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Accidents · NTSB MIA08FA094 · Final report

Mooney M20M accident near Midlothian, Virginia, April 27, 2008

On April 27, 2008 at about 2:19 pm local time, a Mooney M20M, registered N429RM, was destroyed in an accident during maneuvering near Midlothian, Virginia. It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was instrument conditions (cloud, fog or low visibility).

The NTSB's probable cause their words, unchanged

The pilot’s improper control inputs resulting from spatial disorientation.

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

What the record shows

Date
April 27, 2008 · about 2:19 pm local time
Place
Midlothian, Virginia · map
Type
Accident
Injuries
2 people were killed.
Weather
instrument conditions (cloud, fog or low visibility)
Aircraft
Mooney M20M · all M20Ms on the register
Registration
N429RM · registry record · serial 27-0301
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

The instrument-rated private pilot departed with an instrument flight rules clearance and encountered instrument meteorological conditions shortly after takeoff. He did not establish contact with air traffic control at any time during the flight, nor did he enter controlled airspace on the assigned heading of 180 degrees. According to the NTSB Air Traffic Control (ATC) Radar Study, the flight climbed to approximately 1,800 feet msl, and continued in a direction northwest of the departure airport while turning left, right, and then left with slight changes in altitude. The airplane then began a right descending turn with the bank angle and turn rate increasing beyond the standard rates and angles, and the load factor reached close to maximum limits. At some point near the end of the flight, during the right descending turn, the lower fuselage panel separated and the left rear window separated. The airplane impacted the ground then a house and both were destroyed by impact and postcrash fire. The pilot's wife reported a previous concern with a stuck flap. Although the impact and fire destroyed sections of the flight control push/pull tubes and components of the flap system, changes in direction to the left and right were consistent with the pilot controlling the airplane. Examination of the wreckage, including the flight control, flap, and speedbrake systems, did not reveal any preimpact mechanical malfunctions. Additionally, Mooney Flight Test personnel reported that the airplane is controllable with one flap fully extended and the other flap fully retracted. No evidence of preimpact failure or malfunction was noted to the engine or engine accessories. Risk factors for spatial disorientation were present at the time of the accident, including instrument meteorological conditions and maneuvering flight. The airplane’s sequence of turns during the departure and its subsequent spiral dive were conducive to vestibular illusions. Analysis of the radar data in the airplane performance study showed evidence of a flight path and associated increased g-loading that were consistent with the effects of spatial disorientation.

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 maneuvering defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  3. Fire/smoke (post-impact) during post (impact)

The NTSB's findings

  • cause Personnel issues › Psychological › Perception/orientation/illusio › Spatial disorientation › Pilot

Pilot

  • Certificate: private
  • Ratings: single-engine land; instrument: airplane
  • Flight time: 332 hours in all; 271 as pilot in command
  • Last flight review: April 7, 2007
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

Crew member

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
  • Flight time: 500 hours in all
  • Medical certificate: Class 2
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 491 hours
  • Last inspection: annual inspection, November 16, 2007
  • Maximum gross weight: 3,368 lb
  • Seats: 4
  • Landing gear: retractable
  • Engine: Lycoming TIO-540-AF1B (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: FCI Midlothian VA at 2:16 pm
  • Destination: FKN Franklin VA
  • Flight plan: IFR
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 360° at 4 knots
  • Visibility: 10 statute miles
  • Sky: overcast at 800 ft
  • Temperature: 63°F (17°C), dew point 55°F (13°C)
  • Altimeter: 30.14 inHg
  • Observation at 2:19 pm from FCI

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.