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Accidents · NTSB WPR15FA163 · Final report

Amateur-built 114 accident near Laughlin, Nevada, May 18, 2015

On May 18, 2015 at about 1:00 am local time, a 1976 amateur-built 114, registered N4775W, was destroyed in an accident during initial climb near Laughlin, Nevada (Laughlin/Bullhead Intl airport). It was a personal flight under general aviation rules (Part 91). 3 people were killed and 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A partial loss of engine power due to the turbocharger's seizure as a result of a severely worn turbowheel. Contributing to the accident was the failure of the pilot/owner to have the turbo normalization system inspected every 100 hours as required, which allowed erosion on the exhaust side of the turbowheel to go undetected.

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

What the record shows

Date
May 18, 2015 · about 1:00 am local time
Place
Laughlin, Nevada · Laughlin/Bullhead Intl · map
Type
Accident
Injuries
3 people were killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Amateur-built 114 B, built 1976
Registration
N4775W · no longer on the register · serial 14105
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The private pilot/owner reported that, during the climb to between about 300 and 400 ft above the ground, the engine started running roughly, and the airplane was not accelerating or climbing. The terrain ahead was rising, so the pilot turned right. Due to the low altitude and reduced engine power, the pilot chose to conduct an off-airport landing, during which he attempted to troubleshoot the engine issue without success. As the airplane continued to descend, the pilot saw houses and bushes ahead; he aimed the airplane away from the houses, and the airplane eventually hit trees and terrain about 4.6 nautical miles from the airport. A postimpact engine fire ensued. Postaccident examination of the engine revealed that the turbocharger was seized and that the exhaust side of the turbowheel was severely eroded, which led to the engine running rough. A review of the airplane's maintenance records revealed that a turbocharger normalization system had been installed on the airplane under a supplemental type certificate (STC) 13 years before the accident. The STC's instructions for continued airworthiness required that the turbocharger normalization system be inspected every 100 hours. However, a review of the airplane's maintenance records revealed that the system had only been inspected once since its installation and that the inspection was completed 6 years before the accident. No other abnormalities were noted with the airframe or engine that would have precluded normal operation. It is likely that the eroded turbowheel would have been detected if the turbocharger normalization system had been inspected as required.

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 initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent

The NTSB's findings

  • factor Personnel issues › Task performance › Inspection › Scheduled/routine inspection › Maintenance personnel
  • cause Aircraft › Aircraft power plant › Turbocharging (recip only) › Turbocharger › Fatigue/wear/corrosion
  • Environmental issues › Physical environment › Terrain › Rough terrain › Contributed to outcome

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 2,069 hours in all; 9 in the last 90 days; 2.2 in the last 30 days; 1,920 as pilot in command
  • Last flight review: July 12, 2013
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: serious injuries

Passenger

  • Seat: rgt
  • Injury: fatal

Passenger

  • Seat: rear
  • Injury: fatal

Passenger

  • Seat: rear
  • Injury: fatal

The aircraft

  • Airframe total time: 3,436.5 hours
  • Last inspection: 100-hour inspection, October 28, 2014; 20 hours since
  • Maximum gross weight: 3,250 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Lycoming IO-540-T4A5D (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: IFP Bullhead City AZ
  • Destination: GYR Goodyear AZ
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 170° at 13 knots, gusting 21
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 84°F (29°C), dew point 28°F (-2°C)
  • Altimeter: 29.85 inHg

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers3

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.