Accident Aérospatiale AS 350F2 Ecureuil N355DU,
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ASN Wikibase Occurrence # 29993
 
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Date:Monday 16 October 2000
Time:23:55
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Aérospatiale AS 350F2 Ecureuil
Owner/operator:Corporate Jets, Inc.
Registration: N355DU
MSN: 5489
Year of manufacture:1992
Total airframe hrs:4192 hours
Engine model:Rolls-Royce 250-C20F
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:East of 2613 Churchill Drive, Burlington, NC -   United States of America
Phase: Initial climb
Nature:Ferry/positioning
Departure airport:4NC3
Destination airport:Durham, NC (NC92)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
About 5 minutes before landing at a hospital, the main rotor gearbox (MGB) oil pressure warning light illuminated. The pilot continued to the hospital, landed, and performed an immediate engine shutdown. A mechanic disconnected the wiring to the MGB oil pressure switch and the light went out. The mechanic stated he believed the oil pressure switch had failed and he asked the pilot to run the helicopter, hover the helicopter, and if everything was normal, to fly it back to the base hospital. The pilot did the run and hover, and then departed the hospital. The helicopter crashed about 1 minute later. Witnesses stated they heard the helicopter approach the crash site at a low altitude and making a slow thumping noise. Examination of the MGB showed the oil pump idler gear had seized in the oil pump due to undetermined reasons and the oil pump drive shaft had failed due to overstress. The teeth on the engine input gears, intermediate gears, and MGB drive gear in the MGB combining gearbox had failed due to high-temperature overstress, which was the result of oil starvation. The helicopter was not equipped with a MGB oil pressure indicator. The maintenance procedure for trouble shooting an illuminated MGB oil pressure warning light is to first check the electrical circuit, and if this does not correct the problem, to change the oil pressure switch. The mechanic stated he did not have the maintenance manuals with him while working on the helicopter. The MGB had been installed in the helicopter after overhaul, 3 days and 4 flight hours before the accident.
Probable Cause: The mechanics failure to comply with manufacturers instructions for correction of a illuminated main rotor gearbox oil pressure warning light resulting in the helicopter being dispatched on a ferry flight with a failed main rotor gearbox oil pump, failure of the main rotor gearbox combining gearbox gears due to oil starvation, loss of main rotor RPM, and the helicopter colliding with trees and the ground during an uncontrolled descent.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20001212X22206&key=1
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?omni=Home-N-Number&nNumberTxt=355DU

Revision history:

Date/timeContributorUpdates
27-Sep-2008 01:00 ASN archive Added
07-Mar-2009 11:30 harro Updated
09-Jul-2014 23:04 Dr. John Smith Updated [Time, Location, Source, Narrative]
30-Nov-2016 21:05 Aerossurance Updated [Aircraft type, Location, Source, Narrative]
21-Dec-2016 19:16 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
21-Dec-2016 19:20 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
12-Dec-2017 19:14 ASN Update Bot Updated [Operator, Departure airport, Destination airport, Source, Narrative]

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