Crash of a Curtiss C-46F-1-CU Commando in Newark

Date & Time: Aug 11, 1951
Type of aircraft:
Operator:
Registration:
N3908B
Flight Phase:
Survivors:
Yes
Schedule:
Newark – Philadelphia
MSN:
22516
YOM:
1945
Crew on board:
4
Crew fatalities:
Pax on board:
41
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the pilot-in-command noticed a directional control problem, decided to abandon the takeoff procedure and started an emergency braking maneuver. Unable to stop within the remaining distance, the airplane overran, hit a concrete embankment and came to rest in a swampy area with its right engine in flames. All 45 occupants were evacuated safely while the aircraft was damaged beyond repair. The crew was performing a special flight to Philadelphia on behalf of the USAF.

Crash of a Douglas DC-4-1009 in Philadelphia: 7 killed

Date & Time: Jan 14, 1951 at 1413 LT
Type of aircraft:
Operator:
Registration:
N74685
Survivors:
Yes
Schedule:
Newark – Philadelphia – Norfolk
MSN:
43102
YOM:
22
Flight number:
NA083
Crew on board:
3
Crew fatalities:
Pax on board:
25
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
6723
Captain / Total hours on type:
191.00
Copilot / Total flying hours:
4214
Copilot / Total hours on type:
158
Circumstances:
National Airlines’ Flight 83 departed Newark, New Jersey, at 1333, January 14, 1951, for Norfolk, Virginia, with a scheduled stop at Philadelphia. The crew consisted of Captain Howell C. Barwick, Copilot Edward J Zatarain, and Stewardess Mary Frances Housley. The aircraft’s total weight at takeoff was 58,601 pounds, which was within the allowable gross takeoff weight of 64,211 pounds, the load was properly distributed. Flight 83 was scheduled to leave Newark at 1300, but was delayed 33 minutes due to the replacement of a malfunctioning generator. The company flight clearance was filed at 1215 for the scheduled departure at 1300, and this clearance was also used for the delayed departure. Attached to it was the weather information for the flight, and a notice that the ILS (instrument landing system) glide path at Philadelphia was inoperative until further notice Immediately before taking off, the pilot requested and received from the tower the latest Philadelphia weather (reported on the 1328 CAA teletype sequence report and received at Newark after he boarded the aircraft), which was ceiling measured 1,000 feet, overcast, wind south-southwest at four miles per hour, and visibility 1 1/2 miles, with light snow and smoke Flight 83 was cleared by the New York Air Route Traffic Control to proceed to North Philadelphia range station via Amber Airway No 7, to maintain 4,000 feet, with Newark designated as the alternate airport. Thirteen minutes after takeoff, at 1346, Air Route Traffic Control issued the flight a new clearance to proceed to the Philadelphia ILS outer marker, to maintain 4,000 feet, and to contact Philadelphia Approach Control when passing the Northeast Philadelphia range station. At 1354 the flight reported over Northeast Philadelphia at 4,000 feet and was cleared by Approach Control to descend, crossing the Philadelphia range station at 3,000 feet, and to advise the tower when leaving the 4,000 and 3,000-foot levels. It was also advised that the altitude was unrestricted after passing the range station, and that it was cleared to make a straight-in approach to Runway 9 With the above clearance, local weather was given precipitation ceiling 500 feet, sky obscured, visibility 1, 1/4 miles, snow and smoke, and wind south-southwest two miles per hour. Following this clearance, the flight descended and reported over the Philadelphia range station at 3,000 feet, was again cleared for an approach to Runway 9, and was advised to report leaving thousand-foot levels. The flight acknowledged and reported leaving 3,000 feet at 1404, but no report of leaving 2,000 feet was received by Approach Control. According to the captain, they then proceeded to the outer marker and executed a procedure turn. At 1408 the flight reported over the outer marker, inbound, and stated that it was at 1,600 feet and descending. A clearance was immediately reissued to land on Runway 9, and the wind was given as south-southwest, three miles per hour. The flight was advised that the glide path was inoperative, that the frequency of the ILS localizer was 110 3 mc, that a 2,000-foot extension to the west end of the runway was under construction, and that braking action on Runway 9 was poor-to-fair. According to tower personnel this transmission was acknowledged. The crew, however, stated that they did not receive it. The flight continued its approach past the middle marker to the airport, and was first observed by ground witnesses beneath the overcast and directly over the intersection of Runways 4/22 and 9/27, located approximately 1,200 feet east of the threshold of Runway 9. Although the aircraft was first seen beneath the overcast and within the boundaries of the airport, the crew stated that they became contact at an altitude of approximately 500 feet, between the outer and middle markers. The aircraft was next seen to descend steeply, flare out for a landing in a normal manner, and float a considerable distance. After making contact with the runway the aircraft continued straight ahead, passed beyond the end of the runway, and crashed into a ditch at the east boundary of the airport. Fire immediately followed. Seven of the twenty-eight occupants did not evacuate the aircraft, and were fatally burned. The airport fire-fighting equipment was dispatched immediately to the scene, but efforts to extinguish the fire and rescue the remaining occupants were futile.
Probable cause:
The Board determines that the probable cause of this accident was the captain’s error in judgment in landing the aircraft too far down the slippery runway instead of executing a missed approach procedure. The following contributory factors were found:
- The runway was covered with wet snow and braking conditions were poor-to-fair,
- The landing was made too far down the slippery runway to permit stopping within its limits.
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-3-229 in Utica: 16 killed

