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Accidents · NTSB ERA14LA161 · Final report

Cessna Aircraft CO LC41-550FG accident near Palatka, Florida, March 21, 2014

On March 21, 2014 at about 2:50 pm local time, a 2008 Cessna Aircraft CO LC41-550FG, registered N717RR, was substantially damaged in an accident during approach (VFR go-around) near Palatka, Florida (Palatka Municipal airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed and 1 person was seriously injured. The weather was visual conditions (good weather).

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The NTSB's probable cause their words, unchanged

The pilot’s improper management of the fuel mixture and his failure to use the appropriate checklist and guidance during the flight, which resulted in an overrich mixture condition, carbon-fouling of the spark plugs, and a subsequent total loss of engine power during an attempted go-around.

Source: NTSB aviation accident database, copy made October 4, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 21, 2014 · about 2:50 pm local time
Place
Palatka, Florida · Palatka Municipal · map
Type
Accident
Injuries
1 person was killed and 1 person was seriously injured.
Weather
visual conditions (good weather)
Aircraft
Cessna Aircraft CO LC41-550FG, built 2008
Registration
N717RR · no longer on the register · serial 411012
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The private pilot reported that, after departure, he and his pilot-rated passenger flew to a different airport to practice touch-and-go landings. He initially climbed the airplane to 2,500 ft above mean sea level (msl), but due to clouds, he descended to 1,400 ft msl. Upon arriving in the airport area, he descended to 1,200 ft msl and entered and then extended the downwind leg of the traffic pattern due to another airplane passing him. When the airplane entered the left base leg, the pilot determined that the airplane was "high," so he decided to conduct a "low approach" instead of a touch-and-go landing. He then set 12 inches of manifold pressure (mp). When the airplane had descended to about 400 ft msl, he decided to go around and "screwed the throttle in," but the engine did not respond. He then pitched the nose down to achieve the best glide airspeed and attempted to land straight ahead. The pilot stated that, at this point, the engine was still indicating 12 inches mp, and the propeller appeared to be "windmilling." He then pitched up to clear trees ahead and tried to land on a retention pond. The airplane then touched down on the water, skipped twice, slid up onto an embankment, struck a chain link fence and stacks of wooden shipping pallets, and came to rest. Examination of the airplane and engine did not reveal any evidence of preimpact mechanical malfunctions or failures. However, the spark plugs were found carbon-fouled, which can cause a loss of engine power. Testing of the ignition system, fuel injection system, and turbocharger system revealed no anomalies that would have resulted in carbon fouling. During the examination of the airplane, a Normal Procedures-Abbreviated Checklist was found on the pilot's seat. However, it was not the airplane manufacturer's checklist; it was labeled "FOR TRAINING PURPOSES ONLY"; and it did not contain any detailed guidance on power settings, use of the mixture control, or go-around procedures. All of this information was included in the airplane manufacturer's "Normal Procedures Checklist." Specifically, the checklist stated that, during cruise flight, the fuel mixture should be leaned as required. Further, review of the Pilot's Operating Handbook (POH) and Federal Aviation Administration-approved Airplane Flight Manual (AFM) revealed that, during cruise climb and flight, "the mixture must be adjusted" and that the pilot is responsible for leaning the mixture in cruise flight to lower the fuel flow. The POH and AFM also contained cruise performance charts, which included mixture setting information; however, these were not available to the pilot for reference during the flight. The pilot reported that he did not lean the mixture during the accident flight. Therefore, it is likely that the pilot's improper management of the fuel mixture resulted in an overrich mixture condition, carbon-fouling of the spark plugs, and the subsequent total loss of engine power at a low altitude and that, if he had used the correct checklist and leaned the mixture properly, the engine power loss could have been prevented.

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. Miscellaneous/other during enroute
  2. Loss of engine power (total) during approach (VFR go-around) defining event
  3. Off-field or emergency landing during emergency descent
  4. Collision with terrain or object (not controlled flight into terrain) during landing

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Powerplant parameters › Incorrect use/operation
  • cause Aircraft › Aircraft power plant › Engine controls › Mixture control › Incorrect use/operation
  • cause Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Use of checklist › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 466 hours in all; 235 in this make and model; 14 in the last 90 days; 9 in the last 30 days; 363 as pilot in command
  • Last flight review: December 11, 2013
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: serious injuries

Pilot-Rated Passenger

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 400 hours in all
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 469 hours
  • Last inspection: annual inspection, June 1, 2013; 36 hours since
  • Maximum gross weight: 3,600 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Cont Motor TSIO-550-C11B (piston); 469 hours total

The flight

  • Departed from: SGJ St. Augustine FL at 2:30 pm
  • Destination: 28J Palatka FL
  • Flight plan: none
  • Runway 09, 6,000 ft by 100 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 070° at 10 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 68°F (20°C), dew point 50°F (10°C)
  • Altimeter: 30.13 inHg
  • Observation at 2:50 pm from 28J, 1 miles away

Injuries

FatalSeriousMinorNone
Flig1
Passengers1

About this page

Everything above comes from the NTSB's public accident database: the narrative, probable cause and findings are the NTSB's own words, and the coded tables behind its report (pilot, aircraft, flight, weather, injuries, sequence of events) are written out in plain English. Pilots' ages, home towns and medical details are left out on purpose. The docket at the NTSB holds the report as a PDF and the investigation's photographs and documents. This site never names pilots, passengers or anyone else involved. A preliminary report describes what is known soon after the event and can change; the final report, with the probable cause, usually follows one to two years later and this page is refreshed when it does. Case number ERA14LA161.