Crash of a Cessna 414 Chancellor in Coatesville: 4 killed

Date & Time: Jan 31, 1985 at 1310 LT
Type of aircraft:
Registration:
N1994G
Survivors:
No
Schedule:
Latrobe - Coatesville
MSN:
414-0601
YOM:
1975
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
2200
Captain / Total hours on type:
49.00
Aircraft flight hours:
3695
Circumstances:
Aircraft was on its runway 29 approach when it collided with ground one mile from the airport. A witness saw he aircraft fly over the airport to the west between 500 to 1,500 feet. Witnesses near the accident site saw the aircraft making abrupt maneuvers at low altitude prior to the accident. Engine sounds was described as 'racing', 'uneven', and 'loud'. Weather condition was described as fog, low ceiling, and light rain. Another pilot in same type aircraft was unable to land due to weather. Examination of the aircraft did not disclosed evidence of malfunction. Flight approach navaid facilities flight checked to be operational. There was no evidence of pilot physical impairment or incapacitation. The aircraft collided with the ground in a near vertical attitude. All four occupants were killed.
Probable cause:
Occurrence #1: in flight collision with terrain/water
Phase of operation: approach
Findings
1. (f) weather condition - low ceiling
2. (f) weather condition - fog
3. (f) weather condition - rain
4. (c) aircraft handling - inadequate - pilot in command
5. (c) ifr procedure - improper - pilot in command
6. (c) airspeed - not maintained - pilot in command
7. (c) stall - inadvertent - pilot in command
Final Report:

Crash of a Lockheed L-188AF Electra in Chalkhill: 4 killed

Date & Time: May 30, 1984 at 0144 LT
Type of aircraft:
Operator:
Registration:
N5523
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Baltimore - Detroit
MSN:
1034
YOM:
1959
Flight number:
VK931
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
10047
Captain / Total hours on type:
7173.00
Copilot / Total flying hours:
3534
Copilot / Total hours on type:
2558
Aircraft flight hours:
35668
Aircraft flight cycles:
38353
Circumstances:
Zantop ground personnel completed the loading of Flight 931 at 00:40. All cargo was bulk loaded and tied down on the right side of the airplane for the full length of the cargo compartment. Flight 931 departed the gate at Baltimore/Washington International Airport at 01:05 and took off on runway 28 at 01:10. At 01:11:42, Flight 931 contacted Baltimore departure control and was cleared to 13,000 feet. After switching to Washington ARTCC, the flight was cleared further FL220. At 01:32 a no. 2 gyro malfunction made the crew select the no. 1 gyro to drive both approach horizons and the problem appeared resolved. At 01:43:09, Cleveland ARTCC cleared Flight 931 direct to the Dryer VOR. After the turn to the Dryer VOR, the first officer’s approach horizon may have displayed incorrect pitch and roll information. The flightcrew may have received conflicting pitch and roll information from the two approach horizons as they attempted to recover from an unusual attitude. The flightcrew overstressed the airplane in an attempt to recover from the unusual attitude as the aircraft spiralled down. The Electra broke up and falling wreckage damaged some houses; however, most of the wreckage fell in uninhabited, wooded areas.
Probable cause:
The aircraft's entry into an unusual attitude and the inability of the flight crew to analyse the flight condition before there was a complete loss of control. Although the precise reason for the loss of control was not identified, an undetermined failure of a component in the No.2 vertical gyro system, perhaps involving the amplifier and associated circuitry, probably contributed to the cause of the accident by incorrectly processing data to the co-pilot's approach horizon. The in-flight structural failure of the aircraft was due to overload.
Final Report:

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 Rockwell Aero Commander 500 in Franklin: 6 killed

Date & Time: Nov 20, 1983 at 1819 LT
Registration:
N6226X
Survivors:
No
Schedule:
Youngstown – Plattsburgh – Burlington – Youngstown
MSN:
500-1098-52
YOM:
1961
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
1527
Captain / Total hours on type:
33.00
Aircraft flight hours:
5421
Circumstances:
Before departing Youngstown, OH, the pilot filed two IFR flight plans, one for a flight to Plattsburgh, NY, the other for a return flight from Plattsburgh back to Youngstown. After a 2 hour and 10 minutes flight to Plattsburgh, 70 gallons of fuel was added, but the person who serviced the aircraft indicated the tanks were not full after servicing. The plane then made a 10 minutes flight to Burlington, VT, but no fuel was added at Burlington. The pilot then took off on a return flight to Youngstown. During the descent phase to Youngstown, the pilot requested vectors to the closest airport. He was provide vectors to the Chess Lamberton Airport and advised it was 6 miles away. A short time later, the pilot said the aircraft had lost power. Subsequently, it crashed in rolling, wooded terrain. During an exam, no fuel was found in the aircraft. No other evidence of a malfunction or failure was found. With the passenger and cargo load, a maximum of about 104 gallons of fuel could have been used without exceeding the certificated gross weight of the aircraft. At 45 to 55% power, the aircraft burned 17 to 22 gallons per hour. Wind gusts 30 knots. All six occupants were killed.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: descent - normal
Findings
1. (c) preflight planning/preparation - inadequate - pilot in command
2. (c) continued - pilot in command
3. (c) fluid,fuel - exhaustion
4. (c) fuel supply - inadequate - pilot in command
5. Aircraft performance, two or more engines - inoperative
----------
Occurrence #2: forced landing
Phase of operation: other
----------
Occurrence #3: in flight collision with object
Phase of operation: descent
Findings
6. (f) light condition - dark night
7. (f) weather condition - low ceiling
8. (f) weather condition - fog
9. (f) weather condition - rain
10. (f) weather condition - unfavorable wind
11. (f) object - tree(s)
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Rockwell Grand Commander 680FLP in Sunbury: 2 killed

