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Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Coatesville: 2 killed

Date & Time: Jan 10, 2000 at 0519 LT
Registration:
N905DK
Flight Type:
Survivors:
No
Schedule:
Millville – Coatesville
MSN:
61-0308-081
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
350
Circumstances:
While operating in IMC, the pilot was vectored to the final approach course for an ILS approach. Weather at the airport was ceiling 200 feet and visibility 3/4 mile in mist. The pilot was cleared for the approach, which he acknowledged. No other transmissions were received from the accident airplane. Radar data showed the airplane intercept the final approach course, then track inbound. The airplane crossed the outer marker 420 feet below the glide slope. The last radar return showed the airplane at 440 feet agl, 3.9 miles from the runway. The airplane impacted the ground at a shallow angle about 1 mile north of the airport on the opposite side of the missed approach procedure. The elevation of the accident site was approximately 40 feet lower than the airport. The pilot had about 350 hours of total flight
experience. No pre-impact failures were identified with the airframe, engines, flight controls, or flight instruments.
Probable cause:
The pilot's failure to follow the published instrument approach procedure, and his failure to establish a climb after passing the missed approach point.
Final Report:

Crash of a Beechcraft A100 King Air in Cedarville: 2 killed

Date & Time: Feb 1, 1985 at 2147 LT
Type of aircraft:
Registration:
N72BS
Flight Type:
Survivors:
No
Schedule:
Ridgeland – Millville
MSN:
B-113
YOM:
1972
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
17300
Captain / Total hours on type:
4000.00
Circumstances:
The two atp rated pilots were en route back to their home base airport flying on an IFR flight plan in actual instrument weather conditions. Communications with ATC controllers was normal. During a night localizer approach into Millville municipal airport, an ATC specialist observed the aircraft passing through the localizer track and issued a vector for re-interception. The aircraft was subsequently observed tracking inbound on course. The pilot reported crossing the om. This was the last transmission heard from the pilot and was routine. The aircraft crashed into a wooded area just beyond the om and was destroyed in a post impact fire. Post accident examination of the wreckage revealed evidence to indicate the left engine was producing less power than the right engine at impact. Both occupants were killed.
Probable cause:
Occurrence #1: in flight collision with object
Phase of operation: descent - normal
Findings
1. (f) weather condition - low ceiling
2. (f) weather condition - fog
3. (f) weather condition - rain
4. (f) light condition - dark night
5. (c) ifr procedure - improper - pilot in command
6. (c) proper altitude - not maintained - pilot in command
----------
Occurrence #2: loss of engine power
Phase of operation: approach
Findings
7. Engine assembly - failure,partial
8. (c) engine assembly - undetermined
Final Report:

Crash of a Beechcraft E18S in Millville

Date & Time: Jun 7, 1967 at 0030 LT
Type of aircraft:
Operator:
Registration:
N157SC
Flight Type:
Survivors:
Yes
MSN:
BA-404
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8000
Captain / Total hours on type:
3000.00
Circumstances:
The approach to Millville Airport was completed at a too high speed and with the flaps retracted. After touchdown, the pilot completed a heavy braking procedure. Control was lost and the airplane veered off runway and came to rest in flames in a grassy area. All three occupants were uninjured while the aircraft was destroyed.
Probable cause:
The pilot misjudged distance, speed and altitude and failed to extend the landing flaps. Directional control lost after landing.
Final Report: