Dallas-Love Field

Shortly after takeoff, one of the engine failed. The pilot elected to make an emergency landing when the aircraft crashed near the runway end. Both occupants were killed, among them Eduardo Mata, Mexican conductor and composer. He was accompanied by Marina Anaya and was en route to Dallas, TX.

The pilot stated that the airplane was cruising at an altitude of 18,000 feet 30 minutes after refueling when the left engine lost power. He stated that he was in radio contact with Indianapolis ARTCC so he advised them of the situation and requested a lower altitude. The center cleared the flight to 10,000 feet msl. The pilot stated that his attempt to restart the engine was unsuccessful. Shortly thereafter the pilot reported that the right engine lost power. According to the controller at the center, the pilot was nine miles from the nearest airport and he provided the pilot with radar vectors to the nearest airport, and the weather conditions. The airplane touched down in a wooded area. The faa examined the airplane at the accident site. The engines were removed to Pratt & Whitney for further examination. The examination of the engine and engine accessories did not disclose any pre-existing defects. Fuel samples were removed and tested at the laboratory at Pratt & Whitney. The tests revealed evidence of contaminants.

Before takeoff, San Angelo AFSS briefer told the pilot computers were down in south Texas for 1.5 hours and no current weather info was available. Current weather info was available at nws at Midland and FSS's at Midland, McAlester and De Ridder, but the pilot didn't call these, nor did the briefer advise him to do so. Pilot didn't update weather in flight. About 38 minutes after takeoff, in area of potential icing, aircraft slowed from 270 to 150 knots ground speed in 4 minutes, then slowed to 100 knots in next 12 seconds. About 33 seconds before reaching 100 knots, pilot requested descent from 15,000 feet to 13,000 feet. At that time, true ground track was approximately 080° with wind aloft about 213° at 43 knots. Before ATC could clear descent, aircraft descended to 14,800 feet, then radar contact was lost after one return at 9,700 feet. Descent rate between last 2 altitudes: 12,750 fpm. No preimpact malfunction was found. IMC existed above 12,500 feet. Freezing level was forecasted at 10,000 feet to 12,000 feet. Aircraft was certified for flight in known icing conditions, but status of anti-ice/deice equipment wasn't determined due to impact/fire damage. Low levels of ethanol were found in tox samples from all occupants; however, there was evidence that the tox samples were unreliable. All five occupants were killed.

Flight was a 3-engine ferry with the #4 engine shut down. During takeoff roll at V1 the #2 engine overheat light came on. According to the copilot the pilot reduced throttle slightly and continued the takeoff. After lift-off the pilot aborted the takeoff. The airplane could not be stopped on the remaining runway and collided with antennas, approach lights and a construction site 1,180 feet from the departure end of the runway. Postcrash exam of the 3 operating engines did not reveal any evidence of mechanical failure or malfunction. A failed resistor was found in the #2 engine electronic engine control (eec). This would cause the unit to over-schedule fuel to the engine resulting in hotter engine operating temperatures. Retarding the throttle would reduce fuel flow to within normal ranges for engine operation. Under conditions that existed at the time of the accident, the airplane would have a 3-engine rate-of-climb of 1,398 fpm, and a 2-engome rate-of-climb of 350 fpm. The captain was killed while the copilot was seriously injured.

While en route at FL370, the pilots declared an emergency, reported a fire in the right engine and requested vectors to the nearest suitable airport. They were vectored toward the Lexington-Blue Grass Airport and circled to descend. Shortly after declaring an emergency, the pilots reported they secured the right engine and extinguished the fire light. As the aircraft was on final approach to land, the local controller (using binoculars) confirmed that both the gear and flaps were extended. However, as the aircraft continued onto a short final approach, an increase in its pitch attitude was noted. It then dropped below the level of the runway threshold and impacted in a pasture short of the runway. After initial impact, the aircraft went thru a stone fence, hit 2 utility poles, crossed a highway, came to rest at the perimeter fence and burned. An auto was damaged by debris; 2 occupants received minor injuries. An investigation revealed the aircraft impacted with the gear extended, but the flaps and flap handle were found in the up position. An examination of the right engine revealed its outer exhaust cone was cracked in the vicinity of a fire detection loop. No other preexisting mechanical problems were evident. Both pilots were killed and both passengers were seriously injured.

