United States of America

The pilot landed the amphibian landing gear equipped aircraft on water with the wheels extended, and the aircraft flipped over to an inverted attitude on touchdown. The pilot, sole on board, was killed.

Purpose of the flight was to provide training to the copilot for a new (part 135) operation. Witnesses observed the DC-3, N47CE, maneuvering at 3,000 feet msl (approximately 2,200 feet agl) with the gear and flaps extended. Shortly after completing a turn, the aircraft was observed in a nose high attitude, then it entered a spin. According to witnesses, the aircraft seemed to stop spinning, but it entered a secondary spin and crashed before recovery was accomplished. The pilot-in-command (pic) had 30 hours of flight time in the make/model of aircraft. No record was found to show that the pic had been trained in approaches to stalls. No preimpact part failure/malfunction of the aircraft was found, though it was destroyed by impact and fire. The copilot was a retired airline pilot, who had flown the DC-3 in the 1940's. An examination of the wreckage revealed the gear and flaps were (fully) extended and the elevator trim was set in a full nose up (trim) position. All three occupants were killed.

Before the flight, the pilots of 2 Beech 200 aircraft evaluated weather reports at a fixed base operation and made a computer weather inquiry. They departed Santa Monica, CA, on a positioning flight to Farmington, NM, without filing a flight plan. While en route, the lead aircraft was about 1 to 3 minutes ahead of the 2nd aircraft. The 2nd pilot reported they were at about 4,500 feet msl as they neared mountains and the clouds were about 1,000 feet above. As they continued eastward in a valley, the 2nd pilot heard the lead pilot report he was 'going up.' This was the last known transmission from the lead aircraft. The 2nd pilot continued his flight in VMC. Two days later, the lead aircraft was found, where it had crashed about 100 feet below the top of a 7,400 feet mountain ridge. Impact occurred on a heading of about 030°. The mountain ridge was oriented on headings of 060° 240°.

After conducting ground training all day, the instructor/director of operations and his trainee flew an EMB-110P1 to Memphis to exchange airplanes. Ground fog had started to form prior to departure. After exchanging airplanes, they made the return flight to Columbia. They obtained radar vectors to the final approach course for the SDF at Columbia. The thick fog resulted in a missed approach. During the missed approach, the runway was visible from above and the crew indicated that they would try for a VFR approach and landing. The airplane collided with trees 2,350 feet from the runway in a wings level attitude. The tops of the trees were broken 41 feet above the runway threshold altitude. The trainee had been without rest for at least 30 hours prior to the accident. One pilot was killed while the second was seriously injured.

Witnesses saw the airplane depart and last saw and heard it with the landing gear down and both engines running at what they called normal takeoff power. Evidence indicated that the airplane then made a sharp left turn and descended to the ground, left wing first. Evidence indicated that the right engine was developing high power while the left engine was developing somewhat less than takeoff power. Teardown of the left engine revealed metal erosion on the top edges of the pistons with no corresponding marks on the cylinder walls. Some of this erosion was from previous operation and some was from very recent operation. There was no teardown of the right engine. Other than the erosion of the pistons, nothing was found to indicate any preimpact problems with the airframe or powerplants. The pilot, sole on board, was killed.

The flight (a Monroe County Mosquito Control operation) began at about 1740 edt to conduct low altitude spraying. When it did not return, a search was initiated. At about 0245, the aircraft was found in a remote area on water key near the town of Summerland Key, FL. Evidence at the accident scene suggested the aircraft struck 40 feet high mangrove trees with the left wing as the pilots were making a procedure turn to start another spray run. No preimpact failure or malfunction of the aircraft or engines was found. There were no known witnesses, but the accident was estimated to have occurred at about 2030 edt. Sunset was at 1952 edt. About 22 miles southwest at Key West, the 1750 weather was in part: 1,500 feet scat, 10 miles visibility, wind from 330° at 10 knots. Aprx 85 miles north-northeast, the wind was from 100° at 11 knots. Both pilots were killed.

Departed Marion without a weather briefing. Pilot advised during approach that last person making approach reported moderate to severe turbulence on final. Subsequently cleared to land and given wind 360 at 30 gusting 40. Also advised that another aircraft reported a 20 knots windshear on final. The pilot reported that when he had descended to 1,500 feet msl, the aircraft encountered strong turbulence and the airspeed went from stall to redline. Despite adjustment to flaps and throttle, the airplane was uncontrollable.

During a flight from Juneau to Pelican, AK, the aircraft collided with terrain approximately 12 miles east of Pelican while crossing over Chichagof Island. Impact occurred on a vertical rock wall at an elevation of about 1,950 feet. No preimpact part failure or malfunction of the aircraft was evident. Another pilot, who had planned to fly the same route about 1 hr and 45 min earlier, decided to fly around the island due to low clouds, rain and fog in the area. He reported that he flew over icy straits rather than take a more direct route and that ceilings were about 2,000 feet broken with lower stratus in the valleys. A helicopter pilot said he was unable to work in mountain passes in the vicinity of the accident due to low clouds, rain and fog; he also said the passes were 'socked in.' Both occupants were killed.

While completing a local training flight, the US Navy Buckeye collided with a second Buckeye registered 156694. Both aircraft crashed and were destroyed. While both pilots on board 156694 were killed, the crew on 159724 was able to eject in time.

While completing a local training flight, the US Navy Buckeye collided with a second Buckeye registered 159724. Both aircraft crashed and were destroyed. While both pilots on board 156694 were killed, the crew on 159724 was able to eject in time.