Idaho

During the takeoff roll on a contaminated runway, the copilot noted a lack of acceleration. Just beyond midfield, the copilot called for an abort, however, the pilot elected to continue. The airplane did not reach Vr and the pilot attempted to rotate the airplane at the end of the runway. The airplane collided with and travelled through a five foot high snowbank and came to rest in a field approximately 500 feet from the end of the runway. During the post crash investigation, evidence indicated that the parking brake had been in the intermediate position or 23% of maximum braking. The parking brake warning light was found to operate correctly if the panel lights were set in the bright light position. In the dim position, the warning light was inoperative. During the on site investigation, the panel lights were found in the dim position. Both passengers were slightly injured while both pilots were seriously injured.

The pilot of the Cessna 207, who was attempting to complete a VFR flight in mountainous, hilly terrain, flew into falling snow which reduced his visibility to approximately one half mile. When he realized that he was lost, he attempted to reverse course, but impacted the terrain while attempting to turn in the steep canyon. All three occupants were killed.

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.

While en route on a night IFR cargo flight, the pilot requested and was cleared for a descent from an IFR cruise altitude of 16,000 feet to proceed VFR-on-top. The last transmission from the aircraft was at 2106 when the pilot acknowledged that he was familiar with the terrain along the route. At 2121:51 mdt, radar contact was lost after the aircraft made an approximately 360° left turn and descended thru 13,800 feet. Shortly after that, the controller tried to call the pilot to inform him that radar contact was lost, but was unable to make radio contact. Later, wreckage of the aircraft was found where it had crashed about 2 miles southwest of were radar contact was lost. The wreckage was scattered over an area of more than one mile. An investigation revealed the left wing and right horizontal stabilizer had separated upward from overload. No pre-accident fatigue or part failure/malfunction was found. Weather reports and pireps indicated moderate turbulences and towering cumulus clouds in the area. Approximately 60 miles west at Pocatello, ID, snow showers were reported; 2 to 3 inches of snow fell on the wreckage overnight. Both pilots were killed.

Check pilot was conducting captain proficiency check on another company pilot (pic) under dark night conditions. Subsequent to full stop landing on runway 25, takeoff checklist was recited. PIC commenced takeoff on runway 07. Check pilot simulated V1 engine cut after liftoff. PIC was unable to accelerate to V2, climb, or maintain directional control. Aircraft levelled off, air speed began to decay and aircraft drifted to the right. Check captain failed to take control or terminate engine cut simulation as evolution deteriorated. Aircraft collided with ILS glideslope tower marked by red obstruction lights. Loss of control followed when right wingtip/aileron separated. Aircraft then impacted ground and slid to a stop. Takeoff flap position should be 1/4. Both flaps found near 1/2 flap extended position. Handle found in 1/2 flap detent. Performances charts show aircraft able to reach V2 at 50 feet altitude in 6,500 feet roll, then +575 fpm climb (vyse) at acc wt.

During the transition from a DME arc to the ILS final approach course, the pilot allowed the aircraft to prematurely descend into the ground. The reason for the descent could not be determined. However, no preimpact mechanical malfunction with the aircraft was found nor was there any evidence supporting pilot incapacitation. Dark night conditions in fog and low ceilings prevailed during the approach. All three occupants were injured, two seriously.

Shortly after departure and level off, the pilot reported an engine malfunction and initiated a return to the airport. About 2 minutes later, he reported an engine fire and declared an emergency. Approximately one minute thereafter, the right wing separated from the aircraft and the plane crashed. An exam of the wreckage revealed extensive inflight fire damage in the area of separation. A 2.5 by 3 inches hole was found in the right inboard exhaust tube, pn 0850712-6. It was oriented toward the accessory compartment with numerous fuel and oil lines which were fire damaged and charred. Also, much of the engine support structure and wing spar were melted in that area. An exam of the exhaust tube revealed its walls were thin, brittle and discolored in the area of the rupture and several areas of cracks and small holes were found. The exhaust tube had 5,862 hours of total service and 1,762 hours since it was overhauled. Records showed that ad 75-23-08 had been complied with during the last inspection, 25 flight hours prior to the accident. The pilot, sole on board, was killed.

The pilot took off from the Simplot Ranch Airstrip which was located beside the middle fork of the Salmon River, approximately 27 miles northwest of Challis, ID. He departed downriver toward the northeast, but the destination was a usfs strip about 7 miles upriver to the southwest. A course reversal normally would have been made about 6 miles downriver. However, a turn-around was attempted over a relatively shallow (bench) area on the west side of the river, about 1-1/4 mi from the departure strip; where, according to the operator, it could have been made under ideal conditions. The aircraft crashed in the bench area while on a westerly heading. It came to rest in an upright attitude with little evidence of forward velocity, but with severe vertical collapse. No evidence of a pre-impact mechanical malfunction or failure was found. All four occupants were killed.

About 1100 mst, on February 15,1983, a Sierra Pacific Airlines DHC-6, operating as Transwestern Flight 868, crashed during its final approach to a landing on runway 31, 1.7 mile south of the Friedman Memorial Airport at Hailey, Idaho. Flight 868 was a regularly scheduled commuter passenger flight between Boise and Hailey, Idaho. There were two flightcrew members and six passengers on board the flight. One passenger escaped with minor injuries, but all the other occupants sustained serious injuries in the accident. There was no fire. About 800 feet above the small town of Bellevue, 2 miles south of the airport, the captain reduced power in order to configure the airplane for its final approach. Immediately afterward, the captain realized that he had lost eleva control of the airplane. The airplane nosed over and descended steeply. The captain attempted to control the pitch of the airplane by adding power; it began to recover but it crash landed on a highway in a slight nosedown attitude, with the right wing slightly down The airplane then veered off the highway, struck a 4-foot-high snowbank, and broke apart.

The aircraft crashed into the side of a mountain ridge during a VFR attempt to land at an airport with no instrument approach. The mountain ridge was obscured by broken clouds. The pilot had cancelled his IFR clearance, and during the descent to the airport, he had descended below clouds near the airport with clouds still obscuring some of the terrain. One mile visibility was a requirement for the VFR approach. According to witness statements, the aircraft continued to remain below the clouds and the pilot continued the approach even though he was not properly positioned to make a successful landing. The pilot had a partial occlusion of a coronary artery, but its relationship to the accident was not determined. The aircraft impacted at about 6,250 feet msl. The field elevation is 5,315 feet msl. The accident site was about 2 1/2 mi from the airport. The airport was located in a mountain valley about 1 to 1.25 mi wide. Also, the airport and surrounding terrain were covered with snow. Both pilots were killed.