ANC17CA041

NTSB accident investigation · Airbus AS350 · Delta Junction, AK · August 3, 2017

Accident · No injuriesData collectionFinal report
Date
August 3, 2017, 13:00 local (22:00 UTC)
Place
Delta Junction, AK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N351SHAirbus AS350
Defining event
Landing: Collision during takeoff/land
Weather
Visual (VMC) · Day
Status
Completed · report September 22, 2017
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Parties
Safran Helicopter Engines (Technical Advisor), FAA Fairbanks FSDO, Bureau d’Enquêtes et d’Analyses, Airbus Helicopters (Technical Advisor)
FAA report
20170803012769A
Case key
95765

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 failure to maintain clearance from a steel frame attached to a tracked drilling unit. Contributing to the accident was the pilot’s failure to visually identify the steel frame during the reconnaissance process.

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.

Object/animal/substance: ground equipmentEnvironmental issues › Physical environment · Effect on operationEurocopter AS 350 B3: 3 casesAll aircraft: 52 casesProbable cause

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 helicopter pilot reported that he was transporting a passenger to a remote drilling site where a tracked drilling unit was stationed. He reported that he landed into the wind, which necessitated descending over bordering trees into the drilling site. The helicopter touched down on the dirt, and upon lowering the collective, he reported that he heard a "bang," and the helicopter slowly started to "pick up a ground wobble." The pilot shut down the helicopter, and both occupants exited without further incident. A postaccident inspection revealed that the blue and red main rotor blades sustained substantial damage from impacting a black 1.5-inch steel frame attached to the tracked drilling unit, which is used to mount a canvas weather shelter for the drilling crews. The pilot reported that the steel frame was not visible to him from above as he was descending into the drilling site. The pilot further reported that he had made multiple landings at the drilling site in the past 3 months and that, with the previous landings, he had landed farther past the tracked drilling unit, and the steel frame was always behind the helicopter. The pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration Helicopter Flying Handbook (FAA-H-8083-21A, 2012) discusses high and low reconnaissance procedures and states, in part: The purpose of conducting a high reconnaissance is to determine direction and speed of the wind, a touchdown point, suitability of the landing area, approach and departure axes, and obstacles for both the approach and departure. A low reconnaissance is accomplished during the approach to the landing area. When flying the approach, verify what was observed in the high reconnaissance, and check for anything new that may have been missed at a higher altitude, such as wires and their supporting structures (poles, towers, etc.), slopes, and small crevices.

Factual narrative

The helicopter pilot reported that he was transporting a passenger to a remote drilling site, where a tracked drilling unit was stationed. He reported that he landed into the wind, which necessitated descending over bordering trees into the drilling site. The helicopter touched down on the dirt, and upon lowering the collective, he reported he heard a "bang" and the helicopter slowly started to "pick up a ground wobble." The pilot shutdown the helicopter and both occupants exited without further incident. A postaccident inspection revealed that the blue and red main rotor blades sustained substantial damage from impacting a black 1.5-inch steel frame attached to the tracked drilling unit, which is used to mount a canvas weather shelter for the drilling crews. The pilot reported that the steel frame was not visible to him from above as he was descending into the drilling site. The pilot further reported that multiple landings have been made to the drilling site in the past 3 months, and that with the previous landings he landed further past the tracked drilling unit and the steel frame was always behind the helicopter. The pilot reported that there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The Federal Aviation Administration Helicopter Flying Handbook (FAA-H-8083-21A, 2012) discusses high and low reconnaissance procedures and states in part: The purpose of conducting a high reconnaissance is to determine direction and speed of the wind, a touchdown point, suitability of the landing area, approach and departure axes, and obstacles for both the approach and departure. A low reconnaissance is accomplished during the approach to the landing area. When flying the approach, verify what was observed in the high reconnaissance, and check for anything new that may have been missed at a higher altitude, such as wires and their supporting structures (poles, towers, etc.), slopes, and small crevices.

Aircraft

Registration
N351SH
Reported as
Airbus AS350 (B3)
Category
Helicopter
Serial number
4598
Built
2008
Airframe hours
3,823.7
Engine
Safran Helicopter Engines Arriel 2B1, 847 horsepower, turbo shaft
Damage
Substantial damage
Flight
Part 135
Operator
Soloy Helicopters, LLC, doing business as Soloy Helicopters, LLC
Registered owner
Wells Fargo Bank Northwest Na Trustee
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · June 19, 2017
Departed
76AK · Delta Junction, AK
Destination
76AK · Delta Junction, AK
Flight plan
Company VFR
Equipment
None

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
64
Injuries
None
Certificate
Commercial
Medical
Class 2, With waivers/limitations
Last flight review
May 12, 2017
Seat
Right
Restraint
4-point
Flight hours
14,998 total · 2,300 in this make and model · 14,800 as pilot in command · 340 in the last 90 days · 167 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 13 knots
Visibility
10 statute miles
Lowest ceiling
11,000 ft broken
Temperature
72 °F, dew point 46 °F
Altimeter
30.12 inHg
Observed at
PABI, 35 nm away

Docket · 2

The files NTSB released with the investigation on August 31, 2017, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 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.

Other investigations on N351SH · 1

Matched to the same aircraft by N-number and date.