Zone

Crash of a Socata TBM-850 in Kalispell

Date & Time: Aug 11, 2025 at 1407 LT
Type of aircraft:
Operator:
Registration:
N860CA
Flight Type:
Survivors:
Yes
Schedule:
Pullman - Kalispell
MSN:
596
YOM:
2011
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1704
Captain / Total hours on type:
1244.00
Aircraft flight hours:
3312
Circumstances:
The pilot of the airplane reported that the airplane was too high during approach to the airport, and he responded by reducing the engine power to idle. When the airplane was about 40 ft above the runway, the “airspeed” aural caution sounded, and the pilot added engine power; however, the airspeed continued to decay, and the “stall” aural warning sounded. The airplane subsequently rolled left, impacted terrain alongside the left side of the runway, caught fire, and slid into the airport apron. The pilot and passengers were able to exit the airplane through the main cabin door before the airplane was destroyed by postaccident fire. The pilot reported there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.
Probable cause:
The pilot’s unstable approach to the runway, which resulted in an aerodynamic stall at low altitude and impact with terrain.
Final Report:

Crash of a Beechcraft A60 Duke in Snoqualmie Pass: 6 killed

Date & Time: Nov 21, 1992 at 0935 LT
Type of aircraft:
Operator:
Registration:
N100EK
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Seattle - Pullman
MSN:
P-209
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
3250
Circumstances:
While climbing in moderate icing conditions after takeoff, pilot was cleared to 17,000' feet. Radar data showed aircraft climbed at an indicated airspeed (IAS) of 82 to 123 knots. A Beech safety info booklet stated that a minimum airspeed of 140 knots must be maintained in icing conditions. Climbing at reduced airspeed would have increased angle of attack and allowed ice to accumulate under the wings and aft of the de-icing boots. Aircraft climbed to 13,500 feet, descended momentarily to 13,300 feet, then continued climbing as airspeed decreased abruptly. After slowing to 60 knots ias at 13,700 feet, the aircraft entered a steep descending turn and accelerated to high speed (above VNE). An emergency was declared, stating the aircraft 'lost an engine.' Soon thereafter, radar contact was lost and the aircraft crashed. Pieces of empennage surfaces separated in flight and were found at remote location from the main wreckage. Both counterweights separated from the elevators. Post crash tests disclosed no mechanical evidence of engine malfunction. Low ceiling, fog, light rain, snow and icing conditions were reported in area. All six occupants were killed.
Probable cause:
Failure of the pilot to maintain control of the aircraft, his failure to prevent the aircraft from exceeding the never exceed speed (VNE), and subsequent exceeding of the design stress limits of the aircraft. Factors related to the accident were: weather conditions (including icing conditions), improper airspeed, and loss of engine power for undetermined reason(s).
Final Report:

Crash of a Cessna 402C in Pullman: 1 killed

Date & Time: Dec 28, 1981 at 1003 LT
Type of aircraft:
Operator:
Registration:
N2749N
Flight Type:
Survivors:
No
Schedule:
Spokane - Lewiston
MSN:
402-0253
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
13000
Captain / Total hours on type:
1500.00
Circumstances:
On approach to Lewiston Airport, Idaho, the pilot encountered poor weather conditions and decided to divert to Pullman-Moscow Airport. This alternate airport was closed to traffic due to poor weather conditions as well. On approach in snow falls, the pilot failed to realize his altitude was insufficient when the airplane hit a ridge located half a mile north of the airport. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Controlled collision with ground on final approach due to improper IFR operation. The following contributing factors were reported:
- Low ceiling,
- Snow,
- ATC personnel failed to advise of unsafe airport conditions,
- Runway closed,
- Visibility half a mile or less,
- Weather conditions below minimums,
- Airport notamed closed, plowing,
- Controller did not have notam,
- Plows on runway.
Final Report: