Crash of a Rockwell 1121 Jet Commander in Lexington: 2 killed

Date & Time: Nov 14, 1970 at 1917 LT
Operator:
Registration:
N100RC
Flight Type:
Survivors:
No
Schedule:
Columbus – Lexington
MSN:
1121-060
YOM:
1966
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5859
Captain / Total hours on type:
2070.00
Circumstances:
On final approach to Lexington-Blue Grass Airport by night, the crew encountered poor weather conditions. In rain falls, the airplane was observed in a steep right bank descending then rolled to opposite direction before impact. The airplane was destroyed and both pilots were killed.
Probable cause:
Loss of control after the pilot-in-command suffered a spatial disorientation during a night approach in marginal weather conditions. The following factors were reported:
- Low ceiling and rain.
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 a Lockheed L-1049 Super Constellation in New York: 44 killed

Date & Time: Dec 16, 1960 at 1033 LT
Operator:
Registration:
N6907C
Survivors:
No
Site:
Schedule:
Dayton – Columbus – New York
MSN:
4021
YOM:
1952
Flight number:
TW266
Crew on board:
6
Crew fatalities:
Pax on board:
38
Pax fatalities:
Other fatalities:
Total fatalities:
44
Captain / Total flying hours:
14583
Captain / Total hours on type:
267.00
Copilot / Total flying hours:
6411
Copilot / Total hours on type:
268
Aircraft flight hours:
21555
Circumstances:
On December 16, 1960, at 1033 e.s.t., a collision between Trans World Airlines Model 1049A Constellation, N6907C, and a United Air Lines DC-8, N8013U, occurred near Miller Army Air Field, Staten Island, New York. Trans World Airlines Flight 266 originated at Dayton, Ohio. The destination was LaGuardia Airport, New York, with one en route stop at Columbus, Ohio United Air Lines Flight 826 was a non-stop service originating at O'Hare Airport, Chicago, Illinois, with its destination New York International Airport, New York. Both aircraft were operating under Instrument Flight Rules. Following the collision the Constellation fell on Miller Army Field, and the DC-8 continued in a northeasterly direction, crashing into Sterling place near Seventh Avenue in Brooklyn, New York. Both aircraft were totally destroyed. All 128 occupants of both aircraft and 6 persons on the ground in Brooklyn were fatally injured. There was considerable damage to property in the area of the ground impact of the DC-8. TWA Flight 266 departed Port Columbus Airport at 0900, operating routinely under Air Traffic Control into the New York area The New York Air Route Traffic Control Center (ARTCC) subsequently advised that radar contact had been established and cleared the flight to the Linden. Intersection, Control of the flight was subsequently transferred to LaGuardia Approach Control. When the flight was about over the Linden Intersection, LaGuardia Approach Control began vectoring TWA 266 by radar to the final approach course for a landing on runway 4 at LaGuardia. Shortly thereafter TWA 266 was cleared to descend to 5,000 feet, and was twice advised of traffic in the vicinity on a northeasterly heading. Following the transmission of this information the radar targets appeared to merge on the LaGuardia Approach Control radar scope, and communications with TWA 266 were lost. United Air Lines Flight 826 operated routinely between Chicago and the New York area, contacting the New York ARTCC at 1012 Shortly thereafter the New York Center cleared UAL 826 to proceed from the Allentown, Pa., very high frequency omni directional radio range station (VOR) direct to the Robbinsville, New Jersey, VOR, and thence to the Preston Intersection via Victor Airway 123. At approximately 1021, UAL 826 contacted Aeronautical Radio, Inc. (ARINC) to advise their company that the No. 2 receiver accessory unit was inoperative, which would indicate that one of the aircraft's two VHF radio navigational receivers was not functioning. A "fix" is established by the intersection of two radials from two separate radio range stations. With one unit inoperative the cross-bearings necessary can be taken by tuning the remaining receiver from one station to the other. This process consumes considerable time, however, and is not as accurate as the simultaneous display of information on two separate position deviation indicators While UAL 826 advised the company that one unit was inoperative, Air Traffic Control was not advised. At 1025 the New York ARTCC issued a clearance for a new routing which shortened the distance to Preston by approximately 11 miles. As a result, this reduced the amount of time available to the crew to retune the single radio receiver to either the Colt' s Neck, New Jersey, or Solberg, New Jersey, VOR in order to establish the cross-bearing with Victor 123, which would identify the Preston Intersection. In the event the crew would not attempt to retune the single VOR receiver, crossbearings on the Scotland Low Frequency Radiobeacon could be taken with the aircraft direction finding (ADF) equipment. This would be a means of identifying the Preston Intersection but, under the circumstances, would require rapid mental calculation in the interpretation of a display which could be easily misread. Several factors support the conclusion that this occurred. Instructions had been issued to UAL 826 for holding at the Preston Intersection the clearance limit, should holding be necessary. Clearance beyond Preston for an approach to Idlewild Airport would be received from Idlewild Approach Control and the transfer of control of the flight from the New York Center to Idlewild Approach Control would normally take place as the aircraft was approaching Preston. UAL 826 was not receiving radar vectors, but was providing its own navigation. After the flight reported passing through 6,000 feet the New York Center advised that radar service was terminated and instructed the flight to contact Idlewild Approach Control. UAL 826 then called Idlewild Approach Control, stating "United 826 approaching Preston at 5,000." This was the last known transmission from UAL 826. At the time UAL 826 advised it was approaching Preston it had in fact gone on by this clearance limit several seconds before and was several miles past the point at which it should have turned into the holding pattern. This is confirmed by the data obtained from the flight recorder which had been installed in the UAL DC-8, as well as by analysis of the communication tapes At a point approximately 11 miles past the Preston Intersection a collision occurred between TWA 266 and UAL 826. Weather at the altitude of the collision and at the time of the accident was such as to preclude flight by visual means.
Probable cause:
The Board determines that the probable cause of this accident was that United Flight 826 proceeded beyond its clearance limit and the confines of the airspace allocated to the flight by Air Traffic Control A contributing factor was the high rate of speed of the United DC-8 as it approached the Preston intersection, coupled with the change of clearance which reduced the enroute distance along VICTOR 123 by approximately 11 miles.
Final Report:

