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Accidents · NTSB ANC13FA017 · Final report

Eurocopter AS350 B3 accident near Beluga, Alaska, December 15, 2012

On December 15, 2012 at about 7:05 pm local time, a Eurocopter AS350 B3 (helicopter), registered CGYPH, was substantially damaged in an accident during enroute (cruise) near Beluga, Alaska. It was an external-load flight under external-load helicopter rules (Part 133). 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 stabilize the external load, which led to the synthetic long-line separating about midspan and the remaining line becoming entangled in the tail rotor gearbox output shaft and resulted in the separation of the tail rotor gearbox and subsequent loss of control. Contributing to the accident was the pilot's inadequate training.

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

What the record shows

Date
December 15, 2012 · about 7:05 pm local time
Place
Beluga, Alaska · map
Type
Accident
Injuries
1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Eurocopter AS350 B3 · all AS350 B3s on the register
Registration
CGYPH · no longer on the register · serial 3688
Damage
Substantial damage
Flight
External-load flight · external-load helicopter rules (Part 133)

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

The commercial helicopter pilot was transporting a 1,000-pound external sling load attached to a lightweight, synthetic 100-foot long-line when the load began to spin and swing underneath the helicopter. As the helicopter neared its destination, it suddenly yawed, and then started to spin uncontrollably, and the pilot immediately jettisoned the external load. As the helicopter continued to spin uncontrollably, it descended into an area of tall trees and then came to rest on its left side.  A postaccident inspection of the helicopter revealed that portions of the severed lightweight synthetic long-line had become entangled in the tail rotor gearbox output shaft and that the tail rotor gearbox assembly was torn free of the tail boom. Examination of the long-line revealed that its entire length was tightly wrapped, knotted, and kinked. The pilot reported that he had not received training in procedures to adequately stabilize external sling loads. Given the postaccident condition of the lightweight synthetic long-line, the pilot's statements, and the lack of a rotating swivel, it is likely that, once the external load began to spin, the long-line continued to tangle and tightly knot and ultimately reached its breaking point. Once the synthetic long-line separated, the portion still attached to the belly of the helicopter recoiled upward and eventually became entangled with the tail rotor gearbox output shaft. In addition, it is likely the pilot did not adequately monitor the condition of the external sling load while en route, and he failed to recognize the need to stabilize the load.

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. External load event (Rotorcraft) during enroute (cruise)
  2. Loss of control in flight during enroute (cruise) defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft propeller/rotor › Tail rotor drive system › Tail rotor drive shaft › Damaged/degraded
  • factor Personnel issues › Experience/knowledge › Training › Initial instruct/training › Pilot
  • factor Organizational issues › Support/oversight/monitoring › Training › Initial training › Operator
  • Organizational issues › Support/oversight/monitoring › Training › (general) › FAA/Regulator
  • factor Personnel issues › Action/decision › Info processing/decision › Understanding/comprehension › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: commercial pilot
  • Ratings: instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,037 hours in all; 48 in this make and model; 73 in the last 90 days; 37 in the last 30 days; 3,037 as pilot in command
  • Last flight review: April 30, 2012
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 5,559 hours
  • Last inspection: 100-hour inspection, August 13, 2012
  • Maximum gross weight: 6,173 lb
  • Seats: 6
  • Landing gear: fixed
  • Engine: Turbomecca Arriel 2B (turboshaft); 3,868 hours total
  • Operator: Prism Helicopters INC

The flight

  • Departed from: PABG Beluga AK
  • Destination: PABG Beluga AK

Weather at the time

  • Light: daylight
  • Wind: from 340° at 3 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 7,000 ft
  • Temperature: 7°F (-14°C), dew point 3°F (-16°C)
  • Altimeter: 29.14 inHg

Injuries

FatalSeriousMinorNone
Flight crew1

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

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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.