Accident Bell UH-1H Iroquois N711GH,
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ASN Wikibase Occurrence # 240280
 
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Date:Wednesday 19 August 2020
Time:09:45
Type:Silhouette image of generic UH1 model; specific model in this crash may look slightly different    
Bell UH-1H Iroquois
Owner/operator:Guardian Helicopters
Registration: N711GH
MSN: 5071
Year of manufacture:2009
Total airframe hrs:10389 hours
Engine model:Honeywell T53-L-703
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:near Coalinga, CA -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Fire fighting
Departure airport:New Coalinga Municipal Airport, CA (C80)
Destination airport:New Coalinga Municipal Airport, CA (C80)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
On August 19, 2020 about 0945 Pacific daylight time, an Arrow-Falcon Exporters, Inc., UH-1H, N711GH, was destroyed when it was involved in an accident near Coalinga, California. The pilot, the sole occupant was fatally injured. The helicopter was operated as a public use firefighting flight.

The pilot was engaged in external load fire-fighting operations when the accident occurred. After dropping several loads of water, the pilot reported abnormal noises and vibrations and stated "it's my hydraulics" before he lost airspeed and control of the helicopter. The helicopter made several uncontrolled rotations before colliding with terrain and erupting in flames. The wreckage was highly fragmented and most consumed by the postimpact fire.

The hydraulic system continuity could not be confirmed due to fire damage. The servos exhibited exposure to fire, including an oxide layer on the outer surface, micro-cracks, resolidified metal, and deformation damage. Foreign high-density particles were found in the hydraulic system. Hydraulic flight control stiffness and hard-over conditions are most likely a result of a malfunction of the servo irreversible valve.

Only one of the three irreversible hydraulic valves was not destroyed in the postcrash fire. Examination of this valve found high-density metal particles deep within the valve assembly and preexisting damage to the seat of a check valve. Since all the servos were operated from a single hydraulic pressure source, it is likely that the other two irreversible valves also had similar particles within their assemblies.

Foreign high-density particles and a worn check valve within the irreversible valve could have interfered with the valves’ proper operation and resulted in control stiffness or a hard-over condition. There was no evidence of preexisting mechanical damage on the three servo actuator pistons or rods as the internal moving parts within the servo actuators showed no evidence of gouging. There was no wear damage in the bushing areas or around the housing ball assembly.

Toxicological tests detected the antidepressant medication citalopram and an augmenting agent buspirone in the pilot’s system. Given that the pilot was performing complex firefighting tasks when the helicopter developed mechanical problems and he made reasonable decisions to attempt to land the helicopter, he appears to have been functioning at a high level. It appears unlikely that the pilot’s use of the antidepressants or his depression were factors in the accident.

The pilot’s declaration that he had a hydraulic problem and the final uncorrected right hand descending spiral turn flightpath are consistent with what would be expected if the helicopter experienced control stiffness or a hard-over condition. However, due to the extent of the impact and postimpact fire damage, the reason for the loss of control could not be conclusively determined.

Probable Cause: The pilot’s inability to maintain control of the helicopter due to a hydraulic system failure for reasons that could not be fully determined due to the thermal destruction from the postimpact fire.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR20LA280
Status: Investigation completed
Duration: 2 years and 9 months
Download report: Final report

Sources:

https://abc30.com/coalinga-helicopter-crash-firefighter-fresno-county-fire-cal/6378368/
https://www.yourcentralvalley.com/news/local-news/firefighting-helicopter-crashes-near-coalinga-faa-ntsb-to-investigate/
http://thepinetree.net/new/?p=105834
https://fireaviation.com/2020/08/19/pilot-killed-in-crash-of-firefighting-helicopter-near-coalinga-california/
https://fireaviation.com/2020/12/14/preliminary-report-released-for-fatal-helicopter-accident-near-coalinga/

NTSB
https://guardianhelicoptersusa.com/bell-uh-1h-huey-n711-gh/
https://flightaware.com/live/flight/N711GH
https://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N711GH

Location

Images:



Revision history:

Date/timeContributorUpdates
19-Aug-2020 22:48 Geno Added
19-Aug-2020 23:37 RobertMB Updated [Aircraft type, Total occupants, Phase, Source, Damage, Narrative]
20-Aug-2020 00:09 Captain Adam Updated [Registration, Cn, Operator, Location, Departure airport, Source, Narrative]
20-Aug-2020 00:10 Captain Adam Updated [Total fatalities]
20-Aug-2020 03:41 Aerossurance Updated [Aircraft type, Source, Narrative]
20-Aug-2020 07:46 Anon. Updated [Source]
20-Aug-2020 07:47 harro Updated [Cn, Source]
20-Aug-2020 08:02 A.J.Scholten Updated [Source]
20-Aug-2020 14:22 Iceman 29 Updated [Photo]
22-Sep-2020 11:18 Aerossurance Updated [Time, Operator, Location, Source, Narrative]
22-Sep-2020 11:18 Aerossurance Updated [Narrative]
14-Dec-2020 13:16 Aerossurance Updated [Source, Narrative]
14-Dec-2020 13:16 Aerossurance Updated [Embed code]
02-Mar-2021 18:30 rudy Updated [Embed code]

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