Pollux Aviation Robinson Helicopter Company R44 II accident
Robinson Helicopter Company R44 II · Accident: settling with power/vortex ring state during landing
From Wolf Lake Airport (4AK6) to an unrecorded destination
Event
- NTSB case
- ANC25LA099
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- Event fatalities
- Unknown
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- Charter & commuter
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Robinson Helicopter Company R44 II
- Aircraft type
- Robinson R44
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N74435
- Operator
- Pollux Aviation
- Onboard fatalities
- Unknown
- Route
- From Wolf Lake Airport (4AK6), Wasilla, AKTo not recorded
- Aircraft age
- About 20 years (built 2005)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 135: Air Taxi & Commuter
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Landing
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Settling with power/vortex ring state
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Environmental issues › Conditions/weather/phenomena
- Personnel issues › Psychological
- Personnel issues › Task performance
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot reported that he was transporting three passengers and their equipment to a remote landing zone (LZ) in mountainous terrain. According to the operator, the helicopter’s estimated gross weight was 2,440 lbs., approximately 60 lbs. below the maximum gross weight of 2,500 lbs. The pilot stated that a guide onboard the helicopter was directing him to the LZ. He had initially planned to conduct a northwesterly reconnaissance flyover of the landing area; however, he became distracted when the guide pointed out the intended LZ directly ahead. As a result, the pilot immediately turned toward the site and initiated a steep approach without completing the planned flyover. During the approach, the pilot reported an increasing descent rate. He applied additional collective to arrest the descent, after which the full-throttle annunciator illuminated. Despite the collective being fully raised, the helicopter continued descending and subsequently impacted the ground. The helicopter landed hard and rolled over, sustaining substantial damage to the fuselage and the main and tail rotor drive systems. Following the accident, the pilot estimated the wind was from the south at approximately 15 to 20 knots. He reported no preimpact mechanical failures or malfunctions that would have precluded normal operation.
Probable cause
The pilot’s exceedance of the helicopter’s available power while landing in a remote confined area, which resulted in rotor droop and a hard landing.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ANC25LA099
- Event ID
- 20250908200960
- Case number
- ANC25LA099
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates, cause areas. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 6816613ab6a64d7cffcdbf9dbba08fede14211a0e81ae0d3a59b2628d0727207; retrieved 2026-09-16T20:18:54.511Z.