At 1708:48, while cruising at 6,000 feet, a pilot of N711Y advised ATC, 'I think I'd like to turn around, head for Texarkana here, I've got a little problem.' He was provided a vector and advised of closest airports. Shortly after, he stated he would be unable to reach the airports. At 1711:49, he said there was smoke in the cockpit. While landing in a field at 1714, the aircraft hit wires and a pole then continued into trees where it was extensively damaged by impact and fire. The crew egressed thru the cockpit windows. The passengers did not escape. During flight, the crew was unable to start the cabin heater; despite repeated attempts by the captain. Smoke then entered the cabin. Fresh air vents and cockpit windows were opened, but smoke became dense. The crew had difficulty seeing. The oxygen system and hand held fire extinguishers were not used. Fasteners for the heater door were found unfastened. Examination indicated the fire originated in the aft cabin area, right hand side, at or near the floor line. The ignition and fuel sources were not determined. Among those killed were the American singer and actor Ricky Nelson and his girlfriend Helen Blair as well as five members of his band 'Stone Canyon'.

A student pilot in a Cessna 152, N5522L, had departed Redbird Airport at Dallas. He was practicing solo maneuvers in a privately designated practice area that overlapped the extended inbound course to runway 31L and 31R at Love Field. At the same time, a Cessna 441, N400BG, was being vectored for a back course ILS to rwy 31R. DFW approach control cleared N400BG to continue descending to 3,000 feet and fly heading 290°. While N400BG was descending thru approximately 3,600 feet, about 14 miles southeast of Love Field, the two aircraft collided. The Cessna 152 pilot was maneuvering at or near the edge of the practice area when the collision occurred. An investigation revealed the Cessna 152 had just completed an approximately 180° turn toward an easterly heading. Both aircraft were demolished in a quartering head-on collision. Radar info from both aircraft was displayed on the controller's scope. The Cessna 152 was depicted as a 1200 beacon code; however, it was not equipped with a mode C (altitude reporting) transponder. The controller did not provide a traffic advisory for the Cessna 441 pilot; but, in this situation, an advisory was not mandatory. All five pilot on both aircraft were killed.

A PA-31, N100FD, was being vectored by DFW approach control (approach control) for a landing on runway 13L at Dallas-Love Field. The pilot's last received and acknowledged instructions were to descend and maintain 2,000 feet and turn left to 190°. Simultaneously, a Cessna 337, N72430, departed runway 15 at Addison Airport, under tower control, and was to make a right climbing turn of approx 180°. Two min after takeoff, the pilot asked and got approval for freq change. 24 seconds later, he contacted approach control stating he had just departed Addison and was climbing to 2,500 feet on a 300° heading. The controller misunderstood the pilot's departure point and instructed him to change to frequency 120.5. The two aircraft immediately collided. A 2,000 feet ceiling was reported, two witnesses stated they could see more blue sky than clouds. A witness approximately 8 miles away saw a fireball in the clouds. Investigation revealed the controller, vectoring N100FD, prematurely cleared the aircraft to an altitude which was below the ceiling of the Addison Airport traffic area and prior to reaching the airspace delegated for that purpose by an ATC letter of agreement.

After takeoff from Dallas-Love Field Airport, while climbing, one of the engine failed. The pilot elected to return for a safe landing when the aircraft lost height and crashed into residences by the airport. All seven occupants were seriously injured while no one on the ground was injured. The aircraft was destroyed.

Shortly after takeoff from Dallas-Love Field Airport, while climbing, the pilot informed ATC about serious problems and elected to return for an emergency landing. He was cleared to do so and completed a turn to rejoin the airport when he lost control of the airplane that crashed onto several houses by the airfield. The aircraft was destroyed and the pilot was killed. There were no injuries on the ground.