Plane Crash List

Airbus Helicopters AS350-B3 N351SH

28 March 2021 · Palmer, Alaska, United States · Fatal

Summary

On 28 March 2021 at about 02:36 local time, a Airbus Helicopters AS350-B3 registered N351SH, operated by Soloy Helicopters LLC, was involved in an accident near Palmer, Alaska, United States. 6 people were on board and 5 died, one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 02:36
Classification
Accident
Location
Palmer, Alaska, United States
Coordinates
61.4517, -148.3655
Aircraft
Airbus Helicopters AS350-B3
Registration
N351SH
Category
Helicopter
Year built
2008
Engines
1
Operating rule
Part 135: Air Taxi & Commuter
Purpose of flight
Other Work Use
Phase of flight
Not recorded
Route
Wasilla → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR21FA143

People

5 people died.

On board Died Serious Minor Uninjured
6 5 1 0 0

Probable cause

The pilot’s failure to adequately respond to an encounter with whiteout conditions, which resulted in the helicopter’s collision with terrain. Contributing to the accident was the (1) operator’s inadequate pilot training program and pilot competency checks, which failed to evaluate pilot skill during an encounter with inadvertent instrument meteorological conditions, and (2) the Federal Aviation Administration principal operations inspector’s insufficient oversight of the operator, including their approval of the operator’s pilot training program without ensuring that it met requirements. Contributing to the severity of the surviving passenger’s injuries was the delayed notification of search and rescue organizations.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

