Buffalo

While in cruising altitude on a cargo flight from Buffalo to Beaver Falls, the twin engine airplane suffered an fire/explosion. It lost height and crashed in a corn field located near Mercer. The aircraft was totally destroyed upon impact and both crew members were killed.

While on approach to Rochester-Greater Rochester Airport, the pilot lost control of the airplane that entered a dive and crashed in flames in the Cheektowaga County. The aircraft was destroyed and the pilot, sole on board, was killed.

Flight NW6231 departed New York-JFK at 19:14 for a ferry flight to Buffalo and was cleared by departure control to climb to FL140. At 19:21 the flight was cleared to climb to FL310. The aircraft began to climb 2,500 fpm at an airspeed of 305 knots. As the aircraft climbed through FL160, both the airspeed and the rate of climb began to increase. Reaching FL230, the airspeed had reached 405 knots and the rate of climb had exceeded 6,500 fpm. The overspeed warning horn sounded a little later, followed 10 seconds later by a stick shaker stall warning. The aircraft then leveled at 24800 feet with a speed of 420 knots until it turned rapidly to the right, 13 seconds later. The airplane started to descend out of control, reaching a vertical acceleration of +5g until it struck the ground in a slightly nose down and right wing-down attitude. The aircraft had descended from 24000 feet to 1090 feet in 83 seconds.

The crew departed Buffalo Airport on a cargo flight to Pittsburgh. Few minutes after takeoff, the right engine caught fire and the crew declared an emergency. The fire spread to the engine nacelle and the right wing that detached. Out of control, the airplane dove into the ground and crashed in flames in an open field located in Hamburg, about 15,5 miles south of Buffalo Airport. The aircraft was destroyed and both occupants were killed.

Shortly after takeoff from Buffalo Airport, while in initial climb, the left engine lost power. The aircraft banked left, lost height then crashed onto several houses located in the residential area of Cheektowaga, about two miles south of the airport. The airplane was destroyed and all three occupants were killed as well as three people on the ground.

While flying at low altitude, the pilot encountered patches of fog when the single engine airplane hit tree tops and crashed in a wooded area located in Lewis, NY. The wreckage was found two days later and the pilot, sole on board, was killed.

After takeoff from Buffalo Airport, the crew was cleared to climb to 8,000 feet. About an hour into the flight, the airplane went out of control, entered a dive and crashed near Lake Milton, Ohio. The crew was unable to send any distress call. The aircraft disintegrated on impact and all 13 occupants were killed.

Flight 542 departed the ramp at Houston at 2237LT, 22 minutes behind schedule with a total of 34 persons including a crew of six consisting of Captain Wilson Elza Stone, First Officer Dan Hollowell, Second Officer Roland Longhill, and Stewardesses Alvilyn Harrison, Betty Rusch and Leona Winkler, none of whom survived. The delayed departure was due to a mechanical discrepancy involving No. 3 generator. This generator was inoperative on arrival of N9705C at Houston. Prior to departure from Houston the Nos. 3 and 4 voltage regulators were interchanged. Actual gross weight upon departure was calculated at 83,252 pounds, including 17,000 pounds of fuel, and was 16,548 pounds less than the authorized gross weight of 99,800 pounds. The estimated time en route to Dallas was 41 minutes. The flight was given an instrument-flight-rules clearance which was to the Leona omni, via Victor Airway 13 west to the Gulf Coast intersection, direct to Leona, to maintain 2,300 feet altitude to Gulf Coast, then to climb to and maintain 9,000. At approximately 2240 the flight was cleared for takeoff and at 2242 it reported ready for takeoff and was airborne at 2244. After takeoff Houston departure control advised that it had the flight in radar contact and requested it to report when established outbound on the 345-degree radial of the Houston omni. Flight 542 complied and subsequently was cleared to 9,000 feet and advised to contact San Antonio Center on 121.1 mcs. upon passing the Gulf Coast intersection. Flight 542 reported to company radio at 2251 as blocking out of Houston at 37, taking off at 42, to cruise at 15,000 feet when so cleared, estimating Dallas at 2325, and that the Center had this information. At approximately 2252 Flight 542 reported to San Antonio Center as being over Gulf Coast intersection at 9,000 feet. The flight was then issued its destination clearance to the Dallas Airport via direct to Leona, direct to Trinidad, direct to Forney, direct to Dallas, to maintain 15,000 feet. The flight was cleared to climb to its cruising altitude. The next transmission from Flight 542 was to the San Antonio, Center, giving the time over Leona as 05 at 15,000. San Antonio Center acknowledged, and requested Flight 542 to change over and monitor the Fort Worth frequency of 120.8 mcs. at this time. The flight acknowledged. Shortly thereafter Flight 542 contacted company radio with a message for maintenance, advising that the generators were then OK out that there had been insufficient time for maintenance to insulate the terminal strip on No. 3 propeller at Houston and it would like to have it done in Dallas. At this time the flight also said it would give the communication center a Dallas estimate of 25. This was then followed by one other item for maintenance, which was that No. 3 sump pump was inoperative. This was the final transmission from the flight and was logged as completed at 2307. Structural failure of the aircraft occurred at approximately 2309 on course to the next fix, Trinidad intersection. The radial from Leona omni to Trinidad intersection is 344 degrees. The main wreckage was located 19.7 miles 2 north of Leona omni, 3.19 miles east-southeast of Buffalo, Texas. The time, 2309, correlates closely with the information obtained from witnesses to the accident as well as the time indicated on impact-stopped watches recovered at the scene. The aircraft was destroyed upon impact and all 34 occupants were killed.

The DC-4 was on a simulated ILS approach to Pittsburgh when the copilot established visual reference with the runway. The approach was continued visually but the rate of descent was excessive. The captain applied power, but before recovery was complete, the right main gear struck an embankment short of runway. Full power was applied and a go-around was carried out. Severe buffeting and a number three engine fire were experienced as the DC-4 circled for another approach. The landing was carried out safely and all 55 occupants were evacuated. The aircraft was later considered as damaged beyond repair.

While taxiing to Runway 23 the flight received an IFR (Instrument Plight Rules) clearance from ARTC (Air Route Traffic Control). Normal pre-takeoff checks were performed and the takeoff roll was started at 1640. The aircraft became airborne after using approximately one-half of the 5.630-foot runway. Immediately after leaving the ground the gear was raised and the first officer saw the left feathering button light come on dimly which indicated that the left propeller was in the process of being feathered by the auto-feathering system. After definitely determining the light was on and visually checking the left propeller, the auto-feathering system was disarmed and the captain., in an effort to stop the feathering cycle, pulled the feathering button to neutral. This effort was unsuccessful. the left propeller feathered, and the engine stopped. During the climb an air speed of 140 m.p.h. was reached and maintained., the right engine remaining at full takeoff power. Approximately 250 feet above the ground a shallow left turn was started and the first officer was ordered to reinstate the left engine. the captain believing the aircraft would climb no farther. In the effort to restart the left engine by unfeathering the left propeller. only 600 r.p.m. could be obtained and the captain felt a buffeting through the control yoke. The aircraft at this time had progressed in the left turn approximately 180 degrees from the takeoff direction and the captain. fearing he would be unable to clear obstructions. Including high tension lines, decided to make a wheels-up landing. The landing was made in a field approximately one mile south of the airport. When the aircraft stopped, the passengers and crew evacuated it in an expeditious and orderly manner. The airplane was damaged beyond repair.