Crash of a Lockheed L-188C Electra near Tell City: 63 killed

Date & Time: Mar 17, 1960 at 1525 LT
Type of aircraft:
Operator:
Registration:
N121US
Flight Phase:
Survivors:
No
Schedule:
Minneapolis – Chicago – Miami
MSN:
1057
YOM:
1959
Flight number:
NW710
Crew on board:
6
Crew fatalities:
Pax on board:
57
Pax fatalities:
Other fatalities:
Total fatalities:
63
Captain / Total flying hours:
27523
Captain / Total hours on type:
254.00
Copilot / Total flying hours:
2974
Copilot / Total hours on type:
200
Aircraft flight hours:
1786
Circumstances:
The four engine aircraft departed Chicago-Midway at 1438LT bound for Miami, carrying 57 passengers and a crew of six. While cruising at an altitude of 18,000 feet over the south of Indiana State, the aircraft entered a dive and crashed in a huge explosion in a snow covered field located east of Tell City. Some debris were also found in a wooded area. The aircraft disintegrated on impact and all 63 occupants were killed. The crew was unable to send any distress call prior to the accident.
Probable cause:
The Board determines that the probable cause of this accident was the separation of the right wing in flight due to flutter induced by oscillations of the outboard nacelles. Contributing factors were a reduced stiffness of the structure and the entry of the aircraft into an area of severe clear air turbulence.
Final Report:

Crash of a Lockheed L-1049G Super Constellation in Chicago

Date & Time: Feb 29, 1960
Operator:
Registration:
N7101C
Flight Phase:
Survivors:
Yes
Schedule:
Chicago – Phoenix
MSN:
4582
YOM:
1955
Crew on board:
6
Crew fatalities:
Pax on board:
54
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the right main gear collapsed. The aircraft swung on runway and came to rest. All 60 occupants were evacuated safely while the aircraft was considered as damaged beyond repair.
Probable cause:
The right main gear collapsed during takeoff.

Crash of a Lockheed L-1049H Super Constellation in Chicago: 11 killed

Date & Time: Nov 24, 1959 at 0535 LT
Operator:
Registration:
N102R
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Chicago – Denver – Los Angeles
MSN:
4824
YOM:
1957
Flight number:
TW595
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
11
Captain / Total flying hours:
12467
Captain / Total hours on type:
1670.00
Copilot / Total flying hours:
6285
Copilot / Total hours on type:
3919
Aircraft flight hours:
3432
Circumstances:
Flight 595, loaded with cargo, took off on runway 31L of Midway at approximately 0531LT bound for Los Angles, California. As the aircraft began a left turn, the crew notified Midway Tower they had received a fire warning on the No. 2 engine and had shut it down. They also informed the tower the flight would return and land. The aircraft proceeded in a continuing left turn around the airport in an elliptical pattern and below the clouds which were based at an altitude of 500 to 600 feet. In the turn to final approach to runway 31 the aircraft banked in excess of 45 degrees during which it developed an excessive rate of sink. When the aircraft reached the tops of the trees its wings were nearly level and its nose was raised in a climbing attitude; however, the descent continued. The wing flaps were being retracted during the last 5 to 10 seconds of the final descent and were found to be symmetrically extended at 24 percent upon impact. The plane crashed into a residential area about one-fourth of a mile southeast of Midway Airport, Chicago, Illinois, killing all persons aboard, demolishing the aircraft, and fatally injuring eight persons on the ground.
Probable cause:
The Board determines the probable cause of this accident to be the maneuvering of the aircraft in a manner that caused it to develop an excessive rate of sink while in the turn to final approach.
Final Report:

Crash of a Martin B-26C Marauder near Marion: 10 killed

Date & Time: Jul 1, 1959 at 1752 LT
Type of aircraft:
Registration:
N1502
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Chicago – Baltimore
MSN:
8904
YOM:
1943
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
10577
Captain / Total hours on type:
805.00
Copilot / Total flying hours:
3766
Copilot / Total hours on type:
1728
Aircraft flight hours:
2967
Circumstances:
The purpose of this flight was to transport the executives from Midway Airport, Chicago, Illinois, to Baltimore, Maryland. Departure from Midway was at 1645LT. When the flight was near Marion, Ohio, and shortly after it had traversed an area of pronounced thunderstorm activity, it dived violently and nearly vertically to the ground. Destruction was of such extent that it could not be determined if a structural failure occurred in flight and consequently the probable cause of this accident could not be established.
Probable cause:
The Board is unable to determine the probable cause of this accident. However, circumstances suggest control difficulty of an undetermined nature during passage through an active developing line of thunderstorms.
Final Report:

Crash of a Convair CV-240-0 in Chicago

Date & Time: Mar 15, 1959 at 0053 LT
Type of aircraft:
Operator:
Registration:
N94273
Flight Type:
Survivors:
Yes
Schedule:
New York – Chicago
MSN:
150
YOM:
1949
Flight number:
AA2815
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8500
Captain / Total hours on type:
2500.00
Copilot / Total flying hours:
1800
Copilot / Total hours on type:
800
Aircraft flight hours:
22720
Circumstances:
The crew was completing a cargo flight from LaGuardia Airport to Midway Airport in Chicago. On final approach to runway 31, the captain considered his position was incorrect and decided to make a go around. Few minutes later, during a second attempt to land, he failed to realized his altitude was insufficient when the airplane struck a 96-foot steel tower, stalled and crashed in flames on a railroad located about 0,9 mile short of runway 31 threshold. The aircraft and the cargo were destroyed by a post crash fire while both pilots were uninjured.
Probable cause:
The Board determines that the probable cause of this accident was the pilot’s descent below his allowable minimum altitude and his inattention to flight instruments while attempting to locate the runway visually. The Board concludes that this accident was brought about by the captain’s disregard of the minimum altitude during instrument flight. It is evident that he was attempting visually to locate the runway tile flying at a low altitude under conditions of restricted visibility.
Final Report:

Crash of a Lockheed L-188A Electra in New York: 65 killed

Date & Time: Feb 3, 1959 at 2356 LT
Type of aircraft:
Operator:
Registration:
N6101A
Survivors:
Yes
Schedule:
Chicago – New York
MSN:
1015
YOM:
1958
Flight number:
AA320
Crew on board:
5
Crew fatalities:
Pax on board:
68
Pax fatalities:
Other fatalities:
Total fatalities:
65
Captain / Total flying hours:
28135
Captain / Total hours on type:
48.00
Copilot / Total flying hours:
10192
Copilot / Total hours on type:
36
Aircraft flight hours:
302
Circumstances:
At approximately 2356LT, the aircraft crashed into the East River while attempting an instrument approach to runway 22 at LaGuardia Airport. There were 73 persons on board, including one infant. The captain and one stewardess were killed; the first officer, flight engineer, and the remaining stewardess survived. Of the 68 passengers, 5 survived. The Board believes that a premature descent below landing minimums was the result of preoccupation of the crew on particular aspects of the aircraft and its environment to the neglect of essential flight instrument references for attitude and height above the approach surface. Contributing factors were found to be: limited experience of the crew with the aircraft type, fealty approach technique in which the autopilot was used in the heading mode to or almost to the surface, erroneous setting of the captain's altimeter, marginal weather in the approach area, possible misinterpretation of altimeter and rate of descent indicator, and sensory illusion with respect to height and attitude resulting from visual reference to the few lights existing in the approach area.
Probable cause:
The Board determines the probable cause of this accident was premature descent below landing minimums which was the result of preoccupation of the crew on particular aspects of the aircraft and its environment to the neglect of essential flight instrument references for attitude and height above the approach surface. Contributing factors were:
- Limited experience of the crew with the aircraft type,
- Faulty approach technique in which the autopilot was used in the heading mode to or almost to the surface,
- Erroneous setting of the captain's altimeter,
- Marginal weather in the approach area,
- Possible misinterpretation of altimeter and rate of descent indicator,
- Sensory illusion with respect to height and attitude resulting from visual reference to the few lights existing in the approach area.
Final Report:

Crash of a Vickers 744 Viscount in Chicago

Date & Time: Feb 20, 1956 at 0811 LT
Type of aircraft:
Operator:
Registration:
N7404
Survivors:
Yes
Schedule:
Detroit – Chicago
MSN:
90
YOM:
1955
Flight number:
CA141
Crew on board:
4
Crew fatalities:
Pax on board:
38
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17752
Captain / Total hours on type:
610.00
Copilot / Total flying hours:
5539
Copilot / Total hours on type:
53
Aircraft flight hours:
1541
Circumstances:
Capital Airlines flight 141 of February 20, 1956, originated at Willow Run Airport, Detroit, Michigan, and was a regularly scheduled flight to Chicago. The crew consisted of Captain Roger Harrison Taylor, First Officer George Richard Hanst and Stewardesses Jacqueline V. Sadowski and Gloria Galloway. Captain R. E. Gilliland, the fifth assigned crew member, was deadheading to Chicago and rode in the passenger cabin. Following a weather briefing, which included a review of en route and terminal weather forecasts, a VFR flight plan was filed. Departure from Detroit was at 0700. The gross takeoff weight of the air- craft was 54,701 pounds, which was below the specified limit; the load was distributed properly with respect to the center of gravity of the aircraft. The flight to the vicinity of Chicago was routine. Near Chicago Flight 141 reported to the Chicago tower that it was over the shoreline. The flight later reported passing Kedzie and was cleared to land on runway 31R. The flight was observed to make a right turn to final approach and appeared to descend in a normal manner until over the west side of Cicero Avenue (the eastern boundary of the airport) at an altitude of 25 to 50 feet above the ground. At this point the airplane appeared to decelerate and descend rapidly. The aircraft was further observed to strike the ground in a slightly nose-up attitude several hundred feet short of the threshold of threshold of the runway, and the top of the fuselage was seen to break open adjacent to the wing spar to fuselage attachment. As the aircraft proceeded down the runway the landing gear retracted and the aircraft then slid on its belly until it came to rest to the left of the runway, 1,626 feet beyond the point of initial impact. All occupants left the aircraft through emergency exits or the main cabin door. The fire department, having been called by tower personnel, arrived at the scene before all persons had evacuated the aircraft. However, there was no fire. The Chicago weather at 0720 was reported as: Sky clear, visibility 6 miles; smoke; wind north-northwest.
Probable cause:
The Board determines that the probable cause of this accident was a malfunctioning of the propeller control switches which culminated in an abrupt loss of lift. The following findings were reported:
- Three of the four landing gear actuated switches, which are located on the landing gear also struts and which effect operation of the propeller, were found to have been capable of malfunctioning by jamming, sticking, or freezing,
- No periodic inspection for internal examination of these switches had been established by the company prior to the accident,
- At least two of the tending gear actuated switches malfunctioned, making it possible for the 21-degree pitch stops to be withdrawn, and consequently ineffective,
- The crew failed to see the 21-degree pitch warning light on, and, therefore, they did not actuate the emergency switch,
- During the final stage of the approach at Chicago, the propellers moved to the ground fine pitch range,
- When the first officer saw three of the 17-degree pitch warning lights come on, he advanced all four throttles quickly,
- The rapid advance of the throttles caused the propeller governor control to move the propeller blades to the four-degree pitch position, thereby creating both propeller drag and loss of wing lift.
Final Report:

Crash of a Convair CV-340-32 in Chicago: 22 killed

Date & Time: Jul 17, 1955 at 0624 LT
Type of aircraft:
Operator:
Registration:
N3422
Survivors:
Yes
Schedule:
Dallas – Oklahoma City – Wichita – Kansas City – Chicago
MSN:
71
YOM:
1953
Flight number:
BN560
Crew on board:
5
Crew fatalities:
Pax on board:
38
Pax fatalities:
Other fatalities:
Total fatalities:
22
Captain / Total flying hours:
15121
Captain / Total hours on type:
1281.00
Copilot / Total flying hours:
9040
Copilot / Total hours on type:
1989
Aircraft flight hours:
4956
Circumstances:
Flight 560 is a Braniff daily scheduled flight between Dallas, Texas, and Chicago, Illinois, with intermediate stops at Oklahoma City, Oklahoma; Wichita, Kansas; and Kansas City, Missouri. On July 17 the flight crew, assigned at Dallas for the entire trip, consisted of Captain Allen R. Tobin. First Officer Orbin W. Hanks, and Hostess Mary E. Teel. Captain Tobin and First Officer Hanks arrived at the airport more than an hour before the scheduled departure. During this time preflight preparations were made in a normal and routine manner. The pilots were briefed and furnished the latest weather forecasts and reports over the route and for the scheduled stops. No weather conditions of consequence were indicated except that fog was forecast for the Chicago area, and the visibility was expected to be restricted to possibly one-half mile, on arrival. Flight 560 departed Dallas on schedule at 0100. The flight segments between Dallas and Wichita were uneventful; however, while starting the No. 1 (left) engine at Wichita prior to departure a small carburetor intake manifold fire occurred which was immediately extinguished. There was no damage incurred and the engine started easily on the second attempt. The flight proceeded to Kansas City where it landed at 0416. As the aircraft taxied to the terminal several persons noted that the No. 1 propeller was feathered and stopped. Captain Tobin told Braniff personnel that it feathered while being returned to positive pitch after reverse thrust had been used during the landing roll deceleration. The captain unfeathered the propeller before deplaning and maintenance personnel checked it for malfunction; none was indicated. No other mechanical service was requested or performed. The aircraft was serviced to 1,000 gallons of fuel while Captain Tobin and First Officer Hanks received supplemental weather information and completed other preparations for the last segment of the route to Chicago. Flight 560 departed Kansas City at 0435 in accordance with a VFR (Visual Flight Rules) flight plan. The aircraft, according to company records, was loaded to a gross weight of 45,622 pounds. This amount was less than the maximum allowable of 47,000 pounds and the load was properly distributed with respect to the center of gravity limitations. The flight climbed to 15,000 feet m. s. l. (mean sea level. At 0519 it requested and received an IFR (Instrument Flight Rules) flight plan for the remainder of the trip; accordingly, routine en route reports were made. This segment, as well as the previous, was described as very pleasant, smooth, and conducted primarily above or clear of the clouds. At 0547 ARTC cleared the flight as follows: “ATC clears Braniff 560 to the Naperville Omni via Peoria, Victor 116 over Joliet, maintain at least l,000 on top, tops reported 2,000 m. s. l., contact Chicago Center on 118.9 mc. passing Peoria.” This clearance was acknowledged and the flight reported accordingly. At 0556 Chicago ARTC broadcast a Chicago special weather observation which was: “Thin obscuration, visibility one-half mile.” At approximately 0609 the flight was asked by ARTC if it could land with one-half mile visibility and 1,000 feet thin obscuration. Braniff 560 replied that it could. At 0611 the flight reported over Joliet, 1,000 on top, whereupon ARTC advised it to contact the Chicago Midway Approach Control. Immediate contact was made and the flight was given the same weather and the latest altimeter information. The crew reported at 0618 over Naperville and was radar vectored by Approach Control to the outer marker for an ILS (Instrument Landing System) approach to runway 13R for landing. At 0624 the aircraft hit the sign and crashed through the airport boundary fence onto the airport. Another flight, holding off the runway before takeoff saw the wreckage stop and immediately notified the tower; crash emergency procedures were promptly initiated. The weather conditions reported at the time of the accident were: Partial obscuration; visibility one-half mile, fog, and smoke; sea level pressure 1014.2; temperature 71, dewpoint 68; wind south 6; altimeter 29.94; remarks, fog 8.
Probable cause:
The Board determines that the probable cause of this accident was momentary disorientation caused by the lose of visual reference during the final visual phase of the approach resulting in an increased rate of descent at an altitude too low to effect recovery. The following findings were reported:
- The reported weather conditions at Chicago permitted the flight to land and were accurately reported from the observer's position,
- The navigational aids, the ILS components, and ground lighting facilities were functioning normally,
- An ILS approach was made to runway 13R and was executed precisely and accurately until one-half mile from touchdown,
- Radar advisories were furnished in a normal manner supplementing the ILS approach,
- After approximately one-half mile from touchdown the aircraft descended at a high rate,
- The aircraft struck an advertising sign and its supporting steel post located 1,000 feet short of the runway threshold,
- Fog, with near zero flight visibility, enveloped the crash site over an indeterminable area,
- Examination of the aircraft wreckage and its components revealed no evidence indicating malfunction or failure and there was no evidence of an emergency aboard the flight.
Final Report:

