Accident Bell 206L-1 N500CN,
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ASN Wikibase Occurrence # 380187
 
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Date:Sunday 22 January 1984
Time:12:30 LT
Type:Silhouette image of generic B06 model; specific model in this crash may look slightly different    
Bell 206L-1
Owner/operator:Price Air Med
Registration: N500CN
MSN: 45188
Total airframe hrs:1291 hours
Engine model:Allison 250-C28B
Fatalities:Fatalities: 0 / Occupants: 7
Aircraft damage: Substantial
Category:Accident
Location:Huntington, UT -   United States of America
Phase: Taxi
Nature:Executive
Departure airport:Huntington, UT
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
WHILE IN A STABILIZED, OUT-OF-GROUND-EFFECT HOVER, AT ABOUT 300 FEET AGL, THE HELICOPTER STARTED AN UNCONTROLLABLE RIGHT TURN. THE PLT STATED THAT USING FULL LEFT PEDDLE HAD NO EFFECT ON STOPPING THE SPIN. AT THE ONSET OF THE SPIN, THE OCCUPANTS OF THE ACFT FELT A HIGH FREQUENCY VIBRATION. THE PLT STATED THAT HE REDUCED THE ROTOR RPM BY ROLLING OFF THE THROTTLE & LOWERED THE COLLECTIVE. THE HELICOPTER DESCENDED INTO TREES IN A RIGHT SPIN. THE PLT STATED THAT HE DID NOT BELIEVE THAT THERE WAS ANYTHING MECHANICALLY WRONG WITH THE ACFT. THE COPLT STATED THAT HE FELT THAT THEY HAD EXPERIENCED A LOSS OF TAILROTOR AUTHORITY. INVESTIGATION REVEALED NO MECHANICAL PROBLEMS WITH THE HELICOPTER. REVIEW OF HEIGHT-VELOCITY CHART FOR THE BELL 206L-1 INDICATED THAT A SUCCESSUL AUTO-ROTATION FROM HOVER A 300 FEET AGL IS NOT PROBABLE. THE ELEVATION OF THE CRASH SITE WAS APRX 6800 FT MSL.

Probable Cause:

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN84FA073
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB DEN84FA073

Location

Revision history:

Date/timeContributorUpdates
01-Apr-2024 13:45 ASN Update Bot Added

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