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Accidents · NTSB WPR16FA067 · Final report

Flight Design GMBH CTLS accident near Springville, California, February 11, 2016

On February 11, 2016, a 2011 Flight Design GMBH CTLS, registered N911TS, was destroyed in an accident during maneuvering (low-alt flying) near Springville, California (Visalia airport). It was a public-use flight (local) under public-use (government) rules. 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 adequate airspeed while maneuvering at low altitude in hilly terrain, which resulted in the airplane's wing exceeding its critical angle-of-attack and a subsequent aerodynamic stall. Contributing to the accident were the pilot's inability to recognize the rising terrain due to the sun glare and the pilot's operation of the airplane in excess of its gross weight.

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

What the record shows

Date
February 11, 2016
Place
Springville, California · Visalia · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Flight Design GMBH CTLS NO SERIES, built 2011 · all CTLSs on the register
Registration
N911TS · no longer on the register · serial F-11-02-05
Damage
Destroyed
Flight
Public-use flight (local) · public-use (government) rules

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

The airplane, which was owned and operated by the local county sheriff's department, was on a low-altitude observation flight. According to GPS data recovered from the airplane, about 1 minute before the accident, the airplane was flying westbound (heading 242°) over a highway, about 500 feet above ground level (agl), and at a groundspeed of 52 knots. The GPS data and witness observations indicated that the airplane entered a left turn. According to the witnesses, the airplane's wings then dipped left and right, and the airplane descended to ground impact. The witnesses heard the engine operating in a steady tone until ground impact. A postcrash fire ensued, which destroyed the airplane. Examination of the wreckage did not reveal evidence of any preimpact mechanical malfunctions or anomalies that would have precluded normal operation. The airplane's estimated weight at the time of the accident was about 152 lbs over the airplane's maximum gross weight. Because of the higher gross weight, the airplane's stall speed in a 30° banked turn was 3 knots higher than it would have been at the airplane's maximum gross weight. This resulted in a stall speed of about 48 knots calibrated airspeed, which was near the airplane's recorded groundspeed of 52 knots. The sun position at the time of the accident was on a bearing of 241° and was 13° above the horizon, indicating that the pilot was looking directly into the sun before the left turn began. Another pilot who flew in the vicinity shortly after the accident reported that when flying westbound over the highway, he was looking straight into the sun, there was a lot of haze, and he could not distinguish the tops of the hills to the left of the highway from the sky. It is likely that the accident pilot was partially blinded by sun glare and did not see the hills rising above him on his left. After he entered the left turn moving away from the sun line, it is likely that the rising terrain suddenly came into view, and he increased the airplane's bank angle in order to avoid the terrain and exceeded the wing's critical angle-of-attack, which resulted in an aerodynamic stall. The altitude the airplane was operating at was too low to allow for a recovery.

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. Abrupt maneuver during maneuvering (low-alt flying)
  2. Loss of control in flight during maneuvering (low-alt flying)
  3. Aerodynamic stall/spin during maneuvering (low-alt flying) 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 › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • factor Environmental issues › Physical environment › Terrain › Mountainous/hilly terrain › Contributed to outcome
  • factor Environmental issues › Conditions/weather/phenomena › Light condition › Glare › Effect on personnel
  • factor Aircraft › Aircraft oper/perf/capability › Aircraft capability › Maximum weight › Capability exceeded

Pilot

  • Certificate: airline transport pilot, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 3,675 hours in all; 1,002.5 in this make and model
  • Last flight review: December 8, 2015
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

Other crew

  • Medical certificate: None
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 3,103.9 hours
  • Last inspection: 100-hour inspection, February 3, 2016; 28 hours since
  • Maximum gross weight: 1,323 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 912ULS (piston); 1,104 hours total
  • Fire on the ground
  • Operator: County Of Tulare Sheriffs Office

The flight

  • Departed from: KVIS Visalia CA at 10:40 pm
  • Destination: KVIS Visalia CA

Weather at the time

  • Light: daylight
  • Wind: from 300° at 8 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 0°F (-18°C), dew point 0°F (-18°C)
  • Altimeter: 30.18 inHg

Injuries

FatalSeriousMinorNone
Flight crew2

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.