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Accidents · NTSB ERA15FA102 · Final report

Amateur-built AVENTURA II accident near Sebring, Florida, January 16, 2015

On January 16, 2015 at about 4:00 pm local time, a 2005 amateur-built AVENTURA II, registered N511DS, was substantially damaged in an accident during maneuvering (low-alt flying) near Sebring, Florida (Sebring Rgnl airport). It was an air show or air race flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's failure to maintain control while maneuvering at low altitude, which led to the airplane exceeding its critical angle-of-attack and experiencing an aerodynamic stall.

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

What the record shows

Date
January 16, 2015 · about 4:00 pm local time
Place
Sebring, Florida · Sebring Rgnl · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built AVENTURA II, built 2005
Registration
N511DS · registry record · serial AA2A0124
Damage
Substantial damage
Flight
Air show or air race flight · general aviation rules (Part 91)

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

Several witnesses observed the airplane during engine start and reported that, when the engine started, the airplane tipped forward onto its nose and then fell back and its tail struck the ground. The pilot exited the airplane, walked to the back, returned to the cockpit, and then taxied out. No witnesses reported seeing the pilot examine the underside of the tail or the elevators after the tail strike. A video recording made by one of the witnesses after the tail strike showed that the airplane departed, climbed to about 300 feet above ground level (agl), made a 180-degree left turn, and performed a pass down the runway in the opposite direction of the takeoff. A few seconds later, after executing another 180-degree turn, the airplane performed another low pass down the runway, this time in the direction of the takeoff. The airplane then entered a left turn, the bank angle increased until the wings were almost perpendicular to the ground, the nose of the airplane dropped, and the airplane descended in a nose-down attitude to ground impact. The airplane came to rest on its nose with the fuselage nearly perpendicular to the ground. Postaccident examination revealed that the elevator trim cable was separated from the trim tab. Although it is possible the trim cable disconnected when the tail struck the ground during engine start (and would have been noticeable to the pilot if he had looked), the investigation could not conclusively determine when the trim cable separated or whether the separation contributed to the pilot's loss of airplane control. No other mechanical malfunctions or abnormalities were noted that would have precluded normal operation. It is likely that, during the low altitude flyby, the pilot inadvertently entered an aerodynamic stall while maneuvering and did not have sufficient altitude to recover.

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 (low-alt flying)
  2. Aerodynamic stall/spin during maneuvering (low-alt flying) defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot

Pilot

  • Certificate: sport pilot
  • Medical certificate: None
  • Seat: left
  • Injury: fatal

Dual student

  • Flight time: 11 hours in all
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 362.5 hours
  • Last inspection: condition inspection, November 17, 2012; 9 hours since
  • Maximum gross weight: 1,433 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 912 ULS (piston); 363 hours total
  • Operator: Aero Adventure

The flight

  • Departed from: SEF Sebring FL at 3:55 pm
  • Destination: SEF Sebring FL
  • Flight plan: none
  • Runway 14, 4,990 ft by 100 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 360° at 13 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 10,000 ft
  • Temperature: 63°F (17°C), dew point 55°F (13°C)
  • Altimeter: 30.13 inHg
  • Observation at 3:59 pm from KSEF

Injuries

FatalSeriousMinorNone
Flight crew2

Documents from the investigation the NTSB's docket: the evidence folder behind the report

13 documents, released by the NTSB on December 2, 2015. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

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.