Alabama

The airline transport pilot reported that shortly after takeoff from runway 36, he heard a loud noise from the left engine area, and observed smoke trailing the left engine nacelle. He confirmed that the left engine was losing power, and he feathered the left propeller. He was unable to maintain altitude, and the aircraft was force landed on wooded terrain. The aircraft caught fire on the ground after colliding with trees and was destroyed. An inspection of the left engine turbocharger revealed that the rotor shaft was seized, with evidence of metal transfer to the bearing journals.

The aerial photo flight was commencing with the pilot and operator on board. A witness reported that the engines sounded good on the ground and during the t/o ground roll. At about 30 to 40 feet agl, he heard 'surging' sounds from the airplane. He then observed the aircraft in a shallow right hand turn as it approached departure end trees. He then saw the aircraft roll off to the left, into the trees in a steep, nose low, left wing low attitude. The aircraft crashed into trees and terrain and was destroyed by impact forces and fire. Investigation revealed that the aircraft impacted the ground in a left wing low attitude. The main wreckage was found inverted. An inspection of the engines did not reveal evidence of a mechanical failure or malfunction. Exam of both turbochargers revealed evidence of rotation at impact. Exam of both propellers revealed evidence of blade tip twisting toward low pitch and some forward bending. Both occupants were killed.

According to the owner, he and the pilot had flown from Albany, Georgia to swap a Piper 28 for the Aero Commander 680. Prior to completing the trade, the previous owner reconstructed a set of aircraft maintenance logs which revealed the estimated total airframe time and engine serial numbers. The owner assumed that the airplane was airworthy. Since the pilot was not Aero Commander rated, they decided to taxi the airplane on the ramp and runway to gain some experience. While taxiing at a high rate of speed on runway 09, the owner reported that a gust of wind caught the airplane as the taxi speed approached 65 mph. The pilot lost control of the airplane as it became airborne. The airplane rotated to the right and the right wing struck the ground; the airplane cartwheeled to a stop facing the opposite direction. The wreckage examination failed to disclose a mechanical malfunction. Reportedly, the pilot completed a preflight but, the wreckage examination discovered a large bird's nest in the sump area of the left engine and a missing exhaust manifold. The pilot was not multi engine rated. The pilot was killed and the passenger was seriously injured.

This was the first day on duty in the southern region operation for both pilots. In addition, they had never flown together. During the flight, the flight crew lost awareness of their airplane's position, erroneously believed that the flight was receiving radar services from ATC, and commenced the approach from an excessive altitude and at a cruise airspeed without accomplishing the published procedure specified on the approach chart. The crew believed that the airplane was south of the airport, and turned toward the north to execute the ILS runway 05 approach. In actuality, the airplane had intercepted the back course localizer signal, and the airplane continued a controlled descent until it impacted terrain. The captain and two passengers were killed while the copilot and two other passengers were seriously injured.

The airplane crashed into houses while on an ILS approach to runway 05 at the Birmingham Airport. The weather briefing data that the captain received in Mobile was accurate, advising him to expect thunderstorms in the Birmingham area. Birmingham atis information whiskey and xray, mentioning thunderstorms, was also accurate, and the flight crew heard them, as well as information from the approach controller that the airport was experiencing thunderstorm activity. The captain and a passenger survived while 13 other occupants were killed. There were no injuries on the ground.

During an updated 0528 est weather briefing, the pilot was advised of flight precautions for IFR weather conditions in the Georgia and Alabama areas. At 0841 est he departed Macon, GA on an IFR flight plan to Anniston, AL. At 0821 cst, approximately 22 miles southeast from the Anniston Airport, the pilot contacted Atlanta center and cancelled his IFR flight plan. He was advised that the minimum safe altitude in his area was 2,900 feet msl. Two minutes later he contacted Anniston radio and requested local weather conditions. He was given the latest reported (0756 cst) weather as ceiling 1,500 broken, 3,100 overcast, 5 miles with fog. The Anniston airport field elevation is 526 feet. The aircraft subsequently impacted a mountain top 10 miles southwest of the airport at an elevation of approximately 2,300 feet. The 0850 cst Anniston weather was 800 feet overcast, 4 miles in fog. All four occupants were killed.

The airplane collided with trees and power lines during takeoff from a 2,000 foot long open area with 10 parachutists aboard. The pilot said he experienced an unsolicited rollback in engine power prior to the collision. Reportedly, some power was regained. However, not in time to avoid the collision. But, the jump club chairman reported that no change in the engine's operation was observed throughout the mishap. Witnesses at the takeoff area reported that the winds were 12 knots out of the northeast, which would have given the flight a quartering tailwind component for the takeoff. According to the flight manual, the maximum demonstrated crosswind is 12 knots. The examination of the airplane failed to indicate any system malfunction or failure.

A Beech C90 (N3804F) and a Cessna 172 (N52244) collided at an altitude of about 200 to 300 feet agl as the two aircraft were taking off on intersecting runways at an uncontrolled airport. The Beech pilots were departing from runway 06 with an IFR flight plan, while the Cessna pilots were in the pattern on an instructional flight, performing a touch and go. Two ATP pilots were in the Beech; an instructor pilot (cfi) and a low-time student were in the Cessna. Based on witness information, the Cessna crew made at least one radio call on unicom while in the pattern before landing, and another call while taking off. The Beech crew reportedly made a radio call as the takeoff roll was begun. Neither flight crew appeared to take any evasive action until just before impact. The Beech pilots had received a flight plan clearance on another frequency shortly before taking off. Both pilots in the Beech were killed.

The pilot of an aircraft carrying an estimated 317 kilos of cocaine was attempting to land at an airport which did not have a published instrument approach procedure in IMC. Witnesses estimated that the visibility was no more than 1/2 mile in fog about 45 minutes after the estimated time of the accident. The aircraft collided with a tree about 1,400 feet short of the runway threshold and about 600 feet to the right of the extended runway centerline. Ground contact was made about 380 feet after colliding with the tree. The aircraft burned after ground impact. Pilot flight time was obtained from pilot's last CFI application. Both occupants were killed.

The pilot obtained a weather briefing for his proposed flight from Birmingham, AL to Jasper, AL to Allentown, PA. He did not file a flight plan for the 35 mile flight from Birmingham to Jasper, however, he did file a flight plan for the proposed flight from Jasper to Allentown. He stated that he 'felt like he got a little slow and the tail stalled' during his VFR landing approach at Jasper. The aircraft contacted the ground at the east end of the east-west runway on a northerly track. The aircraft continued on the northerly track for 288 feet before colliding with trees. The aircraft was destroyed by the post crash fire. Witnesses reported fog in the area and the pilot reported that he had encountered patches of fog on the flight from Birmingham.