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Crash of a Convair CV-880-22-2 in Atlanta: 4 killed

Date & Time: May 23, 1960 at 1152 LT
Type of aircraft:
Operator:
Registration:
N8804E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Atlanta - Atlanta
MSN:
22-00-16
YOM:
1960
Flight number:
DL1903
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
13197
Captain / Total hours on type:
179.00
Copilot / Total flying hours:
17221
Copilot / Total hours on type:
10
Circumstances:
The flight was scheduled for training for two pilots who were to “check out” in the CV-880. A pilot-trainee occupied the left seat and a qualified instructor-pilot occupied the right. Immediately after liftoff the aircraft assumed an extremely nose-high attitude and banked steeply to the left. It then rolled to a vertical right bank, the nose fell through, and the aircraft struck the ground and burned. Four crew members, the only occupants, received fatal injuries.
Probable cause:
The Board determines the probable cause of this accident to be the stalling of the aircraft, for reasons undetermined, at an altitude too low to effect recovery.
Final Report:

Crash of a Douglas C-47A-25-DK in Atlanta

Date & Time: Jun 15, 1954 at 1745 LT
Operator:
Registration:
N51359
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Atlanta – Chattanooga – Knoxville – Cincinnati – Chicago
MSN:
13759
YOM:
1944
Flight number:
DL134X
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6014
Captain / Total hours on type:
4575.00
Copilot / Total flying hours:
6803
Copilot / Total hours on type:
6800
Aircraft flight hours:
18827
Circumstances:
As the aircraft became airborne the landing gear was retracted. Light rain was encountered at this time. When the air-craft had climbed to 200 to 250 feet, power was reduced to 35 inches of manifold pressure and a shallow right turn was begun. Before a reduction in r.p.m. was made the aircraft began to settle and the airspeed was observed to decrease rapidly from above 105 to 80 knots. The nose was immediately lowered to level flight, & the turn stopped, and full power applied. When this was done, the air-speed returned to about 100 knots and the settling appeared to lessen considerably. The increased airspeed with the attendant better flying characteristics was monetary, however, as the airspeed abruptly dropped to 60 knots and the airplane again began to settle. As the aircraft continued to settle and it became obvious that it was going to strike the ground, the first officer attempted to raise tile nose. Upon feeling the aircraft strike the ground, both throttles were closed. The aircraft then skidded to a stop in a wooded area approximately 600 feet north-west of the far end of runway 21. The airplane was destroyed and both pilots were injured.
Probable cause:
The Board determines that the probable cause of this accident was a rapid loss of airspeed immediately following takeoff caused by unexpected, strong gusts or divergent winds accompanying a local rain shower. The following findings were reported:
- At the time of takeoff a large thunderstorm was 8 to 10 miles south of the airport and a local rain shower was approaching the southeast end of runway,
- The aircraft took off from runway 21 and climbed to approximately 200 to 250 feet,
- A portion of the rain shower was encountered which contained strong gusts,
- While in the rain shower the aircraft lost airspeed and settled to the ground.
Final Report:

Crash of a Douglas DC-3DST-318 near Marshall: 19 killed

Date & Time: May 17, 1953 at 1415 LT
Type of aircraft:
Operator:
Registration:
N28345
Flight Phase:
Survivors:
Yes
Schedule:
Dallas – Shreveport – Atlanta
MSN:
2224
YOM:
1940
Flight number:
DL318
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
7120
Captain / Total hours on type:
7120.00
Copilot / Total flying hours:
2114
Copilot / Total hours on type:
803
Aircraft flight hours:
39000
Circumstances:
Flight 318 departed Dallas, Texas, on a VFR Flight Plan at 1310, on time, for Atlanta, Georgia, with a scheduled stop at Shreveport, Louisiana. The crew consisted of Captain Douglas B. yolk, First Officer James P. Stewart and Stewardess Joanne Carlson; there were 17 passengers including one infant. The aircraft’s gross weight on departure from Dallas was 24,099 pounds, which was within the allowable weight of 25,200 pounds, and the center of gravity was within the prescribed limits. Flight 318 proceeded normally and at 1352 reported to the company station at Longview, Texas, that it was then west of Gladewater, Texas. Longview gave the flight the latest Shreveport weather which was dark scattered clouds at 1,000 feet, ceiling estimated 4,000 feet broken clouds, overcast at 20,000 feet, visibility 10 miles, thunderstorms, light rain showers, wind south 10. Remarks were thunderstorms south, occasional lightning cloud to cloud south. The flight was also advised by the company’s Longview operator that he had been watching thunderstorms east and southeast of the Longview field and suggested that the flight stay well to the north. Flight 318 answered “OK.” At 1408, in the vicinity of Marshall, Texas, the flight made a routine radio contact with Delta’s Shreveport station, during which it was given the Shreveport altimeter setting of 29.78. At this time the flight advised it was changing over to the Shreveport Control Tower frequency. At about 1412, four minutes later, Flight 318 called the Shreveport Control Tower, which cleared it to make a right-hard turn for landing approach to Runway 13 and gave the wind as southeast 10 miles per hour, Flight 318 acknowledged this message and requested the Shreveport weather which was transmitted as dark scattered clouds at 1,000 feet, ceiling estimated 4,000 feet, overcast at 20,000 feet, visibility 10 miles, thunderstorm, light rain shower. The tower also advised of a thunderstorm approximately 15 miles west of Shreveport. This transmission also was acknowledged by the flight. At 1416 the Shreveport Control Tower asked Flight 318 to give a position report. No reply was received, and a number of unsuccessful attempts were then made to contact the flight. At 1428 the tower was advised that an aircraft had crashed near Marshall, Texas. A passenger was seriously injured while 19 other occupants were killed. The aircraft was destroyed.
Probable cause:
The Board determines that the probable cause of this accident was:
- the encountering of conditions in a severe thunderstorm that resulted in loss of effective control of the aircraft, and
- the failure of the captain to adhere to company directives requiring the avoidance of thunderstorms when conditions would allow such action.
The following findings were pointed out:
- The carrier had prepared adequate written instructions against the unnecessary traversing of thunderstorms,
- The captain should have had knowledge of these company instructions,
- While en route, close to and approaching the storm, it was suggested to the captain by company ground personnel that he stay well to the north to avoid the thunderstorm,
- The captain flew directly into the storm without changing course or altitude,
- The captain while on an airway proceeded from VFR into IFR weather without first obtaining an appropriate IFR clearance,
- A very intense localized thunderstorm, accompanied by frequent cloud-to-ground lightning, hail, heavy rain, turbulence, and high winds, was entered by the flight,
- The flight met extraordinary conditions within the storm and was forced to the ground,
- The carrier’s dispatching, pilot briefing and weather dissemination, were satisfactory.
Final Report:

Crash of a Douglas DC-4 in Chicago: 12 killed

Date & Time: Mar 10, 1948 at 2258 LT
Type of aircraft:
Operator:
Registration:
N37478
Flight Phase:
Survivors:
Yes
Schedule:
Chicago – Miami
MSN:
18390
YOM:
1944
Flight number:
DL705
Crew on board:
4
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
9830
Captain / Total hours on type:
1611.00
Copilot / Total flying hours:
2976
Copilot / Total hours on type:
1366
Aircraft flight hours:
6509
Circumstances:
The takeoff roll and the first part of the climb appeared to be normal until the aircraft and progressed three-quarters of the way down the runway, at which time it had reached an altitude between 150 and 200 feet. Then, while still within the airport boundaries, it assumed a very steep, near vertical, climbing attitude. Airport, tower, and flight personal observing from the ground believed the flight to be in difficulty, and though no distress signal was received from the airplane, the tower promptly telephoned the crash and fire facilities on the field. At an altitude between 500 and 800 feet the airplane appeared to stall, and the nose and right wing dropped. A partial recovery from the stall was made before the aircraft crashed to the ground and burst into flames. A passenger was seriously injured while 12 other occupants were killed.
Probable cause:
The Board determines that the probable cause of this accident was the loss of longitudinal control of the airplane. The cause for the loss of control remains undetermined.
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 Douglas DC-3-454 in Meridian

Date & Time: Nov 10, 1946 at 1717 LT
Type of aircraft:
Operator:
Registration:
NC20750
Survivors:
Yes
Schedule:
Fort Worth – Dallas – Shreveport – Monroe – Jackson – Meridian – Birmingham – Atlanta
MSN:
4993
YOM:
1942
Flight number:
DL010
Crew on board:
3
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3725
Captain / Total hours on type:
3100.00
Copilot / Total flying hours:
3207
Copilot / Total hours on type:
301
Aircraft flight hours:
8819
Circumstances:
The aircraft left Jackson at 1630LT bound for Meridian and the crew obtained the permission to continue at an altitude of 3,000 feet in IFR mode. The approach to Meridian was started in the following weather conditions: ceiling 800 feet, overcast, visibility 3 miles, thunder storm, light rain showers, surface wind northeast 10, thunder storms overhead moving east-northeast, frequent vivid lightning all quadrants. The aircraft was seen to make contact with the runway within the first 1,000 feet, however. it continued rolling down the entire length of the runway with little apparent deceleration. Its forward motion continued beyond the end of the runway and up the western slope of a ditch adjoining the highway adjacent to the airport. on striking this ditch, the aircraft left the ground and bounced over the highway, coming to rest with its nose extended partially over a railroad right-of-way. All 22 occupants escaped unhurt while the aircraft was damaged beyond repair.
Probable cause:
The Board determines that the probable cause of this accident was the poor judgement of the pilot in landing on a wet runway under conditions of varying winds without ascertaining visually the direction of the wind. A contributory factor was the error of the company radio communicator in transmitting the wind direction.
Final Report:

Crash of a Stinson Model A in Atlanta

Date & Time: Aug 27, 1936
Type of aircraft:
Operator:
Registration:
NC15134
Survivors:
Yes
MSN:
9111
YOM:
1935
Location:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Suffered an accident at Atlanta Airport. There were no casualties.

Crash of a Lockheed 8C Sirius in Birmingham

Date & Time: Dec 24, 1935 at 0515 LT
Type of aircraft:
Operator:
Registration:
NC167W
Flight Type:
Survivors:
Yes
Schedule:
Jackson – Birmingham
MSN:
167
YOM:
1930
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, departed Jackson, Mississippi, on a cargo flight to Birmingham. On final approach at night, the engine failed. The airplane lost height, impacted trees and crashed short of runway. The pilot R. B. Reinhart was slightly injured and the airplane was damaged beyond repair. The cargo of Christmas mail was salvaged without damage.
Probable cause:
Engine failure on final approach.

Crash of a Stinson Model A in Gilmer: 4 killed

Date & Time: Aug 14, 1935 at 2345 LT
Type of aircraft:
Operator:
Registration:
NC14599
Flight Phase:
Survivors:
No
Schedule:
Dallas – Shreveport – Jackson – Birmingham – Atlanta
MSN:
9103
YOM:
1935
Flight number:
DL004
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
While cruising south of Gilmer, a propeller blade detached from the left engine. The crew reduced his altitude to attempt an emergency landing. On approach at night, the left engine torn off. The airplane went out of control and crashed in a desert area. All four occupants were killed.
Probable cause:
Investigation disclosed that the left outboard engine had been tern from the plane as the result of an unbalanced condition caused by the breaking of a propeller blade. The engine was found at a spot about one mile southwest of the wreckage and a portion of the propeller blade was found about 300 yards west of the engine. From the appearance of the wreckage and facts available, it is believed that the pilot, while attempting to complete an emergency landing, lost control of the plane due to the absence of the weight of the left outboard engine and the resulting disturbed airflow over the wing.