NTSB Prelim: Hiller UH-12E | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-05.13.24

Airborne-NextGen-05.07.24

Airborne-Unlimited-05.08.24 Airborne-FlightTraining-05.09.24

Airborne-Unlimited-05.10.24

Wed, Oct 20, 2021

NTSB Prelim: Hiller UH-12E

Pilot Experienced A “Jolt” And Suddenly The Helicopter “Dropped”

Location: Bovill, ID Accident Number: WPR21LA354
Date & Time: September 23, 2021, 15:00 Local Registration: N5334V
Aircraft: Hiller UH-12E Injuries: 1 Minor
Flight Conducted Under: Part 137: Agricultural

On September 23, 2021, about 1500 Pacific daylight time, a Hiller UH-12E helicopter, N5334V, was substantially damaged when it was involved in an accident near Bovill, Idaho. The pilot was not injured.

The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight. The pilot reported that he had been applying dry fertilizer over trees as part of a timber company contract and had flown about 5.7 hours that day. As he was approaching the service truck to refill his bucket, about 40 ft above ground level and about 20 ft from the truck, the pilot experienced a “jolt” and suddenly the helicopter “dropped” to the sloping terrain below.

The pilot stated he had no time to react and that the helicopter didn’t turn or yaw after the “jolt.” He did recall the torque gauge indicated between 85% and 90% during the accident sequence. The pilot further stated that everything on the helicopter had involuntarily shut down before he had exited. The witness that was manning the truck reported to the pilot didn’t hear anything abnormal. He also stated that the wind was light and variable at the time of the accident.

The helicopter impacted the ground and came to rest on its side. The cabin area and windshield structure were bent and distorted. The tailboom separated near the midsection and the main rotor blades were buckled in multiple areas.

The helicopter was recovered by the operator and secured at the operator’s facility for further examination.

FMI: www.ntsb.gov

Advertisement

More News

ANN's Daily Aero-Term (05.10.24): Takeoff Roll

Takeoff Roll The process whereby an aircraft is aligned with the runway centerline and the aircraft is moving with the intent to take off. For helicopters, this pertains to the act>[...]

Aero-News: Quote of the Day (05.10.24)

“We’re proud of the hard work that went into receiving this validation, and it will be a welcome relief to our customers in the European Union. We couldn’t be mor>[...]

Aero-News: Quote of the Day (05.11.24)

"Aircraft Spruce is pleased to announce the acquisition of the parts distribution operations of Wag-Aero. Wag-Aero was founded in the 1960’s by Dick and Bobbie Wagner in the >[...]

ANN's Daily Aero-Term (05.11.24): IDENT Feature

IDENT Feature The special feature in the Air Traffic Control Radar Beacon System (ATCRBS) equipment. It is used to immediately distinguish one displayed beacon target from other be>[...]

ANN's Daily Aero-Linx (05.11.24)

Aero Linx: Pararescue Air Force Pararescuemen, also known as PJs, are the only DoD elite combat forces specifically organized, trained, equipped, and postured to conduct full spect>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC