Accident Bell 212 N911KW,
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ASN Wikibase Occurrence # 265258
 
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Date:Wednesday 7 July 2021
Time:16:45 LT
Type:Silhouette image of generic B212 model; specific model in this crash may look slightly different    
Bell 212
Owner/operator:Rogers Helicopters Inc
Registration: N911KW
MSN: 30592
Year of manufacture:1973
Total airframe hrs:14543 hours
Engine model:Pratt & Whitney PT6T-3B
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Lake Shastina, Siskiyou County, CA -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Fire fighting
Departure airport:Dunsmuir, CA (1O6)
Destination airport:Weed , CA
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The flight was on an approach to a lake to retrieve water for a water bucket drop operation. During the approach, the instruments scanned normal, and the radar altimeter was set to 200 ft above ground level to provide a buffer between the bucket and terrain. When the helicopter crossed the shoreline, the pilot visually confirmed that the 100-ft long line and bucket were slightly trailing the helicopter and had not dipped in the water. Shortly afterward, he felt a “sudden onset of a significant vibration.' The pilot aborted the water retrieval and noticed that helicopter lost altitude. He applied forward cyclic and raised the collective, but the helicopter continued to descend. The pilot realized that he would not be able to fly out of the descent, so he decided to make a forced water landing. The pilot did not jettison the long line and bucket. After he leveled the helicopter and the skids touched down on the water, he made another attempt to take off, but the helicopter settled into the lake. The pilot reduced both throttle settings to idle in preparation to ditch the helicopter and applied right cyclic as the main rotors slowed. The helicopter rolled right, and the main rotor blades struck the water, which resulted in substantial damage to the fuselage, rotor, and drive systems.
Postaccident examination of the engine revealed no preimpact mechanical anomalies. The airframe examination revealed an out-of-tolerance condition of both pylon damper rod end bearings that likely caused the vibration reported by the pilot. It is likely that, after the lateral vibration, the pilot allowed the helicopter to descend while he tried to determine the source of the vibration. As the helicopter settled into the lake, the bucket filled with water. The resulting increased weight, combined with the pilot's failure to release the water bucket, decreased the helicopter's out-of-ground-effect performance.

Probable Cause: The pilot's failure to maintain altitude during an approach to a lake. Contributing to the accident was the pilot's failure to release the full water bucket as the helicopter was settling, which reduced the helicopter's out-of-ground-effect performance.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR21LA268
Status: Investigation completed
Duration: 1 year and 11 months
Download report: Final report

Sources:

NTSB WPR21LA268

Location

Media:

Revision history:

Date/timeContributorUpdates
08-Jul-2021 03:58 Geno Added
08-Jul-2021 05:01 Aerossurance Updated [Location, Phase, Source, Damage, Narrative]
08-Jul-2021 12:50 RobertMB Updated [Time, Aircraft type, Registration, Cn, Operator, Departure airport, Source, Narrative]
15-Jul-2021 10:45 Aerossurance Updated [Source, Embed code, Narrative]
14-Feb-2022 18:11 TheGreatCalCom Updated [Operator, Source, Embed code, Narrative]
12-Nov-2022 01:25 Ron Averes Updated [Operator]
30-May-2023 00:40 Ron Averes Updated [[Operator]]
01-Jul-2023 07:30 ASN Update Bot Updated [[[Operator]]]

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