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Accidents · NTSB WPR13LA390 · Final report

Bell Helicopter Textron 206L-1 accident near Payson, Arizona, August 28, 2013

On August 28, 2013 at about 5:30 pm local time, a 1981 Bell Helicopter Textron 206L-1, registered N2018R, was substantially damaged in an accident during enroute (cruise) near Payson, Arizona (Payson airport). It was flown under charter and air-taxi rules (Part 135). 1 person was seriously injured; 5 others were unhurt. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A partial loss of engine power due to an overtemperature event that thermally damaged the turbine blades and vanes, which resulted in a hard landing.

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

What the record shows

Date
August 28, 2013 · about 5:30 pm local time
Place
Payson, Arizona · Payson · map
Type
Accident
Injuries
1 person was seriously injured; 5 others were unhurt.
Weather
visual conditions (good weather)
Aircraft
Bell Helicopter Textron 206L-1, built 1981 · all 206L-1s on the register
Registration
N2018R · registry record · serial 45681
Damage
Substantial damage
Flight
Flight · charter and air-taxi rules (Part 135)

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

The pilot reported that the engine lost power while the helicopter was in cruise flight about 1,500 ft above ground level. He subsequently entered an autorotation and performed an emergency off-airport landing. During the descent, he maneuvered the helicopter to avoid obstacles; the helicopter subsequently landed hard, and the tailboom separated. Examination of the engine revealed that the outer portion of the engine's first-stage turbine blades and three vanes from the first-stage nozzle were thermally damaged. The turbine blades' microstructure exhibited signatures consistent with an engine overtemperature event; however, it could not be determined when the overtemperature damage occurred. The postaccident examination of the airframe and engine revealed no additional evidence of a mechanical malfunction that would have precluded normal operation. Weight and balance calculations revealed that, when the helicopter departed, it was over its allowable gross takeoff weight but that it was under its allowable gross operational weight at the time of the engine power loss.

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. Loss of engine power (partial) during enroute (cruise) defining event
  2. Autorotation Loss of engine power (partial)
  3. Hard landing during landing (flare/touchdown)

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Turbine section › Damaged/degraded
  • Personnel issues › Task performance › Planning/preparation › Weight/balance calculations › Pilot

Pilot

  • Certificate: commercial pilot, military
  • Ratings: multi-engine land; single-engine land; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 15,000 hours in all; 5,000 in this make and model; 35.2 in the last 90 days; 17.8 in the last 30 days; 15,000 as pilot in command
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 18,462.6 hours
  • Last inspection: annual inspection, June 10, 2013
  • Maximum gross weight: 4,150 lb
  • Seats: 7
  • Landing gear: fixed
  • Engine: Alllison 250-C30P (turboshaft); 9,426 hours total
  • Operator: Airlift Helicopters INC

The flight

  • Departed from: SDL Scottsdale AZ at 4:10 pm
  • Destination: FLG Flagstaff AZ

Weather at the time

  • Light: daylight
  • Wind: from 080° at 4 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 12,000 ft
  • Temperature: 81°F (27°C), dew point 57°F (14°C)
  • Altimeter: 30.18 inHg
  • Observation at 4:53 pm from PRC, 50 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers5

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.