Loss of control Accident Enstrom F-28F Falcon N63VP,
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ASN Wikibase Occurrence # 145765
 
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Date:Sunday 20 May 2012
Time:09:00
Type:Silhouette image of generic EN28 model; specific model in this crash may look slightly different    
Enstrom F-28F Falcon
Owner/operator:Private
Registration: N63VP
MSN: 812
Total airframe hrs:1593 hours
Engine model:Lycoming HIO-360
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:near Joslin Field/Magic Valley (KTWF), Twin Falls, ID -   United States of America
Phase: Approach
Nature:Private
Departure airport:Elko, NV (EKO)
Destination airport:Twin Falls, ID (TWF)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that on a previous flight, he encountered an uncommanded roll, so he checked the three main rotor Lamiflex bearings prior to departure. He said one bearing showed no indication of a pending failure, the second showed some indication of approaching failure, and the third showed a minor indication that it was beginning to fail. From past experience, the pilot said that he believed that he still had several hours before the bearings would fail and that he could safely proceed with the flight. A few miles from the intended destination, a vibration started and became progressively worse to the point where the pilot was losing control of the helicopter. The pilot subsequently made what he described as a “controlled crash landing,” which resulted in substantial damage to the helicopter. A postaccident examination revealed that the No. 2 main rotor Lamiflex bearing failed, which resulted in the loss of control. A review of maintenance logbooks found that the helicopter was not in compliance with either its annual inspection requirement or with FAA Airworthiness Directive 94-17-15, which required repetitive inspections of the helicopter’s main rotor Lamiflex bearings.
Probable Cause: The pilot's inability to maintain helicopter control during cruise flight due to the failure of the No. 2 main rotor Lamiflex bearing. Contributing to the accident was the pilot's decision to operate the helicopter with a known deficiency and the helicopter’s noncompliance with the mandatory scheduled inspection of the main rotor bearings.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR12LA219
Status: Investigation completed
Duration: 11 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
21-May-2012 06:55 gerard57 Added
21-May-2012 07:28 harro Updated [Aircraft type]
21-May-2012 08:23 RobertMB Updated [Time, Aircraft type, Registration, Cn, Location, Phase, Destination airport, Narrative]
21-May-2012 08:25 RobertMB Updated [Narrative]
22-May-2012 13:29 Geno Updated [Location, Departure airport, Source, Narrative]
30-Apr-2013 14:53 TB Updated [Operator, Location, Destination airport, Source, Narrative]
30-Apr-2013 15:01 TB Updated [Location]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
27-Nov-2017 20:41 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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