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Accidents · NTSB WPR13LA210 · Final report

Piper PA46-500TP accident near Bryce, Utah, April 29, 2013

On April 29, 2013 at about 1:59 am local time, a 2013 Piper PA46-500TP, registered N2589U, was substantially damaged in an accident during takeoff near Bryce, Utah (Bryce Canyon airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 6 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to establish the minimum liftoff speed during takeoff with the airplane over its maximum gross weight, which resulted in the airplane’s failure to climb and a subsequent loss of directional control and a runway excursion.

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

What the record shows

Date
April 29, 2013 · about 1:59 am local time
Place
Bryce, Utah · Bryce Canyon · map
Type
Accident
Injuries
No one was hurt; 6 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Piper PA46-500TP, built 2013 · all PA46-500TPs on the register
Registration
N2589U · no longer on the register · serial 4697513
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot reported that, during the takeoff roll, as the airplane was about 80 knots indicated airspeed (KIAS) and as he was pulling the control yoke back per his normal practice, the airplane lifted off the runway, but it would not climb higher than about 10 to 20 ft above ground level. He further reported that the takeoff rotation occurred about 3,100 ft down the 7,395-ft-long runway, that the airplane's nose rose to a higher pitch attitude than expected, and that the tail felt heavy or "squishy." The pilot reduced the throttle setting to lower the airplane's nose, but the airplane entered a left yaw with the left wing down. The pilot reapplied full throttle, but the airplane rolled slightly left. At this point, the airplane was over the dirt area between the main runway and the adjacent taxiway. The pilot suspected that the main landing gear dragged at different points with the airplane's nose still in a high-pitch attitude. The fuselage struck the ground, and the airplane subsequently slid to a stop. A postaccident examination of the airframe and engine revealed no anomalies that would have precluded normal operation. According to the Pilot's Operating Handbook, given the reported meteorological conditions at the time of takeoff, the airplane's normal rotation speed would have been 82 KIAS for a 0-degree flap configuration at the maximum gross weight of 5,092 lbs, and the liftoff speed would have been 85 KIAS; the airplane's computed gross weight at the time of the accident was 5,218 lbs. In addition, the normal takeoff ground roll would have been 3,150 ft, and 4,800 ft would have been required to clear a 50-ft obstacle. Based on the evidence, it is likely that the pilot rotated the airplane at a slower airspeed than the published normal rotation speed with the airplane over its maximum gross weight limit and that the airplane was unable to climb after liftoff. The airplane's high-pitch attitude also likely prevented it from accelerating once the airplane lifted off.

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 control in flight during takeoff
  2. Runway excursion during takeoff defining event

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Directional control › Not attained/maintained
  • cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Not specified

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 417 hours in all; 99 in this make and model
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 66 hours
  • Maximum gross weight: 5,092 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: P&W Canada PT6A-42A (turboprop); 66 hours total

The flight

  • Departed from: BCE Bryce UT at 1:59 am
  • Destination: 36U Heber City UT
  • Flight plan: none
  • Runway 03, 7,395 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 300° at 7 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 63°F (17°C), dew point 16°F (-9°C)
  • Altimeter: 30.12 inHg
  • Observation at 1:53 am from KBCE

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.