Date & Time: Feb 3, 1983 at 1202 LT
Registration:
N12LF
Flight Phase:
Survivors:
No
Schedule:
Teterboro - Clintonville
MSN:
680-1491-12
YOM:
1965
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5650
Captain / Total hours on type:
300.00
Aircraft flight hours:
5052
Circumstances:
At approximately 0928 est, the pilot obtained a FSS weather briefing by telephone. He was briefed on conditions of low ceilings, fog, light rain, drizzle, snow and blowing snow along his route. However, he did not ask about icing conditions and the briefing did not include a fight precaution for icing nor a sigmet (issued at 0820 est) which forecasted moderate to severe mixed icing. While en route, the pilot made several altitude changes by request. When he was queried about a heading deviation, he replied 'we're having a little problem.' this was the last radio contact. ATC received no radio calls concerning icing problems or an emergency. Witnesses near the crash site saw the aircraft come out of the clouds in a near vertical descent, rotating in a nose down attitude, then impact and burn. Airframe ice up to 1/2 inch thick was found on/near parts that were not fire damaged.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (f) weather condition - icing conditions
2. (c) preflight briefing service - inadequate - ATC personnel (FSS)
----------
Occurrence #2: loss of control - in flight
Phase of operation: cruise
Findings
3. (c) in-flight planning/decision - inadequate - pilot in command
4. (c) wing - ice
5. (c) stabilizer - ice
6. (c) aircraft performance - deteriorated
7. (c) stall/spin - inadvertent - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Cessna 402B in Meadville

Date & Time: Nov 1, 1982 at 0900 LT
Type of aircraft:
Operator:
Registration:
N402DL
Survivors:
Yes
Schedule:
Allentown - Meadville
MSN:
402B-0598
YOM:
1974
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5500
Captain / Total hours on type:
400.00
Aircraft flight hours:
2592
Circumstances:
The pilot approached high and fast for landing on runway 04. The wind was from 240° at 10 to 12 knots. The aircraft floated and after touchdown, the pilot was unable to stop on the wet, downsloping runway. After departing the runway, the aircraft continued down a steeper slope and into an area of brush and trees. All three gear collapsed, there was leading edge spar damage on both wings, and the right side fuselage skin, forward of the right wing, was damaged.
Probable cause:
Occurrence #1: overrun
Phase of operation: landing - roll
Findings
1. (f) weather condition - tailwind
2. (f) wrong runway - selected - pilot in command
3. (c) distance - misjudged - pilot in command
4. (c) airspeed - misjudged - pilot in command
5. (c) go-around - not performed - pilot in command
6. (f) airport facilities,runway/landing area condition - downhill
7. (f) airport facilities,runway/landing area condition - wet
8. (f) aircraft performance,hydroplaning condition - water
----------
Occurrence #2: complete gear collapsed
Phase of operation: landing - roll
Findings
9. (f) terrain condition - downhill
10. (f) terrain condition - high vegetation
11. Landing gear - overload
----------
Occurrence #3: on ground/water collision with object
Phase of operation: landing - roll
Findings
12. (f) object - tree(s)
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 Cessna 401A in State College: 1 killed

Date & Time: Apr 21, 1981 at 2000 LT
Type of aircraft:
Registration:
N6265Q
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
State College - State College
MSN:
401A-0065
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6215
Circumstances:
After takeoff from State College-University Park, while in a local training flight, one of the engine failed. The pilot lost control of the airplane that stalled and crashed, bursting into flames. The pilot, sole on board, was killed.
Probable cause:
Stall during initial climb due to powerplant failure for undetermined reasons. The following contributing factors were reported:
- The pilot failed to maintain flying speed.
Final Report:

Crash of a Cessna 402B in Bloomsburg

Date & Time: Mar 11, 1981 at 0930 LT
Type of aircraft:
Operator:
Registration:
N7888Q
Flight Phase:
Survivors:
Yes
Schedule:
Bloomsburg - Gardner
MSN:
402B-0216
YOM:
1972
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8064
Captain / Total hours on type:
1604.00
Circumstances:
While taking off from a contaminated runway at Bloomsburg Airport, the pilot lost control of the airplane that stalled, veered off runway and crashed. Both occupants were injured, the passenger seriously, and the airplane was destroyed.
Probable cause:
Stall during initial climb for undetermined reasons. The following contributing factors were reported:
- Collision with dirt bank,
- Snow,
- Icing conditions including sleet, freezing rain,
- Airport conditions: snow on runway,
- Visibility one mile or less,
- Blowing snow,
- The pilot removed snow before takeoff,
- After takeoff, shuddered, 100 knots in ground effect,
- Ice beads frozen on wet wings of other aircraft.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Bermudian Valley Airpark

Date & Time: Feb 2, 1981 at 0859 LT
Type of aircraft:
Registration:
N45437
Flight Type:
Survivors:
Yes
Schedule:
Hagerstown - Harrisburg
MSN:
AF-452
YOM:
1953
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11300
Captain / Total hours on type:
4250.00
Circumstances:
En route from Hagerstown to Harrisburg, the crew reported engine problems and was cleared to divert to the nearest airport. He eventually decided to attempt an emergency landing in a field near Bermudian Valley Airpark, PA. Both occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Engine failure in normal cruise due to improper maintenance on part of the maintenance personnel. The following contributing factors were reported:
- Carburetor deicing system,
- Ice carburetor,
- The pilot-in-command failed to follow approved procedures,
- Improper emergency procedures,
- Failure to provide adequate directives, manual, equipment,
- Intentional wheels-up landing,
- Conditions conducive to carburetor/induction system icing,
- Partial loss of power on one engine,
- Bolts vice taper pins installed in right carburetor air system,
- Improper flight manual,
- Full power not applied.
Final Report: