Landing (descent or approach)

According to the pilot, the airplane was high and fast on final approach, because of restricted visibility in haze, and he executed a go-around. The pilot and copilot do not recall retracting the landing gear. During the second approach, the pilot stated he did not extended the gear because he was 'sure in his mind that the gear was already down'. The airplane landed with the gear retracted. The airplane slid approximately 3,000 feet. Following the landing, the airplane caught fire under the right wing root, and the fire could not be extinguished with hand held fire extinguishers. Both pilots safely evacuated the airplane.

The crew was completing a local training flight at Pope AFB. For unknown reasons, the aircraft landed very hard, causing the nose gear to collapse. The aircraft was stopped on the runway and all 11 occupants escaped uninjured. The aircraft was damaged beyond repair.

On approach to Puerto Inírida Airport, the single engine airplane collided with a private Cessna 206 registered OB-1450 and carrying two passengers and one pilot. Both aircraft dove into the ground and crashed about 5 km from the airport. Both aircraft were destroyed and all 12 occupants were killed.

En route from Guayaquil to San Cristóbal, the crew encountered technical problems with the antiskid system. It was decided to perform a low approach to runway 16 to land on the first metres of the runway. On short final, the aircraft was too low, struck approach lights and landed 36 metres short of runway 16 threshold. On impact, the undercarriage were torn off and the aircraft skidded for about 700 metres before coming to rest. All 56 occupants escaped uninjured while the aircraft was damaged beyond repair.

After landing at Bamyan Airport, the aircraft was unable to stop within the remaining distance. It overran and crashed in a ravine. Two people survived while 13 others were killed.

During a landing approach, the pilot noted that the right engine remained at a high power setting, when he moved the power levers to reduce power. He executed a missed approach and had difficulty keeping the airplane straight and level. The pilot maneuvered for a second approach to land. After landing, he could not maintain directional control of the airplane and tried to go around, but the airplane went off the end of the runway and impacted the localizer antenna. The pilot did not advise ATC of the problem nor did he declare an emergency. The Pilot's Operating Handbook stated that for a power plant control malfunction, the affected engine should be shut down, and a single engine landing should be made. The power control cable was found disconnected from the anchoring point. A safety tab was broken off the housing, allowing it to unscrew. About one month before the accident, maintenance had been performed on the right engine to correct a discrepancy about the right engine power lever being stiff. The mechanic re-rigged the right engine power cable.

Damaged beyond repair following a hard landing at Lucapa Airport. All four crew members escaped uninjured.

The pilot was cleared for a localizer approach by Atlanta Center and told to maintain 5,000 feet until crossing the final approach fix (FAF). Normal altitude at the FAF was 2,700 feet. The pilot was unable to land from this approach and performed a missed approach. He was handed off to Chattanooga Approach, then was cleared to cross the FAF at 3,000 feet and perform another localizer approach. About one mile from the FAF, the pilot was told to change to the airport advisory frequency. The pilot acknowledged, then there was no further communication with the aircraft. A short time later, witnesses heard the aircraft crash near the approach end of the runway. Examination of the crash site showed the aircraft had touched down in a grass area about 1,100 feet from the end of the runway, while on the localizer. Propeller slash marks showed both engines were operating at approach power and the aircraft was at approach speed. No evidence of precrash mechanical failure or malfunction of the aircraft structure, flight controls, systems, engines, or propellers was found. The 0621 weather was in part: 300 feet overcast and 1/2 mile visibility with fog. Minimum descent altitude (MDA) for the localizer approach was 1,180 feet msl; airport elevation was 710 feet. The pilot had flown 8 flight hours, was on duty for 13.6 hours the day before the accident, was off duty for about 6 hrs, and had about 4 hours of sleep before the accident flight.

On final approach to Semarang-Ahmad Yani Airport runway 31, the twin engine aircraft went out of control and crashed in the district of Bongsari, less than 3 km from the airport. All seven occupants were injured.

The Beech 1900C cargo aircraft was loaded with more than 4,962 pounds of cargo during an approximate 20 minute period. No scale was available at the aircraft, forcing loaders to rely on tallying either waybill weights or estimates of total cargo weight and center of gravity (CG) during the brief loading period. Additionally, a strike had shut down a major cargo competitor at the time with substantial cargo overflow to the operator. Post-crash examination determined the cargo load was 656 pounds greater than that documented on the pilot's load manifest, and the CG was between 6.8 and 11.3 inches aft of the aft limit. The airplane behaved normally, according to the pilot, until he initiated full flaps for landing approaching the threshold of runway 34L at the Seattle-Tacoma International airport. At this time, the aircraft's airspeed began to decay rapidly and a high sink rate developed as the aircraft entered into a stall/mush condition. The aircraft then landed hard, overloading the nose and left-main landing gear which collapsed. A post-impact fuel system leak during the ground slide led to a post-crash fire.