The U.S. aircraft register, updated daily
Accidents · NTSB ANC19LA031 · Final report

Cessna 208 accident near Bethel, Alaska, July 8, 2019

On July 8, 2019 at about 11:05 pm local time, a 1988 Cessna 208, registered N9448B, was destroyed in an accident during approach (VFR go-around) near Bethel, Alaska (Bethel airport). It was flown under charter and air-taxi rules (Part 135). 6 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s failure to maintain adequate airspeed while maneuvering during an attempted go-around, which resulted in an exceedance of the airplane's critical angle of attack and an aerodynamic stall at low altitude. Contributing to the accident, was the pilot’s decision to perform an approach to a short runway at an excessive airspeed and his late decision to perform a go-around, which resulted in a slow climb at a reduced safe margin above stall airspeed.

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

What the record shows

Date
July 8, 2019 · about 11:05 pm local time
Place
Bethel, Alaska · Bethel · map
Type
Accident
Injuries
6 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Cessna 208 B, built 1988 · all 208s on the register
Registration
N9448B · no longer on the register · serial 208B0121
Damage
Destroyed
Flight
Flight · charter and air-taxi rules (Part 135)

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

The commercial pilot was conducting a visual flight rules scheduled passenger flight with five passengers. During the return leg to the company’s base airport, the pilot requested, and was given clearance to, a short gravel runway of 1,858 ft that terminated at parallel cross-runways and had inbound airplanes. The wind was reported as variable at 3 knots, and the outside air temperature was 88°F which was 25° warmer than usual. The pilot stated that he conducted a steeper than normal approach and performed a normal 30° flap landing flare; however, the airplane floated halfway down the runway. He initiated a go-around by advancing the throttle to takeoff power and retracting the flaps to 20° as the main landing gear briefly touched down. Automatic dependent surveillance-broadcast (ADS-B) data indicated that the airplane arrived 0.1 mile from the runway threshold at 149 ft above ground level (agl) and 110 knots of ground speed, which was 32 knots faster than the short field landing approach speed listed in the pilot operating handbook. A witness in the air traffic control tower (the ground controller) stated that the airplane “bled off a lot of airspeed,” during the landing attempt and climbed out in a very flat profile. The tower local controller stated that after liftoff, the airplane’s right wing dropped and the airplane appeared to be turning right into conflicting landing traffic, so he twice instructed the airplane to “left turn out immediately.” The pilot stated that he attempted to comply with the tower controller’s instruction, but when he applied left aileron, the airplane appeared to stall, rolled rapidly right, and descended in a right-wing-low attitude. It subsequently impacted the surface between runways. A postimpact fire ensued, and the pilot helped the passengers egress. The airplane was destroyed by postimpact fire. Given the evidence, it is likely that the pilot decided to land on the short runway to expedite the arrival and did not perform an appropriate short field landing approach, which resulted in excessive airspeed and altitude over the runway threshold, a long landing flare, rapid deceleration, and a self-initiated go-around from a slow airspeed. Had the pilot initiated the go-around as he approached the runway with indications of an unstable visual approach, the airspeed would have been well above stall speed, which would have allowed for the desired positive climb out on runway heading. The pilot likely attempted to comply with the tower local controller’s urgent commands to turn while the airplane was near the limit of performance (the temperature was about 25 degrees warmer than average, which would have resulted in a higher density altitude than the pilot was accustomed to and degraded aircraft and engine performance). The pilot’s maneuvering resulted in the exceedance of the critical angle-of-attack of the high wing (right wing) during the left turn, and an aerodynamic stall.

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. Collision during takeoff/land during approach (VFR go-around)
  2. Loss of control in flight during approach (VFR go-around) defining event
  3. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 2,258 hours in all; 787 in this make and model; 179 in the last 90 days; 40 in the last 30 days; 2,059 as pilot in command
  • Last flight review: February 7, 2019
  • Medical certificate: Class 1 (with waivers/limitations)
  • Seat: left
  • Injury: minor injuries

Passenger

  • Seat: unk
  • Injury: minor injuries

Passenger

  • Seat: unk
  • Injury: minor injuries

Passenger

  • Seat: unk
  • Injury: minor injuries

Passenger

  • Seat: unk
  • Injury: minor injuries

Passenger

  • Seat: unk
  • Injury: minor injuries

The aircraft

  • Airframe total time: 21,206.5 hours
  • Last inspection: approved inspection programme, June 17, 2019
  • Maximum gross weight: 8,752 lb
  • Seats: 9
  • Landing gear: fixed
  • Engine: Pratt And Whitney PT-6A (turboprop); 0 hours total
  • Fire on the ground
  • Operator: Grant Aviation INC

The flight

  • Departed from: EWU Newtok AK
  • Destination: BET Bethel AK
  • Runway 12, 1,858 ft by 75 ft

Weather at the time

  • Light: daylight
  • Visibility: 3 statute miles
  • Sky: clear
  • Temperature: 88°F (31°C), dew point 66°F (19°C)
  • Altimeter: 29.84 inHg
  • Observation at 10:53 pm from PABE

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers5

Documents from the investigation the NTSB's docket: the evidence folder behind the report

10 documents, released by the NTSB on November 4, 2021. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Other NTSB records under N9448B the same tail number, which may have belonged to a different aircraft at the time

1995-03-02FTW95FA129 · accident near Ardmore, OK · substantial damage · minor injuries

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.