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Accidents · NTSB CEN10LA188 · Final report

Beech 95 accident near Eden Prairie, Minnesota, April 1, 2010

On April 1, 2010 at about 7:40 pm local time, a Beech 95, registered N20FP, was substantially damaged in an accident during initial climb near Eden Prairie, Minnesota (Flying Cloud Airport). It was a personal flight under general aviation rules (Part 91). 2 people were seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The fatigue failure of an intake valve spring on the right engine, which resulted in a partial loss of engine power on takeoff.

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

What the record shows

Date
April 1, 2010 · about 7:40 pm local time
Place
Eden Prairie, Minnesota · Flying Cloud Airport · map
Type
Accident
Injuries
2 people were seriously injured.
Weather
visual conditions (good weather)
Aircraft
Beech 95 · all 95s on the register
Registration
N20FP · no longer on the register · serial TD-14
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

The pilot stated that he had no recollection of the events leading up to the accident. The passenger reported that the airplanes' engines seemed to come up to full power during takeoff. The airplane lifted off about halfway down the runway; however, it didn't climb very well. The stall warning sounded just as the airplane was off the end of the runway, and the pilot's efforts to continue flight were unsuccessful. The right wing dropped, and the airplane descended and impacted the ground. A witness reported that the airplane's nose was pitched up 10 to 15 degrees and the wings appeared to be level, as it was flying in ground effect about 10 feet agl. He noted that the engines seemed to be running without any obvious problems. A postaccident examination revealed a lack of compression on the right engine No. 4 cylinder. Further investigation determined that the intake valve spring on the cylinder had fractured. Metallurgical examination noted that the fracture surfaces exhibited features indicative of fatigue progression initiated by corrosion pitting. Corrosion pits and red rust deposits were observed on many areas of the spring. The fatigue initiation also coincided with longitudinal tooling marks consistent with the original forming of the spring. Maintenance records indicated the right engine had been overhauled nearly 2 years prior to the accident. The cylinders were replaced with new non-original equipment manufacturer (OEM) assemblies at that time. The replacement cylinder assemblies were furnished with the valves and valve springs installed. According to the pilot, the right engine had accumulated 18 hours since overhaul.

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. Powerplant sys/comp malf/fail during initial climb defining event
  2. Loss of engine power (partial) during initial climb
  3. Aerodynamic stall/spin during initial climb
  4. Loss of control in flight during initial climb
  5. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft power plant › Engine (reciprocating) › Recip eng cyl section › Failure
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Attain/maintain not possible
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 11,320 hours in all; 55 in this make and model; 60 in the last 90 days; 20 in the last 30 days; 11,220 as pilot in command; 1,070 on instruments
  • Last flight review: January 11, 2010
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: serious injuries

The aircraft

  • Airframe total time: 7,078 hours
  • Last inspection: annual inspection, October 5, 2009
  • Maximum gross weight: 4,000 lb
  • Seats: 5
  • Landing gear: retractable
  • Engine 1: Lycoming O&VO-360 SER (piston); 0 hours total
  • Engine 2: Lycoming O&VO-360 SER (piston); 0 hours total
  • Operator: Fischer Air LLC

The flight

  • Departed from: FCM Minneapolis MN at 7:38 pm
  • Destination: RNH New Richmond MN
  • Flight plan: none
  • Runway 18, 2,691 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 150° at 11 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 79°F (26°C), dew point 52°F (11°C)
  • Altimeter: 29.45 inHg
  • Observation at 7:53 pm from FCM, 2 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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.