Landing (descent or approach)

The aircraft departed Shanghai-Hongqiao Airport at 2116LT on a cargo flight to Subic Bay with a load of electronics and garments. Weather conditions at Subic Bay Airport was at follow: scattered at 1,800 feet and 7,000 feet, light rain, wind calm and visibility six km. At 2315LT, the aircraft landed on runway 07 (2,400 metres long). Unable to stop within the remaining distance (the runway was wet), the aircraft overran and plunged in the Subic Bay. Both pilots were injured and the aircraft was totally destroyed.

While on an ILS approach to runway 24 at Kinshasa-N'Djili Airport, the captain decided to initiate a go-around procedure. While in a circuit in the vicinity of the airport, the pilot informed ATC he would complete the second approach visually and made a short pattern because of low fuel reserve. On approach with a 6 knots tailwind, the aircraft was unstable and not properly aligned when it landed hard on the left of the centerline. Out of control, it veered off runway to the left, lost its undercarriage and came to rest few hundred metres further, bursting into flames. All eight occupants were rescued, among them one was slightly injured. The aircraft was totally destroyed by impact forces and a post crash fire.

While on an ILS approach to Parma Airport in poor weather conditions, the aircraft struck the ground and crashed in an open field about 3,5 km short of runway. All eight occupants were rescued, among them one pilot was injured. The aircraft was damaged beyond repair. The visibility was limited to 800 metres due to foggy conditions.

On approach, the single engine aircraft collided with trees and crash landed. There were no casualties but the aircraft was damaged beyond repair.

On final approach to Pekanbaru-Simpang Tiga Airport, the four engine aircraft struck the ground and crashed 1,300 metres short of runway and came to rest, broken in two. All seven crew members escaped with minor injuries. The aircraft was completing a cargo flight on behalf of Mandala Airlines.

The pilot received a weather briefing before departure and when near the destination airport, cleared for the NDB approach. The pilot reported the procedure turn inbound; published MDA is 1,300 feet msl. Witnesses on the airport reported heavy low fog and heard the pilot announce over the UNICOM frequency, 'Oh there is fog rolling into Starkville too?' One of the witnesses advised the pilot they could go to another airport due to the fog; the pilot responded he would execute the approach. The witnesses heard the engines operating at full power then heard the impact and saw a fireball. The airplane impacted the runway inverted, slid across the runway, and came to rest in grass off the runway. A post crash fire destroyed the airplane. Tree contact approximately 972 feet northwest of the runway impact location separated approximately 51 inches of the left wing. Examination of the engines, propellers, and flight controls revealed no evidence of preimpact failure or malfunction. The pilot had twice failed his airline transport pilot checkride. The designated examiner of the second failed flight test indicated the pilot was marginal in all flight operations. The NDB was checked after the accident; no discrepancies were noted.

The pilots stated that approach and landing were normal. During landing rollout, about 2,000 feet down the runway, the brakes became ineffective. The aircraft continued to roll off the end of the runway, down an embankment, across a 4 lane road, and came to rest in a drainage ditch. Post-crash examination of the main landing gear brakes showed that 3 out of the 4 brake assemblies were worn beyond allowable limits and all 4 antiskid wheel generators were not producing voltage within the allowable limits. The outboard right main tire had failed during landing roll do to the antiskid becoming inoperative due to the low voltage of the wheel generator. The airplane had received an A-1 through A-6 inspection 2 days before the accident and this was the first flight since the inspection. The A-5 inspection requires inspection of the landing gear brake assemblies for wear, cracks, hydraulic leaks, and release.

During the final approach, while executing a VOR-A instrument approach, the airplane landed hard, collided with the runway VASI display, and caught fire. The airplane had received radar vectors for the approach and was turned to a 20-degree intercept for the final approach course when 2.5 miles from the initial approach fix. Radar track data showed the airplane continued inbound to the field slightly left of course with a ground speed varying between 135 and 125 knots and a descent rate of approximately 700 feet per minute. The pilot said he descended through the clouds about 850 feet above ground level and saw the airport approximately 1 to 2 miles ahead. He noticed that he was left of the runway centerline and corrected to the right. He realized that he had overcorrected and turned back to the left. The pilot reported that he felt that the approach was stabilized although the descent rate was greater than usual. The airplane impacted the ground about 1,000 feet from the approach end of the runway abeam the air traffic control tower on an approximate heading of 185 degrees. The impact collapsed the landing gear and the airplane slid forward another 1,000 feet down the runway and came to rest approximately midfield on the runway. The pilot stated that he had not experienced any mechanical problems with the aircraft or the navigation equipment prior to the accident. A Special Weather Observation taken at the time of the accident contained the following: sky condition overcast at 500 feet; winds from 230 degrees at 3 knots; visibility 2 miles.

The flight was cleared for a localizer approach to runway 32 at Newnan-Coweta County Airport during dark night conditions. About 8 minutes later the pilot reported to air traffic control that he had missed approach and would like to try another approach. The flight was radar vectored to the final approach course and again cleared for the localizer runway 32 approach. The flight was observed on radar to continue the approach until a point about 4 nautical miles from the airport, at which time radar contact was lost. The last observed altitude was 1,600 feet msl. The aircraft collided with 80-foot tall trees, while established on the localizer for runway 32, about 1.3 nautical miles from the runway. About the time of the accident the weather at the airport was reported as a cloud ceiling 200 feet agl, and visibility .75 statute miles. Post crash examination of the aircraft structure, flight controls, engines, propellers, and systems showed no evidence of pre-crash failure or malfunction.

On approach to a private airstrip located near Santa Catalina La Tinta, the twin engine aircraft crashed in unknown circumstances 300 metres short of runway. The aircraft was destroyed and all six occupants were killed. Weather conditions at the time of the accident were poor with low clouds and rain falls. Thunderstorm activity was reported all along the route.