Douglas DC-3

Before departure from Damascus on a regular schedule flight to Aleppo, the crew was informed about the recent disappearance of a Netherlands Navy Catalina over Lebanon. Thus, it was requested to the crew to make a detour over Lebanon to see if it was possible to locate the wreckage. While cruising in poor weather conditions, the Dakota hit the slope of a mountain located in Dahr el-Kadib. Nine occupants were killed while six others were injured.

The crew was performing a cargo flight in Czechoslovakia, carrying a load of newspapers on behalf of the national career CSA Czech Airlines. While on a night approach to Brno-Tuřany Airport, the aircraft hit the slope of Mt Bradlo (548 meters high) located in the Chriby Mountain Range, about 2,5 km northwest of Vřesovice. The wreckage was found 35 km east of Tuřany Airport and all five crew members were killed.
Crew:
Větroň Antonín,
Antal Viliam,
Dvořák Jiří,
Gregr František,
Koval Vlastimil.

The TS-62 took off from Leningrad-Shosseynaya Airport and its crew received the permission to climb to the altitude of 2,700 meters via the corridor number two. While climbing into clouds, the airplane collided with an Aeroflot Ilyushin II-12 that was approaching the same Airport. Inbound from Minsk, the II-12 was registered CCCP-L1328 and was carrying 19 passengers and a crew of five. Its pilot obtained the permission from ATC to descend to the altitude of 1,200 meters via the same corridor number two. At the altitude of 1,200 meters, both aircraft collided, dove into the ground and crashed in a field located near the village of Skvoritsy, about 23 km southwest of Leningrad-Shosseynaya Airport. Both wreckage were found 1,200 meters from each other and all 31 occupants were killed.

The crew was performing a positioning flight to Khartoum to meet the Sudanese people who chartered the plane to complete a pilgrim flight from Aden to Djeddah. As the airplane failed to arrive in Khartoum, SAR operations were conducted and the wreckage was found nine days later, on September 20, on the slope of a mountain located about 80 km southeast of Wadi Halfa. The aircraft was destroyed and all three crew members have been killed.

Just after liftoff, the airplane hit successively a truck and few houses before crashing into flames. Three people on the ground were killed while all 23 occupants survived. It is believed that the crew decided to takeoff from an unsuitable terrain for such aircraft type.

While approaching Ipoh on a flight from Medan, the crew encountered poor weather conditions when control was lost. The aircraft crashed into the Malacca Strait, few km off shore, killing all 17 occupants.

While approaching San Felipe from the east in a limited visibility, the airplane hit the slope of the Cerro Grande located about 30 km from the San Felipe Airport. All 12 occupants were killed.

On final approach to Uberlândia Airport, the airplane was too low and hit trees with its left wing, stalled and crashed. Six passengers and three crew members were killed while 22 other occupants were injured. The aircraft was destroyed.

United Air Lines operates a Flight Training Center at Denver, Colorado, to train applicants for first officer positions with the company. The crew of United Trainer 16 consisted of Senior First Officer Jordan D. Kocher, who had been designated by United Air Lines as captain and instructor, and Trainee First Officers Laurence G. Wilson and Wayne C. Moen. The flight departed Stapleton Airfield at 0655LT. The 0628 weather conditions, upon which the crew had been briefed, were ceiling measured 15,000 feet, visibility 25 miles, and wind northwest 14 knots Ceiling and visibility were unlimited at the time of the accident, with the wind northwest 16 knots. No radio contacts were made by United Trainer 16 after reporting departure time. It was cleared for a training flight of four hours’ duration within a 25-mile radius of Denver Captain Kocher occupied the left pilot’s seat at takeoff. Upon departure, the aircraft load, in addition to the crew, was 820 gallons of gasoline, full oil tanks, and 650 pounds of sand ballast tied down in the rear baggage pit. The load was properly distributed with relation to the aircraft’s center of gravity, and the 22,910-pound gross weight at takeoff was within allowable limits. Witnesses reported that at between 0720 and 0725 the aircraft was seen to stall, enter a spin, and strike the ground in a diving attitude before recovery was effected.

The aircraft took off from Paris-Le Bourget Airport at 0750LT on a flight to test a new type of air scoop. The new scoop was fitted to one engine only to allow comparison tests to be made. Five minutes later, the aircraft reached the altitude of 4,300 feet and four minutes later, at 0759LT, the starboard engine was stopped and the test commenced with a climb on the port engine with cooling gills open. At 0811LT, at an altitude of 6,980 feet, the crew commenced the second phase of the test with the port engine cooling gills in the trail position. Level off was completed at 0822LT at an altitude of 7,900 feet with the cooling gills closed. About an hour later, while flying at a relative low speed, the airplane went out of control and entered a spin, lost its empennage and eventually crashed in a field located in Moisville. The aircraft was destroyed and all five crew members were killed.
Crew:
René Gallichet, pilot,
Louis Pichard, flight engineer,
Jacques Légalité, radio navigator,
Lucien Goulay, engineer,
Paul Martin, engineer.