ASN logo
ASN Wikibase Occurrence # 177989
Last updated: 23 November 2019
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:20-JUL-2015
Time:17:40
Type:Silhouette image of generic UH1 model; specific model in this crash may look slightly different
Bell UH-1H
Owner/operator:Lrh Equipment Llc
Registration: N121PT
C/n / msn: 64-13711
Fatalities:Fatalities: 0 / Occupants: 1
Other fatalities:0
Aircraft damage: Written off (damaged beyond repair)
Category:Accident
Location:9 miles east of Walla Walla, Washington -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Fire fighting
Departure airport:Walla Walla, WA
Destination airport:Walla Walla, WA
Investigating agency: NTSB
Narrative:
The commercial pilot reported that the helicopter was in a 165-ft hover in a narrow creek valley, over a shallow creek and that he was filling a fire bucket, which was attached to the helicopter via a long line. The terrain rose between 200 and 400 ft on either side of the creek. About 1 minute into the hover, the pilot felt the helicopter start to settle. He applied collective to arrest the settling, but the helicopter continued to settle. The pilot said that there was no yaw or unusual vibration or noise during the event, only a smooth settling of the helicopter and that the engine did not respond when he manipulated the collective. He immediately lowered the collective and performed a hovering autorotation toward an embankment. When the pilot raised the collective for the landing, the engine did not respond. The rotors struck several trees, then the helicopter spun 180°, landed hard, and rolled over onto its right side. After the accident, the engine continued to run until the pilot shut off the fuel and secured the battery. The helicopter was destroyed by postcrash fire.
Postaccident examination of the helicopter did not reveal any evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation. Examination of the engine revealed compressor blade damage, rotational scoring witness marks, and metal splatter, consistent with the engine operating at the time of the accident.
An automated surface observation system (ASOS) located 10 miles west of the accident reported that, about 1 hour before the accident, the wind was from 250°, gusting to 22 knots. An unofficial weather station located 6 miles southwest of the accident site recorded that, about 3 minutes before the accident, the wind was from 239o at 20 knots, gusting to 30 knots. The ASOS reported that, about 13 minutes after the accident, the wind was from 239o at 14 knots. Given these conditions, orographic wind turbulence could not be ruled out as a factor.


Probable Cause: The helicopter’s reduction in aerodynamic lift while operating in variable wind conditions for reasons that could not be determined because postaccident examination did not reveal any evidence of preimpact mechanical malfunctions or failures that would have precluded normal operation.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20150721X35946&key=1
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N121PT

Accident investigation:
cover
  
Investigating agency: NTSB
Status: Investigation completed
Duration: 2 years and 10 months
Download report: Final report


Revision history:

Date/timeContributorUpdates
21-Jul-2015 07:31 gerard57 Added
22-Jul-2015 15:15 Geno Updated [Aircraft type, Registration, Cn, Operator, Source, Damage, Narrative]
23-Jul-2015 05:32 stevethehumbersider Updated [Cn, Narrative]
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
08-Jun-2018 12:00 ASN Update Bot Updated [Cn, Operator, Nature, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description