Omaha-Eppley

While in cruising altitude, the pilot encountered problems with the left propeller and lost control of the airplane that dove into the ground and crashed in Roosevelt. The aircraft was destroyed and both occupants were killed.

The takeoff from Lincoln Airport was initiated in low ceiling and fog. Just after liftoff, the twin engine airplane went out of control and crashed. The aircraft was destroyed and all three occupants were killed.

The crew started an ILS approach to Cedar Rapids Airport in poor weather conditions when control was lost. The airplane dove into the ground and crashed in an open field located few miles from the airport. The twin engine airplane was totally destroyed and all five occupants have been killed. It was determined that in poor weather conditions, the left wing, left engine and tail separated in flight, causing the aircraft to be uncontrollable.

While in cruising altitude, the right engine lost power. Unable to maintain the assigned altitude, the crew decided to attempt an emergency landing. The airplane belly landed in a prairie and slid for dozen yards before coming to rest. All 12 occupants were uninjured while the aircraft was damaged beyond repair.

Flight 250 was a scheduled domestic passenger/cargo flight from New Orleans, Louisiana, to Minneapolis, Minnesota, with intermediate stops at Shreveport, Louisiana, Fort Smith, Arkansas, Tulsa, Oklahoma, Kansas City, Missouri, and Omaha, Nebraska. The flight departed from New Orleans at 1835 hours CST and arrived at Kansas City without reported incident. It departed from Kansas City at 2255 hours on an IFR clearance to Omaha via Jet Route 41 at FL 200. Just prior to take-off, the flight was restricted to 5 000 ft due to conflicting traffic. When the flight was about 12 miles north of Kansas City, control of the aircraft was transferred to the Kansas City Air Route Traffic Control Centre (ARTCC). Radar contact was confirmed and the flight was cleared to climb to and maintain FL 200. After some discussion with ARTCC about the weather the flight crew advised that they would like to maintain 5 000 ft to Omaha. They reported they were at 6 000 ft and ARTCC cleared the flight to maintain that altitude until 5 000 ft was available. At 2303 hours the Kansas City ARTCC initiated a transfer of control of the flight to the Chicago ARTCC but before the transfer could be accomplished the flight requested and received permission from the Kansas City controller to deviate to the left of course. At 2306 hours the Kansas City controller cleared the flight to descend to and maintain 5 000 ft and contact the Chicago ARTCC. After some discussion of the weather as it was displayed on the Chicago controller's radar, the flight was advised that another Braniff flight, Flight 255, was on the same frequency and was at 10 000 ft climbing to 17 000 ft after departing Omaha. The crews of the two aircraft exchanged weather information and the crew of Flight 255 advised that they had encountered light to moderate turbulence from about 15 miles southeast of the Omaha airport and that it appeared they would be out of it in another 10 miles based on their radar observations. Flight 250 terminated this conversation at approximately 2308:30 hours. This was the last transmission received from the flight. Ground witnesses stated that they observed the aircraft approach and either fly into or over a shelf of clouds preceding a line of thunderstorms that was approaching frbm the north and northwest, and that shortly thereafter they saw an explosion in the sky followed by a fireball falling out of the clouds. The aircraft crashed at approximately 2312 hours, 7.6 statute miles on a true bearing of 024.50 from Falls City, Nebraska, at an elevation of 1 078 ft AMSL. All 42 occupants have been killed.

During the takeoff roll, the pilot-in-command attempted to rotate when an unexpected situation was encountered. The captain decided to abort the takeoff and started an emergency braking procedure. Unable to stop within the remaining distance, the airplane overran and struck ditches before coming to rest in a field. While all four passengers were unhurt, both pilots were seriously injured. The aircraft was written off.

On July 11, 1961, at 1136 M.S.T., a United Air Lines DC-8 crashed during its landing roll at Stapleton Airfield, Denver, Colorado. None of the 122 occupants was severely injured as an immediate result of the impact; however, there were 16 passenger fatalities as a result of carbon monoxide poisoning when the aircraft burned. One other passenger, an elderly woman, broke both ankles during evacuation of the airplane and later succumbed to shock. In addition, the driver of a panel truck, which the aircraft struck after leaving the runway, also suffered fatal injuries. After experiencing hydraulic difficulties following takeoff from Omaha, Nebraska, the crew of N8040U continued the flight to Denver, using procedures set forth in the flight manual for abnormal hydraulic situations. When the flight arrived in the Denver area, preparations were made for landing. The ejectors were extended hydraulically, however, when an attempt was made to extend flaps to 25 degrees the hydraulic pressure dropped to zero. The hydraulic system selector was then placed in the No. 3 position (flap and gear downlock), and the approach was continued. After touchdown, the throttles were placed in the idle reverse thrust position and when power was applied, an uncontrollable deviation from the runway occurred.

