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Crash of a Cessna 207 Skywagon in Grants Pass: 2 killed

Date & Time: Apr 9, 2003 at 0850 LT
Registration:
N9785M
Survivors:
No
Site:
Schedule:
North Bend – Grants Pass
MSN:
207-0729
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
34976
Aircraft flight hours:
4516
Circumstances:
During a visual flight rules (VFR) cross-country flight from North Bend, Oregon, to Grants Pass, Oregon, the airplane collided with mountainous terrain approximately seven miles northwest of the pilot's planned destination. Weather data and witness reports outlined areas of low ceilings and low visibility throughout the area during the approximate time of the accident. Post-accident inspection of the aircraft and engine revealed no evidence of a mechanical malfunction or failure.
Probable cause:
The pilot's failure to maintain clearance from mountainous terrain while in cruise flight. Factors include low ceilings and mountainous terrain.
Final Report:

Crash of a Cessna 421B Golden Eagle II in North Bend: 2 killed

Date & Time: Mar 8, 1999 at 2145 LT
Operator:
Registration:
N41096
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
North Bend - Aurora
MSN:
421B-0446
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1200
Captain / Total hours on type:
135.00
Aircraft flight hours:
2342
Circumstances:
Witnesses reported hearing the engines start and shortly thereafter, the airplane taxied to the runway. The pilot then contacted ATC for an IFR clearance. The clearance was given with a short void time. The pilot acknowledged the clearance and began the takeoff ground roll. Witnesses reported that the night-time takeoff roll and engine sound appeared normal. Witnesses near the end of the runway reported that the airplane was observed at about 50 feet above the runway with about 1,000 feet of runway remaining when engine power was reduced on both engines. The airplane was heard to touch down, then engine power was reapplied. Shortly thereafter, the sound of the impact was heard. The airplane collided with the terrain about 600 feet from the end of the runway. During the post-accident inspection of the airplane and engines, no evidence was found to indicate a mechanical failure or malfunction. Documentation of the events indicated that from the time the aircraft began its taxi to the runway, to the time the takeoff roll began, was approximately six minutes in duration. Before the takeoff roll began, the pilot had accepted a clearance with a void time of four minutes. By the time the pilot correctly read back the clearance, less than two minutes remained before the void time. Post accident documentation of the accident site revealed that neither the pilot nor the passenger were wearing their lap belts or shoulder harnesses. It was also noted that the pilot had not yet selected the discrete transponder code as indicated by the clearance.
Probable cause:
A delayed aborted takeoff for an undetermined reason.
Final Report:

Crash of a Rockwell Grand Commander 680 in North Bend: 3 killed

Date & Time: Jun 1, 1995 at 1554 LT
Operator:
Registration:
N6877S
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
North Bend - North Bend
MSN:
680-462-132
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1450
Aircraft flight hours:
4785
Circumstances:
Approximately two minutes after takeoff, witnesses saw the airplane pull up sharply into a steep climb from underneath an 800-foot ceiling. The airplane went into an uncontrolled, nearly vertical dive and impacted into a river. The pilot did not hold multi-engine or instrument ratings. Individuals who knew the pilot, including an instructor who had flown with him, stated that they had doubted the pilot's competence but that the pilot had been confident of his own flying ability.
Probable cause:
The pilot initiating flight into weather conditions beyond what he was capable of handling. The pilot's overconfidence in his personal ability and the low ceiling were factors in the accident.
Final Report: