Operator Image

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 Beechcraft A100 King Air in Brooksville

Date & Time: Nov 8, 1986 at 0616 LT
Type of aircraft:
Operator:
Registration:
N78L
Survivors:
Yes
Schedule:
Brooksville – Miami
MSN:
B-167
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7290
Captain / Total hours on type:
150.00
Aircraft flight hours:
5500
Circumstances:
The pilot stated that shortly after departure the cockpit filled with smoke. While returning for landing his visibility was reduced due to the smoke and ground fog. On landing roll the the aircraft ran off the left side of the runway, went through a cow fence and came to rest against a tree. A post crash fire erupted in the left wing area where a fence post punctured the wing and the aircraft was destroyed by the fire. The cause of the smoke in the cockpit could not be determined. The pilot, sole on board, escaped with minor injuries.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: climb - to cruise
Findings
1. (f) other system - smoke
2. (c) reason for occurrence undetermined
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
3. (f) weather condition - fog
4. (f) light condition - night
5. (f) other system - smoke
6. (c) visual lookout - not possible - pilot in command
7. Object - fence
8. Object - tree(s)
Final Report: