Accident Brantly B-2B N2284U,
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ASN Wikibase Occurrence # 200104
 
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Date:Sunday 1 October 2017
Time:14:47
Type:Silhouette image of generic BRB2 model; specific model in this crash may look slightly different    
Brantly B-2B
Owner/operator:Private
Registration: N2284U
MSN: 454
Year of manufacture:1965
Total airframe hrs:2074 hours
Engine model:Lycoming IVO-360-A1A
Fatalities:Fatalities: 1 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Sanford, west of Midland, Midland County, MI -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Private
Departure airport:Midland, MI (N/A)
Destination airport:Midland, MI (N/A)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The private pilot was conducting a local flight in the helicopter with a passenger. After departing from an open field, the pilot flew along the perimeter of the field, and the passenger recalled that about halfway around the perimeter of the field, the helicopter began descending, slowly at first and then more rapidly. According to the passenger, the rotor speed increased, but the helicopter continued to descend.

Ground-based video footage revealed that before it began descending, the helicopter was moving forward slowly when it yawed about 270° to the right. As it neared the ground, the helicopter again yawed to the right, completing nearly a 360° turn either immediately before or just after it contacted the ground. The helicopter came to rest on its left side. The engine continued to run after the helicopter came to rest, and the passenger shut it off.

Airframe and engine examinations did not reveal evidence of any anomalies consistent with a pre-impact failure or malfunction. Surface wind conditions recorded at nearby airports were light and variable.

Federal Aviation Administration publications regarding a loss of tail rotor effectiveness (LTE) state that in the event of a sudden, unanticipated right yaw, a pilot should apply full left pedal, simultaneously move the cyclic control forward to increase airspeed, and if altitude permits, reduce engine power. Factors that contribute to LTE are a high-power setting, which induces considerable main rotor downwash and more turbulence relative to a low power setting, and a slow forward speed, which may create variations in airflow around the tail rotor. The video footage showing a right yaw followed by a descent suggests that the pilot encountered LTE, which resulted in the 270° right yaw before the pilot was able to regain control. The additional power required by the tail rotor during the recovery reduced the power available to the main rotor and resulted in a descent that could not be arrested with the engine power available. It appeared that the pilot did not attempt to increase airspeed during the recovery, which reduced his ability to avoid impacting the ground.

Probable Cause: The pilot's failure to maintain control of the helicopter, which resulted in a loss of tail rotor effectiveness, and his failure to promptly initiate the proper recovery technique, which resulted in a descent that could not be arrested before impacting the terrain.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN18FA001
Status: Investigation completed
Duration: 1 year and 9 months
Download report: Final report

Sources:

NTSB

FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N2284U

History of this aircraft

Other occurrences involving this aircraft
11 September 1978 N2284U 1 near Brook, In w/o
10 July 1990 N2284U Private 0 Christiansted, sub

Location

Media:

Revision history:

Date/timeContributorUpdates
02-Oct-2017 06:44 gerard57 Added
02-Oct-2017 14:28 Geno Updated [Location, Phase, Source, Narrative]
02-Oct-2017 17:56 Geno Updated [Aircraft type, Registration, Cn, Operator, Source]
02-Oct-2017 23:50 Iceman 29 Updated [Embed code]
15-Jul-2019 18:03 ASN Update Bot Updated [Time, Operator, Departure airport, Destination airport, Source, Damage, Narrative, Accident report, ]

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