ANC25LA097

NTSB accident investigation · Airbus Helicopters AS350B3e · Skwentna, AK · August 20, 2025

Accident · No injuriesClass 4 · LimitedFinal report
Date
August 20, 2025, 14:30 local (22:30 UTC)
Place
Skwentna, AK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N589SHAirbus Helicopters AS350B3e
Defining event
Standing-engine(s) operating: Miscellaneous/other
Weather
Visual (VMC) · Day
Status
Completed · report October 23, 2025
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Alaska Regional Office
Parties
Federal Aviation Administration (FAA)
FAA report
20250820017389A
Case key
200883

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot’s inadvertent entanglement of a lightweight Kevlar long line into the helicopters operating main rotor system, resulting in a severe imbalance and separation of the main rotor gearbox.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Terrain: rough terrainEnvironmental issues › Physical environment · Effect on operationEurocopter AS 350 B3: 1 caseAll aircraft: 442 cases

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The operator reported that the helicopter was being used to sling construction equipment to a remote mine site located in an area of steep mountainous terrain. After the pilot placed the external load at a prearranged site next to the drill pad, he maneuvered the helicopter to a landing site in an area of rock-covered terrain to disconnect and stow the lightweight Kevlar long line that was still attached to the helicopter’s cargo hook. After a successful landing, the pilot reduced the engine throttle to ground idle, locked the flight controls, then exited the helicopter with the engine and rotor still operating. As the pilot coiled the Kevlar long line into the helicopter, a portion of the line became entangled in the rock covered terrain, and the pilot pulled hard to free it. As the Kevlar long line suddenly released from the rocks, the recoiling line became entangled in the operating main rotor blades which resulted in a severe main rotor imbalance. As a result, the main rotor gearbox and entire main rotor system were subsequently ripped from the helicopter. The helicopter sustained substantial damage to the fuselage, tail boom assembly, and main rotor drive system. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation.

Aircraft

Registration
N589SH
Reported as
Airbus Helicopters AS350B3e
Category
Helicopter
Serial number
7745
Built
2013
Airframe hours
5,664.5
Engine
Safran ARRIEL 2D, turbo shaft
Damage
Substantial damage
Flight
External load · Part 133
Operator
Soloy Helicopters LLC
Registered owner
Csc Delaware Trust Co Trustee
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · August 9, 2025 · 5 hours before
Destination
Same as departure
Flight plan
Company VFR
Equipment
Video recording device, Satellite tracking device, ADS-B

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
58
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Last flight review
March 25, 2025
Seat
None
Flight hours
15,500 total · 9,900 in this make and model · 15,400 as pilot in command · 290 in the last 90 days · 50 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
25 statute miles
Temperature
55 °F, dew point 52 °F
Altimeter
30.12 inHg
Observed at
APT, 21 nm away
METAR
PAPT 201857Z COR 00000KT 25SM FEW027 13/11 A3012 RMK NO SPECI

Docket · 2

The files NTSB released with the investigation on October 23, 2025, on NTSB’s docket system: statements, records, photos and specialists’ reports. 3.1 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.