ASN logo
ASN Wikibase Occurrence # 190536
Last updated: 30 November 2021
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:06-OCT-2016
Time:16:45
Type:Silhouette image of generic FH11 model; specific model in this crash may look slightly different
Fairchild Hiller FH-1100
Owner/operator:Private
Registration: N4035G
MSN: 502
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Written off (damaged beyond repair)
Category:Accident
Location:Lino Lakes, Anoka County, MN -   United States of America
Phase: En route
Nature:Private
Departure airport:Minneapolis, MN (ANE)
Destination airport:Minneapolis, MN (ANE)
Investigating agency: NTSB
Narrative:
The airline transport pilot was conducting a local flight with one passenger. The accident flight was the pilot's third flight in the helicopter on the day of the accident; before that day, he had not flown the helicopter in nearly one year. One witness stated that he saw the helicopter rocking back and forth before it "spun sideways" and "a bunch of parts" departed the airframe. Some reported hearing a "clunk" sound, and others reported hearing a "pop" sound. Another witness saw the main rotor blades "seize," then "snap off," followed by the tail rotor departing the helicopter. The witness stated that the helicopter then "dropped out of the sky." The fuselage impacted in an open field, and a postcrash fire erupted. The separated main rotor blades and hub were found in a pond about 500 ft south of the main wreckage.

Examination of the rotor mast showed deformation and fractures consistent with overstress under bending and torsion loads but no evidence of preexisting cracks or corrosion. The observed deformation of the mast was consistent with a mast bumping event. Mast bumping can occur in low acceleration of gravity (G) flight conditions, causing the rotor blade to exceed its flapping limits and resulting in the main rotor hub bumping into the rotor shaft. This often results in structural failure of the rotor shaft and a subsequent separation of the main rotor.

Due to the extensive thermal damage to the wreckage, only a limited examination could be conducted; however, no mechanical malfunctions or anomalies were noted that would have precluded normal operation.

The pilot had accumulated about 15,000 flight hours in airplanes but only had about 55 hours flight time in helicopters, most of which were accumulated more than 1 year before the accident. Although the pilot had received instruction on how to avoid mast bumping, given his low helicopter experience relative to his airplane experience, it is possible that he made a large, abrupt flight control input that resulted in a low-G flight condition and led to the observed mast bumping. However, the pilot's control inputs are unknown, and the initiating event for the mast bumping could not be determined.
Probable Cause: The separation of the main rotor assembly due to mast bumping.

Sources:

NTSB

FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N4035G

Accident investigation:
cover
  
Investigating agency: NTSB
Status: Investigation completed
Duration:
Download report: Final report
Location

Media:


Revision history:

Date/timeContributorUpdates
07-Oct-2016 04:42 Geno Added
07-Oct-2016 12:33 gerard57 Updated [Operator, Total fatalities, Total occupants, Source, Narrative]
07-Oct-2016 14:24 Anon. Updated [Aircraft type]
07-Oct-2016 15:18 Geno Updated [Registration, Cn, Operator, Source]
08-Oct-2016 02:52 Geno Updated [Departure airport, Source]
17-Oct-2016 09:12 Iceman 29 Updated [Source, Embed code, Narrative]
20-May-2017 14:53 Aerossurance Updated [Time, Operator, Phase, Nature, Destination airport, Source, Narrative]
19-Aug-2017 15:00 ASN Update Bot Updated [Time, Other fatalities, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description