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Crash of a Cessna 207A Turbo Stationair 8 into Lake Powell: 2 killed

Date & Time: Aug 13, 2022 at 1609 LT
Operator:
Registration:
N9582M
Flight Phase:
Survivors:
Yes
Schedule:
Page - Page
MSN:
207-0705
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The single engine airplane departed Page on a local sightseeing flight, carrying one pilot and six French tourists. In unknown circumstances, the aircraft crashed into Lake Powell. Two passengers were killed while five other occupants were injured, three seriously.

Crash of a Cessna T207A Turbo Stationair 7 in Page: 1 killed

Date & Time: May 10, 2014 at 1545 LT
Operator:
Registration:
N7311U
Survivors:
Yes
Schedule:
Page - Page
MSN:
207A-0395
YOM:
1977
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6850
Captain / Total hours on type:
48.00
Aircraft flight hours:
14883
Circumstances:
During a local sightseeing flight, the pilot noticed that the engine had lost partial power, and he initiated a turn back toward the airport while troubleshooting the loss of power. Despite the pilot's attempts, the engine would not regain full power and was surging and sputtering randomly. The pilot entered the airport's traffic pattern on the downwind leg, and, while on final approach to the runway, the airplane encountered multiple downdrafts and wind gusts. It is likely that, due to the downdrafts and the partial loss of engine power, the pilot was not able to maintain airplane control. The airplane subsequently landed hard short of the runway surface and nosed over, coming to rest inverted. The reported wind conditions around the time of the accident varied between 20 and 70 degrees right of the runway heading and were 14 knots gusting to greater than 20 knots. In addition, a company pilot who landed about 8 minutes before the accident reported that he encountered strong downdrafts and windshear while on final approach to the runway and that he would not have been able to reach the runway if he had a partial or total loss of engine power. Postaccident examination of the airframe and engine revealed no evidence of any preexisting mechanical malfunctions or failures that would have precluded normal operation. The engine was subsequently installed on a test stand and was successfully run through various power settings for several minutes. The reason for the partial loss of engine power could not be determined.
Probable cause:
The pilot's inability to maintain aircraft control due to a partial loss of engine power and an encounter with downdrafts and gusting crosswinds while on final approach to the runway. The reason for the partial loss of engine power could not be determined because postaccident examination revealed no mechanical malfunction or failure that would have precluded normal operation.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Estes Park: 2 killed

Date & Time: Apr 30, 2000 at 1211 LT
Registration:
N7421S
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Page - Fort Collins
MSN:
61-0006
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4400
Circumstances:
While on a cross-country flight, according to radar data and weather information, the pilot descended below terrain clearance altitude and entered IMC conditions. The aircraft impacted a mountain peak approximately 100 feet below the summit. No flight plan had been filed and the pilot was not instrument rated.
Probable cause:
A descent below the surrounding terrain, by the pilot, in IMC conditions. Factors were high mountainous terrain, clouds, inaccurate weather evaluation by the pilot, and the pilot's flight into IMC conditions.
Final Report:

Crash of a Cessna 208B Grand Caravan in the Uncompahgre National Forest: 9 killed

Date & Time: Oct 8, 1997 at 0723 LT
Type of aircraft:
Operator:
Registration:
N12022
Flight Phase:
Survivors:
No
Site:
Schedule:
Montrose - Page
MSN:
208B-0432
YOM:
1995
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
12900
Captain / Total hours on type:
1546.00
Aircraft flight hours:
2599
Aircraft flight cycles:
3680
Circumstances:
The airplane departed under visual flight rules (VFR) for a flight over mountainous terrain. It was tracked by radar from the departure area to the accident site. While climbing at the normal rate of climb to 15,400 feet, the airplane abruptly disappeared from radar. The wreckage was located among pine trees and exhibited evidence of a steep flight path angle and damage consistent with a stall/spin event. Investigation revealed no indication of airframe or flight control anomalies, and the powerplant and propeller damage was consistent with engine operation at moderate to high power. Evidence indicated that the airplane was free of airframe ice at impact. Postaccident calculations indicate that the airplane was near the maximum certificated gross weight and aft center of gravity limit. The pilot did not maintain instrument flying currency and reportedly avoided instrument meteorological conditions (IMC). Evidence indicated that the pilot did not use oxygen, as required (when flying above 12,000 feet). Ground observations and satellite and Doppler radar imagery indicated widespread cloudiness over the mountains west of Montrose on the day of the accident. Satellite data showed variable cloud tops higher than the airplane's flight altitude in the vicinity of the accident. The radar plot of the aircraft during the climb above 10,000 feet indicated course changes from the southwest to the northwest, back to the southwest and then a sharp turn to the right just prior to the rapid descent.
Probable cause:
the pilot's failure to maintain sufficient airspeed for undetermined reasons while maneuvering the airplane near the maximum gross weight and aft cg in or near instrument meteorological conditions, resulting in the loss of control and entry into a stall/spin. Factors contributing to the accident were the pilot's improper in-flight planning and decision-making and his failure to use proper stall/spin recovery techniques.
Final Report:

Crash of a Cessna T207A Skywagon in Grand Canyon

Date & Time: Oct 10, 1989 at 1242 LT
Registration:
N7602U
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Page - Page
MSN:
207-0442
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2765
Captain / Total hours on type:
1000.00
Aircraft flight hours:
6302
Circumstances:
The airplane was flying a scenic tour when there was a loss of engine power. The pilot switched fuel tanks to the fullest tank and power was regained momentarily. The engine stopped. The propeller did not windmill. The pilot accomplished an off airport landing in rugged mountainous terrain. Disassembly of the engine revealed the crankshaft had fractured. Examination of the fracture revealed subsurface metal fatigue. The aircraft was destroyed and all three occupants were seriously injured.
Probable cause:
The inflight failure of the airplane's powerplant as a result metal fatigue which allowed the crankshaft to fracture. Contributing to the accident was mountainous terrain of the grand canyon which did not allow a suitable forced landing area.
Final Report:

Crash of a Douglas R4D-7 near Page: 14 killed

Date & Time: Oct 31, 1945
Operator:
Registration:
99834
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
16444/33192
YOM:
1945
Location:
Crew on board:
14
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
Enroute, the aircraft hit the slope of a mountain located near Page, killing all 14 occupants.