Airport (less than 10 km from airport)

A float-equipped Cessna Caravan, 5N-PAN, departed Lagos (LOS) on a chartered flight to Warri with a scheduled stop-over at Lekki. The aircraft was airborne at 07:34 hours UTC and was cleared to 1,000 feet by Lagos Tower and landed at Lekki at 07:42 hours UTC. At 08:20 hours UTC, the aircraft departed Lekki and called Lagos Approach which cleared it to 3,500 feet with further instructions for the aircraft to report at TMA. The aircraft reported at TMA and continued its normal flight at 3,500 feet. On contact with Escravos Tower, it requested for a descent from 3,500 feet to 700 feet in order to overfly the Chevron facility at Opuekaba for an aerial inspection. After the inspection, the aircraft was cleared to 2,500 feet to resume its normal flight to Warri. The pilot made an outbound turn to line up for the final approach to runway 03. At about five nm DME from Warri the pilot chose to reduce speed to 120 knots and he selected gear down with flap 15°. At three nautical miles out, the aircraft was about 900 feet high above the approach path, and cleared to land. The aircraft was now configured for landing with flap at 30° and the pilot reduced the speed to between 85 and 90 knots. At about 1.5 miles out, the aircraft was between 350 - 400 feet high, gliding with 400 lb of torque, the pilot felt a small shudder from the engine which was instantaneously followed by a need for power input, so he advanced the throttle but there was no response from the engine. He quickly retracted the flaps and feathered the propeller. Then the pilot re-selected flap 30° and also unfeathered the propeller which restored the engine to full torque. The pilot decided to abandon the approach mainly because of the a building structure ahead, close to the runway threshold. The pilot chose to veer the airplane to the left of the approach path centerline and ditched into the swampy terrain, cutting through some scattered trees and shrubbery.

After takeoff from Lago Argentino Airport, a red warning light came on in the cockpit panel, informing the crew about the incomplete retraction of the left main gear. The crew proceeded to a visual inspection and after confirmation that the left main gear was properly secured in its wheel well, the crew decided to continue to Río Gallegos. On approach, the left main gear did not deploy. After the crew failed to extend it manually, he raised the other landing gear and completed a belly landing. On short final, just prior to flare, both engines were shut down and their propellers were feathered. The aircraft landed on its belly, slid for few dozen metres and came to rest. All seven occupants escaped uninjured and the aircraft was damaged beyond repair.

Regency Express Air Operations Flight 434, a Cessna 208 Caravan (serial number 208B0061), was en route from Vancouver International Airport to Victoria International Airport, British Columbia, on a night visual flight rules (VFR) flight when it collided with trees on Saltspring Island, about five nautical miles (nm) north of the Victoria International Airport. The aircraft broke apart on impact and a post-crash fire occurred. The two pilots, who were the sole occupants of the aircraft, sustained fatal injuries, and the aircraft was destroyed. The accident occurred at 0030 Pacific standard time (PST).

During the takeoff roll at Mexico City-Benito Juárez Airport, at Vr, the pilot-in-command initiated the rotation but the aircraft failed to respond. For unknown reasons, the crew wait few seconds and attempted a second rotation but the aircraft still failed to respond. The captain decided to abort the takeoff and started an emergency braking procedure, deploying the tail parachute. Approaching the end of the runway, the pilot made a left turn then the aircraft veered off runway, lost its undercarriage and came to rest 150 metres further, bursting into flames. All seven occupants escaped uninjured while the aircraft was damaged beyond repair.

The airplane impacted terrain during takeoff initial climb in dark night conditions with a 100 ft ceiling and 1/4 mile visibility in fog. The instrument rated private pilot sustained serious injuries and does not recall the flight. No discrepancies were found with the aircraft, flight instruments, or engines that would have contributed to the accident. A weather briefing was obtained and an IFR flight plan was filed. The pilot had 312.8 hrs total time (54.2 hrs in this aircraft), 61 hrs night flight time (36.9 hrs in this aircraft) and 26.8 hrs actual instrument time (19.6 hrs in this aircraft). Toxicological findings were positive for benzoylecgonine (metabolite of cocaine), ethanol, and cocaethylene (substance formed when cocaine and alcohol are simultaneously ingested) in a urine sample subpoenaed by the NTSB from the hospital that treated the pilot. Benzoylecgonine can be found in urine for 3 to 5 days after cocaine use. Since blood was not available for analysis, it could not be determined how much of each substance was ingested and when they were ingested. The pilot stated that he was not under the influence of cocaine or alcohol on the day of the crash.

The single engine airplane was completing a charter flight with seven passengers and two pilots on board. While approaching Koror Airport, the crew encountered poor weather conditions with limited visibility due to heavy rain falls. The crew decided to abandon the approach and made a go-around procedure. Few minutes later, a second attempt to land was also abandoned, as well as a third and a fourth attempt. During the fifth approach, the aircraft crashed few km from the airport, killing all nine occupants. It was reported that the crew was trying to land under VFR mode in IMC conditions.

The aircraft departed Ostend Airport at 0328LT on a cargo flight to Lagos, carrying five crew members and a load of 35 tons of electronics. About 20 minutes into the flight, while cruising at an altitude of 24,000 feet over the border between Brussels and Paris ARTCC, the crew informed ATC about severe turbulences. Few seconds later, he reported the loss of the engine n°3 that separated and elected to return to Ostend. After being cleared, the crew started a circuit and while descending to Ostend Airport, the hydraulic systems failed. The crew completed a holding pattern to burn fuel and was later cleared to land on runway 26. After touchdown, the aircraft was unable to stop within the remaining distance, overran, lost its undercarriage, slid for few dozen metres and eventually came to rest near the localizer antenna. All five crew members escaped uninjured while the aircraft was damaged beyond repair.

The aircraft was completing a cargo flight from Novosibirsk to MIrny with an intermediate stop in Krasnoyarsk, carrying six passengers, seven crew members and a load of 13,380 kilos of various goods consisting of food, tobacco, clothing and footwear. Weather conditions were marginal with snow falls and icing conditions. During the takeoff roll, after a course of 2,400 metres, the pilot-in-command started the rotation at a speed of 280 km/h. After liftoff, the aircraft started to roll left and right but the crew was able to continue to climb with a rate of about 4 metres per second. During initial climb, at a height of 150 metres and at a speed of 330 km/h, the crew raised the flaps. At this time, the aircraft started to lose height, entered an uncontrolled descent, collided with trees and crashed in a wooded area located 5 km from the airport. The aircraft was totally destroyed by impact forces and a post crash fire and all 13 occupants were killed.

The Ilyushin II-62M was parked at gate with its 12 crew members on board, awaiting the passengers for the next leg to San Francisco. An Asiana Boeing 747-400 (HL7414) was taxiing to gate N6 for a refueling stop on the flight Seoul - New York (flight 211). While trying to make a U-turn, the Boeing's n°1 engine struck the wing of the Ilyushin. Then the left winglet struck the base of the Ilyushin's tail. The Asiana crew added more power causing the wing to cut through nearly half of the tail of the Russian aircraft. The maximum ground speed recorded by the on-board recorders was 16 knots, while according to the company flight manual it should have been "10 knots or below (5 knots if wet or slippery)".

The twin engine aircraft was approaching Giebelstadt AFB when it crashed in the Sommerhausen zoo located about 8 km northeast of the airfield. Both pilots were killed.