Cessna 402

Following an engine failure, the aircraft crashed in the Lake Malawi. There were no casualties.

The aircraft was engaged in a voluntary relief flight for the victims of hurricane Andrew. All of the seats had been removed from the cabin section of the aircraft. There were no weight scales used in the loading of the cargo onto the aircraft. The private pilot did not have a multi engine rating on his pilot certificate. The aircraft crashed into a residence one half mile from the departure end of the runway. Witnesses stated that the aircraft used most of the available runway prior to liftoff. After liftoff, the aircraft appeared to climb in an unstable condition prior to the accident. Investigation revealed that the aircraft was 1112.2 pounds over the maximum gross takeoff weight at the time of the departure. All three occupants were killed.

Pilot began takeoff on a 5,200 feet dirt runway (upslope to the south, elevation 4,775 feet) with wind from the south at 18-20 knots, density altitude about 7,250 feet. Witnesses observed the aircraft taking off, with the landing gear retracting as it passed their position. Soon thereafter, the pilot transmitted he had 'a problem.' Aircraft was then seen about 200-300 feet agl in right turn, which progressed into a dive. Aircraft impacted in flat attitude 1/2 mile south of runway 17. Passenger video tapes revealed props went out of sync about 6 seconds after takeoff. About 15 seconds later, right prop slowed until blades could be seen turning. Video showed one engine fuel flow at about 90 gph, other engine at minimum setting (about 3 psi), 5° increase in pitch attitude. Exam revealed right engine driven fuel pump drive coupling was scored and only partially engaged. SB ME88-3 complied with; auxiliary fuel pump switches found in low position. Right propeller blades found at fine pitch, lacking rotational damage. Landing gear found up, but unlocked; flaps extended 15°. Emergency procedure training did not replicate high density altitude and max gross weight performance. All 10 occupants were killed.

During cruise flight, the pilot reported that the right engine cowling partially separated and the left forward cylinder of that engine separated, followed by an engine compartment fire. He attempted to feather the propeller but was unable. He initiated a descent to extinguish the fire and was successful but after leveling off, was unable to maintain directional control. He ditched the airplane and both he and the passenger exited the aircraft. The pilot dragged the seriously injured passenger with him to a nearby island where they were rescued the following day. The aircraft was not recovered; therefore, no determination could be made as to the reason for the separation of the cylinder. Review of the aircraft logbook indicates that on 8/27/91, the n°5 cylinder of the right engine was removed and replaced. Also, the n°1 cylinder was removed and reinstalled following repair. There were no further entries in the aircraft logbook regarding cylinder removal or replacement to the right engine.

The twin engine aircraft departed Nayarit Airport with one passenger and one pilot on board. While flying by night, it crashed in unknown circumstances near El Zapote. Both occupants were killed.

The scheduled passenger flight departed without a flight plan and was last heard from while descending in attempt to remain in VFR conditions. Witnesses on the ground stated that there was extremely heavy rain and thunderstorms at the time of the accident. The wreckage was located the next day and evidence indicated that the airplane hit the ground in a 50° nose down attitude at a high rate of speed. Both occupants were killed.

Flight departed and upon reaching a point approx 35 miles north of airport pilot requested return to airport from ATC. Pilot did not declare emergency or report an engine problem. Upon entering traffic pattern at uncontrolled airport pilot stated he would follow a Cessna 152 for landing. On short final aircraft was seen making s turns to maintain spacing behind 152. Pilot then declared he had an engine shutdown and needed to land. 152 was in landing flare and landed. With 152 on runway pilot attempted a go around with full flaps extended, gear down, left engine shutdown, and at a slow airspeed. Aircraft rolled to left upon application of right engine power and nosed down from which it crashed. The number two cylinder of the left engine had suffered separation of the head from the barrel. Pilot logbook did not reflect pilot having current biennial flight review. The pilot, sole on board, was killed.

During daylight flight, the airplane lost its right engine due to failed piston assembly because of engine overheating. The overheating was due to the engine air cooling baffle not being installed and the improper oil filter being installed. The airplane would not sustain flight due to the inoperative main landing gear which was locked in the down position and the propeller that could not feather due to corrosion. The pilot and his passenger were seriously injured in the landing due to the lack of seat belts. The airplane was operated with 137 known deficiencies.

The pilot announced he had an engine failure during initial climb at 300-400 feet agl after takeoff on a VFR night cargo flight. The tower controller cleared the flight to return to the airport and land on any runway. The aircraft entered a right descending turn, impacted the ground one mile from the airport, and ignited in flames. Evidence indicated the right engine was not operating at impact. The landing gear was down and the right propeller was in the high pitch position. Exam of the right engine revealed blocked fuel injectors, incorrect size fuel injectors, fuel pump out of adjustment, and burned/pitted breaker points in a magneto. Both occupants were killed.

On final approach to Ketapang Airport, the twin engine aircraft crashed in unknown circumstances few hundred metres short of runway threshold. A passenger was killed while eight other occupants were injured.