20220626008299A

Accident · Destroyed

FAA accident report · Bell UH-1B · Anderson, AK · June 26, 2022

Date
June 26, 2022 · 19:38 local
Place
Anderson, AK
Airport
Clear Airport
Phase of flight
Hover/Holding
Operating rules
Rotorcraft external load (Part 133)
Operator
NP6L
Damage
Destroyed
Aircraft
N9970F
NTSB investigation
NTSBANC22FA047
Reported as
Bell UH-1B
People aboard
1
Fatal injuries
1
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
4,878 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Numerous witnesses reported that after a normal liftoff, the helicopter hovered with the longline fully extended as it maneuvered to hook up to the external load. A loud “snap” or “bang” was heard, and the helicopter “bucked”. Subsequently, the helicopter rolled right, entered a nose low descent and impacted the ground. Prior to impact with ground, the transmission and rotor head assembly departed the aircraft. At the time of transmission seperation, a main rotor blade severed the tailboom. Following the impact, a post-crash fire ensued, which consumed a majority of the helicopter.

As the FAA filed it

Numerous witnesses reported that after a normal liftoff, the helicopter hovered with the longline fully extended as it maneuvered to hook up to the external load. A loud “snap” or “bang” was heard, and the helicopter “bucked”. Subsequently, the helicopter rolled right, entered a nose low descent and impacted the ground. Prior to impact with ground, the transmission and rotor head assembly departed the aircraft. At the time of transmission seperation, a main rotor blade severed the tailboom. Following the impact, a post-crash fire ensued, which consumed a majority of the helicopter.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.