Galveston

The non-instrument-rated pilot departed on a cross-country flight in a twin-engine turboprop airplane on an instrument flight plan. As the pilot neared his destination airport, he received heading and altitude vectors from air traffic control. The controller cleared the flight for the approach to the airport; shortly afterward, the pilot radioed that he was executing a missed approach. The controller then issued missed approach instructions, which the pilot acknowledged. There was no further communication with the pilot. The airplane collided with terrain in a near-vertical angle. About the time of the accident, the automated weather reporting station recorded a 300-foot overcast ceiling, and 5 miles visibility in mist. Examination of the wreckage did not reveal any anomalies that would have precluded normal operation. Additionally, both engines displayed signatures consistent with the production of power at the time of impact. The pilot's logbook indicated that he had a total of 1,281.6 flight hours, with 512.4 in multi-engine airplanes and 192.9 in the accident airplane. The logbook also revealed that he had 29.7 total hours of actual instrument time, with 15.6 of those hours in the accident airplane. Of the total instrument time, he received 1 hour of instrument instruction by a flight instructor, recorded about 3 years before the accident. The accident is consistent with a loss of control in instrument conditions.

The twin engine airplane had been cleared for a night instrument approach to Galveston, Texas, after flying non-stop from San Diego, California, when the pilot reported that he had lost the right engine and did not have much fuel left. The controller vectored the airplane toward the closest airport, and the airplane was approximately 1 mile northeast of that airport when radar contact was lost. A witness observed the airplane enter a spin, descend in a nose down attitude, and impact near the center of a lake. When the pilot filed his flight plan for the cross country flight, he indicated the airplane carried enough fuel to fly for 7 hours and 30 minutes. At the time radar contact was lost, 7 hours and 32 minutes had elapsed since the airplane departed San Diego. Examination of the airplane revealed no evidence of any preimpact mechanical discrepancies. The landing gear was down, the flaps were extended to about 15 degrees, and neither propeller was feathered. The single engine approach procedure in the airplane owner's manual indicated that the landing gear should be extended when within gliding distance of the field and the flaps placed down only after landing is assured.

At liftoff, the twin engine rolled to the right and crashed in flames. The aircraft was destroyed by a post crash fire and the pilot, sole on board, was slightly injured.

Shortly after takeoff from Galveston-Scholes Field Airport, while in initial climb at an altitude of 400 feet, the airplane became unstable, lost height then crashed in a field past the south runway end. A pilot and five passengers were killed while six other occupants were seriously injured. The aircraft was destroyed by impact forces and a post crash fire.

The crew was completing a local training flight at Galveston-Scholes Airport, Texas. Following several approached, the twin engine aircraft was again approaching the airport when it stalled and crashed into the Galveston Bay, about a mile from the runway threshold. The aircraft was destroyed and all three occupants were killed.

While performing a maritime patrol flight over the Gulf of Mexico, the seaplane crashed in unknown circumstances off the Texas coasts. Debris were found few days later on a beach near Galveston. All nine crew members were killed.

Upon landing, the single engine airplane went out of control, veered off runway and came to rest, bursting into flames. The pilot was injured and the aircraft was destroyed by a post crash fire.