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Accidents · NTSB ERA23FA194 · Final report

Amateur-built VELOCITY accident near Andrews, North Carolina, April 15, 2023

On April 15, 2023 at about 2:39 pm local time, a 1996 amateur-built VELOCITY, registered N2357, was destroyed in an accident during initial climb near Andrews, North Carolina (Western Carolina Regional Airp airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s failure to engage the turbocharger for takeoff and his improper decision to continue the takeoff with partial power, rather than reject the takeoff.

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

What the record shows

Date
April 15, 2023 · about 2:39 pm local time
Place
Andrews, North Carolina · Western Carolina Regional Airp · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built VELOCITY, built 1996
Registration
N2357 · no longer on the register · serial FGA-001
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The owner recently purchased the experimental amateur-built, modified airplane. He did not have a lot of experience in the make and model airplane, so he hired the accident pilot to conduct the first flight since recent modifications. Witness statements and recorded video showed that during the takeoff roll from the 5,500-ft-long asphalt runway, the airplane accelerated slower than normal, used more runway than normal, and lifted off the runway in a nose-high attitude. The airplane then descended back to the runway and bounced before lifting off nose-high again toward the end of the runway. It climbed about 300 ft above ground level while flying a left traffic pattern back to the runway. Near the crosswind to downwind turn, the engine sounded loud, and the airplane descended into a wooded field and a postimpact fire ensued. The owner stated that the engine was equipped with a fixed-pitch cruise propeller. With the turbocharger engaged, the engine would produce 2,300 rpm; however, with the turbocharger bypassed, the engine would only produce about 2,050 rpm. A spring switch in the cockpit controlled the turbocharger wastegate, to select whether the turbocharger was engaged or bypassed (or midrange). The owner added that, at 2,050 rpm, the airplane would not be able to fly with one pilot and full fuel, which it had for the accident takeoff. The owner reported that he discussed the turbocharger operation with the pilot. Examination of the wreckage revealed that the turbocharger wastegate was found in an open position. No other anomalies were noted that would have precluded normal operation. It is likely that the pilot had inadvertently bypassed the turbocharger and then attempted to continue the takeoff with the with the engine only developing partial power. His decision to continue, rather than reject the takeoff, resulted in the airplane’s subsequent powered descent and collision with terrain.

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 initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  3. Aerodynamic stall/spin during initial climb
  4. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • Personnel issues › Task performance › Use of equip/info › Use of equip/system › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
  • Aircraft › Aircraft power plant › Turbocharging (recip only) › Turbocharger › Incorrect use/operation

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; instructor: helicopter; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 450 hours in all
  • Medical certificate: Class 1
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 197 hours
  • Last inspection: condition inspection, March 31, 2023; 0 hours since
  • Maximum gross weight: 2,300 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming IO-360-A1D (piston); 0 hours total
  • Fire on the ground

The flight

  • Flight plan: none
  • Runway 26, 5,500 ft by 100 ft

Weather at the time

  • Light: daylight
  • Wind: from 260° at 6 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 2,900 ft; scat at 1,200 ft
  • Temperature: 63°F (17°C), dew point 54°F (12°C)
  • Altimeter: 30.05 inHg
  • Observation at 10:39 am from RHP, 1 miles away

Weather report (METAR): KRHP 151429Z AUTO 26006KT 10SM SCT012 BKN029 OVC034 17/12 A3005

Injuries

FatalSeriousMinorNone
Flight crew1

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

11 documents, released by the NTSB on June 5, 2024. 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.

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.