Landing (descent or approach)

After landing at Kupang-El Tari Airport, the twin engine aircraft went out of control, veered off runway, lost its left wing and came to rest. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

At 1136 AST, the twin engine airplane departed San Juan, PR, on a flight to St Vincent. About 1208 AST, the pilot contacted ATC and indicated that he would like to divert to St Thomas. He informed the controller that he had 'feathered' the left engine due to loss of the left engine cowling, but he did not declare an emergency. He requested wind information for St Thomas, then at about 1613 AST, he changed his destination to Roosevelt Roads, PR. At 1120 AST, the pilot reported that the airplane was losing about 300'/min, then about 1 minute later, he said he was going to attempt an engine restart, and that the airplane was getting close to the water. A short time later, he informed ATC that he was not going to make it to shore. The pilot acknowledged info that search and rescue personnel were responding, then there was not further contact with the airplane. The airplane was located about 6 miles east of Roosevelt Roads NAS, but the pilot was not found. Review of weight and balance info revealed the pilot did not follow written procedures, and that the airplane exceeded the maximum authorized gross weight for take off. Flight crews had been informed of a communique from the manufacturer that there was no need to shut down an engine and feather the propeller unless engine performance or a major vibration problem confirmed the need.

The crew was completing a local training at Orléans-Bricy AFB. Following several circuits, the crew was attempting a new approach by night when the aircraft struck power cables, lost height and crashed in a field located near Chevilly, few km from the runway threshold. All three crew members were injured and the aircraft was destroyed. It was reported that the crew was forced to shut an engine down few seconds prior to the accident while flying in icing conditions. Despite the aircraft was established on the ILS, the crew was descending at an insufficient altitude. At the time of the accident, the visibility was limited.

Shortly after takeoff from Banjarmasin-Syamsudin Noor Airport, while climbing, the crew informed ATC about an engine fire and was cleared to return for an emergency landing. On final approach, the aircraft became unstable, rolled left and right then lost height and crashed on a factory located 2 km short of runway. A passenger was seriously injured while 16 other occupants as well as two people in the factory were killed.

On final approach to Fort Chipewayn Airport, the twin engine aircraft was unstable and rolling left and right. Upon landing, the right propeller struck the runway surface. The right engine partially torn off and the right wing was severely bent. The aircraft came to a halt few dozen metres further. All 14 occupants escaped uninjured.

Learjet L36A (serial number 033), N14TX, was on an instrument flight rules (IFR) flight from Grand Rapids, Michigan, to Stephenville, Newfoundland. At 0216 Newfoundland standard time (NST1), N14TX was cleared by Gander Area Control Centre (ACC) for an approach to the Stephenville airport. The co-pilot contacted the St. John=s Flight Service Station (FSS) and advised that they would be conducting an approach to runway 28. The FSS specialist relayed the latest Stephenville weather observation and runway surface condition report to the aircraft and requested that the crew advise St. John=s FSS when they had landed. When the crew of N14TX did not report after landing at Stephenville, the St. John=s FSS specialist advised Gander ACC that the aircraft was missing, and a search was begun. Initial information received by the agencies searching for the missing aircraft did not include the aircraft=s last recorded radar position. The wreckage was located approximately three hours and ten minutes after the aircraft was reported missing, within the airport perimeter, close to the last observed aircraft radar position. The aircraft struck a service road embankment in an inverted, wings-level attitude. The two crew members were fatally injured. The accident occurred during the hours of darkness at approximately 0238 NST.

On final approach to Nyagan Airport, the crew realized he was not properly aligned with the runway but decided to continue. Upon touchdown, the right wing struck the runway surface. The aircraft rolled left and right for about 800 metres then veered off runway and came to rest in a ravine. All 15 occupants were injured, six seriously.

After 2 previous attempts, the pilot was cleared for a third VOR Runway 14 Approach. He was issued landing information, and he reported the airport in sight. The minimum descent altitude (MDA) for the approach was 1,620 ft msl. The airport elevation was 1297 ft. The airplane was observed by an ATC controller to descend, and the controller's Brite scope (radar) displayed 1,400 ft. The controller observed the airplane's landing light bob up and down, followed by the nose pitching up. At about the same time, a ground witness in the area saw the airplane at low altitude; according to this witness, the pilot tried to 'pull the plane up' just before it collided with the static cable of a power line. The cable was about 85 feet above ground level (1,382 feet MSL) and approximately 2 miles from the approach end of the runway. No preimpact malfunction of the airplane, engine, or VOR was found.

After touchdown at San Jose Airport, the aircraft collided with a dog. On impact, the right main gear collapsed and the aircraft came to rest on its belly. The right engine struck the ground and caught fire. All three occupants escaped uninjured while the aircraft was damaged beyond repair. The dog was killed.

