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Crash of a Beechcraft A90 King Air in Crestview: 3 killed

Date & Time: Nov 13, 1990 at 0831 LT
Type of aircraft:
Operator:
Registration:
N2EP
Flight Type:
Survivors:
No
Schedule:
Crestview - Crestview
MSN:
LJ-284
YOM:
1967
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9726
Captain / Total hours on type:
135.00
Circumstances:
The pic/cfi was conducting a public use instructional flight with two military rated student pilots. The airplane was observed at about 60 to 80 feet agl south of the approach end of an active runway. It yawed to the right, and back to the left, colliding with the terrain in a 45° leftwing-low attitude, and disappeared from view. He flight had been in the pattern making touch-and-go's, and had earlier reported a single engine approach. This landing was to be a full-stop. All three occupants were killed.
Probable cause:
The pilot-in-command/cfi improper supervision of the dual student. This resulted in an in flight loss of control, and collision with terrain for failure to maintain minimum control airspeed (VMC) while conducting a simulated emergency procedure.
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith 600) in Florala

Date & Time: Aug 29, 1983 at 1500 LT
Registration:
N139TS
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Florala – Crestview
MSN:
60-0139-059
YOM:
1973
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4616
Captain / Total hours on type:
430.00
Aircraft flight hours:
1400
Circumstances:
The pilot stated that during takeoff roll he experienced a power surge but the engine did not quit. He aborted the takeoff by reducing power on both engines and applying brakes. This resulted in the aircraft swerving off the right side of the runway, rolling thru the grass and striking a culvert which separated the landing gear. Wreckage examination revealed: both throttles at idle, mixture and prop controls were full forward and full rich and high rpm on respective engine controls. All cables attaching hardware was intact.
Probable cause:
Occurrence #1: loss of control - on ground/water
Phase of operation: takeoff - roll/run
Findings
1. (c) directional control - not maintained - pilot in command
2. (f) ground loop/swerve - inadvertent - pilot in command
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Occurrence #2: on ground/water encounter with terrain/water
Phase of operation: takeoff - roll/run
Findings
3. (f) terrain condition - rough/uneven
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Occurrence #3: main gear collapsed
Phase of operation: takeoff - roll/run
Final Report: