Indiana

The pilot reported that while on final approach to runway 35, the aircraft encountered 'extreme windshift' and was blown about 550 feet right of course with a 30 knot loss of airspeed (from 130 to 100 knots). He stated the aircraft lost about 300 feet, then was blown back on course with an additional loss of altitude. Subsequently, the aircraft touched down hard on the approach end of the runway. During touchdown, the right main tire blew out, the right propeller struck the runway 9 times and the right wing was damaged. The surface wind was reported to be from 240° at 10 knots with no gusts. All four occupants escaped uninjured.

During an ILS to runway 35, the approach was normal until the aircraft was approximately 100 feet above the decision height, except there was condensation on the windshield. Touchdown was hard. A witness said the aircraft landed approximately 1/3 of the way down the 5,200 feet runway. After landing, with the props in 'ground fine,' braking action was ineffective on the wet runway. The aircraft was not equipped with an anti-skid braking system. Subsequently, the aircraft continued off the runway and went down an embankment into a field. Scrub marks on the runway and reverted rubber on the tires indicated the aircraft was hydroplaning. According to the flight manual, 4,500 feet (plus a 10% factor for no anti-skid) would have been required to stop on a dry runway in the prevailing weather conditions, which included a slight tailwind. Two pax, acting as flight attendants (f/a's), assisted the other pax in evacuating. An investigation revealed the f/a's were not properly trained; the pax were not completely briefed before the flight; and the passenger briefing cards were inadequate. The aircraft was on a business flight to transport an entertainment troupe.

The aircraft entered an embedded thunderstorm after being advised by artc of several large areas of heavy precipitations in his area and along the vicinity of his flight path. The pilots response was that his aircraft radar showed no build-ups or returns. ATC allowed deviations at pilot's discretion according to the recorded taped conversation. The pilot continued his flight path and was lost on radar shortly thereafter in a descending right turn at 16,800 feet msl. Witnesses saw him exit the bottom of the cloud at about 1,000 feet agl. The wings were seen to separate from the fuselage. Other witnesses saw the fuselage descend inverted, minus the wings, empennage and engines, to impact in a corn field. The wreckage was scattered over an area 1 and 1/2 miles long and 1/2 mile wide. Witnesses who had observed the aircrafts preparations for departure described it as 'mass confusion' in the cockpit. The aircraft reportedly crept forward six times during an extended 10-15 minute checklist while the engines were running at a high rpm setting on a ramp with other aircraft and people around. All four occupants were killed.

After taking off from runway 23, the aircraft crashed ssw of the airport about 6,300 feet from the departure end of the runway and about 1,800 feet to the left of the runway centerline. Impact occurred while the aircraft was in a steep descent. The wreckage path was scattered along a heading of 035° from the initial impact point. The aircraft was demolished by impact and fire and no preimpact part failure or malfunction was found that would have caused the accident. All three occupants were killed.

At 1604 est, the aircraft departed Fort Wayne on a ferry flight. IFR conditions prevailed and the pilot had filed an IFR flight plan. While climbing after takeoff, the pilot passed his assigned altitude of 2,500 feet msl and flew to 4,200 feet. Also, he failed to turn to his initial assigned heading of 130°. He had problems contacting departure control as he was not on the assigned frequency. He reported problems with his heading indicator and his 'gyro'. Shortly after his last transmission, the aircraft left 4,200 feet msl and crashed in a steep dive. Before takeoff, the atp pilot reported he had flown all King Air aircraft and was currently flying the Beech 200. A review of his last log book revealed over 2,000 hours in the Beech 200, but showed no time in the Beech C90. A witness that reviewed the aircraft with the pilot before the flight believed he (the pilot) was very familiar with the aircraft systems. During an inspection of the wreckage, no evidence was found to verify a pre-impact malfunction or failure of the aircraft or engines. All instruments were destroyed. The pilot, sole on board, was killed.

The pilot reported that during a climb after takeoff, he engaged the autopilot. While making an entry on a trip sheet, he felt a bump and noted that the aircraft had started to descend. He disengaged the autopilot and the nose pitched down violently. Reducing power had an adverse effect, so he increased power again. He finally leveled the aircraft just prior to impacting in a field at cruise power. The elevator trim tab cables were found to have been crossed between the tab actuator and the pulley in the tail cone. The tab was also found fully trimmed nose down. The aircraft had just been given an annual inspection during which the elevator trim actuator had been removed, inspected and lubricated. This was the first flight since the inspection. All eight occupants escaped with minor injuries.

During a VOR approach to runway 05 when 3 miles away from the airport at minimums ground contact was not made. The pilot stated that she elected to perform a missed approach but before power was applied the copilot raised the flaps. She further stated that she then felt a sinking feeling and put in more power. The aircraft crashed in an open field approximately 2.3 miles southwest of the airport. A pilot was killed while two other occupants were seriously injured.

While in cruising altitude from Peru to Louisville, both engines failed. The pilot reduced his altitude and attempted an emergency landing in an open field. Upon landing, the undercarriage collapsed and the airplane came to rest on its belly. All five occupants were seriously injured and the aircraft was damaged beyond repair.

After takeoff from Walketon, while in initial climb, the twin engine airplane stalled and crashed. The pilot, sole on board, was killed.

While approaching Michigan City on a taxi flight from Chicago, the twin engine airplane went out of control and crashed into Lake Michigan few miles off shore. The aircraft was destroyed and all four occupants were killed.