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Crash of a Cessna 340 in Lytle Creek: 2 killed

Date & Time: Jan 18, 2010 at 1508 LT
Type of aircraft:
Registration:
N2217B
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Henderson – Compton
MSN:
340-0532
YOM:
1975
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
474
Aircraft flight hours:
3105
Circumstances:
The pilot was on a cross-country flight near mountainous terrain when he encountered clouds along the flight path. A comparison of recorded radar data and weather reports in the local area indicated that the pilot was maneuvering near the cloud bases in an area with low visibility and ceilings. Based on the erratic and circling flight path, it is likely that the pilot was having difficulty determining his location and desired flight track when the airplane collided with terrain. Post accident examination of the airframe and engine revealed no mechanical failures or malfunctions that would have precluded normal operation.
Probable cause:
The pilot’s loss of situational awareness while maneuvering under a cloud layer and failure to maintain sufficient clearance from mountainous terrain.
Final Report:

Crash of a Consolidated B-24D-40-CO Liberator near Lytle Creek: 5 killed

Date & Time: Mar 5, 1943 at 0858 LT
Operator:
Registration:
42-40242
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
March - March
MSN:
1319
YOM:
1943
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The airplane departed March AFB on a routine training exercise. En route, it suffered a catastrophe structural failure, lost its tail section and crashed in a mountainous area located near Lytle Creek. All five crew members were killed.
Crew:
Cpt Marvin J. Frum, pilot,
2nd Lt Marshall E. Oberg, copilot,
T/Sgt Merle F. Draper, flight engineer,
S/Sgt Fred Bedford, radio operator,
S/Sgt Russell P. Boyd, air gunner.
Probable cause:
Catastrophic structural failure in flight. Investigators speculated that the pilots may have put the aircraft through maneuvers that exceeded the structural limitations of the airframe, causing the tail section to separate and then the port wing to fail between the n°1 and n°2 engines.