Zone

Crash of a De Havilland DHC-6 Twin Otter 100 in Fentress

Date & Time: Apr 9, 2016 at 1700 LT
Operator:
Registration:
N122PM
Survivors:
Yes
Schedule:
Fentress - Fentress
MSN:
15
YOM:
1966
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6000
Captain / Total hours on type:
1000.00
Aircraft flight hours:
53624
Circumstances:
The pilot reported that he was landing in gusty crosswind conditions following a parachute jump flight, and that the gusty conditions had persisted for the previous 10 skydiving flights that day. The pilot further reported that during the landing roll, when the nose wheel touched down, the airplane became "unstable" and veered to the left. He reported that he applied right rudder and added power to abort the landing, but the airplane departed the runway to the left and the left wing impacted a tree. The airplane spun 180 degrees to the left and came to rest after the impact with the tree. The left wing was substantially damaged. The pilot did not report any mechanical malfunctions or failures with the airplane that would have precluded normal operation.
Probable cause:
The pilot's failure to maintain directional control during the aborted landing in gusty crosswind conditions, which resulted in a runway excursion and a collision with a tree.
Final Report:

Crash of a Beechcraft A90 King Air in Fentress

Date & Time: Oct 17, 2003 at 1530 LT
Type of aircraft:
Operator:
Registration:
N511BF
Survivors:
Yes
Schedule:
San Marcos - San Marcos
MSN:
LJ-179
YOM:
1966
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1127
Captain / Total hours on type:
247.00
Aircraft flight hours:
10399
Circumstances:
The airplane lost engine power during descent. The 1,127-hour pilot elected to perform emergency engine out procedures and prepared for an emergency landing. After impact, the pilot observed the right engine nacelle engulfed in flames, which then spread to the fuselage. Review of the engine logbook revealed the engine was being operated in excess of 1,000 hours of the manufacturer's recommended time between overhauls of 3,600 hours. The airplane received post-impact fire damage. Further examination of the engine revealed severe fire damage, but no mechanical deficiencies.
Probable cause:
The loss of engine power for undetermined reasons.
Final Report: