Ambulance

The twin engine aircraft was engaged in an ambulance flight from Nantes to Limoges, carrying one pilot and one doctor who should embark a patient in Limoges. During the takeoff roll, just before V1 speed, the nose gear collapsed. The aircraft slid on its nose for few dozen metres before coming to rest on the runway. Both occupants escaped uninjured and the aircraft was damaged beyond repair.

While loading a patient & his personal gear in the aircraft for an air ambulance flight, the aircraft tipped onto its tail. As a result, the tail bumper was forced upward into the belly of the empennage. The pilot refused the offer to have a mechanic look at the damage, and remarked 'this has happened before.' after takeoff, the pilot radioed to the tower that he had a jammed elevator, and was coming around to land. While maneuvering on a base leg, control was lost & the airplane was observed to crash with one wing perpendicular to the ground. Another airplane was in the takeoff position on the runway. The airplane was configured with a hospital litter/stretcher and oxygen bottle on the right side of the cabin. There was no record for the approval for, or installation of, the stretcher. In addition, there was no weight & balance record for the airplane with the stretcher installation. All three occupants were killed.

The pilot of the air ambulance feathered the right propeller after reporting 'a bit of a problem' with the right engine. He attempted to divert to the nearest suitable airport, but after receiving its latest weather report, elected to return to base. The airplane made a left turn, reentered IMC, and impacted a mountainside on a magnetic heading of 092°. The heading to the airport of intended landing was 272°. The accident occurred during a snowstorm at night. All five occupants survived and were rescued the following afternoon. Thick grease on the right engine fuel control camshaft prevented a spring from returning the 3d cam to a lower altitude position. The cam was found struck on the shaft at a position equating to an altitude of approximately 15,000 feet. The fuel flow schedule for flight idle was below specifications. In addition, shroud material was found delaminated from the left engine second stage compressor housing.

The aircraft departed São Paulo-Congonhas Airport on an ambulance flight to Uberlândia, carrying two doctors and two pilots who should pick-up a patient. The copilot was pilot flying. This was his first flight on a Learjet without an instructor. This was against regulations since the copilot was not fully qualified yet and the captain was not qualified to act as an instructor. Upon arrival at Uberlândia, weather conditions were poor with a low ceiling at 100 meters (clouds 8/8), fog and an horizontal visibility less than 200 meters (below minimums weather conditions). The crew abandoned the approach and initiated a go-around procedure. Few minutes later, a second approach was also abandoned. Rather than diverting to the alternate airport, the crew attempted a third approach when the aircraft struck the ground and crashed short of runway threshold. All four occupants were seriously injured and the aircraft was destroyed.

The twin engine aircraft departed Papeete-Faaa Airport on an ambulance flight to Maupiti, carrying two doctors and one pilot. After takeoff, while climbing by night, the pilot informed ATC about minor problems with the engine but preferred to return for a safe landing. On final approach, the aircraft went out of control and crashed in the sea few km from the airport. All three occupants were killed. At the time of the accident, it was dark but weather conditions were excellent.

Witnesses reported that shortly after lift-off, the aircraft entered an unusually steep, nose high attitude, while still at low airspeed. One witness (an ATP pilot) reported the aircraft attained an altitude of approximately 75 to 100 feet and appeared to slow down and enter a VMC roll, then it crashed. Impact occurred in an inverted, nose down attitude, left of the runway. An investigation revealed that a coupling shaft (PN 865888-3) had failed in the left engine and the left prop had feathered. A metallurgical examination of the coupling showed evidence of fatigue. One pilot was killed and three other occupants were injured, one seriously.

Shortly after takeoff from Aweil Airport, while in initial climb, the twin engine aircraft was shot down by a SAM-7 surface-to-air missile. Out of control, it crashed 800 meters past the runway end. All four occupants were killed. The aircraft was completing an ambulance flight to Khartoum.

The aircraft departed Tromsø-Langnes Airport at 2248LT on an ambulance flight to Bardufoss, carrying one patient and three crew members. Four minutes later, at an altitude of 8,000 feet, the crew contacted Bardufoss control and obtained information for an ILS approach to runway 29. At 2254LT, the crew awas cleared to descend to 6,000 feet and was instructed by ATC to report once established on the ILS. At about 22:57:50 at a position about 8 NM north of the Målselv (MLV) NDB, the airspeed increased from 265 knots to 285 knots over a distance of about 5 NM. This speed was maintained up to the NDB. At 22:59:30 LN-AAE passed the MLV NDB. Instead of performing the left hand procedure turn from 174° to 122°, the crew continued a straight heading for about 30 seconds at an airspeed about 100 knots above the recommended approach speed. The aircraft was about 2 NM (4 km) south in relation to the established procedure pattern. The airplane should still have been at 6,000 feet until established on the ILS but it had descended 1,250 feet below the minimum altitude when it collided with a relatively flat mountain ridge just south of the summit of Langfjelltind (4,935 feet). The wreckage was found about 35 km east-southeast of the airport and all four occupants were killed.

The twin engine aircraft was dispatched at Pelée Airport to evacuate to Windsor a patient. On board were one patient, his spouse, one ambulance officer and two pilots. Shortly after a night takeoff from runway 28, while climbing, the aircraft went out of control and crashed in Lake Erie. The copilot and the patient survived while three other occupants were killed.

The pilot stated that 15 minutes prior to arrival he notified the hospital and asked them to check the runway. As he entered downwind security advised him of animals on the runway so he circled until they called back stating it was clear. Just as the airplane was touching down, two horses began to cross the runway. The pilot attempted to go-around; however, the airplane contacted both animals and the pilot elected to abort the go-around. The left main landing gear collapsed and the airplane slid to a stop. A post crash fire ignited and was extinguished shortly thereafter. The landing was being made during dark night conditions.