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Accidents · NTSB ERA12LA150 · Final report

M-Squared Aircraft BREESE 2 accident near Bayou la Batre, Alabama, January 19, 2012

On January 19, 2012 at about 10:30 pm local time, a M-Squared Aircraft BREESE 2, registered N582MS, was substantially damaged in an accident during initial climb near Bayou la Batre, Alabama (Roy e. Ray airport). It was an instructional flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's inability to maintain control of the airplane for reasons that could not be determined because postaccident examination of the rudder control system did not reveal any anomalies that would have precluded control of the airplane.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
January 19, 2012 · about 10:30 pm local time · cases in 2012
Place
Bayou la Batre, Alabama · Roy e. Ray · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
M-Squared Aircraft BREESE 2 · all BREESE 2s on the register
Registration
N582MS · registry record · serial 000721
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

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

The student pilot and a flight instructor completed three landings without incident. The flight instructor then exited the airplane, and the student pilot performed a full-stop landing without incident. During the subsequent climb after takeoff, the airplane yawed to the right, nearly 90 degrees from the departure runway heading. The student pilot noted that he was unable to depress the left rudder pedal more than 1 or 2 inches and that the right rudder pedal moved without resistance. He also noticed that the elevator control felt "loose and sloppy." The student pilot determined that he did not have enough controllability to safely land the airplane and subsequently chose to maneuver over a field and deploy the airplane's ballistic recovery parachute system. The forward portion of the fuselage was substantially damaged upon ground contact. Postaccident examination of the airplane revealed that the tail skid/rudder control tube was fractured. The rudder pedals were displaced during the impact with the ground; however, all connections remained intact. No other discrepancies of the flight control system were observed. Metallurgical examination of the fractured tube revealed that it failed due to bending overstress. Although it is possible that contacting the tail skid on the runway at a high-pitch attitude could produce similar loading, it is more likely that the inertial loads on the tail structure during the impact were responsible for the fracture. The airplane had been operated for 575 total hours since new and 75 hours since its most recent condition inspection, which was performed about 4 months before 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. Flight control sys malf/fail during initial climb defining event
  2. Collision with terrain or object (not controlled flight into terrain) during emergency descent
  3. Unknown or undetermined during unknown

The NTSB's findings

  • Aircraft › Aircraft systems › Flight control system › Rudder control system › Not specified other cases naming the flight controls
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Student pilot
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined

Dual student

  • Certificate: student
  • Flight time: 14 hours in all; 13 in this make and model; 0 in the last 90 days; 14 in the last 30 days
  • Medical certificate: Sport Pilot
  • Seat: frt
  • Injury: no injuries

The aircraft

  • Airframe total time: 575 hours
  • Last inspection: condition inspection, September 30, 2011; 75 hours since
  • Maximum gross weight: 1,320 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 582UL-99 (piston); 0 hours total
  • Operator: M Squared Aircraft

The flight

  • Departed from: 5R7 Bayou la Batre AL
  • Destination: 5R7 Bayou la Batre AL
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 160° at 9 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 2,400 ft
  • Temperature: 61°F (16°C), dew point 54°F (12°C)
  • Altimeter: 30.06 inHg
  • Observation at 10:53 pm from BFM, 13 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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

9 documents, released by the NTSB on March 20, 2013. 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.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/ERA12LA150.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

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 does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.