Douglas C-118 Liftmaster

The flight crew was landing the transport-category airplane at a remote, gravel-covered runway. According to the captain, the terrain on the approach to the runway sloped down toward the approach end, which positioned the airplane close to terrain during the final stages of the approach. A video recorded by a bystander showed that while the airplane was on short final approach, it flew low on the glidepath and dragged its landing gear through vegetation near the approach end of the runway. The video showed that, just before the main landing gear wheels reached the runway threshold, the right main landing wheel impacted a dirt and rock berm. The captain said that to keep the airplane from veering to the right, he placed the No. 1 and No. 2 engine propellers in reverse pitch. The flight engineer applied asymmetric reverse thrust to help correct for the right turning tendency, and the airplane tracked straight for about 2,000 ft. The video then showed that the right main landing gear assembly separated, and the airplane continued straight down the runway before veering to the right, exiting the runway, and spinning about 180°, resulting in substantial damage to the fuselage. On-site examination of the runway revealed several 4-ft piles of rocks and dirt at the runway threshold, which is likely what the right main landing wheel impacted. Given that the airplane landing gear struck vegetation and rocks on the approach to the runway, it is likely that they were below the proper glidepath for the approach. The crew stated there were no preaccident mechanical malfunctions or anomalies that would have precluded normal operation.

The four engine aircraft was completing a cargo flight from Punta Arenas, carrying two passengers, six crew members and several sleigh dogs. On final approach, the captain decided to slightly deviate from the approach path to avoid local patches of fog and thus maintaining a visual contact with the ground. At an altitude of 450 feet, he increased engine power but the aircraft continued to descent until it struck the ground near the camp. All eight occupants and all animals were evacuated safely while the aircraft was damaged beyond repair.

While cruising by night on a cargo flight from Willemstad-Hato Airport to Miami-Intl Airport, the four engine aircraft entered an uncontrolled descent and crashed in the Caribbean Sea. Few debris floating on water and the dead body of the copilot were found about 210 km northwest of Curaçao Island. The aircraft was flying in poor weather conditions with thunderstorm activity and turbulences when the accident occurred.

The four engine aircraft was chartered by the Colombian Army to transfer 80 soldiers from Bogotá to Arauca. They were seating on the cabin floor with their equipment. In the morning, the crew encountered technical problems after takeoff from Bogotá Airport and was forced to return. After repairs were completed, the aircraft departed again before noon. During initial climb, the engine n°1 caught fire. The crew declared an emergency and was cleared to return when the fire spread to the engine n°2. The captain realized he could not reach the airport so he attempted an emergency landing in a pasture located 16 km from the airfield. The aircraft belly landed and slid for about 400 meters before coming to rest, bursting into flames. All 85 occupants escaped uninjured while the aircraft was destroyed by fire.

A Douglas C-118A (DC-6A) fire fighting plane was destroyed in an accident near Sainte-Anne-des-Monts, QC, Canada. All four crew members were killed. The Conifair plane took off from Bonaventure Airport, QC (YVB) at 19:15 for a spray operation 30 miles southeast of Sainte-Anne-des-Monts. This was to be the last spraying flight of the season out of the Bonaventure base. A crew of four was on board, including two flight engineers who were on a familiarization training flight. The aircraft was carrying 2,952 U.S. gallons of Dipel 132, a non-toxic microbial insecticide. The aircraft arrived over the spray area at 19:35. An inertial navigation system (INS) to follow pre-established spraying tracks. The first track was sprayed uneventfully. At the end of the first track, the aircraft made a 180-degree turn to spray the second track, which was parallel to and about 800 feet northeast of the first track. This meant that the aircraft had to fly from a valley at an elevation of 1,000 feet above sea level (asl) up a mountain consisting of two levels. The first level is about 1,800 feet asl and about 3,280 feet along the flight path. After the first level, the terrain rose within approximately 1,000 feet along the flight path, to the summit of the mountain at an elevation of 2,175 feet asl. The two occupants of a Cessna 310 spotter aircraft observed a decrease of the DC-6A ground speed during the climb over the first level of the mountain. They then noticed that the aircraft yawed and started a steep, left turn. The spotter crew stated that, shortly after the start of the left turn, the DC-6A left wing began to strike trees. The aircraft nosed down, crashed on the side of the mountain, and exploded at an elevation of 2,050 feet asl.