The U.S. aircraft register, updated daily
Accidents · NTSB ANC16LA022 · Final report

Airbus AS350 accident near Juneau, Alaska, May 5, 2016

On May 5, 2016 at about 10:05 pm local time, a 1992 Airbus AS350 (helicopter), registered N194EH, was substantially damaged in an accident during approach near Juneau, Alaska. It was an other work-use flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain terrain clearance while on approach to land in flat light conditions. Contributing to the severity of the pilot's injuries was the inadequately restrained internal cargo, which shifted forward during the impact and struck the pilot and/or the pilot's seat.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
May 5, 2016 · about 10:05 pm local time
Place
Juneau, Alaska · map
Type
Accident
Injuries
1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Airbus AS350 B2, built 1992
Registration
N194EH · no longer on the register · serial 2608
Damage
Substantial damage
Flight
Other work-use flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The instrument-rated commercial pilot was making a visual flight rules internal-cargo company flight in the helicopter. He reported that flat light conditions were present as he made a visual approach for landing at a remote dog camp situated on a glacier. During the approach, the helicopter impacted terrain, coming to rest about 3/4 mile from the dog camp. The pilot reported that there were no preimpact mechanical anomalies with the helicopter and characterized the accident as controlled flight into terrain. It is likely that the pilot failed to maintain terrain clearance due to his inability to distinguish distances and closure rates because of the flat light optical illusion. The single cargo strap securing a plastic box containing a metal heater to the rear cabin floor remained intact during the accident sequence; however, the plastic box shifted forward due to the momentum of the helicopter impacting terrain, which allowed the metal heater to escape from the lidded box. It is likely that the metal heater struck the pilot and/or the pilot's seat in the accident sequence, contributing to the serious injuries sustained by the pilot. The single cargo strap used to secure the plastic box was installed such that it provided lateral restraint of the box but no forward restraint of the box. If the box had been restrained to prevent forward movement, it is likely that the metal heater would not have escaped from the box. Review of the helicopter's rotorcraft flight manual (RFM) revealed that it provided only a total weight limit for the rear cabin floor and did not provide any guidance about how to properly secure internal cargo in the cabin. Further, although the manufacturer indicated in a systems manual that cargo could be secured to the cabin floor using 11 mooring points embedded into the floor and provided a force limit for each mooring point, the systems manual provided no guidance regarding how the cargo should be attached to the mooring points; for example, no information was provided about the type and number of restraints to be used or how they should be configured. Airbus, the manufacturer of the helicopter, stated that it was the responsibility of the operator "to define an adapted cargo, freight, or baggage securement that is in respect to the limitations permissible force on the floor stowing mooring rings." The Federal Aviation Administration (FAA) stated that operators do not have certification approval to install cargo in the cabin unless it is mentioned in the RFM or RFM supplement and that, if an FAA-approved cargo configuration has been published for a specific aircraft, the RFM for that aircraft is where information on how and where to install cargo will be found. However, the FAA also stated that it "is not aware of any documentation that would prohibit Part 27 rotorcraft from carrying cargo in the cabin, even if a certification does not exist for that helicopter."

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Other weather encounter during approach
  2. Loss of visual reference during approach defining event
  3. Controlled flight into terrain or object (CFIT) during approach

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained
  • cause Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Pilot
  • cause Personnel issues › Psychological › Attention/monitoring › Monitoring equip/instruments › Pilot
  • cause Personnel issues › Psychological › Perception/orientation/illusion › Visual illusion/disorientation › Pilot
  • cause Environmental issues › Conditions/weather/phenomena › Light condition › Flat light › Effect on operation
  • cause Environmental issues › Conditions/weather/phenomena › Ceiling/visibility/precip › (general) › Ability to respond/compensate
  • factor Aircraft › Aircraft systems › Equipment/furnishings › Passenger compartment equip › Incorrect use/operation
  • factor Aircraft › Aircraft handling/service › Loading › (general) › Incorrect use/operation

Pilot

  • Certificate: commercial pilot
  • Ratings: instructor: helicopter; instructor: instrument helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,428 hours in all; 2,084 in this make and model; 15 in the last 90 days; 15 in the last 30 days; 3,375 as pilot in command
  • Last flight review: March 30, 2016
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 11,735.9 hours
  • Last inspection: continuous airworthiness programme, May 3, 2016
  • Maximum gross weight: 4,961 lb
  • Seats: 6
  • Landing gear: fixed
  • Engine: Safran (Formerly Turbomeca) Arriel 1D1 (turboshaft); 8,742 hours total
  • Operator: Era Helicopters LLC

The flight

  • Departed from: Juneau AK
  • Destination: Juneau AK

Weather at the time

  • Light: daylight
  • Wind: from 120° at 15 knots
  • Visibility: 8 statute miles
  • Sky: broken clouds at 3,900 ft; a few clouds at 1,300 ft
  • Temperature: 45°F (7°C), dew point 41°F (5°C)
  • Altimeter: 30.20 inHg
  • Observation at 9:53 pm from PAJN, 13 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

16 documents, released by the NTSB on September 10, 2018. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.