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Crash of a Socata TBM-700 in Lancaster

Date & Time: Dec 27, 2005 at 1446 LT
Type of aircraft:
Operator:
Registration:
N198X
Flight Type:
Survivors:
Yes
Schedule:
Camarillo - Lancaster
MSN:
138
YOM:
1998
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6296
Captain / Total hours on type:
2921.00
Copilot / Total flying hours:
1126
Copilot / Total hours on type:
15
Aircraft flight hours:
1603
Circumstances:
The airplane stalled on short final approach, and it impacted the ground. The purpose of the flight was for the student to receive dual flight instruction to become more acquainted with the airplane's handling characteristics. The student met with his certified flight instructor and received a briefing regarding the upcoming lesson involving, in part, takeoff and landing practice. The instructor directed his student to perform a simulated engine out approach, and engine power was reduced as the airplane glided toward the airport. The student entered a close in downwind approach and, at the direction of the instructor, then performed a left circling turn onto the base and final approach legs. The landing gear was lowered, and the student questioned the instructor regarding whether they could glide all the way to the runway. The instructor advised his student to maintain 90 knots airspeed. During the descent, as the airplane turned from the close in base leg onto the final approach leg, the instructor told his student "don't bank." The student rolled the wings level. Immediately thereafter, the left bank began a second time and the instructor again said, "Don't bank." The student replied, "I'm not." The instructor applied engine power and right rudder to reduce the left bank. The airplane stopped rolling left, and then rolled into a right bank, whereupon the right wing impacted the ground. At no time did the instructor direct his student to release the airplane's flight controls.
Probable cause:
The student's failure to maintain adequate airspeed, and the instructor's inadequate supervision and delayed remedial action, which resulted in a stall/mush.
Final Report:

Crash of a Learjet 24 in Lancaster: 1 killed

Date & Time: Oct 17, 1978 at 0913 LT
Type of aircraft:
Operator:
Registration:
N123RE
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Lancaster - Lancaster
MSN:
24-154
YOM:
1967
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8390
Captain / Total hours on type:
379.00
Circumstances:
The crew departed Santa Ana in the early morning to follow a training program at Lancaster-General William J. Fox Airport. He was completing several touch-and-goes when control was lost during initial climb. The airplane swerved on runway and eventually crashed. The copilot was seriously injured while the captain was killed.
Probable cause:
Ground loop and controlled collision with ground during initial climb after the crew failed to maintain directional control while completing touch and go landing.
Final Report:

Crash of a Piper PA-61 Aerostar in Dubois: 2 killed

Date & Time: Jan 24, 1978 at 2005 LT
Registration:
N1BE
Flight Phase:
Survivors:
No
Schedule:
Dubois - Lancaster
MSN:
61-0245-041
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1230
Captain / Total hours on type:
560.00
Circumstances:
After takeoff from Dubois-Jefferson County Airport, while in initial climb, the pilot encountered engine trouble. He attempted an emergency landing when the airplane went out of control and crashed near the airport. Both occupants were killed.
Probable cause:
Loss of control during initial climb due to foreign material affecting normal engine operations. The following contributing factors were reported:
- Ice in fuel,
- Fuel starvation,
- Improper emergency procedures,
- Improper operation of flight controls,
- Complete engine failure,
- Forced landing off airport on land,
- Ice was found in fuel flow divider and lines.
Final Report: