Crash of a Douglas DC-9-15 in Urbana: 25 killed

Date & Time: Mar 9, 1967 at 1153 LT
Type of aircraft:
Operator:
Registration:
N1063T
Flight Phase:
Survivors:
No
Schedule:
New York – Harrisburg – Pittsburgh – Dayton – Chicago
MSN:
45777/80
YOM:
1967
Flight number:
TW553
Location:
Crew on board:
4
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
25
Captain / Total flying hours:
9832
Captain / Total hours on type:
193.00
Copilot / Total flying hours:
1560
Copilot / Total hours on type:
15
Circumstances:
Flight 553 was a scheduled domestic passenger flight from New York to Chicago, Illinois, with en-route stops at Harrisburg, Pittsburgh, Pennsylvania, and Dayton, Ohio. The flight departed Pittsburgh for Dayton at 1125 hours Eastern Standard Time on an IFR flight plan and was operated under radar surveillance for the duration of the flight. As the flight approached the Dayton terminal area it was cleared to descend from FL 200, its cruising altitude, to 5 000 ft, and a transfer of radar control from Indianapolis Air Route Traffic Control Centre (ARTCC) to the Dayton Radar Approach Control facility (RAPCON) was made when the flight was approximately 8 miles northeast of the Urbana Intersection on Victor Airway 12 North. The Dayton RAPCON approach controller established radio contact with the flight at 1152:36 hours. The flight was again cleared to 5 000 ft, instructed to take a heading of 240° for a vector to the final approach course (ILS) and to report leaving 6 000 ft. At 1153:22 hours, the controller cleared the flight to descend to and maintain 3 000 ft and turn left to a heading of 230'. This was correctly acknowledged by the pilot- in-command at 1153:28 hours. Immediately after the issuance of this clearance the controller observed for the first time an unidentified radar target ahead and slightly to the right of the flight and issued at 1153:32 hours the following traffic advisory: "TWA five fifty three, roger, and traffic at twelve thirty, one mile, southbound, slow moving." This was acknowledged by the pilot-in-command at 1153:36 hours. Approximately 14 seconds later, the flight and the unidentified radar target merged, separated, changed shape on the radar screen and then disappeared. At 1154:02 hours the controller advised the flight that it was clear of traffic but no reply was received. Subsequent efforts to establish contact with the flight were unsuccessful. The unidentified radar return was from a Beechcraft Baron B-55 on a company business flight, en route from Detroit, Michigan, to Springfield, Ohio. The aircraft had departed Detroit City Airport at 1101 hours on a special VFR clearance to leave the control zone 5 miles from the airport. No flight plan was filed, nor was one required. Approximately two minutes after take-off, the pilot reported on top of the smoke and haze and then left the Detroit tower frequency. No record of any further communication with any FAA communication facility or air traffic control facility could be found that related to the Beechcraft, nor was such communication required. The operator of Springfield Aviation Inc., at the Springfield Airport, testified that at approximately 1154 hours the pilot of the Beechcraft established radio contact with his office and requested a courtesy car. During this conversation the pilot stated that he would be landing shortly. There was no record of any subsequent radio contact with the aircraft. The aircraft collided at 1153:50 hours, in bright daylight, approximately 25 NM northeast of the Dayton Municipal Airport at an altitude of about 4 525 ft AMSL, and both aircraft crashed. The wreckage of the DC-9 was found in a wooded area. All 26 occupants in both aircraft were killed.
Probable cause:
The Board determined that the probable cause of this accident was the failure of the DC-9 crew to see and avoid the Beechcraft. Contributing to this cause were physiological and environmental conditions and the excessive speed of the DC-9 which reduced visual detection capabilities under an air traffic control system which was not designed or equipped to separate a mixture of controlled and uncontrolled traffic.
Final Report:

Crash of a Convair CV-580 near Marseilles: 38 killed

Date & Time: Mar 5, 1967 at 2007 LT
Type of aircraft:
Operator:
Registration:
N73130
Flight Phase:
Survivors:
No
Schedule:
Chicago – Lafayette – Cincinnati – Columbus – Toledo – Detroit
MSN:
23
YOM:
1952
Flight number:
LK527
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
38
Captain / Total flying hours:
22425
Captain / Total hours on type:
403.00
Copilot / Total flying hours:
4166
Copilot / Total hours on type:
250
Aircraft flight hours:
16216
Circumstances:
While descending to Toledo Airport and flying at an altitude of 7,000 feet, all four propeller blades on the right engine detached simultaneously. The blade number two penetrated the fuselage, causing a sudden cabin decompression. The pilot lost control of the airplane that entered a dive and eventually crashed in an open field located two miles southeast of Marseilles, Ohio. The aircraft was totally destroyed and none of the 38 occupants survived the crash.
Probable cause:
Failure of the right propeller due to the omission of the torque piston nitriding process during manufacture, and the failure of manufacturing quality control to detect the omission.
The following findings were reported:
- Loads on the torque cylinder caused by the failed torque piston of the n° 3 blade of the right propeller exceeded the finite fatigue of the cylinder and it failed in fatigue,
- The loss of oil pressure in the right propeller due to the failed torque cylinder caused the propeller pitch to decrease at a rate which exceeded the propeller pitch lock capability,
- The right propeller oversped, causing the blades to separate in overstress,
- The n°2 propeller blade of the right propeller penetrated the fuselage, destroying the structural integrity to the extent that together with the force of a right yaw attending the propeller separation, the fuselage failed along the line of the propeller penetrations,
- The torque piston n°3 blade had not been nitrided to surface hardening of the helical splines during the manufacture,
- The omission of the nitriding process was not detected by inspection,
- The omission of the nitriding process was associated with the movement of 10 torque pistons from the normal production flow to the Allison laboratory and return to the production process,
- The Allison quality control system lacked the accountability necessary to assure the requisite quality of the individual parts,
- The metal contamination oil check to isolate defective torque piston did not serve the intended purpose,
- Allison underestimated the seriousness of the defective torque piston problem.
Final Report:

Crash of an Armstrong Whitworth AW.650 Argosy 101 in Piqua

Date & Time: Oct 14, 1965 at 1743 LT
Operator:
Registration:
N601Z
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Madison - Wright-Patterson
MSN:
6659
YOM:
1960
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5616
Captain / Total hours on type:
146.00
Circumstances:
The crew departed Madison-Truax Field at 1610LT on a cargo flight to Wright-Patterson AFB on behalf of the US Air Force. While descending to the airbase, north of Dayton, all four engines stopped simultaneously. The crew attempted an immediate emergency landing in a field. The aircraft slid on the ground and eventually collided with a bridge pile and several vehicles before coming to rest. All three crew members were slightly injured while no one on the ground was hurt. The aircraft was damaged beyond repair.
Probable cause:
Engine failure caused by a fuel exhaustion. Inadequate preflight preparation and miscalculated fuel consumption on part of the flying crew.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Bellefontaine: 2 killed

Date & Time: Apr 9, 1965 at 0030 LT
Type of aircraft:
Operator:
Registration:
N84R
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
AF-767
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
14096
Captain / Total hours on type:
85.00
Circumstances:
En route on a cargo flight to Chicago-Midway Airport by night, the pilot encountered poor weather conditions with fog, low clouds and rain showers. The VOR receiver failed en route and the pilot decided to reduce his altitude, probably to maintain a visual contact with the ground when the airplane struck a hill and crashed. Both occupants were killed.
Probable cause:
It was determined that the pilot attempted the flight with known deficiencies in equipment as the transmitter/receiver was inoperative prior to takeoff. The second system failed in flight while in poor weather conditions.
Final Report:

Crash of a Beechcraft H18S in Cincinnati

Date & Time: Aug 9, 1964 at 2020 LT
Type of aircraft:
Registration:
N517DC
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
BA-627
YOM:
1962
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4016
Captain / Total hours on type:
600.00
Circumstances:
Shortly after takeoff from Cincinnati-Lunken Field Airport, while in initial climb, the pilot informed ATC about the failure of the left engine. He elected to make an emergency landing in a field when control was lost. The airplane crashed in a field located near the runway end. All four occupants were injured and the aircraft was destroyed.
Probable cause:
Failure of malfunction of the left engine during initial climb and stall due to the failure of the ignition system (spark plug). The loss of control was caused by improper emergency procedures and single engine flight procedures.
Final Report:

