N124HA

Substantial
None

Hiller UH-12E S/N: HA3024

Accident Details

Date
Saturday, July 20, 1996
NTSB Number
LAX96LA279
Location
HEALDSBURG, CA
Event ID
20001208X06291
Coordinates
38.629318, -122.890426
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the pilot to confirm a loss of power before entering autorotation after reading an erroneous instrument indication on the helicopter's dual tachometer. Factors in the accident were the erratic instrument, and maintenance personnel who failed to properly repair the system after the discrepancy was previously reported.

Aircraft Information

Registration
N124HA
Make
HILLER
Serial Number
HA3024
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
UH-12E UH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
MARQUIS AVIATION INC
Address
845 E REDWOOD CIR
Status
Deregistered
City
HANFORD
State / Zip Code
CA 93230-2382
Country
United States

Analysis

On July 19, 1996, at 1830 hours Pacific daylight time, a Hiller UH-12E, N124HA, collided with trees after the pilot entered autorotation after reacting to an erroneous rotor/engine tachometer reading near Healdsburg, California. The helicopter was substantially damaged. The certificated private pilot and passenger were not injured. The helicopter was being operated as a personal flight by the pilot/owner when the accident occurred. The flight originated from a private ranch at 1825, and was destined for the Healdsburg Municipal Airport. Visual meteorological conditions prevailed at the time.

The pilot said he was flying at 1,400 feet msl and 70 knots when the needles on the rotor/engine tachometer instrument split. The engine decelerated to idle. The pilot entered an autorotation over unsuitable steep terrain and struck trees during the emergency descent.

According to the Federal Aviation Administration (FAA), the helicopter had a previous rotor-tach generator failure. The failure was attributed to a loose connection and was allegedly repaired by the previous owner.

The rotor-tach generator electrical connection was examined by an airframe and powerplant mechanic. The connection produced intermittent and inaccurate instrument readings when the wire bundle was moved or flexed. The mechanic attributed the erroneous instrument reading to the poor condition of potting material within the electrical connector.

There was no evidence of mechanical failure or malfunction found with the helicopter's powerplant after the accident.

The pilot indicated on his accident report his total aeronautical experience consisted of 485 hours, of which 157 were accrued in helicopters.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX96LA279