ASN Wikibase Occurrence # 289943
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Date: | Friday 28 June 2013 |
Time: | 11:20 LT |
Type: | Bell 47D1 |
Owner/operator: | Lake Ozark Helicopters Inc |
Registration: | N78900 |
MSN: | 480 |
Year of manufacture: | 1952 |
Total airframe hrs: | 7653 hours |
Engine model: | Franklin 6V4 |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Lake Ozark, Missouri -
United States of America
|
Phase: | En route |
Nature: | Unknown |
Departure airport: | Lake Ozark, MO |
Destination airport: | Lake Ozark, MO |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot stated that, during the preflight inspection, he observed no contamination in the fuel sumped from the helicopter. During the helicopter's second air tour flight of the day, it experienced a total loss of engine power during cruise flight. The pilot performed an autorotation to a field, which resulted in damage to the tailboom and main rotor blade.
The helicopter had been in a previous accident and was subsequently rebuilt; it was sold to the operator about 6 months before the accident. During the rebuild, parts were sand and bead blasted. The pilot stated that, about 2 months before the accident, fuel samples from the helicopter showed contamination. He described the contaminated fuel as "discolored…from sitting." The operator drained and replaced the fuel, ran the engine on the ground, and performed numerous sumps until the fuel was "clean" and up to the operator's standards. The helicopter was then flown for about 12 hours before the accident flight occurred. During postaccident examinations, a substance consistent with silicon-glass blasting was found within the carburetor bowl, carburetor screen, and fuel sump. No other anomalies were found that would have precluded normal operation of the helicopter. It is likely that the fuel was contaminated by the blasting substance at the time of the rebuild and that the substance was not found during subsequent preflight inspections, which resulted in a total loss of engine power during cruise flight.
Probable Cause: The improper rebuild and maintenance of the helicopter and inadequate subsequent inspections, which resulted in undetected fuel contamination and a subsequent total loss of engine power during cruise flight.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN13LA396 |
Status: | Investigation completed |
Duration: | 8 months |
Download report: | Final report |
|
Sources:
NTSB CEN13LA396
History of this aircraft
Other occurrences involving this aircraft Location
Revision history:
Date/time | Contributor | Updates |
06-Oct-2022 06:02 |
ASN Update Bot |
Added |
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