Crash of a Beechcraft E18S in Wooster: 1 killed

Date & Time: Jun 3, 1964 at 1450 LT
Type of aircraft:
Operator:
Registration:
N9921
Flight Type:
Survivors:
No
MSN:
BA-2
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2403
Captain / Total hours on type:
320.00
Circumstances:
On final approach to Wooster-Wayne County Airport, the twin engine aircraft was too low, struck power cables and crashed in flames. The aircraft was destroyed and the pilot was killed.
Probable cause:
The pilot misjudged the distance and altitude during the final approach, causing the airplane to struck power cables and to crash.
Final Report:

Crash of a Kaiser-Frazer C-119G Flying Boxcar near Wilmington: 7 killed

Date & Time: Apr 18, 1964 at 2053 LT
Operator:
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wilmington - Wilmington
Location:
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
While completing a local training mission, the Kaiser-Frazer C-119G Flying Boxcar collided with a second USAF C-119 and crashed 10 miles east of Wilmington Airport. Seven occupants were killed while two others survived. All 10 occupants on board the other aircraft were killed. The exact circumstances of the collision remains unclear as well as both aircraft's registration.

Crash of a Kaiser-Frazer C-119G Flying Boxcar near Wilmington: 10 killed

Date & Time: Apr 18, 1964 at 2053 LT
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wilmington - Wilmington
Location:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
While completing a local training mission, the Kaiser-Frazer C-119G Flying Boxcar collided with a second USAF C-119 and crashed 10 miles east of Wilmington Airport. All ten occupants were killed and seven of the nine occupants on the second aircraft were killed as well. Two survived. The exact circumstances of the collision remains unclear as well as both aircraft's registration.

Crash of a Lockheed 18-56-24 LodeStar in Lake Milton: 13 killed

Date & Time: Sep 4, 1962 at 2100 LT
Type of aircraft:
Operator:
Registration:
N1000F
Flight Phase:
Survivors:
No
Schedule:
Buffalo – Ashland
MSN:
2463
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
13
Captain / Total flying hours:
13250
Copilot / Total flying hours:
1000
Aircraft flight hours:
6557
Circumstances:
After takeoff from Buffalo Airport, the crew was cleared to climb to 8,000 feet. About an hour into the flight, the airplane went out of control, entered a dive and crashed near Lake Milton, Ohio. The crew was unable to send any distress call. The aircraft disintegrated on impact and all 13 occupants were killed.
Probable cause:
The Board determines that the probable cause of this accident was a malfunction of the electric elevator trim tab unit which resulted in aircraft uncontrollability and subsequent structural failure of the wing.
Final Report:

Crash of a Curtiss C-46F-1-CU Commando in Toledo: 22 killed

Date & Time: Oct 29, 1960 at 2202 LT
Type of aircraft:
Registration:
N1244N
Flight Phase:
Survivors:
Yes
Schedule:
Toledo – Kansas City – Albuquerque – Santa Maria – Oakland
MSN:
22458
YOM:
1945
Crew on board:
3
Crew fatalities:
Pax on board:
45
Pax fatalities:
Other fatalities:
Total fatalities:
22
Captain / Total flying hours:
6364
Copilot / Total flying hours:
3200
Copilot / Total hours on type:
1300
Circumstances:
The aircraft was chartered to transport the California State Polytechnic College football team from Santa Maria, California to Toledo, Ohio and return. The aircraft took off from Toledo Express Airport on the return flight to San Luis Obispo, California, weighing approximately 2,000 lb more than its maximum certificated gross weight of 47,100 lb. During initial climb, the airplane stalled and crashed in flames a field 1,1 mile past the runway end. Both pilots and 20 passengers, among them 16 members of the football team, were killed while 26 other occupants were injured. The aircraft was destroyed.
Probable cause:
The accident was due to loss of control during a premature lift-off. Contributing factors were the overweight aircraft, weather conditions, and partial loss of power in the left engine.
Final Report: