Accident Eurocopter AS 350 N354PA,
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ASN Wikibase Occurrence # 278796
 
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Date:Sunday 6 September 2020
Time:09:05 LT
Type:Silhouette image of generic AS50 model; specific model in this crash may look slightly different    
Eurocopter AS 350
Owner/operator:Pathfinder Aviation
Registration: N354PA
MSN: 3330
Year of manufacture:2000
Total airframe hrs:15111 hours
Engine model:Turbomeca ARRIEL 2B
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Fort Greely, Alaska -   United States of America
Phase: En route
Nature:Ferry/positioning
Departure airport:Delta Junction, AK (72AK)
Destination airport:Anchorage-Merrill Field, AK (MRI/PAMR)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
While in cruise flight, at about 700 ft above ground level and 110 kts, a 'sudden loud bang” and associated left yaw was experienced as the sliding left side cabin door vacated the helicopter from the closed position. The door impacted a main rotor blade during the separation sequence, which resulted in substantial damage. Subsequently an emergency landing was made to a nearby grass area with no further incident.

Airbus Helicopters has two Alert Service Bulletins (ASB) out for the cabin doors on the AS350-B3. The operator reported that the ASBs from the helicopter manufacturer regarding the cabin doors had not been complied with prior to the accident.

During a post-accident examination, the FAA inspector reported that he was not able to find any definitive reason for the departure of the door. He added that the door rollers were displaced and were not recovered, and a partial slide piece on the lower rail was not recovered either. Since the door rollers were not recovered, they were not able to be examined, and therefor their condition and function could not be tested.

Airbus Helicopters has two Alert Service Bulletins (ASB) published in response to door seperations that occurred as a result of door roller failures on AS350-B3 helicopters. The operator reported that these ASBs had not been complied with prior to the accident. Because the affected components were not recovered, the investigation could not determine if compliance with these ASBs could have prevented the accident.

Airbus noted that the damage was consistent with the door lock not being effective due to the presence of a cargo box that was stored in the cabin that interfered with the door, which resulted in the door opening and separating in flight due to the interference load introduced by the cargo box in the cabin.

Although some affected components were not recovered and examined, the accident is consistent with the door lock failing inflight, likely due to interference between the door and the cargo box.

Probable Cause: Failure of the door lock due to interference between the door and a cargo box.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ANC20LA089
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB ANC20LA089

History of this aircraft

Other occurrences involving this aircraft
20 May 2004 N216HP California Highway Patrol 0 Livermore, CA sub

Location

Revision history:

Date/timeContributorUpdates
04-Jun-2022 07:24 ASN Update Bot Added

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