Crash of a Lockheed 18-56-24 LodeStar in Aguila: 2 killed

Date & Time: Apr 11, 1967 at 1930 LT
Type of aircraft:
Operator:
Registration:
N699C
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
2354
YOM:
1943
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While cruising in poor weather conditions, the twin engine aircraft struck a hilly terrain and crashed in the region of Aguila, Arizona. The wreckage was found two days later and both crew members were killed. At the time of the accident, the visibility was reduced due to low clouds, strong winds, heavy rain falls and thunderstorm activity. The airplane was owned by Edwin L. Byrd.
Probable cause:
The crew continued under VFR mode in adverse weather conditions. Inadequate preflight preparation.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Lexington: 9 killed

Date & Time: Apr 3, 1967 at 1633 LT
Type of aircraft:
Registration:
N3727G
Flight Phase:
Survivors:
No
MSN:
AF-214
YOM:
1952
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
16144
Circumstances:
Shortly after takeoff from Lexington-Blue Grass Airport, while in initial climb, the left engine caught fire. The pilot elected to return for an emergency landing and made a turn when control was lost. The airplane dove into the ground and crashed in a huge explosion in a field. All nine occupants were killed, among them several doctors and scientists.
Crew:
Robert Yonk, pilot.
Passengers:
Dr. Richard Schweet,
Dr. R. C. Simonini,
Dr. Jerome Cohn,
Dr. S. O. Navarro,
G. Reynolds Watkins,
Richard H. Southwood Jr.,
Dr. Arnold Salop,
Max Horn.
Probable cause:
Uncontrolled descent following a fire of undetermined origin that occurred in area of left engine nacelle during climb-out. At the time of the accident, the airplane was improperly loaded, which was considered as a contributing factor.
Final Report:

Crash of a Douglas DC-8-51 in New Orleans: 19 killed

Date & Time: Mar 30, 1967 at 0050 LT
Type of aircraft:
Operator:
Registration:
N802E
Flight Type:
Survivors:
No
Site:
Schedule:
New Orleans - New Orleans
MSN:
45409/19
YOM:
1959
Flight number:
DL9877
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
19008
Captain / Total hours on type:
475.00
Copilot / Total flying hours:
16929
Copilot / Total hours on type:
15
Aircraft flight hours:
23391
Circumstances:
Delta Air Lines DC-8-51 N802E was scheduled as Flight 9877, to provide crew training for a captain-trainee and a flight engineer-trainee. In addition the flight engineer-instructor was being given a routine proficiency check. At 23:14 a weather briefing was given to the instructor pilot, indicating, "... the only significant weather was a restriction in visibility which was expected to reduce to about two miles in fog and smoke near 0600...". The flight departed the ramp at 00:40 with the captain-trainee in the left seat and the check captain in the right seat. At 00:43 the crew advised the tower they were ready for takeoff and would "...like to circle and land on one (runway 1)." The tower controller then cleared them as requested. The aircraft was observed to make what appeared to be a normal takeoff and departure. At 00:47 the crew reported on base leg for runway 01, and the controller cleared the flight to land. A subsequent discussion revealed that they would execute a simulated two-engine out approach, execute a full stop landing and then takeoff on runway 19. The tower controller observed Flight 9877 in a shallow left turn on what appeared to be a normal final approach. The degree of bank increased to approximately 60° or greater when the aircraft hit the power lines approximately 2,300 feet short and 1,100 feet west of the runway threshold. The DC-8 crashed into a residential area, destroying several homes and the Hilton complex. All six crew members were killed as well as 13 people on the ground, clients and employees at Hilton Hotel. 18 other people were injured, some of them seriously. The aircraft was totally destroyed by impact forces and a post crash fire.
Probable cause:
Improper supervision by the instructor, and the improper use of flight and power controls by both instructor and the Captain-trainee during a simulated two-engine out landing approach, which resulted in a loss of control.
Final Report:

Crash of a Douglas C-47A-70-DL near Castle AFB

Date & Time: Mar 24, 1967 at 1500 LT
Registration:
N54370
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
19220
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5435
Captain / Total hours on type:
700.00
Circumstances:
While on a cargo flight, the crew informed ATC about a fire in the cabin and elected to divert to Castle AFB for an emergency landing. During the descent, the fire spread to the cargo compartment and the captain eventually decided to make an emergency landing in an open field. The airplane belly landed few miles from the airbase and came to rest in flames. While both crew members escaped uninjured, the aircraft was destroyed by fire.
Probable cause:
Fuel leaking from the APU ignited in flight and set fire to the cargo stacked around the APU. Inadequate maintenance and inspection on part of the Company.
Final Report:

Crash of a Beechcraft D18S in Kodiak: 2 killed

Date & Time: Mar 16, 1967 at 0751 LT
Type of aircraft:
Registration:
N80194
Flight Phase:
Survivors:
No
MSN:
AF-175
YOM:
1946
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
8726
Captain / Total hours on type:
38.00
Circumstances:
At liftoff from Kodiak Airport, the twin engine airplane struck a gravel pile, stalled and crashed, killing both occupants. At the time of the accident, the visibility was reduced due to foggy conditions.
Probable cause:
The pilot failed to obtain a sufficient flying speed for takeoff and the first portion of takeoff run was in fog at south end of runway.
Final Report:

Crash of a Fairchild F27A in Klamath Falls: 4 killed

Date & Time: Mar 10, 1967 at 0503 LT
Type of aircraft:
Operator:
Registration:
N2712
Flight Phase:
Survivors:
No
Schedule:
Klamath Falls – Medford – North Bend – Portland – Seattle
MSN:
73
YOM:
1960
Flight number:
WC720
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
9271
Captain / Total hours on type:
4684.00
Copilot / Total flying hours:
1064
Copilot / Total hours on type:
258
Aircraft flight hours:
16202
Circumstances:
Fairchild F-27 N2712 operated on a flight from Klamath Falls to Seattle via Medford, North Bend and Portland. Because snow was falling at Klamath Falls, the aircraft was loaded in the hangar instead of on the ramp. There was some delay in pushing out the aircraft onto the ramp because the tow tractor lost traction in the snow. The aircraft was exposed to the falling snow for about 11 minutes before the plane was able to taxy out to runway 14. A few minutes later, at 05:01 the aircraft took off. During the takeoff roll, after rolling about 1000 feet, the aircraft gradually served to the left. The nose wheel left the ground 600 feet prior to the main gear at a point where the track was half way between the center of the runway and the left row of runway lights. The left main gear was about 12 feet off the left edge of the runway for a distance of 250 feet prior to lift-off. Just after lift-off the aircraft swerved sharply to the right and immediately back to the left. On climb out the aircraft tended to the left, despite several course corrections. After reaching 5250 feet, the altitude dropped again to 4700 feet. The aircraft continued to climb until it crashed on a steep ridge on the northwest slope of Stukel Mountain at an elevation of 5049 feet (1539 m). The F-27 was in a right wing low attitude when this wing contacted the mountain; the aircraft then cartwheeled up the 30° up slope of the mountain. The aircraft was destroyed and all four occupants were killed.
Probable cause:
Loss of control due to ice accretion on airframe surfaces. The Board further determines that the pilot should have required that deicing fluid be applied to the aircraft to remove the accumulation of ice and snow prior to takeoff. This had not been done by the appropriate maintenance personnel.
Final Report:

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 a Beechcraft C-45H Expeditor in Middletown: 2 killed

Date & Time: Feb 28, 1967 at 1605 LT
Type of aircraft:
Operator:
Registration:
N830K
Flight Phase:
Flight Type:
Survivors:
No
MSN:
AF-730
YOM:
1954
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5527
Captain / Total hours on type:
86.00
Circumstances:
Shortly after takeoff from Middletown-Summit Airpark, while in initial climb, the twin engine aircraft banked left and crashed in a huge explosion. Both occupants were killed and the aircraft was destroyed.
Probable cause:
Lower cap of left wing failed approximately 8 inches outboard of the outer panel attach point, causing the left wing to detach. Fatigue fracture.
Final Report:

Crash of a Douglas DC-6 in New York

Date & Time: Feb 24, 1967 at 0225 LT
Type of aircraft:
Operator:
Registration:
N8224H
Flight Phase:
Survivors:
Yes
Schedule:
Philadelphia - Boston
MSN:
43741/290
YOM:
1952
Crew on board:
5
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6232
Captain / Total hours on type:
3348.00
Circumstances:
While cruising at an altitude of 15,500 feet over Holmdel, New Jersey, the aircraft suffered an explosive decompression of the cabin. A 60 by 125 inches 'panel' detached from the fuselage and struck the engine number three, causing the detachment of its propeller. The crew started an emergency descent and was able to complete an emergency landing at New York Airport. All 14 occupants were evacuated safely while the aircraft was later declared as damaged beyond repair.
Probable cause:
Fatigue fracture of the fuselage and explosive decompression caused by an inadequate maintenance and inspection on part of the ground maintenance personnel. Investigations reported that at the time of the decompression, the cabin was pressurized for 2,500 feet while the aircraft was flying at an altitude of 15,500 feet.
Final Report: