.
- Registered owner: Smith Helicopter, Inc.
- Airworthiness certificate: Standard, Utility; Standard, Normal
- Last inspection: 100 hour, December 20, 1991, 85 hours before
- Departed: TAHOE CITY, CA
- Flight plan: Company VFR

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 53; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, valid medical--w/ waivers/lim; seat: right; flight hours: 3,999 total, 950 in this make and model, 3,791 as pilot in command, 221 in the last 90 days, 68 in the last 30 days, 1 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 310° at 8 knots
- Visibility: 15 statute miles
- Lowest ceiling: 18,000 ft overcast
- Temperature: 45 °F, dew point 25 °F
- Altimeter: 29.00 inHg
- Observed at: TVL, 10 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 (OpenAirDocs).

- [Accident 19920302004859A](https://openairdocs.org/incident/19920302004859A), Mar 2, 1992: Bell 206B3, Glenbrook, NV, Substantial damage. Lost tail rotor effectiveness on slow speed climbout. Uncontrolled spin into lake. Density altitude and wind factor

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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