Texas

The aircraft was found abandoned. Wreckage scene indicates collision with trees prior to collision with terrain. Aircraft suspected of being used for illegal cargo operations. The pilot was not found.

According to law enforcement officers, the aircraft experienced double engine failure and made a forced landing in unimproved terrain. During the landing rollout the aircraft struck several trees. An intense post crash fire erupted destroying all but one wing tip of the wreckage. Repeated efforts to contact the pilot and operator have been unsuccessful. It is assumed that there were no injuries and no passengers.

Crashed on approach to Orange Grove AFB, killing all three crew members.

During a cross country flight the pilot could not locate a refueling stop and landed 100 miles away. No refueling was accomplished and he decided to go on to his destination with the fuel remaining. Enroute his right engine coughed and he realized he was running out of fuel. After switching to crossfeed normal engine operation was restored. Even though he was only about 3 miles from his destination he decided to land on a 4,000 feet dirt agricultural airstrip which he saw directly below him. He forced the aircraft down and landed downwind at high speed about midway down the runway. The aircraft did not stop on the runway and overran into a dirt bank and a fence. The landing gear was knocked off and the aircraft became airborne for 700 more feet before impacting and tumbling. The aircraft came to rest inverted about 825 feet past the dirt bank. A fire developed in the left wing and consumed most of the area in the vicinity of the left fuel tank outboard of the left engine. The pilot stated that there were no malfunctions of the aircraft or systems.

The aircraft was on a flight from the El Paso Intl Airport to the West Texas Airport. A hard landing was made causing all three landing gear to collapse, folded the left wing aft just inboard of the engine and twisted the entire right wing about 30° leading edge down. According to the pilot the aircraft was flown with 30° of flaps on downwind and 47° of flaps on base. He also reported that both airspeed indicators were stuck at 110 knots. According to photographs taken by an unidentified party, the flaps were in the up position in the pattern and during touchdown. Touchdown was made with the right main gear off the right side of the rwy. The aircraft wheel track is only 4 feet less than the width of the runway. The pilot did not have a type rating nor authorization in lieu of a type rating for the 15 minutes ferry flight. The pilot had 4,140 hours copilot time in the aircraft, during which he had never landed the aircraft.

The pilot had just taken off at night on a flight to Mexico when he declared an intent to return and land with some unspecified emergency. While he was using his radio, the sound of both engines, running at high power, was audible. When asked if he required assistance, he gave an affirmative reply, but when asked if he required a crash crew, he gave a negative reply. Shortly after that, the aircraft collided with power lines about 1 mile from the runway, then impacted the ground and was demolished by fire. Impact with the power lines occurred at about 55 feet agl. A wire impact mark on the nose door indicated the aircraft was in a vertical bank when the collision occurred. An exam of the wreckage revealed no evidence of a preimpact/mechanical malfunction or failure; however, there was extensive damage from fire. There was evidence that the aircraft was loaded beyond its max certificated gross weight. The pilot had a temporary US license based on his canadian license. The pilot, sole on board, was killed.

The aircraft crashed while completing a charter flight that began at 1220 cst on 11/25/83 to transport a TV Sports film crew. The flight began at Midland, TX and proceeded to Fort Worth and Wichita Falls, TX, then began a return flight to Midland. During arrival, the pilot transmitted that he was turning on a 1/2 mile final approach for runway 16R. Witnesses observed what appeared to be a normal approach, but at 30 to 50 feet agl, the pilot initiated a go-around, the aircraft pitched up in an extremely nose high attitude, then entered a left bank, stalled and crashed. To duplicate the aircraft's observed profile, simulation tests showed full aft yoke pressure had to have been applied with full nose-up trim engaged thru-out the maneuver. No preexisting mechanical defects were found during the investigation. A test of the right front seat passenger's blood showed a blood/alcohol level of .144%. A test of the pilot's blood showed no drugs or alcohol, but a microscopic tissue exam showed changes possibly indicative of myocardial infarction; no cause of an infarction was conclusively established. All eight occupants were killed.

The original flight was aborted due to a magneto problem. The defect was corrected, but due to the delayed takeoff, the pilot elected to fly to McAllen, TX, for further repairs. During the takeoff roll, the aircrew noted sparks/flares on the left side of the cargo/cabin area, behind a bulkhead. The aborted the takeoff and attempted to extinguish the fire, but were unable. The crew then evacuated the aircraft and the aircraft was destroyed by fire. An investigation was made, but the source of the fire was not determined.

After transporting passengers from Longview, TX to Oklahoma City, OK and return to Longview, the aircraft was refueled for a flight back to Nacogdoches, TX, where the aircraft was based. About 12 min after takeoff, the pilot was cleared for an NDB approach to Nacogdoches and instructed to contact the Lufkin FSS for weather and current altimeter setting. During the NDB approach, the aircraft collided with trees, crashed and burned. An investigation revealed no evidence of either an engine or airframe failure or malfunction. Initial impact occurred with trees about 700 yards east of the NDB site. Initially, trees were cut in an upsloping manner where the terrain sloped upwards. Elevation of the crash site was 530 feet msl. The minimum descent altitude (MDA) was 900 feet msl. About 28 miles north, the 1955 cdt weather at Lufkin was, in part: 3,500 feet broken, visibility 5 miles. However, witnesses at Nacogdoches reported considerably lower ceilings, reduced visibility and some hilltops obscured by clouds. A pilot witness reported light rain, fog in the treetops. Reportedly, the airport was below minimums. Both occupants were killed.

The pilot was executing a high speed pass over the runway at about 250 feet agl. The pilot then began a rapid pull-up and both wings separated just outboard of the engine nacelles. Reconstruction of the sequence from a videotape revealed that the aircraft's speed at the time of the wing separations was 220 knots. Vne for the aircraft is 193 knots. It was calculated that, at 220 knots and an 8° nose-up pitch, the 'g' load at the time of the wing separations would have been 8.3 g's. The pilot, sole on board, was killed.