N67064

Substantial
None

Hiller UH-12E S/N: 1355

Accident Details

Date
Sunday, January 24, 1999
NTSB Number
LAX99LA081
Location
LEMOORE, CA
Event ID
20001204X00083
Coordinates
36.290092, -119.820549
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The inadequate nature of the operator's maintenance, which failed to detect the primer and magneto discrepancies. An overly lean fuel mixture and/or magneto cross firing resulted in detonation, an ensuing connecting rod failure, and a total loss of engine power. Contributing factors were the helicopter's low altitude and the uneven, soft nature of the terrain.

Aircraft Information

Registration
N67064
Make
HILLER
Serial Number
1355
Engine Type
Reciprocating
Year Built
1962
Model / ICAO
UH-12E UH12
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
BREEN AVIATION INC
Address
PO BOX 676
X
Status
Deregistered
City
LENIOOK
State / Zip Code
CA 92345
Country
United States

Analysis

On January 24, 1999, about 0900 hours Pacific standard time, a Hiller UH-12E, N67064, operated by Breen Aviation, Inc., experienced a total loss of engine power while maneuvering during an aerial application flight about 7 miles north of Lemoore, California. The flight was being conducted under the provisions of 14 CFR Part 137. The pilot reported that he heard a noise emanating from the engine. Thereafter the engine seized, and the pilot stated he made a forced landing from his altitude of 15 feet above ground level. Following touchdown in the soft, uneven alfalfa field, the helicopter rolled over and was substantially damaged. The commercial pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from a nearby field about 0800.

The helicopter was recovered and examined by Federal Aviation Administration (FAA) airworthiness inspectors from the Fresno, California, Flight Standards District Office. Maintenance records indicated that the helicopter's engine had been operated about 482 hours since being overhauled. The FAA inspectors reported that the engine's number two connecting rod was found broken at its crankshaft end, and the break did not appear related to the rod bolts. Additionally, an inspection of the associated cylinder and piston showed signatures consistent with detonation. Similar signatures indicative of exposure to elevated temperatures were observed with the other five piston heads. Maintenance discrepancies were also noted with the primer line and magnetos. A small hole was found chaffed in the primer line. The magneto distributor blocks for both magnetos showed evidence of carbon and burning of the rotor fingers. The magnetos were subsequently bench tested and were found functional.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX99LA081