Scheduled Revenue Flight

Crashed in unknown circumstances somewhere in Russia, date exact unknown (somewhere in April 1987). No casualties.

Shortly after the initial power reduction during takeoff, the pilot noted a partial loss of power in the right engine. He said he 'went to full power on both engines' and noted an 'extremely high' fuel flow indication to the right engine. He said, 'thinking that the engine was flooding, I placed the boost pump switch from high to off to possibly eliminate the problem with no result. I then placed the pump back to high and tried to decrease the fuel flow by leaning the mixture. This also did not seem to eliminate the problem.' While troubleshooting the problem, he turned to a downwind and stayed in the traffic pattern, but could not maint altitude. Subsequently, a wheels-up landing was made in an area of small trees approximately 1/2 mile before reaching runway 24. An examination of the right engine revealed the spark plugs were wet with fuel and black with soot. Also, its #5 fuel nozzle had been cross-threaded and was knocked out of its hole during impact. During an initial test, the right fuel pressure sensing switch did not sense operating pressure (over 6 psi); this would have resulted in a high boost/fuel flow condition. Later, the switch was tested ok. All nine occupants escaped uninjured.

On final approach to Medan-Polonia Airport, pilots encountered poor weather conditions with thunderstorm activity, turbulences and heavy rain falls. On final, the aircraft became unstable and lost height. The pilot increased engine power when the aircraft struck a television antenna, stalled and crashed in a field, bursting into flames. 23 occupants were killed while 22 others were injured.

The aircraft was on the last leg of a scheduled commuter flight, when it crashed in a heavily wooded area while making a VFR approach to Merrill Field, Anchorage, AK. The captain and his sole passenger were killed in the crash when the airplane struck the ground upside-down in a near vertical attitude. The airplane's copilot, who had deplaned minutes before the accident flight, said he did not see the captain use the aircraft's auxiliary fuel tanks at any time during that evening's earlier flights. The airplane's main fuel tanks hold 100 gallons of useable fuel; it is estimated that the airplane would have consumed slightly more than 100 gallons of fuel at the time of the accident. Ample fuel remained in the auxiliary tanks, but an engine restart cannot be readily accomplished if the auxiliary tanks are not selected prior to the engine's quitting. Both occupants were killed.

The twin engine aircraft departed La Serena-La Florida Airport at 1900LT on a regular schedule service to Santiago de Chile. About 45 minutes into the flight, the crew encountered engine problems, declared an emergency and was cleared to divert to San Felipe Airport. On approach, the aircraft stalled and crashed in a peach plantation located 10 km from the airport, bursting into flames. A passenger was seriously injured while eight other occupants were killed.

At 14:30 the flight was cleared for a runway 21R visual approach and was cleared to land one minute later, At a height of 60-70 feet the aircraft suddenly yawed violently to the left and banked left 80-90° in a descent. The aircraft then rolled right and struck the ramp area 1,010 feet inside and to the left of the runway 21R threshold. It then skidded 398 feet, struck three ground support vehicles in front of Gate F10 at Concourse F and caught fire. Both pilots and seven passengers were killed, 10 other occupants were injured.

While approaching Sampit Airport, the twin engine aircraft went out of control and crashed in the Sampit River few km from the airfield. Four passengers were killed while five other occupants were rescued.

DC-9 "Gissur Viking" was approaching Trondheim runway 27 with the co-pilot at the controls. Descending through 2500 feet the ATC controller asked the crew to contact SAS Station in Trondheim over company frequency. The captain was working through the checklist but contacted SAS, contrary to company regulations (it's not allowed use company frequency while on final approach). The captain then forgot to arm the spoilers because he had not completed the checklist. He co-pilot noticed that the spoilers had not been armed and, while descending through 100 feet, called "Spoilers". The pilot instinctively extended the spoilers and, realizing his mistake, immediately retracted them. The aircraft entered a high sink rate and touched down heavily. A go-around was executed and after landing severe structural damage was found to the undercarriage, engines (30° respectively 15° tilted down), and tail cone (the APU was pushed halfway up the tail). All 107 occupants escaped uninjured while the aircraft was damaged beyond repair.

Suffered an accident somewhere in Taiwan in February 1987, exact date unknown. There were no casualties.

Upon landing on relative rough sea, the right float was torn off. The aircraft came to rest and partially sank few dozen meters offshore. All 16 occupants were rescued, some of them were slightly injured. The aircraft was written off.