Ethiopian Airlines flight ET961 had taken off from Addis Ababa, Ethiopia, at 08:09 hours UTC for a scheduled flight to Abidjan, Ivory Coast via Nairobi, Kenya; Brazzaville, Congo; and Lagos, Nigeria. Twenty minutes after takeoff, at about 08:29 UTC, one passenger stood up from his seat and ran up the aisle to the cockpit, and two other passengers followed him heading for the cockpit. While rushing to the cockpit one of the men said "Everybody should be seated, I have a bomb!". Then they opened the cockpit door and stormed in. They declared to the pilots that there were eleven hijackers on board and beat the First Officer and forced him out of the cockpit. They then grabbed the fire axe and fire extinguisher bottle from their respective stowages and ordered the pilot-in-command to change direction and fly to Australia. The pilot-in-command explained to the hijackers that he had not enough fuel to reach Australia and demanded to make a refueling stop at Mombasa. The hijackers refused the refueling stop and continued arguing with the pilot-in-command. They insisted that they had learned from the inflight magazine that the B767 could fly 11 hours without refueling. After passing Dar es Salaam one of the hijackers ordered him to fly away from the coast, head to Australia and indicating to the altimeter not to descend below FL390. The pilot-in-command turned left towards the Comoros Island. The lead hijacker was sitting in the first officer's seat and was fiddling with the aircraft's controls, kicking the rudder, whilst also drinking whisky. The pilot-in-command kept on telling them that he was running short of fuel pointing to the fuel quantity indicators, but the hijackers did not listen. The leader continued fiddling with the controls, trying to turn the aileron and pulling the reverse thrust lever at random. As the flight came over the Comoros Islands the pilot-in-command saw the Moroni International Airport runway and circled 15-20 nm south of the field. Then the LOW FUEL CAUTION came on. The pilot-in-command pleaded to land because of low fuel. The hijackers were unconcerned and only insisted that the pilot not descend below FL390. At about 11:41 UTC the right engine ran down to wind milling speed. The pilot-in-command showed the red warning message for the right engine on the EICAS to the hijacker. At this moment, the hijacker left the right seat and went to the cabin door to discuss with the other two hijackers. This gave the captain the opportunity to pick up his microphone and address the passengers: "....ladies and gentlemen this is your pilot, we have run out of fuel and we are losing one engine this time, and we are expecting crash landing and that is all I have to say. we have lost already one engine, and I ask all passengers to react ..... to the hijackers ....". The hijacker then came back to the cockpit and hit the microphone out of the pilot's hand. After the right engine failed, the pilot started to descend the aircraft in order to increase speed, but the hijacker again interfered and violently played with the controls which resulted in improper control inputs. As a result the autopilot was disconnected and the flight became erratic with the airspeed varying between 216 and 336 kts. As the pilot regained control of the aircraft, the left engine went dead. The hijacker kept on instructing the pilot not to descend and again went to the cabin. Upon returning to the cockpit he saw that the altitude was decreasing, and angrily shouted at the pilot not to go any lower. The pilot said that the fuel was already finished and that the engines were without power. This time the hijacker instructed the captain not to touch the controls, and threatened to kill him. The captain said, "I am already dead because I am flying an airplane without engine power." The first officer, who had earlier been forced out to the First Class cabin, got up and, via the right aisle, went to the rear of the aircraft where he saw that a lot of economy class passengers had their life jackets on and that some had already inflated them. The first officer, along with the cabin crew members, helped the passengers to deflate the life jackets and showed them how the jackets should be re-inflated and how to assume the brace position during impact. While returning to the front of the aircraft, they repeated the same instructions as many times as they could. About less than 2 minutes before the ditching, the co-pilot forced his way to the cockpit shouting "let me help the pilot ...". After adjusting his seat and seat belts the pilot asked him for help since the controls were heavy. The hijackers still kept on struggling with the controls. By now, the aircraft was descending into the Indian Ocean over the Comoros Islands. The aircraft now had only standby instruments and RAT (Ram Air Turbine). The altimeter was indicating 150 feet and the airspeed was 200 kts. By this time the flight crew had been left alone to assume control. They turned the aircraft to the left in order to parallel the waves. However, the aircraft brushed the water in a left-wing-low attitude. It was then held straight and level after which it broke into four sections and came to rest in the sheltered waters 500 metres off Le Galawa Beach. Of the 175 occupants, 6 crew members and 119 passengers were fatally injured in the accident. Six crew members and 38 passengers sustained serious injuries, 2 passengers sustained minor injuries and 4 passengers received no injury.