Madison

The on-demand cargo flight departed for the destination airport and was delayed en route due to repetitive destination airport closures. The closures were the result of snow-contaminated runways. The pilot then diverted to an alternate airport due to concerns about remaining fuel reserves. The airplane experienced a loss of engine power during an instrument approach at the alternate airport and impacted the ground about 200 yards short of the landing runway. A postaccident inspection of the airplane revealed no usable fuel on board.

The pilot said that the copilot was flying a visual approach to runway 15 at the Lawrence Municipal Airport, Lawrence, Kansas. The pilot said, "With gear down and full flaps at approximately 15 to 20 feet above the runway and 115 KTS, the nose abruptly dropped and there was no elevator effectiveness with the yoke pulled back to the mechanical stop." The pilot said, "After landing, I noticed that the stabilizer trim indicated full nose down in the cockpit and, upon exterior inspection, the stab was in that position." The copilot said, "I made my turn to base and proceeded to make my turn to final. No problems with the controllability were noted at this time. The turn to final was made and the airplane was lined up with the runway on final approach with normal glide path. My altitude was dropping normally and my airspeed was approximately 140 knots." The copilot said, "When it got time to pull the power back to idle for landing our airspeed was approximately 110 knots and power was reduced. At that point in time the nose of the aircraft seemed to pitch over towards the runway and increase speed. I pulled back on the yoke to raise the nose and at that same instance the pilot recognized the pitch over and pulled back on the yoke at the same time. The yoke did not seem to pull all of the way to its full extent of travel and felt to mechanically stop at about 3/4 the way travel. Even with both pilot's pulling on the yoke it seemed unresponsive and failed to raise the nose back to a proper landing attitude. The aircraft hit the runway very hard and came to a stop on the runway." A preliminary inspection of the airplane showed the stabilizer positioned at 4 degrees nose down. An examination of the airplane's systems revealed no anomalies.

Witnesses observed the flight enter downwind for runway 30, after it had completed a published approach to runway 12, with a circle to land on runway 30. The witnesses, one of which was a commercial pilot said that there were jagged ceilings at the time about 400 to 500 feet above the ground. He and two other men with him saw the airplane below the clouds. As the airplane proceeded downwind, it momentarily entered a cloud. As the airplane came out of the cloud, it turned left in about a 30 degree turn. The angle of bank increased to about 70 to 80 degrees, the tail of the airplane came up, and the airplane impacted the ground nose first. Several pilots at the airport heard someone from N69BS make a radio transmission on the UNICOM frequency. What was heard by several people was that N69BS had broken out at 2200 feet. They then heard, 'N69BS turning base,' immediately followed by 'lookout' and 'oh ....' All of the eye witnesses agreed that at no time did they see or hear any problems with the engine. They all said that the sounds coming from the engine never changed. The published approach in use at the time of the accident was the GPS (global positioning system) runway 12. The pilot made his initial approach to runway 12, broke off the approach to the right, entered a right downwind for a landing on runway 30. The published circling minimums for the approach were MDA (minimum descent altitude) 4,800 feet, HAT (height above terrain) 869 feet. Using an approach speed of 90 knots, the minimum visibility was 1 mile. Using an approach speed of 120 knots, the minimum visibility was 1 1/4 miles. The field elevation was 3,931 feet. The profile for the GPS runway 12 approach showed that after the IAF (Jesee way point), the course was 204 degrees, at 7,000 feet, to the Dezzi way point, from Dezzi the course was 114 degrees, descend to 5,600, to Sophi way point, after Sophi descend to 4,800 feet to the missed approach point at the Ruste way point. The distance from Dezzi to Ruste was 10 miles.

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 pilot reported that as he overflew the Tri-City airport, Tennessee at 9,000 feet, the right engine power slowly decreased. The airplane was in the clouds with an outside air temperature of about zero degrees Celsius. Right engine manifold heat was applied for a few seconds, with no noticeable difference in engine performance. The right magnetos were also checked with no obvious malfunctions noted. A descent for landing was initiated to the Tri-City airport and manifold heat was applied and removed several times, with no appreciable effect. On short final approach, when the landing gear was extended, the right main gear did not indicate down. There was insufficient time to perform the emergency gear extension procedure. A go-around was initiated, during which the pilot discovered that the left manifold heat control was now stuck in the 'ON' position. The pilot stated that with less than full power available on the left engine, and the right propeller unfeathered, the airplane could be climbed to about 200 feet. He flew the airplane until terrain clearance was no longer possible, then landed in a field, gear up. The airplane slid into trees and was substantially damaged.

On final approach, after being cleared to land, the pilot informed the controller that he might have to shut down an engine. He declined to declare an emergency or request assistance. On short final, the aircraft was observed to roll to the left and descent into the terrain. Subsequent examination revealed evidence that the left engine was not developing power, although the left propeller was not feathered. There was evidence that the right engine was producing high power during impact. No mechanical deficiency of the left engine or propeller was found. The pilot, sole on board, was killed.

The pilot reported that after he taxied to the rwy, the n°1 oil temperature was not up to the minimum temperature. He set the parking and advanced the n°1 throttle to 1,500 rpm until the engine warmed up. When both oil temperatures were within limits, he advanced both throttles to 30 inches manifold pressure and 2,250 rpm for a pretakeoff check. At that time, he used the normal (toe) brakes, since the parking brake would not hold the aircraft above approximately 1,700 rpm. He then applied full power and released the brakes for takeoff. As he started to roll with a slight left crosswind, the aircraft began drifting left. He corrected with right rudder, some right brake and right aileron. The aircraft then began drifting right and the pilot suspected a wind-shift from that direction. He applied left rudder and right aileron, but the plane veered right, went off the runway and headed for a ditch. Unable to stop, the pilot tried to clear the ditch. As the aircraft became airborne, the left wing dropped and hit the ground, and the aircraft yawed and crashed. The parking brake was found partially engaged. Tire marks were evident on the runway. All four occupants escaped uninjured.

After takeoff from Park Falls Municipal Airport, the twin engine airplane encountered difficulties to gain height. It struck power cables then stalled and crashed in a field, bursting into flames. All five occupants were seriously injured and the aircraft was destroyed.

While cruising by night on a flight from Madison to Wheeling, the single engine airplane went out of control, entered a dive and crashed in East Troy. Both occupants were killed. The pilot was intoxicated at the time of the accident.

After a night takeoff at Madison Airport, the twin engine airplane encountered difficulties to gain height when it struck tree tops and crashed in a wooded area. The aircraft was destroyed and both pilots were killed.