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Accidents · NTSB ERA18FA208 · Final report

Champion 8GCBC accident near Foley, Alabama, August 4, 2018

On August 4, 2018 at about 3:00 pm local time, a 2012 Champion 8GCBC, registered N424A, was destroyed in an accident during initial climb near Foley, Alabama (Irwin Farms airport). It was a banner-towing 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 exceedance of the airplane's critical angle of attack, which resulted in a subsequent aerodynamic stall and spin at an altitude that was too low for recovery.

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

What the record shows

Date
August 4, 2018 · about 3:00 pm local time
Place
Foley, Alabama · Irwin Farms · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Champion 8GCBC No Series, built 2012 · all 8GCBCs on the register
Registration
N424A · no longer on the register · serial 553-2012
Damage
Destroyed
Flight
Banner-towing flight · general aviation rules (Part 91)

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

The commercial pilot was conducting a banner-tow flight with a pilot-rated passenger. A witness (a ground crewmember) stated that, after takeoff, the approach and pickup of the banner appeared normal and that the engine sounded strong. According to the ground crewmember, the pilot successfully hooked the banner with the airplane tow cable and initiated a steep climbout with the banner in tow. The trailing edge of the banner had just come off the ground when the airplane reached an altitude of about 300 ft above ground level. At that point, the right wing dropped. The pilot attempted to maintain directional control by releasing the banner and applying left rudder; however, the airplane entered a right descending spin to the ground. Postaccident examination revealed no malfunctions that would have precluded normal operation of the airplane or engine. It is likely that after the banner pickup and during initial climb, while the airplane had a high power setting, high pitch angle, and low airspeed, the airplane exceeded the critical angle of attack and entered an aerodynamic stall and spin from which recovery was not possible due to the airplane's altitude at the time. Even though the weight and balance were within limits for the accident flight, it is possible the presence of the back seat passenger reduced the airplane's performance, and that the pilot did not account for the effect of the back seat passenger on the performance of the airplane during the pickup maneuver.

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. Low altitude operation/event during initial climb
  2. Abrupt maneuver during initial climb
  3. Attempted remediation/recovery during initial climb
  4. Aerodynamic stall/spin during initial climb defining event
  5. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • 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 › Capability exceeded

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land
  • Flight time: 2,617 hours in all
  • Last flight review: April 6, 2017
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: frt
  • Injury: fatal

Pilot-Rated Passenger

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 240 hours in all
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: rear
  • Injury: fatal

The aircraft

  • Airframe total time: 3,785 hours
  • Last inspection: 100-hour inspection, July 27, 2018; 100 hours since
  • Maximum gross weight: 2,150 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-360-C1G (piston); 1,738 hours total
  • Fire on the ground
  • Operator: Gcaa, LLC

The flight

  • Departed from: PVT Foley AL at 2:50 pm
  • Destination: PVT Foley AL
  • Flight plan: none
  • Runway 18, 1,200 ft by 50 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Visibility: 10 statute miles
  • Sky: scat at 2,400 ft
  • Temperature: 84°F (29°C), dew point 75°F (24°C)
  • Altimeter: 30.14 inHg
  • Observation at 2:55 pm from JKA, 6 miles away

Injuries

FatalSeriousMinorNone
Flight crew2

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

11 documents, released by the NTSB on March 18, 2020. 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.