Date & Time: Sep 4, 1950 at 1410 LT
Type of aircraft:
Operator:
Registration:
N18936
Flight Phase:
Survivors:
Yes
Schedule:
Ithaca – Syracuse – Utica – Newark
MSN:
2011
YOM:
1937
Flight number:
RBS032
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
4431
Captain / Total hours on type:
1900.00
Copilot / Total flying hours:
3600
Copilot / Total hours on type:
2273
Aircraft flight hours:
19023
Circumstances:
Prior to takeoff, the engines were given a pre-flight check, following which the takeoff roll was commended. The flaps were in the "full up" position for the takeoff. The aircraft became airborne in a normal manner approximately 1,500 feet down the runway and climbed to an altitude of approximately 50 feet and leveled off. At this time, the landing gear was retracted and the air speed was estimated to be 105 to 110 miles per hour by qualified observers. Approximately 3,000 feet from the point of take-off parts were observed falling from the left engine and the aircraft made a shallow turn to the left. At this time, the left propeller appeared to be fully feathered. The flight continued in a left turn, slowly losing altitude until it struck a grove of trees 1.5 miles southeast of the airport. The elevation of the terrain at this point was 480 feet which is 256 feet below the elevation of the airport. The tree tops were 80 feet above the ground. First impact with the trees was made on a heading of approximately 60 degrees and as the aircraft descended through the trees, it turned anti-clockwise 180 degrees to the original heading. Following impact with the trees, the fuel tanks ruptured causing a fire which consumed the fuselage. Sixteen of the occupants were fatally injured and seven seriously injured. The survivors escaped either through broken windows on the right side, or the right rear escape hatch.
Probable cause:
The Board determines that the probable cause of the accident was the failure of the left engine shortly after take-off, coupled with increased drag due to loss of left engine cowling and reduced power output of the right engine because the right propeller was in the high pitch position.
Final Report:

Crash of a Lockheed 18-10 LodeStar in Newark

Date & Time: Sep 29, 1949
Type of aircraft:
Operator:
Registration:
NC2020
Survivors:
Yes
Schedule:
White Plains – Newark
MSN:
18-2134
YOM:
1941
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Newark Airport, the twin engine aircraft hit power cables and crashed in a swampy area. All three occupants were injured and the aircraft was written off.

Crash of a Curtiss C-46E-1-CS in Columbus: 2 killed

Date & Time: May 16, 1948 at 2042 LT
Type of aircraft:
Operator:
Registration:
NC59489
Flight Type:
Survivors:
No
Schedule:
Newark – Chicago – Denver – Burbank – San Francisco
MSN:
2938
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2580
Captain / Total hours on type:
600.00
Copilot / Total flying hours:
4675
Copilot / Total hours on type:
1354
Aircraft flight hours:
5641
Circumstances:
The flight departed from Newark, New Jersey, at 1733 May 16, 1948, for Chicago, Illinois, Denver, Colorado, Burbank, and San Francisco, California. In addition to a crew consisting of Captain William R. McCauley and Copilot Jack R. Foote, the flight carried 5,280 pounds of fuel, and 10,263 pounds of cargo. According to the hourly weather reports available to the crew in Newark prior to departure, thunderstorm activity which existed over the vicinity of Goshen and Fort Wayne, Indiana, was moving eastward. Chicago Municipal Airport was reported to have a ceiling of 2,000 feet. The flight plan specified a cruising altitude of 4,000 feet to Chicago, the first intended point of landing. South Bend, Indiana, was designated as the alternate airport. No unusual incident was reported for approximately the first two hours of the trip, then, at 1931 the flight reported over Cleveland, Ohio, at 4,000 feet, stating that there was extreme turbulence approximately five miles east of the Cleveland Airport. At this time the flight acknowledged receipt of a weather report from Toledo, Ohio, to the effect that light thunderstorms with cloud to cloud lightning were moving northeasterly from Toledo. At 2013 the flight reported at 4,000 feet over Mansfield, Ohio, 58 miles south southwest of Cleveland. The crew stated that they had changed course to the south to avoid thunderstorms, and intended to proceed to Columbus, Ohio, in accordance with visual flight rules. A special weather observation taken at Cleveland at 2003 which reported a ceiling of 2,000 feet, visibility 10 miles, light rain, wind from the northwest at 30 miles per hour with strong gusts, and cloud to cloud and cloud to ground lightning was transmitted to the flight Cleveland Radio also transmitted a weather observation taken at Columbus at 1930 which reported an unlimited ceiling, visibility of 15 miles, and wind from the south at 14 miles per hour. After acknowledging receipt of this weather information, the flight stated "For your information advise no one to go through the turbulence we just went through." The next position report was received at 2032 at which time the flight reported being five miles north of Columbus. Following this report it was cleared by Columbus Tower for landing. In reply the flight stated to the tower, "We are declaring an emergency. Our rudder is locked, and I don’t think we will have any directional control on the ground." A landing approach was made for runway twenty-three, 4,490 feet long. Information concerning wind direction and velocity was transmitted repeatedly by the tower to the flight throughout the course of the approach. Although the first touchdown on runway 23 appeared normal, power was immediately applied and the aircraft took off. The crew then informed the tower that they wished to land directly into the wind, which at that time was from the south at five to ten miles per hour. They were accordingly cleared to land on runway eighteen, 3,580 feet long. The second approach appeared normal, and a touchdown was made on the runway without any apparent difficulty, but power was again applied and the flight took off again. When the flight reached a point 2 1/2 miles east of the field in its left circle of the field, it was observed to spin to the ground. Flames were observed immediately after the crash.
Probable cause:
The Board determines that the probable cause of this accident was the in-flight failure of the fuselage carry-in structure beneath the fin, due to extreme turbulence.
The following factors were considered as contributory:
- The aircraft was flown through severe turbulence approximately one-half hour before the accident,
- The rivets and fuselage skin immediately beneath the vertical fin failed during flight,
- The separation of the fuselage skin allowed the vertical fin to rock across its longitudinal axis until the fuselage carry-in structure beneath the fin failed completely,
- The failure of the vertical fin caused loss of control of the aircraft, and it crashed.
Final Report:

Crash of a Lockheed R50-4 LodeStar in Baltimore: 4 killed

Date & Time: Jan 24, 1948
Type of aircraft:
Operator:
Registration:
05049
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Newark – Washington DC
MSN:
2175
YOM:
1941
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The twin engine aircraft was returning from Newark and was diverted from National Airport due to a severe snowstorm, to Baltimore Municipal Airport. While approaching, the airplane crashed in unknown circumstances, killing all four crew members. The wreckage was located two days later after an extensive search by Army, Navy and Coast Guard aircraft.
Crew:
Lcdr Charles W. Schuh,
Lt Jg William N. Killebrew,
Amm1 Charles A. MacArthur,
Arm1 Rudolph H. Schoning.

