Loss of Control in Flight · NTSB ERA10FA342

NORTH AMERICAN AT-6 — Destin, FL

2 fatal High-time pilot
DateJuly 2, 2010
LocationDestin, FL
AircraftNORTH AMERICAN AT-6
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceUncontrolled descent Collision with terr/obj (non-CFIT)
Pilot age57
Pilot total time1,924 hrs · Experienced
Time in type500 hrs
Fatalities2

Probable cause

The pilot's failure to maintain adequate airspeed while maneuvering, which resulted in an aerodynamic stall and spin. Contributing to the accident was the pilot's improper decision to perform the maneuvers at a low altitude and over water.

NTSB findings

  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
  • Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - F

What happened

The pilot was giving airplane rides to his family members when the accident occurred. Witness interviews and global positioning system (GPS) data revealed that the pilot was performing lazy-eights, over water, about 1 mile south of the beach. The airplane descended to an altitude of 355 feet, reversed course from east to west with its "smoke on," and increased groundspeed to 184 knots. The airplane then climbed to about 1,200 feet and completed three lazy-eight turns. During the third turn, at an altitude of 1,254 feet, the airplane's groundspeed slowed to 66 knots. The airplane stalled and completed a one-half turn spin. The pilot recovered from the spin and was in the process of recovering from the ensuing dive, when the airplane impacted the water. Two of the witnesses were experienced in the accident airplane make and model. They were surprised that the pilot was performing maneuvers low over the water, as the water did not provide any ground reference with regard to altitude, position, or horizon. They also expected the airplane to be about 3,000 feet, while maneuvering, as that make and model airplane needed "significant altitude" to recover from a stall or spin. Examination of the wreckage did not reveal any preimpact mechanical malfunctions.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →