CEN09LA388

NTSB accident investigation · Beech B100 · Rapid City, SD · June 15, 2009

Accident · Serious injuriesLimited investigationFinal report
Date
June 15, 2009, 16:52 local (22:52 UTC)
Place
Rapid City, SD
Injuries
1 serious, 4 minor
Damage
No damage
Phase of flight
Enroute
Aircraft
N4490MBeech B100
Defining event
Enroute-descent: Clear air turbulence encounter
Weather
Visual (VMC) · Day
Status
Completed · report December 20, 2010
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration - Rapid City FSDO
Case key
74135

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The flight crewmembers’ failure to secure the patient using the available over-the-shoulder restraints and the encounter with clear-air turbulence during cruise descent.

Findings · 3

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.

Equipment/furnishings: passenger compartment equipAircraft › Aircraft systems · Incorrect use/operationBeech B100: 1 caseAll aircraft: 24 casesProbable cause
Use of equip/info: use of equip/systemPersonnel issues › Task performance · Flight crewBeech B100: 1 caseAll aircraft: 1,391 casesProbable cause
Turbulence: clear air turbulenceEnvironmental issues › Conditions/weather/phenomena · Effect on personnelBeech B100: 1 caseAll aircraft: 78 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 air-ambulance flight encountered clear-air turbulence during cruise descent. During the turbulence encounter, the patient’s unrestrained upper-torso fell off the aircraft mounted stretcher assembly. After the turbulence had subsided, the patient’s unrestrained head, neck, and upper-torso were laying off the stretcher in the center aisle. His restrained lower body remained attached to the stretcher which was elevated off the cabin floor. The cabin flight crewmembers stabilized the patient’s neck before repositioning him back onto the stretcher. The airplane then made an uneventful landing at its intended destination. The patient suffered a fracture of the C3 cervical vertebra during the turbulence encounter. The stretcher’s available over-the-shoulder restraints were not used because of an interference caused by a flexible lift system that was used to transfer the patient from the ambulance gurney to the aircraft’s stretcher. After the accident the aeromedical transport company discontinued the use of the flexible patient lift system model used during the accident flight and required flight crewmembers to only use lift systems that allowed the use of the aircraft stretcher’s available over-the-shoulder restraints.

Factual narrative

On June 15, 2009, about 1652 mountain daylight time (mdt), a Beech B100 (King Air) airplane, N4490M, operated by Air Methods Corporation, encountered clear-air-turbulence while descending through 7,000 feet mean sea level (msl) en route to Rapid City Regional Airport (KRAP), Rapid City, South Dakota. Visual meteorological conditions prevailed during the flight. The air-ambulance flight was conducted in accordance with 14 Code of Federal Regulations (CFR) Part 135 while on an instrument flight plan. The patient was seriously injured as result of the turbulence encounter. The 4 flight crew members sustained minor injuries. The flight departed Gordon Municipal Airport (KGRN), Gordon, Nebraska, at 1619 mdt. Before being loaded onto the airplane, the patient was lying on an ambulance gurney and was already secured to a flexible lift system at the waist and legs. The use of the flexible lift system allowed the easy transfer from the ambulance gurney to the aircraft-mounted stretcher assembly. The lift system comprised of a plasticized sheet and full body length foam pad. The patient was secured to this lift system using the available waist and leg straps. For patient transfers, flight crewmembers grab the edges of the flexible lift system to lift and transfer the patient from the ambulance gurney to the airplane’s stretcher. The airplane’s stretcher also incorporated a full body pad, and its support frame articulated at the waist to elevate the patient’s upper body from a supine position into an inclined position. The airplane’s stretcher had leg, waist, and left and right over-the-shoulder straps. The over-the-shoulder straps combined at the waist strap buckle assembly. The patient, who was already restrained in the flexible lift system by waist and leg straps, was then restrained to the airplane’s stretcher using the stretcher’s available waist and leg straps. The full body pad and plasticized sheet of the flexible lift system completely covered and prevented the use of the over-the-shoulder restraints installed on the airplane’s stretcher. During the flight, the stretcher’s back support was raised into an inclined position for added patient comfort. During cruise descent, the airplane encountered clear-air-turbulence, during which the patient’s upper-torso fell off the stretcher. After the turbulence encounter, the patient’s unrestrained head, neck, and upper-torso were laying off the stretcher in the center aisle. His restrained lower body remained attached to the stretcher which was elevated off the cabin floor. The cabin flight crewmembers stabilized the patient’s neck before repositioning him back onto the stretcher. The airplane then made an uneventful landing at its intended destination. The patient suffered a fracture of the C3 cervical vertebra during the turbulence encounter. After the accident, the aeromedical transport company discontinued the use of the flexible patient lift system model utilized during the accident flight and requiredflight crewmembers to only use lift systems that allowed the use of the aircraft stretcher’s available over-the-shoulder restraints.

Aircraft

Registration
N4490M
Reported as
Beech B100
Category
Airplane
Serial number
BE-64
Airframe hours
9,898
Engines
Garrett Airesearch TPE-331, 1,428 horsepower, turbo propGarrett Airesearch TPE-331, 1,428 horsepower, turbo prop
Damage
No damage
Flight
Part 135
Operator
Air Methods Corporation, doing business as Black Hills Life Flight
Registered owner
Vesey Air, LLC.
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · May 12, 2009
Departed
KGRN · Gordon, NE
Destination
KRAP · Rapid City, SD
Flight plan
IFR

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
34
Injuries
Minor
Certificates
Flight instructor, Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
May 7, 2009
Seat
Left
Flight hours
3,305 total · 516 in this make and model · 3,150 as pilot in command · 40 in the last 90 days · 1 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
66 °F, dew point 50 °F
Altimeter
29.73 inHg
Observed at
KRAP, 10 nm away

Docket · 8

The files NTSB released with the investigation on August 18, 2010, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 MB in all.