Crash of a Beechcraft H18 in Allentown: 2 killed

Date & Time: Nov 25, 1983 at 0808 LT
Type of aircraft:
Registration:
N105PE
Flight Type:
Survivors:
No
Schedule:
Philadelphia - Wilkes Barre
MSN:
BA-672
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3800
Captain / Total hours on type:
145.00
Aircraft flight hours:
7046
Circumstances:
While en route, the pilot encountered icing conditions, then reported he was unable to maintain altitude and was having engine problems. He diverted toward Allentown, PA, then advised he had lost power in the left engine. Approach control began issuing vectors for a VOR approach; however, the pilot advised he was unable to open his approach plates and requested a surveillance radar approach. Radar vectors and advisories were provided until the pilot reported he had the airport in sight. Several witnesses observed that the left prop was feathered as the aircraft approached the airport. The pilot maneuvered the aircraft to a left downwind for runway 24 at about 400 feet agl with the landing gear extended. Witnesses reported the aircraft's nose pitch up, then down, then the aircraft rolled to the left and crashed. In a trailer court it hit a mobile home and a propane tank and burned. A person in the mobile home was fatally injured. An exam of the wreckage revealed the left prop blades were at the low pitch stops. No preimpact failures were found.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise - normal
Findings
1. (f) weather condition - carburetor icing conditions
2. (f) planning/decision - improper - pilot in command
----------
Occurrence #2: loss of engine power (total) - nonmechanical
Phase of operation: cruise
Findings
3. (f) delayed - pilot in command
4. (f) fuel system, ram air/induction air - ice
5. (f) fuel system, ram air/induction air - blocked (total)
----------
Occurrence #3: loss of control - in flight
Phase of operation: approach - VFR pattern - downwind
Findings
6. Precautionary landing - initiated - pilot in command
7. (c) airspeed (vmc) - not maintained - pilot in command
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Findings
8. Emergency procedure - attempted - pilot in command
Final Report:

Crash of a Beechcraft G18S in New Cumberland

Date & Time: Jun 12, 1981 at 2222 LT
Type of aircraft:
Registration:
N547DA
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
New Cumberland - Columbus
MSN:
BA-599
YOM:
1962
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7070
Captain / Total hours on type:
1455.00
Circumstances:
During the takeoff roll at New Cumberland Airport, the pilot decided to abort the takeoff due to technical issues on the left engine. Unable to stop within the remaining distance, the airplane overran, struck a moving vehicle on a road and crashed. The pilot was slightly injured while no one on the ground was injured.
Probable cause:
Engine failure or malfunction during takeoff due to blower, impeller assembly failure. The following contributing factors were reported:
- Material failure,
- Complete engine failure,
- Left engine supercharger,
- Rear bearing failed.
Final Report:

Crash of a Beechcraft D18S off Manitou Beach: 2 killed

Date & Time: Jul 27, 1970 at 0045 LT
Type of aircraft:
Registration:
N332R
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Rockford - Detroit
MSN:
A-8
YOM:
1945
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3050
Captain / Total hours on type:
1200.00
Circumstances:
The pilot and his passenger departed Rockford in the early morning and completed several flights in the region all along the day. While cruising by night over Lake Michigan, the pilot lost control of the airplane that crashed into the lake off Manitou Beach. Both occupants were killed.
Probable cause:
Loss of control in flight after the pilot became lost/disoriented. The following factors were considered as contributing:
- Physical impairment,
- Pilot fatigue,
- Departed Rockford approximately 18 hours prior to the accident,
- Flew 10 hours during the day,
- Attended copilot picnic observed with can beer,
- Toxicologic not decisive.
Final Report: