Accident Boeing CH-46E Sea Knight N461WY,
ASN logo
ASN Wikibase Occurrence # 343327
 
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:Sunday 6 August 2023
Time:15:20
Type:Silhouette image of generic H46 model; specific model in this crash may look slightly different    
Boeing CH-46E Sea Knight
Owner/operator:Sky Aviation
Registration: N461WY
MSN: 2438
Year of manufacture:1968
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:Springerville, AZ -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Fire fighting
Departure airport:Show Low Airport, AZ (SOW/KSOW)
Destination airport:Springerville, AZ
Investigating agency: NTSB
Confidence Rating: Information verified through data from accident investigation authorities
Narrative:
On August 5, 2023, about 1520 mountain standard time, a Boeing CH-46 helicopter, N461WY, was destroyed when it was involved in an accident near Springerville, Arizona. The pilot, copilot and passenger were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 133 external load flight in support of firefighting operations.

The privately owned helicopter was performing firefighting operations under a contract with the United States Forest Service (USFS) in response to the Corduroy Fire.

The pilot reported that they had performed firefighting water drop activities for about 2 hours. After they had filled the bucket with water and began to climb, the crew heard an extremely loud horn in their helmets; loud enough that it was difficult to understand what was being said. The pilot noticed that the No. 2 torque indicator was “maxed out” and the No. 1 torque indicator was about 60%.

The pilot released the water in the bucket and initiated a turn to an open field. The pilot then slowly retarded the No. 2 engine control lever to match the torque. He noted that the torque for both engines matched about 90%. Upon turning final for his intended landing field, the pilot noticed that the descent rate increased. The pilot told his crew chief to jettison the bucket as he placed the No. 2 engine control lever to the fly position. Subsequently, the helicopter landed hard and rolled onto its right side. The engines were shut down and the co-pilot and crewchief assisted the pilot in exiting the helicopter. Moments later, a post impact fire ensued.

The wreckage was recovered to a secured facility for further examination.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR23LA306
Status: Preliminary report
Duration:
Download report: Preliminary report

Sources:

NTSB
FAA

Location

Revision history:

Date/timeContributorUpdates
08-Aug-2023 08:21 harro Added
08-Aug-2023 08:33 harro Updated
29-Aug-2023 18:40 Captain Adam Updated

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org