Accident Hughes 369A N336SP,
ASN logo
ASN Wikibase Occurrence # 296626
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Sunday 15 September 2002
Time:13:45 LT
Type:Silhouette image of generic H500 model; specific model in this crash may look slightly different    
Hughes 369A
Owner/operator:Killian Cable Contracting Co.
Registration: N336SP
MSN: 67-0068
Year of manufacture:1966
Total airframe hrs:4406 hours
Engine model:Allison T63-A-700
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Burtonsville, Maryland -   United States of America
Phase: Unknown
Nature:Private
Departure airport:Burtonsville, MD
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
About one minute after liftoff, on the helicopters first flight after an annual inspection, the pilot experienced a sudden shuttering of the fuselage, followed by a chip detector light and a loss of directional control. The helicopter began to turn to the left, and would not respond to anti-torque pedal input. As the helicopter neared the heliport, "everything in the cockpit lit up," and the pilot observed the rotor tachometer decrease below 96 percent. The engine then lost total power, and the pilot performed a forced landing to a reservoir. As the helicopter neared the water, the engine "ignited" again, and the helicopter began to rotate to the right. The pilot set the helicopter down on the water, where it rolled to the right, and sank. According to a manufacturer's report of the examination, no abnormalities were noted with the engine or its related components. Damage to the tailrotor drive system was consistent with sudden stoppage or gradual binding of the tailrotor gearbox. Review of the helicopters maintenance records revealed that the tailrotor swash-plate assembly, the tailrotor pitch bearings on both blades, and the tailrotor bellcrank bearing at the swash-plate, were replaced during an annual inspection completed 2 days prior to the accident; however, the component history of the tailrotor gearbox could not be determined.

Probable Cause: The failure of the tailrotor gearbox for undetermined reasons.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC02LA192
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB NYC02LA192

Revision history:

Date/timeContributorUpdates
14-Oct-2022 08:46 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org