Crash of a Lockheed L-649 Constellation in Boston

Date & Time: Jan 21, 1948 at 0417 LT
Operator:
Registration:
NC111A
Survivors:
Yes
Schedule:
Miami – Newark
MSN:
2532
YOM:
1947
Flight number:
EA604
Crew on board:
5
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
10312
Captain / Total hours on type:
363.00
Copilot / Total flying hours:
3001
Copilot / Total hours on type:
145
Aircraft flight hours:
1499
Circumstances:
Flight 604 departed Miami, Florida, at 2301, January 20, 1948, on an instrument flight rules clearance, non-stop to Newark, New Jersey, to cruise at 15,000 feet via Airway Amber 7 to Jacksonville, Florida, and Airway Amber 6 to Alma, Georgia, thence direct to Spartanburg, South Carolina, Winston-Salem, North Carolina, and Washington, D. C., and via Airway Amber 7 to Newark, Boston, Massachusetts, and Providence. Rhode Island, were designated as alternate air ports. In order to remain above the overcast, the flight requested changes of cruising altitude between Winston-Salem and Washington, and at 0232, at which time it reported over Washington, the flight was cruising at 21,000 feet. Shortly after passing Washington, Flight 604 was cleared to descend en route to Newark and to cross Philadelphia at 7,000 feet, and was advised that no traffic was reported above 7,000 feet. A descent was established and at 0253 the flight reported over Philadelphia "at 8,000 feet descending." Shortly thereafter the company radio station at LaGuardia Field, New York, advised the flight that the 0240 weather observation for Newark indicated a ceiling of 700 feet and visibility of one-half mile. Immediately thereafter the flight was given an air traffic control clearance "to Flatbush and LaGuardia Approach Control" to cross Keyport and Flatbush at 2,500 feet. Upon receiving this clearance the captain immediately requested a confirmation from the New York dispatcher, inasmuch as no prior notice had been received of a change of destination from Newark to LaGuardia. In acknowledgment the flight was informed that the dispatcher desired the flight to proceed to LaGuardia Field. During the period of the flight from midnight until 0300, the ceilings had lowered throughout the New York-New Jersey area. At the time of the re-clearance the LaGuardia weather was being reported as ceiling 500 feet, visibility one and one-quarter miles, and light snow. The flight continued its descent on the east course of the Philadelphia radio range and reached 2,500 feet in the vicinity of Freehold, New Jersey, over which the crew reported passing at 0309. Immediately after this report the flight changed to the LaGuardia Approach Control frequency. LaGuardia Approach Control immediately cleared the flight to descend to 1,500 feet and approved a straight-in landing on Runway 4. Since no material change had been observed in the LaGuardia weather, the flight was again informed that the ceiling was reported as 500 feet, the visibility one and one-quarter miles, and the wind calm. The flight passed directly over the airport without attempting a landing approach and shortly thereafter reported over the range station which is located three and two-tenths miles northeast of the airport. The flight was then cleared to use the reciprocal runway, 22, but the aircraft returned southeastward, passing to the east of LaGuardia Field again without attempting a landing approach. During this period the LaGuardia weather observer completed the 0325 weather observation and approximately 3 minutes thereafter the flight was advised that this report indicated an indefinite ceiling 400 feet and visibility one and one-half miles. The flight continued southwestward in order to establish an approach to Runway 4. Approach Control asked the flight at this time whether it desired a GCA (Ground Controlled Approach Radar) monitored approach. The captain declined a controlled approach but stated that he would accept a monitored approach. At approximately 0330 the aircraft again passed over the airport in a northeasterly direction; the flight advised Approach Control that the ceiling was not 500 feet and requested a report of the current Boston weather. The 0230 Boston weather report was transmitted to the flight, indicating a ceiling of 8,000 feet, 3 miles visibility, smoke, and haze. Upon receiving this report, the flight requested and received clearance to Boston from Air Traffic Control and from the company dispatcher. At 0337, the flight reported leaving Rye, New York, en route to Boston, climbing to 5,000 feet. Shortly after the flight passed over Hartford, Connecticut, at 0354, the company station at Boston advised the captain that the flight was cleared to the Boston Tower. Before reaching Boston the flight was informed that the 0400 weather report for that station indicated "ceiling 600 feet, sky obscured, visibility one mile, light snow; surface wind southeast 8 miles per hour." After passing Franklin, Massachusetts, at 0409, the flight changed to the Boston Tower frequency. When asked by the flight whether the Instrument Landing System (ILS) was operating, the tower advised the flight that the monitor panel indicated this system to be operating normally. Shortly thereafter the tower cleared the flight for a straight-in approach to Runway 4 and cautioned that due to the runway condition braking action was "fair to poor." Initial touchdown was made on Runway 4, at 0417, approximately 2,000 feet beyond the approach end of the runway. After completing approximately 600 feet of its landing roll, the aircraft was seen to skid to the left and crash into a snowbank along the left side of the runway. The right landing gear and nose gear collapsed and the aircraft fell on the right wing, coming to rest on the left side of the runway heading in a westerly direction. Fire broke out in the vicinity of the No. 3 and No. 4 engines and spread rapidly toward the fuselage. However, all passengers were deplaned and were removed from the vicinity of the aircraft without injury resulting from the crash or subsequent fire. Five of the occupants were injured during the evacuation due to the necessity for jumping from the rear exit, which was estimated to be 12 to 16 feet above the ground. Several fire fighting units from the airport and from East Boston were alerted and proceeded to the scene of the accident; however, the aircraft continued to burn for approximately one hour and 30 minutes after the crash.
Probable cause:
On the basis of the above findings, the Board determines that the probable cause of this accident was the loss of directional control of the aircraft on the runway due to excessive snow accumulation. A contributing factor was the lack of precaution exercised by the air carrier’s station manager, the Civil Aeronautics Administration’s operations inspector and the airport management in determining that the conditions of the runways were adequate for safe aircraft landing.
Final Report:

