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Accidents · NTSB ANC14FA022 · Final report

Cessna 208B accident near Kwethluk, Alaska, April 8, 2014

On April 8, 2014 at about 11:57 pm local time, a 2002 Cessna 208B, registered N126AR, was destroyed in an accident during maneuvering near Kwethluk, Alaska. It was an instructional flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The check airman's delayed remedial action and initiation of a recovery procedure after a simulated pitch trim excursion, which resulted in a loss of airplane control.

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

What the record shows

Date
April 8, 2014 · about 11:57 pm local time
Place
Kwethluk, Alaska · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Cessna 208B, built 2002 · all 208Bs on the register
Registration
N126AR · no longer on the register · serial 208B1004
Damage
Destroyed
Flight
Instructional flight · general aviation rules (Part 91)

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

The check airman was conducting the first company training flight for the newly hired second-in-command (SIC). Automatic Dependent Surveillance-Broadcast (ADS-B) data showed that, after departure, the airplane began a series of training maneuvers, consistent with normal operations. About 21 minutes into the flight, when the airplane was about 3,400 ft mean sea level, it began a steep descent and subsequently impacted terrain. An airplane performance study showed that the airplane reached a nose-down pitch of about -40 degrees and that the descent rate reached about 16,000 ft per minute. Numerous previous training flights conducted by the check airman were reviewed using archived ADS-B data and interviews with other pilots. The review revealed that the initial upset occurred during a point in the training when the check airman typically simulated an in-flight emergency and descent. Postaccident examination for the airframe and control surfaces showed that the airplane was configured for cruise flight at the time of the initial upset. Examination of the primary and secondary flight control cables indicated that the cables were all intact at the time of impact. Trim actuator measurements showed an abnormal trailing-edge-up, nose-down configuration on both trim tabs. The two elevator trim actuator measurements were inconsistent with each other, indicating that one of the actuators was likely moved during the wreckage recovery. Based on the supporting data, it is likely that one of the actuators indicated the correct trim tab position at the time of impact. Simulated airplane performance calculations showed that, during a pitch trim excursion, the control forces required to counter an anomaly increases to unmanageable levels unless the appropriate remedial procedures are quickly applied. Given the simulated airplane performance calculations, the trim actuator measurements, and the check airman's known training routine, it is likely that the check airman simulated a pitch trim excursion and that the SIC, who lacked experience in the airplane type, did not appropriately respond to the excursion. The check airman did not take remedial action and initiate the recovery procedure in time to prevent the control forces from becoming unmanageable and to ensure that recovery from the associated dive was possible.

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. Inflight upset during maneuvering
  2. Loss of control in flight during maneuvering defining event

The NTSB's findings

  • cause Personnel issues › Action/decision › Info processing/decision › Identification/recognition › Instructor/check pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Instructor/check pilot
  • cause Personnel issues › Action/decision › Action › Delayed action › Instructor/check pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained
  • Aircraft › Aircraft structures › Wing structure › Trailing edge flaps › Not specified

Pilot (unmanned)

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 14,417 hours in all; 5,895 in this make and model; 376 in the last 90 days; 159 in the last 30 days
  • Last flight review: March 15, 2014
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: airplane
  • Flight time: 593 hours in all; 1 in this make and model; 1 in the last 90 days; 1 in the last 30 days; 482 as pilot in command
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 11,206 hours
  • Last inspection: approved inspection programme, March 13, 2014; 85 hours since
  • Maximum gross weight: 7,449 lb
  • Seats: 9
  • Landing gear: fixed
  • Engine: P&W PT6A 114A (turboprop); 7,421 hours total
  • Fire on the ground
  • Operator: Hageland Aviation

The flight

  • Departed from: BET Bethel AK
  • Destination: BET Bethel AK
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 020° at 8 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 19°F (-7°C), dew point 3°F (-16°C)
  • Altimeter: 29.87 inHg
  • Observation at 11:53 pm from PABE, 27 miles away

Injuries

FatalSeriousMinorNone
Flight crew2

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.