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Accidents · NTSB ERA12FA326 · Final report

Amateur-built HUMMEL BIRD accident near Defuniak Springs, Florida, May 9, 2012

On May 9, 2012 at about 4:10 pm local time, a 2010 amateur-built HUMMEL BIRD, registered N9001N, was substantially damaged in an accident during initial climb near Defuniak Springs, Florida (Defuniak Springs airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain airplane control due to the airplane’s exceedence of its maximum gross weight and center of gravity’s most rearward limit and his lack of familiarity with the airplane make and model, which resulted in an aerodynamic stall and subsequent spin. Contributing to the accident was the pilot's decision to knowingly operate the airplane over the maximum allowable gross weight with reduced longitudinal stability.

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

What the record shows

Date
May 9, 2012 · about 4:10 pm local time
Place
Defuniak Springs, Florida · Defuniak Springs · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built HUMMEL BIRD, built 2010
Registration
N9001N · no longer on the register · serial 001
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

Witnesses reported observing the airplane porpoising along its longitudinal axis during its climb after takeoff. About 300 feet above ground level, the airplane pitched up to a nose-high attitude and rolled to the right; it subsequently impacted the ground in a right-wing-low, nose-down attitude. Postaccident examination did not reveal any preimpact mechanical malfunctions or abnormalities that would have precluded normal operation. However, the weight of the airplane (not including fuel) plus the weight of the pilot exceeded the airplane's maximum gross takeoff weight and the center of gravity (CG) was aft of the most rearward limit. Although any fuel would have moved the CG forward of the most rearward limit, it also would have increased the airplane's takeoff weight. The pilot reported to his aviation medical examiner (AME) that the airplane was having "great" difficulty with longitudinal stability. He also noted that his weight gain caused the airplane to be "over gross," most likely causing the control problems. The AME advised the pilot to stop flying the airplane. Because the airplane was at or aft of the rear CG limit, it would have been very sensitive in pitch control and may even have been at or near a dynamically unstable flight regime in terms of pitch handling. Accordingly, the airplane would have required more nose-down trim adjustment. Additionally, because stall speeds increase as gross weight increases, the airplane would have stalled at a higher airspeed. Therefore, it is likely that, during the climb, the airplane stalled at a higher airspeed than the pilot would have expected due to its exceedence of the maximum gross weight and that it subsequently entered a spin. A review of the pilot's logbook indicated that he had accumulated only 4.4 flight hours in the 2 years preceding the accident flight with only 0.3 hour in the accident airplane. It is likely that the pilot's lack of experience in the airplane make and model contributed to his decision to take off with the airplane in an overweight condition and his inability to understand the seriousness of the situation. Although the postmortem toxicology testing was positive for three drugs used in the treatment of hypertension, none of the medications should have been impairing and were unlikely to have contributed to the accident.

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. Aircraft loading event during prior to flight
  2. Loss of control in flight during initial climb
  3. Aerodynamic stall/spin during initial climb defining event
  4. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › CG/weight distribution › Capability exceeded
  • cause Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded
  • cause Personnel issues › Task performance › Planning/preparation › Weight/balance calculations › Pilot
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Personnel issues › Experience/knowledge › Experience/qualifications › Total experience w/ equipment › Pilot
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: airplane
  • Flight time: 527.5 hours in all; 0.3 in this make and model
  • Last flight review: August 22, 1997
  • Medical certificate: Class 3 (waiver time limited special)
  • Seat: frt
  • Injury: fatal

The aircraft

  • Airframe total time: 0 hours
  • Last inspection: condition inspection, January 10, 2010; 8 hours since
  • Maximum gross weight: 530 lb
  • Seats: 1
  • Landing gear: fixed
  • Engine: Hummel Engine 92X78 (piston); 8 hours total

The flight

  • Departed from: 54J Defuniak Springs FL at 4:10 pm
  • Destination: 54J Defuniak Springs FL
  • Flight plan: none
  • Runway 27, 4,146 ft by 60 ft

Weather at the time

  • Light: daylight
  • Wind: at 4 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 11,000 ft; scat at 2,200 ft
  • Temperature: 81°F (27°C), dew point 68°F (20°C)
  • Altimeter: 29.88 inHg
  • Observation at 4:25 pm from KCEW, 19 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.