Accident Sikorsky S-58DT N581BG,
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ASN Wikibase Occurrence # 35146
 
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Date:Monday 21 February 1994
Time:11:15 LT
Type:Silhouette image of generic S58T model; specific model in this crash may look slightly different    
Sikorsky S-58DT
Owner/operator:Air One, Inc
Registration: N581BG
MSN: 58-1487
Total airframe hrs:12735 hours
Engine model:P&W PT6T-3
Fatalities:Fatalities: 3 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:near Walnut Creek, CA -   United States of America
Phase: En route
Nature:Unknown
Departure airport:Concord, CA
Destination airport:San Jose, CA (KSJC)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE HELICOPTER WAS OBSERVED FLYING LOW IN A GRADUAL DESCENT OVER A RESIDENTIAL AREA HEADING TOWARD AN OPEN FIELD. WITNESSES SAID THE HELICOPTER NOISE LEVEL WAS QUIET, BUT NOT SOUNDLESS. AT 200 FEET ABOVE THE GROUND, THE HELICOPTER ROLLED LEFT TO AN INVERTED FLIGHT ATTITUDE AND THEN DESCENDED IN A NOSE-DOWN ATTITUDE. WRECKAGE EXAMINATION DID NOT FIND ANY PREIMPACT MECHANICAL FAILURES WITH THE HELICOPTER'S FLIGHT CONTROL OR DRIVE SYSTEMS. SIGNATURES ON THE INTERNAL ROTATING COMPONENTS OF BOTH ENGINES, THE DRIVE SYSTEM, MAIN ROTOR BLADES, AND TAIL ROTOR BLADES WERE INDICATIVE OF LOW RPM. EXAMINATION OF THE ENGINE FUEL SYSTEM REVEALED EVIDENCE OF FOREIGN PARTICLES IN THE FLOW DIVIDER AND FUEL NOZZLES. POSTACCIDENT FUEL SAMPLES FROM THE REFUELING TRUCK WERE TESTED IN A LABORATORY. ACCORDING TO THE LAB REPORT, THE FUEL HAD A TENDENCY TO ABSORB AND RETAIN WATER, AND A PRESENCE OF MICROBIAL CONTAMINATION WAS NOTED. IN ADDITION TO THE LAB TESTS, FUEL SAMPLES FROM THE OPERATORS REFUELING TRUCKS WERE INDEPENDENTLY TESTED WITH WATER DETECTION PASTE AND TESTED POSITIVE FOR WATER.

Probable Cause: Inadequate fuel quality control procedures by the helicopter operator resulting in fuel contamination and a loss of engine power. The pilot's decision to extend the autorotative glide to avoid striking residential homes, which resulted in low main rotor rpm and a subsequent in-flight loss of control, is also causal in this accident. A factor in the accident was the unsuitable nature of the residential area over which the loss of power occurred for a successful forced landing.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX94FA130
Status: Investigation completed
Duration: 1 year and 2 months
Download report: Final report

Sources:

NTSB LAX94FA130

Location

Images:


San Jose Intl Airport, San Jose, CA KSJC/SJC June 1990 apprx photo date. Tom Vance

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
15-Jul-2010 02:56 TB Updated [Time, Aircraft type, Operator, Other fatalities, Location, Nature]
30-Jun-2018 13:33 Anon. Updated [Photo, ]
10-Apr-2024 08:48 ASN Update Bot Updated [Time, Operator, Other fatalities, Nature, Destination airport, Source, Narrative, Category, Accident report]

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