Crash of a Douglas C-47A-10-DK near Barnesville: 1 killed

Date & Time: May 8, 1955
Operator:
Registration:
44-108869
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Baltimore – Columbus
MSN:
12538
YOM:
1944
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The aircraft was completing a flight from Baltimore to Columbus on behalf of the Ohio National Guard. Enroute, an engine failed and all ten passengers bailed out. The crew elected to make an emergency landing when the aircraft struck trees and crashed in a dense wooded area located about 15 miles east-southeast of Barnesville. A passenger whose parachute failed to open was killed.
Probable cause:
Engine failure in flight.

Crash of a Douglas C-47A-10-DK in Columbus: 1 killed

Date & Time: Feb 25, 1948 at 0600 LT
Registration:
NC36498
Flight Type:
Survivors:
Yes
Schedule:
Pittsburgh – Columbus
MSN:
12527
YOM:
1944
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2150
Copilot / Total flying hours:
2400
Copilot / Total hours on type:
500
Aircraft flight hours:
3300
Circumstances:
Captain De Cicco took over the controls of the aircraft shortly after the flight had passed the Newark fan marker, and started an instrument approach to the Port Columbus Airport. Altitude was reduced to 1,600 feet which was the minimum for that part of the instrument approach to Columbus. However, Captain De Cicco continued his descent below 1,600 feet despite the objections of Mr. Cole. Mr. Cole stated that he immediately engaged himself in a search of the cockpit for an instrument approach chart for Columbus, presumably to show Captain De Cicco that an altitude of 1,600 feet was required until over the Summit Hill fan marker. The descent was continued, and just as the aircraft emerged below the overcast Mr. Cole looked up to see the trees into which the aircraft flew. The first tree struck extended approximately 90 feet above the terrain, the elevation of which was 1,055 feet. The aircraft continued in a straight line, striking a second tree 60 feet away from the first. At this point the right horizontal stabilizer tip and the right elevator were sheared from the empennage A third tree was struck, 265 feet from the first point of contact, and miscellaneous fuselage parts and the right wing were torn from the aircraft. The airplane then made contact with the ground at which time both propellers were broken from the engines. The main body of the wreckage came to rest and burned 1,150 feet from the first point of impact. The pilot was killed, but the co-pilot, although seriously injured has substantially recovered.
Probable cause:
The Board determines that the probable cause of this accident was the continuation of an instrument approach below an altitude sufficient to clear the terrain en route.
The following factors were considered as contributory:
- At the scene of the crash, 6 miles east of Port Columbus Airport, the ground elevation is 1,055 feet, and at the time of the accident the ceiling was reported over the Port Columbus Airport to be 300 feet and visibility one mile,
- The pilot did not follow the standard instrument approach procedure to the Columbus Airport but reduced his altitude below the minimum allowable of 1,600 feet between the Newark and Summit Hill fan markers, located 23 and 5 miles east of Port Columbus Airport respectively; and the aircraft struck the top of trees at an altitude of approximately 1,140 feet.
Final Report:

Crash of a Douglas DC-3C in Columbus: 8 killed

Date & Time: Apr 22, 1947 at 1040 LT
Type of aircraft:
Operator:
Registration:
NC49657
Survivors:
No
Schedule:
Macon – Columbus
MSN:
9066
YOM:
1943
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
11091
Captain / Total hours on type:
1800.00
Aircraft flight hours:
2899
Circumstances:
On final approach to runway 05, while at a height of 10 feet, the DC-3 was hit by a private Vultee BT-13 registered NC55312 and carrying one pilot. Following the collision, both aircraft climbed to a height of 150 feet and then stalled and crashed in a huge explosion. Both aircraft were destroyed and all nine occupants were killed.
Probable cause:
The Board determines that the probable cause of this accident was the failure of the pilot in the BT-13 to fly a standard left hand pattern in his approach to the airport and to Keep a diligent lookout for other traffic.
Final Report:

Crash of a Keystone XLB-5 in Reynoldsburg: 1 killed

Date & Time: May 28, 1927
Type of aircraft:
Operator:
Registration:
26-208
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Columbus - Columbus
MSN:
01
YOM:
1927
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The crew was engaged in a local test flight on this first prototype, a Keystone XLB-5. While cruising at a height of 1,200 feet southeast of Columbus Airport, the aircraft experienced a catastrophic failure of its right engine when a blade separated from the hub with explosive power, and tearing the engine apart. Shrapnel sprayed the five-man crew, which included 2nd Bombardment Group commander Major Lewis H. Brereton, flying copilot, and all except the nose gunner immediately parachuted. The nose gunner died in the crash, and the gasoline-soaked wreckage subsequently exploded and burned on the ground.
Probable cause:
Propeller blade failure and separation in flight.