A local lodge had contracted with the helicopter operator to transport passengers from a private residence to a heli-ski area at a nearby mountain. The surviving passenger stated that, before the last ski run of the day, the pilot attempted to land on a ridgeline but that the helicopter lifted off for an attempted second landing. The passenger also stated that, during the second landing attempt, the snow was “real light” but that the helicopter became “engulfed in a fog which made it appear like a little white room.” The helicopter subsequently began “going backward real fast” and impacted the ridgeline and rolled backward down the mountain. Postaccident examination of the airframe and engine revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation of the helicopter. The passenger’s recollection of the conditions just before the accident was consistent with whiteout conditions caused by rotor wash while the helicopter was hovering near the ridgeline. Thus, the pilot likely experienced whiteout conditions during the second landing attempt, which caused him to lose visual reference with the ridgeline and resulted in the helicopter impacting terrain. Title 14 Code of Federal Regulations Part 135 required flight-locating for the helicopter in case it was overdue so that information about the helicopter’s location could be reported to a Federal Aviation Administration (FAA) or a search and rescue facility. The helicopter operator stated that it had delegated the responsibility for flight-locating to the local lodge. However, this delegation was not documented in the company’s FAA operations specifications or general operations manual, as required by Part 135. On the day of the accident, the local lodge was providing flight-following for the accident helicopter, which, unlike flight-locating, was not required by Part 135. The helicopter was expected to depart the heli-ski area for the principal operations base once all the ski runs had been completed. The flight-follower informed his supervisor that 40 minutes had elapsed since the helicopter moved from its last recorded position and that there had been “no positive comms” with the ski guide during the last 1.5 hours; this notification was made 41 minutes after the last “ping” from the helicopter. However, the remote area in which the accident flight was operating had limited communication capabilities, and no clear evidence indicated that an accident had occurred. The flight-follower’s supervisor contacted another heli-ski company to help determine the status of the helicopter. The heli-ski company considered the flight to be “ops normal” and expected that the last lift would occur shortly. The supervisor instructed the flight-follower to “keep an eye on” the accident helicopter; however, the lodge’s emergency response plan stated that a search and rescue facility should be contacted “if communication with the helicopter is not established by the end of the prearranged [time] or 30-minute grace period.” Therefore, it would have been reasonable for the lodge to activate its emergency response plan at this point given that the helicopter’s location was unknown at the time. The flight-follower continued to try to reach the helicopter but was unsuccessful. About 90 minutes after the last flight-following “ping” for the helicopter, the lodge received erroneous information from the heli-ski operator that the accident helicopter was “inbound” for the private residence; however, lodge personnel did not realize that this information was not accurate and that the accident had occurred immediately after the last ping. This incorrect information likely played a role in the lodge’s further delay in activating its emergency response plan. About 1 hour and 50 minutes after the accident (and the last flight-following ping), the heli-ski operator notified the accident helicopter operator about the overdue aircraft. Five minutes later, the lodge notified the helicopter operator that it was activating its emergency response plan. About 2 hours after the accident occurred, the helicopter operator activated its emergency response plan. About 17 minutes later, the helicopter operator notified the Alaska Rescue Coordination Center. The director of operations for the helicopter operator stated that the search and rescue notification did not occur before that time because he had been “working through the information that was provided” about the helicopter. The helicopter wreckage was located about 3.5 hours after the accident. Rescue personnel launched within 1 hour of notification and arrived on scene less than 30 minutes later (about 5 hours 40 minutes after the accident). The surviving passenger was transported via helicopter to a local hospital. Upon arrival at the hospital, the surviving passenger had hypothermia and severe frostbite. A shorter exposure to the cold would likely have decreased the severity of the surviving passenger’s injuries. However, a faster emergency response time (and thus shorter exposure to the cold) could only have occurred if the notification to search and rescue personnel had been timelier. Thus, because the lodge and the helicopter operator did not activate their emergency response plans sooner, the initiation of search and rescue operations was delayed. Given the circumstances of this accident, the investigation considered three types of training that the pilot should have received: inadvertent instrument meteorological conditions (IIMC) training; controlled flight into terrain-avoidance (CFIT-A) training, during which instruction in whiteout conditions would be conducted; and ridgeline training. Review of the operator’s pilot training program showed that ridgeline training was not provided for the make and model of the accident helicopter (or the previous helicopter in which the accident pilot had been trained). Further, IIMC training was a part of CFIT-A training, and the CFIT-A manual stated that pilots were required to complete IIMC training annually. However, the chief pilot for the helicopter operator stated that the related test for pilots (to demonstrate understanding of the subject) was only administered when a pilot was first hired, and the director of operations stated that the company’s only IIMC flight training involved recovery from unusual attitudes. In addition, review of the accident pilot’s flight training records found that he completed IIMC training 14 months before the accident (which was about 1 year after he began working for the operator), but the records did not reflect the specific IIMC training that the pilot received. Based upon the information provided by the operator, it could not be determined if the accident pilot had fulfilled the training requirement. The director of operations reported that the helicopter operator did not accomplish flight training as part of its CFIT-A training; however, flight training was not required for that subject, and the pilot received CFIT-A ground training. The CFIT-A manual stated that, if inadvertent whiteout conditions were encountered, the pilot was to rely on flight instruments and carefully attempt to maneuver the helicopter away from obstacles and terrain. Additional review of training records revealed that, during competency checks, the helicopter operator was not evaluating several requirements of 14 CFR 135.293, including recovery from IIMC, navigation, air traffic control communication, and instrument approach flying. Paragraph (c) of the regulation required a pilot to demonstrate the ability to maneuver the helicopter into visual meteorological conditions after a simulated encounter with IIMC, a skill that was needed during the accident flight. The operator stated that it did not have any instrument-flight-rules (IFR) aircraft capable of IFR approaches, but the GPS model installed on the accident helicopter had IFR capabilities with instrument approach procedures in its database. Thus, given the deficiencies in the operator’s pilot training program and Part 135 checkrides, particularly regarding IIMC, it is likely that the pilot did not meet the qualification standards to be the pilot in-command of the accident flight. The FAA principal operations inspector (POI) for the operator failed to ensure that the company’s operations specifications (specifically, paragraph A008) contained the operational control information required by 14 CFR 119.7 and 135.77. (Flight-locating was part of operational control.) The company’s operations specifications did not describe who would be responsible for the safe operation of company flights and how those flights would be operated to meet requirements; thus, the operations specifications were incomplete. Although the company should have noticed this omission before the operational specifications were signed, the POI was ultimately responsible for ensuring that the operations specifications contained all the required information. FAA Order 8900.1, paragraph 3-1255, discusses helicopter flight training maneuvers that “must be conducted for satisfactory completion of each category of flight training.” The order also stated that all helicopter pilots operating under Part 135 “must be trained on procedures for the avoidance and recovery from IIMC” and that inspectors were required to ensure that operational procedures for recovery from IIMC are incorporated into the certificate holder’s training curriculums. Thus, the POI failed to ensure that the operator’s training program contained all required elements, which also included ridgeline training, before approving the training program. In addition, the POI was also unaware that the operator was not conducting competency checks in accordance with section 135.293(c) and that its checkrides were only assessing a pilot’s recovery from unusual attitudes. From 2011 to 2013, the POI was the chief pilot for the accident operator; from 2001 to 2011, she worked at another helicopter company with the person who later became the president of the accident operator. The POI started her employment with the FAA in 2016 and, 2 years later, became the POI for the accident operator. The available evidence for this investigation was insufficient to determine whether the POI’s previous employment history was a factor in the inadequate oversight of the accident operator. Toxicology testing of specimens from the senior lead ski guide identified two central nervous system stimulant drugs: amphetamine and cocaine. Given the drug levels measured in his blood, the senior lead ski guide was likely impaired by drug effects at the time of the accident. Toxicology testing of specimens from the other lead ski guide identified delta-9-tetrahydrocannabinol (THC), the primary psychoactive component in cannabis. The low THC level measured in his blood indicates that he was not likely experiencing significant impairment from THC effects at the time of the accident. Although ski guides are not considered crewmembers according to the Federal Aviation Regulations, they have safety-related responsibilities during heli-ski flights such as coordinating with pilots about landing and pickup zones and assisting pilots with hazard and pickup zone identification. However, the investigation was unable to determine whether the senior lead guide’s illicit drug use played a role in the accident.

Quoted verbatim from the NTSB record.

Other Airbus Helicopters AS350 accidents

Date Aircraft Location Operator Outcome Died
3 May 2020 Airbus Helicopters AS350
N1WT
Clewiston, Florida, United States MacNeil Aviation LLC No injuries -
7 Aug 2024 Airbus Helicopters AS350
9N-AJD
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no coordinates
- Fatal 5
27 Jun 2024 Airbus Helicopters AS350
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28 Jun 2025 Airbus Helicopters AS350
HB-ZNR
Naters, Switzerland
no coordinates
- Fatal 1
16 Dec 2015 Airbus Helicopters AS350
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Superior, Arizona, United States Air Methods Corp Fatal 2

All 6 records for this type

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2 Dec 2021 Cessna 208
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5 Aug 2021 Alaskan Air Adventures SQ2
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13 May 2021 Piper PA-18-105 SPECIAL
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All 170,864 records in United States