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Crash of a Cessna 402B in Bronson: 1 killed

Date & Time: Jan 23, 2002 at 0735 LT
Type of aircraft:
Operator:
Registration:
N371JD
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sturgis - Ann Arbor
MSN:
402B-1322
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1800
Aircraft flight hours:
7339
Circumstances:
The airplane was destroyed when it impacted the ground while maneuvering at a low altitude following a loss of control in instrument meteorological conditions. The airplane was on a flight in instrument meteorological conditions when radar and voice contact were lost. Prior to the loss of communication, controllers advised the pilot to check altitude. At this point, the radar data shows that the airplane was about 400 feet below the assigned altitude. Subsequently, the pilot said, "roger sir my auto pilot i just cut off uh correcting immediately." This was the last received transmission from the pilot. The radar data shows that the airplane then began a descending right turn at an average rate of descent of 1,276 feet per minute. This descent was followed by a climbing left turn with an average rate of climb of 5,423 feet per minute. The radar data shows that the radius of the left turn continued to decrease until radar contact was lost about 500 feet above the last assigned altitude. A witness who saw the airplane just prior to impact described the airplane maneuvering beneath the clouds prior to pulling up sharply and then pitching down and impacting the ground. There was a utility wire and associated poles running across the airplane's flight path in the field where the wreckage was located. The airplane exploded and burned upon impact. No anomalies were found with the airplane or associated systems. The autopilot section of the Pilot's Operating Handbook states, "Sustained elevator overpower will result in the autopilot trimming against the overpower force." The result is that if up elevator pressure is applied with the autopilot engaged, the autopilot will trim the airplane nose down.
Probable cause:
The maneuver to avoid the utility wire while maneuvering resulting in an inadvertent stall and subsequent impact with the ground. Factors were the pilot's inadvertent activation of the elevator trim, resulting in a loss of control during flight in instrument meteorological conditions, as a result of pilot's lack of knowledge concerning the operation of the autopilot system. Another factor was the utility wire.
Final Report:

Crash of a Cessna 340A in Oxford

Date & Time: Nov 20, 1988 at 1820 LT
Type of aircraft:
Operator:
Registration:
N468CM
Flight Type:
Survivors:
Yes
Schedule:
Ann Arbor – Oxford
MSN:
340A-1017
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Total fatalities:
0
Captain / Total flying hours:
22092
Captain / Total hours on type:
25.00
Circumstances:
According to witnesses, the weather was changing from minute to minute as the aircraft was arriving. Witnesses reported the wind was blowing from east to northeast at 10 to 15 knots, rain fall was varying from strong to periods of light rain, and the ceiling (cloud level) was variable. The pilot began an ILS runway 36 approach; however, before reaching the airport, the aircraft collided with trees and crashed about 2 miles short of the runway. The pilot was seriously injured and could not remember the accident, but did recalled receiving a wind shear alert. The pilot reported an intermittent problem with the autopilot heading mode; however, no other preimpact malfunction or failure of the acft was evident. All five occupants were injured, two seriously.
Probable cause:
Collision with trees and terrain due to the pilot exceeding approach minimum altitude during an ILS approach.
Occurrence #1: in flight collision with object
Phase of operation: approach - faf/outer marker to threshold (ifr)
Findings
1. (f) light condition - dusk
2. (f) weather condition - low ceiling
3. (f) weather condition - fog
4. (f) weather condition - rain
5. (f) weather condition - unfavorable wind
6. (f) weather condition - windshear
7. (c) ifr procedure - not followed - pilot in command
8. (c) decision height - not used - pilot in command
----------
Occurrence #2: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Beechcraft G18S in Ann Arbor

Date & Time: Dec 29, 1973 at 1336 LT
Type of aircraft:
Operator:
Registration:
N118W
Flight Phase:
Survivors:
Yes
Schedule:
Ann Arbor - Allentown
MSN:
BA-470
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2700
Captain / Total hours on type:
700.00
Circumstances:
While taking off from Ann Arbor in poor weather conditions with snow falls and low ceiling, the pilot lost control of the airplane that stalled and crashed in a field. All five occupants were evacuated and the aircraft was damaged beyond repair. The aircraft was not deiced prior to departure.
Probable cause:
Inadequate preflight preparation on part of the pilot who failed to maintain flying speed after takeoff. The following factors were reported:
- Airframe ice,
- Low ceiling and snow,
- Encrusted snow approximately 1/8 to 1/4 inch thick on top of wing and tail surfaces.
Final Report:

Crash of a Cessna 421B Golden Eagle II in Pataskala: 1 killed

Date & Time: Jul 3, 1972 at 1132 LT
Operator:
Registration:
N5977M
Survivors:
No
Schedule:
Ann Arbor - Columbus
MSN:
421B-0220
YOM:
1972
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1563
Captain / Total hours on type:
500.00
Circumstances:
While approaching Columbus-John Glenn in marginal weather conditions, the pilot failed to realize his altitude was too low when the airplane struck power cables and trees, stalled and crashed in Pataskala, about 10,5 miles east of the airport. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
The accident was caused by the incapacitation of the pilot. The following factors were reported:
- Low ceiling and fog,
- The pilot had moderate to severe arteriosclerosis.
Final Report: