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Accidents · NTSB CEN14LA441 · Final report

Amateur-built STOL CH 750 accident near Grain Valley, Missouri, August 19, 2014

On August 19, 2014 at about 7:00 pm local time, a 2014 amateur-built STOL CH 750, registered N484XB, was substantially damaged in an accident during takeoff near Grain Valley, Missouri (East Kansas City airport). It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot’s failure to maintain airplane control during a low-speed, high-pitch climb after the airplane experienced a loss of electrical power and subsequent total loss of engine power, which resulted in an aerodynamic stall. Contributing to the accident was the airplane’s modified electrical system and the pilot’s failure to obtain adequate familiarization and experience in the airplane with the recent slat-removed configuration.

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

What the record shows

Date
August 19, 2014 · about 7:00 pm local time
Place
Grain Valley, Missouri · East Kansas City · map
Type
Accident
Injuries
1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Amateur-built STOL CH 750, built 2014
Registration
N484XB · no longer on the register · serial 75-8420
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

Data from the onboard avionics device revealed that, after conducting a touch-and-go landing, the amateur-built airplane immediately began a low-speed, high-pitch-angle climb. The airplane's airspeed began to decrease as the airplane climbed to about 47 ft above ground level and then began rolling left; the recording then ended. Witnesses reported observing the airplane roll, descend, and impact terrain. The data and the witness statements are consistent with the airplane having experienced an aerodynamic stall. A postaccident examination of the composite propeller found that it did not display signatures of rotation during impact, consistent with a total loss of engine power. The engine manufacturer's initial installation used a single battery with a series of breakers and relays to provide power to the engine components and other equipment. This design was subsequently replaced by a dual-battery design that incorporated a simpler wiring harness. The airplane was originally wired for a single-battery operation, and a second battery was subsequently added. However, the simpler wiring harness was not used; instead the electrical path from the alternator to the alternator sense wire used a complex series of fuses to provide power to the components; one of these fuses was found open, which is indicative of an electrical power failure and would have led to the loss of engine power. Although the onboard avionics device did not record the airplane's loss of engine power, descent, or impact with terrain, the interruption of the recorded data likely resulted from the electrical failure. The pilot had removed the airplane's slats 9 days before the accident; the accident flight was the pilot's first flight in the airplane with the new configuration. According to the kit designer, the airplane was not designed to fly with the slats removed because it would result in a higher stall speed with a distinct stall break and roll if the flight was not coordinated. In addition, the pilot had recently resumed flying after not having flown in about 45 years. Although he had received 2 hours of dual instruction about 2 months before the accident, after a test flight in a company airplane, another pilot assessed the accident pilot's piloting skills as poor and advised him to obtain further instruction; however, the accident pilot did not do so. Given his lack of recent flight experience, he was likely not properly prepared for how to respond to a loss of engine power and the subsequent 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. Electrical system malf/failure during takeoff
  2. Loss of engine power (total) during takeoff
  3. Aerodynamic stall/spin during takeoff defining event
  4. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • factor Personnel issues › Experience/knowledge › Training › Recent instruct/training recvd › Pilot
  • factor Personnel issues › Experience/knowledge › Knowledge › Knowledge of equipment › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
  • factor Aircraft › Aircraft systems › Electrical power system › Electrical pwr sys wiring › Incorrect service/maintenance
  • cause Aircraft › Aircraft systems › Electrical power system › Electrical pwr sys wiring › Failure

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 204.5 hours in all; 5 in this make and model; 5 in the last 90 days; 5 in the last 30 days
  • Medical certificate: Sport Pilot
  • Seat: left
  • Injury: serious injuries

The aircraft

  • Airframe total time: 0 hours
  • Last inspection: condition inspection, June 21, 2014; 5 hours since
  • Maximum gross weight: 1,320 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Viking 110 (piston); 0 hours total

The flight

  • Departed from: 3GV Grain Valley MO at 5:30 pm
  • Destination: 3GV Grain Valley MO
  • Flight plan: none
  • Runway 27, 4,507 ft by 44 ft

Weather at the time

  • Light: daylight
  • Wind: from 220° at 7 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 88°F (31°C), dew point 72°F (22°C)
  • Altimeter: 29.84 inHg
  • Observation at 6:53 pm from KLXT, 8 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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.