Boeing 737-200

During the takeoff roll from Najran Airport runway 06/24, at a speed of 95 knots, the right engine thrust suddenly increased. Few seconds later, at a speed of 120 knots, the exhaust gas temperature warning came on in the cockpit panel. The captain decided to abort and initiated an emergency landing procedure. Speed brakes were deployed but the thrust reversers could not be activated. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and right engine before coming to rest. All 85 occupants evacuated safely.

During the takeoff roll on runway 23 at Douala Airport, at a speed of 110 knots, the crew noted a loud bang and decided to abort. The crew initiated an emergency braking procedure but the aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and both engines before coming to rest 130 metres further, bursting into flames. All 114 occupants were evacuated, among them 20 were slightly injured. The aircraft was destroyed.

The aircraft departed Belém-Val de Cans Airport on a flight to Brasília with intermediate stops in Marabá and Carajás, carrying 48 passengers and a crew of six. The approach to Carajás-Parauapebas Airport was completed in poor weather conditions with rain falls, clouds down to 120 metres and a limited visibility due to rain and fog. On final the aircraft was unstable and landed hard on runway 10. On touchdown, the right main gear was torn off and the aircraft went out of control. It veered off runway to the right, collided with trees and eventually came to rest in a wooded area. The copilot was killed as the right side of the cockpit was destroyed upon impact. Ten other people were injured and 43 escaped unhurt. The aircraft was destroyed.

During the takeoff roll, the captain noted a difference in the engine N1 readings. He decided to abandon the takeoff procedure and initiated an emergency braking manoeuvre. Unable to stop within the remaining distance, the aircraft overran, lost its nose gear and came to rest 40 metres further. All 106 occupants escaped uninjured and the aircraft was damaged beyond repair.

A United States Air Force Boeing T-43A (USAF designation for the Boeing 737-200) was destroyed after impacting a hillside during an NDB approach to Dubrovnik Airport, Croatia. All 35 on board were killed. The aircraft was engaged in a mission to fly United States Secretary of Commerce Ron Brown and a delegation of industry executives around the region for visits. The party was to be flown from Zagreb to Tuzla and Dubrovnik before returning to Zagreb. Operating with a call sign of IFO21, the accident aircraft departed Zagreb at 06:24 hours. The crew landed at Tuzla at 07:15 after an uneventful flight. The passengers deplaned, and the aircraft was then repositioned to Split because of insufficient ramp space at Tuzla to park the aircraft for the duration of the visit. At 12:47, the aircraft landed at Tuzla, where the passengers reboarded. The accident flight departed Tuzla for Dubrovnik at 13:55. After crossing Split at 14:34 the flight was cleared to descend from FL210 to FL140. Further descent clearance was given to FL100. After the aircraft reached FL100 at 14:45, south of Split VOR, Zagreb Center transferred control to Dubrovnik Approach/Tower. The controller cleared IFO21 direct to the Kolocep (KLP) NDB. After opposite-direction traffic had been cleared, IFO21 was cleared to descend to 5000 feet. At 14:52, the crew told Dubrovnik Approach/Tower that they were 16 NM from the airport. They were cleared to descend to 4,000 feet and told to report crossing the KLP beacon. At 14:53, the aircraft crossed KLP, which was the Final Approach Fix (FAF), at 4100 feet and began the approach without approach clearance from Dubrovnik Tower. At that point the aircraft was slightly high and fast and not completely configured for the approach, as it should have been. At 14:54, the copilot of IFO21 called Dubrovnik Approach/Tower and said, "We’re inside the locator, inbound." IFO21 was then cleared for the NDB approach to runway 12. The aircraft tracked a course of 110 degrees after crossing KLP, instead of tracking the published course of 119 degrees. The aircraft maintained this track from KLP to the point of impact. The accident aircraft descended to 2200 feet which was consistent with the published minimum descent altitude of 2,150 feet. At 14:57, the aircraft impacted a rocky mountainside approximately 1.7 NM to the left (northeast) of the extended runway centerline and 1.8 NM north of the approach end of runway 12 at Dubrovnik Airport.

The approach to Arequipa-Rodríguez Ballón Airport was completed by night and poor weather conditions with heavy rain falls. On final approach, the crew failed to realize his altitude was insufficient when the aircraft struck a hill and crashed 6,3 km from runway 09 threshold. The aircraft disintegrated on impact and all 123 occupants were killed.

While on a night approach to Douala Airport, at a distance of 3,5 NM, the crew was cleared to land on runway 30. At this time, the aircraft initiated a slight climb and about 15 seconds later, the copilot informed ATC about technical problems. Three seconds later, the aircraft rolled to the left, struck trees and crashed in a mangrove located about 1,700 metres south of runway 30, bursting into flames. Three passengers and two crew members (the copilot and a stewardess) were seriously injured while 71 other occupants were killed.

Following a wrong approach configuration, the aircraft landed too far down the runway, about 600 metres from the runway end. Unable to stop within the remaining distance, the aircraft overran, struck a concrete wall (45 cm high) and came to rest 450 metres further. All 108 occupants were evacuated safely and the aircraft was damaged beyond repair.

Nigeria Airways flight WT357 departed Yola (YOL) at 07:00 en route to Lagos (LOS). Intermediate stops were planned at Jos (JOS) and Kaduna (KAD). The Boeing 737 landed at Jos at 07:40 and departed fifty minutes later. The flight to Kaduna was uneventful. Kaduna ATC gave the aircraft an inbound clearance with no delay for a locator approach to runway 05. Though, the initial landing clearance was for runway 05, the captain requested to land on runway 23. He was reminded by the controller that the wind was from 090 magnetic, but he still insisted on using the 23 approach. At 08:42, the aircraft commenced its initial descent at 48 miles on the ILS/DME to 4,500 ft. At 08:49 UTC, it was cleared to 3,500 ft at 10 miles out and was later descended to 500 ft. The aircraft turned left from the track 310 to align with runway 23 and the aircraft was still in the turn when the threshold was sighted just 1.5 miles to the left of the aircraft. The first officer asked the captain "Can you make it to land from that position?". The observer in the jump seat also suggested going on the downwind, presumably to re-position the aircraft for landing on runway 05. There was no response at all from the captain and the approach was continued for runway 23. The left turn was very steep and it took the aircraft to the left of the runway centreline and a right correction was applied. The observer shouted "Watch the wing" as the wings could have struck the ground on the final approach. By this time, the aircraft crossed the threshold with the flying pilot still struggling to maintain directional control for runway centreline alignment. The aircraft touched down 7820 feet down the runway, leaving just 2020 ft (615.85 m) of runway length. The captain was reported to have used 1.8 and 1.6 EPR on the reversers. When a runway overrun became inevitable, the captain turned the aircraft to the left with the intention to take advantage of the last rapid exit intersection to avoid the runway end lights. At this juncture, the aircraft entered an uncontrollable skid. The right wing hit the ground, thus rupturing the fuel tanks and a huge fire erupted. The aircraft was destroyed by the fire.