Flight 329 departed Des Moines on a VFR (Visual Flight Reed) night plan at 1608 for Omaha, Nebraska. The gross weight of the aircraft was 45,215 pounds 1,685 pounds less than the allowable 46,900 pounds. According to company records, the load was properly distributed with respect to the canter of gravity of the aircraft. The climb to 5,000 feet was uneventful but at that altitude the crew noticed vibration and a slight fore-and-aft movement of the control column. The climb was continued to 6,000 feet, where the aircraft was leveled off and power was reduced. As the vibration was still present at this time, the captain attempted to dampen it by engaging the autopilot; however, this was unsuccessful and it was immediately disengaged. The first officer next lowered the flaps, first to 5 degrees and then to 15 degrees, without any noticeable effect. The “Fasten Seat Belt" sign was turned on and the captain told the first officer to advise the company of their difficulty via radio. About this time a sudden failure in the control system was felt and it was with extreme difficulty that any semblance of elevator control was maintained. The first officer again tried lowering the flaps, this time to the 24-degree position, but as this did not help to maintain control he returned them to the 15-degree position, where it was found the most favorable results were attained. Accordingly, the first officer transmitted "Mayday” (distress call) on the radio and said that they were attempting to return to Des Moines but were experiencing control trouble. The buffeting became so severe it was then necessary for the copilot to help the can hold the control column. However, the buffeting lessened and the captain advised the first officer to depressurize the aircraft and tell the stewardess to prepare the passengers for an emergency landing. This was done. By that time the aircraft had descended below 3,000 feet. Both throttles were retarded in turn to see if the trouble could possibly be caused by one of the engines. This also proved to no avail. The vibration built up to high level and suddenly another failure in the control system was felt and the air-plane went into a steep climb. As it seemed that a stall was imminent, the captain quickly moved the propellers to a high r. p. m. and pushed the throttles forward until about 50 inches of manifold pressure was seen on the gauges. The airplane then nosed over and began to dive at a very steep angle. During this rapid descent the captain reduced power and headed toward open country to his right. When the aircraft reached 500 feet above the ground the captain was successful in flaring the aircraft and it struck the ground in a flat attitude. All occupants were quickly deplaned as soon as the aircraft stopped.

Flight 16 departed Kansas City, Missouri, at 0724LT, bound for Omaha, Nebraska, Sioux City, Iowa, and other intermediate stops with final destination as Minneapolis, Minnesota. The crew consisted of Captain James H. Graham, First Officer Philip K. Toler, and Stewardess Marilyn Woodbury. Ernest F. Eilert, a trainee copilot, was riding in the cockpit as the fourth crew member. From Kansas City, the aircraft carried 21 passengers, cargo, and fuel, which resulted in a total gross weight of 25,100 pounds, which was within the certificated unit of 25,200 pounds The load was properly distributed with relation to the center of gravity of the aircraft. Weather conditions over the intended route were instrument with a general overcast lowering from 4,200 feet at Kansas City to about 1,000 feet at Omaha. No difficulty was experienced as the flight proceeded to Omaha at 4,000 feet in accordance with an instrument flight plan. A normal landing was made on Runway 11 about 1,000 feet from its approach end, but near the completion of the landing roll the aircraft ran off the right side of the runway, passing over one of the high intensity runway lights. Captain Graham reported this to one of the ground crew at Omaha, and both the aircraft and light were inspected for damage. None was found and the aircraft was prepared for departure to Sioux City. At 0841 the flight took off for Sioux City on an instrument flight plan with Omaha as the alternate airport. There were 21 passengers, 920 pounds of cargo, and 1,500 pounds of fuel, which resulted in a take-off weight of 24,630 pounds. The take-off was without incident and no difficulty was encountered en route to Sioux City, the flight proceeding at 3,000 feet altitude. At 0904 Flight 16 reported over the Sloan Fan Marker, 11.9 miles south-southeast of the approach end of Runway 35 at the Sioux City Airport. It was immediately cleared by the Sioux City Airport tower for a “straight-in” approach and landing on Runway 35. Weather information was furnished to the flight as precipitation, ceiling 500 feet, sky obscured, visibility one mile in light snow showers, and wind from the east at 14 miles per hour. The medium-intensity lights for Runway 17/35 were turned on and placed at the position of full brilliance. Following receipt of this information, the flight requested permission to land to the southeast on Runway 13 and received clearance to do so. At 0909 the flight reported that it was contact over the southeast corner of the field and was cleared to land. At the same time the aircraft was seen by a ground witness one mile southeast of the airport. Shortly thereafter, it was sighted approximately over the intersection of Runways 4/22 and 17/35 on an east-southeast heading. A left climbing turned to the north was then made and the pilot was advised that he was cleared to land on either Runway 17 or Runway 13. The pilot was also advised by the tower that there would be a 90-degree cross-wind if he elected to land on Runway 17. All transmissions to the flight were acknowledged The aircraft was not further observed, and crashed about 600 feet north and west of the approach end of Runway 17. Fire developed immediately. Three crew members and 13 passengers were killed while nine other occupants were seriously injured. The aircraft was destroyed by fire.

While on final approach to runway 21 in poor weather conditions, the aircraft was too low and hit a hill located less than one mile from the runway threshold. The aircraft was destroyed and both crew members were killed.