Crash of a Douglas C-54B-15-DO Skymaster near Bainbridge: 53 killed

Date & Time: May 30, 1947 at 1741 LT
Type of aircraft:
Operator:
Registration:
NC88814
Flight Phase:
Survivors:
No
Schedule:
Newark – Miami
MSN:
18380
YOM:
1944
Flight number:
EA605
Crew on board:
4
Crew fatalities:
Pax on board:
49
Pax fatalities:
Other fatalities:
Total fatalities:
53
Captain / Total flying hours:
11514
Captain / Total hours on type:
683.00
Copilot / Total flying hours:
2550
Copilot / Total hours on type:
488
Aircraft flight hours:
3623
Circumstances:
The four engine aircraft left Newark Airport at 1704LT on a flight to Miami. While climbing to an altitude of 4,000 feet, the aircraft went out of control, dove into the ground and crashed in a huge explosion in a field located 2 miles east of Bainbridge. The aircraft was totally destroyed and all 53 occupants were killed.
Probable cause:
The Board determines that the probable cause of this accident was a sudden loss of control, for reasons unknown, resulting in a dive to the ground.
Final Report:

Crash of a Douglas DC-3C in Newark: 2 killed

Date & Time: May 4, 1947
Type of aircraft:
Registration:
NC53196
Survivors:
Yes
Schedule:
Louisville – Newark
MSN:
19435
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The aircraft was approaching Newark Airport for landing. The airplane was too far to the right for an approach to runway 06 and the tower controller radioed that he was in line for an approach to runway 28. The approach was then made to runway 28 which is 7,100 feet long with an additional usable 500 feet at the end. The approach was fast, however and contact was not made with the runway until within the last 2,000 feet. The aircraft continued off the runway and ran into a drainage ditch where a fire broke out, which was quickly extinguished.
Source:
https://aviation-safety.net/database/record.php?id=19470504-0