Crash of a Curtiss C-46D-15-CU Commando in Chicago

Date & Time: Jan 4, 1951 at 0228 LT
Type of aircraft:
Registration:
N79982
Flight Phase:
Survivors:
Yes
Schedule:
Chicago – Newark
MSN:
33564
YOM:
1945
Flight number:
MAS1090
Crew on board:
3
Crew fatalities:
Pax on board:
45
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18000
Captain / Total hours on type:
2170.00
Copilot / Total flying hours:
3700
Copilot / Total hours on type:
300
Aircraft flight hours:
1257
Circumstances:
Monarch's Flight 1090 was cleared by Air Route Traffic Control (ARTC) to proceed on an instrument flight plan at 9,000 feet, nonstop Chicago to Newark, New Jersey. The crew consisted of Captain Marvin C. Staddon, Copilot Arthur J. Howarth, and Stewardess Thelma Dennis. Total aircraft weight at the time of take-off was approximately 46,100 pounds, 1,100 pounds in excess of the authorized gross weight. According to the crew the disposable load was so distributed as to be within the certificated limits with respect to the center of gravity. Prior to being cleared for take-off, preflight checks were accomplished in accordance with company operating procedures. All items checked satisfactorily, and the captain started his take-off at 0227 on Runway 31. He advanced the throttles to approximately 45 inches manifold pressure and 2700 RPM. The copilot then continued to advance the throttles to a manifold pressure of 47 inches, tightened the friction locks and guarded the throttles with his left hand to prevent creepage. The aircraft became airborne approximately half-way down the runway, which is 5,730 feet in length According to the copilot, manifold pressure and RPM's remained constant, and engine performance was normal. At the captain's command to raise the landing gear, the copilot moved the handle into the retract position and noticed at this time that the aircraft, now airborne, was turning slightly to the left and the air speed indicator read approximately 85 miles per hour. With the left wing down and with but a few feet of altitude, the copilot, realizing an emergency existed, immediately applied emergency take-off power--55 inches manifold pressure However, the C-46, still turning, struck several small aircraft parked on the west side of the airport, and continued beyond the airport boundary, striking a fence and railroad embankment Both throttles were then closed by the captain, but the electrical system switches were not turned off. The aircraft came to rest beyond the embankment and about one-half mile west of the airport's west boundary on a heading of approximately 250 degrees. A fire developed immediately, but all passengers and crew were evacuated before it assumed major proportions. The aircraft was destroyed. The maximum indicated air speed attained in flight, approximately 100 MPH, was noticed by the captain shortly after the landing gear was retracted. The maximum altitude attained was estimated as 25 feet.
Probable cause:
The Board determines that the probable cause of this accident was loss of control of the aircraft due to faulty piloting technique and overloading of the aircraft. The following findings were pointed out:
- The copilot was not properly certificated in that he had not accomplished the required six-month's equipment check in this type equipment,
- The aircraft was loaded approximately 1,100 pounds in excess of its authorized take-off weight,
- Take-off was made using less than the recommended power,
- The aircraft became airborne at an indicated air speed of 85 miles per hour, or less, and before a safe flying speed had been attained.
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: