Crash of a Douglas SC-47A near Hawthorne: 7 killed

Date & Time:
Operator:
Registration:
42-108944
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Reno - Reno
MSN:
13288
YOM:
1944
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew left Reno-Stead Airport on a classified mission with six other similar aircraft. While cruising in limited visibility at an altitude of 6,000 feet, the airplane hit the slope of a mountain located in the Gillis Mountain Range, about 12 miles northeast of Hawthorne. The wreckage was found few feet below the summit and all seven crew members were killed.
Probable cause:
It is believed that the accident was the consequence of a controlled flight into terrain.

Crash of a Convair CV-240-0 at Fort Leonard Wood AFB: 30 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N94221
Survivors:
No
Schedule:
Tulsa – Joplin – Springfield – Saint Louis – New York
MSN:
40
YOM:
1948
Flight number:
AA476
Crew on board:
3
Crew fatalities:
Pax on board:
27
Pax fatalities:
Other fatalities:
Total fatalities:
30
Captain / Total flying hours:
15540
Captain / Total hours on type:
5000.00
Copilot / Total flying hours:
8500
Copilot / Total hours on type:
2500
Aircraft flight hours:
14865
Circumstances:
Flight 476 of August 4 was a scheduled operation between Tulsa, Oklahoma, and La Guardia Field, New York, with several intermediate stops including Joplin, Springfield, and St. Louis, Missouri. The flight departed Tulsa at 1006 (one minute behind schedule) with Captain Hugh C. Barren, First Officer William G. Gates, and Stewardess Thelma R. Ballard as crew. En route stops were made at Joplin and Springfield, and no discrepancies were reported or noted at either point. However, a traffic delay in the Joplin area resulted in the flight arriving and departing Springfield 21 minutes behind schedule. Two of the eight passengers deplaned at Springfield, 21 passengers boarded the flight there. Gross weight of the aircraft at takeoff was 38,663 pounds, 2,302 pounds under that allowable, and the center of gravity was located within prescribed limits. Flight 476 departed Springfield VFR for St. Louis, its next scheduled stop, at 1153 via Victor Airway 14 to cruise at 7,000 feet. It was off the ground at 1156. Twenty-one minutes later (1217) the crew initiated a general call asking, "Does anyone read 476?" Springfield company radio acknowledged but received no reply. Two other American Airlines flights, one cruising in the vicinity of Springfield at 7,000 feet, the other 30 miles north-northeast of St. Louis, heard a transmission from Flight 476 that No. 2 engine was on fire. This message was also heard by American's ground station at St. Louis. Three minutes later the American flight in the Springfield area intercepted the following message, "Springfield, are you reading 476? We have bad engine fire." This was the last message heard from the flight. All transmissions were on company frequency. During this interval numerous witnesses on the ground back along the flight path saw the aircraft with smoke and flame coming from the right engine. The aircraft was also tracked by a military radar installation near Springfield until it disappeared from the scope in the vicinity of Fort Leonard Wood. At approximately 1222 the operations officer on duty at Forney Field, Fort Leonard Wood, received a radio message from an Army pilot flying nearby that a two-engine aircraft with a fire in the right engine was on final approach to runway 14. The tower operator at Forney Field saw the approaching aircraft and gave it clearance to land. Before the operations officer could alert the crash crew another call from the Army pilot informed him that the airplane had crashed short of the runway. The time was 1223. Army personnel with portable fire-fighting equipment reached the wreckage on foot. There were no survivors. Heavy fire-fighting equipment and ambulances could not reach the scene until the Army engineers had bulldozed a road through the densely wooded area in which the crash occurred.
Probable cause:
The Board determines that the probable cause of this accident was installation of an unairworthy cylinder, the failure of which resulted in an uncontrollable fire and subsequent loss of a wing in flight. The following findings were reported:
- Weather was not a factor,
- N° 12 cylinder of the right engine was not airworthy and failed near its base after less than six hours of operation, causing a fire that the crew could not control,
- Visual inspection procedures being used by the carrier did not reveal the unairworthy condition of the cylinder,
- The right main tank fuel shutoff valve was open, which greatly increased the intensity and duration of the fire,
- Fire damage prevented the closing of this valve,
- Procedures recommended by the manufacturer and specified in the carrier's overhaul manual had been countermanded by verbal instructions approved by the carrier's engineering department and were not being followed by the carrier's inspectors with respect to the handling of cylinders.
Final Report:

Crash of a Lockheed P2V-5 Neptune in USA: 5 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
122458
Flight Type:
Survivors:
No
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Crashed in unknown circumstances, probably somewhere in the US (to be confirmed). All five crew members were killed.

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

Date & Time:
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 Boeing KC-97G -25-BO Stratotanker near Cressey: 10 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
52-2637
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Castle - Castle
MSN:
16668
YOM:
1952
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
Shortly after takeoff from Castle AFB, while climbing, the aircraft suffered serious technical issues and crashed in a huge explosion about seven miles northwest of the airbase, near the city of Cressey. All ten crew members were killed.

Crash of a Douglas C-47A-85-DL on Sitkinak Island: 10 killed

Date & Time:
Operator:
Registration:
43-15594
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Kodiak – Elmendorf
MSN:
20060
YOM:
1944
Crew on board:
4
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
While flying in low visibility (marginal weather conditions ?), the airplane hit the slope of a mountain located on Sitkinak Island. All ten occupants were killed.
Probable cause:
It is believed the accident was the result of a controlled flight into terrain.

Crash of a Lockheed P2V-5 Neptune on Saint-Lawrence Island

Date & Time:
Type of aircraft:
Operator:
Registration:
131515
Flight Phase:
Survivors:
Yes
MSN:
426-5396
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was engaged in a maritime patrol over the Bering Sea. While cruising at an altitude of 8,000 feet about 40 miles west of the Saint Lawrence Island, the airplane was attacked by two Soviet MiG-15 fighters. The crew was able to leave the area and elected to make an emergency landing on St Lawrence Island when the aircraft crash landed. There were no injuries.
Probable cause:
Attacked by two Soviet MiG-15.

Crash of a Boeing KC-97G-22-BO Stratotanker near Fort Myers: 1 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
52-0891
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
16585
YOM:
1952
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
An engine failed in flight. All nine crew members decided to bail out and abandoned the aircraft that dove into the ground and crashed in a prairie located two miles north of Fort Myers. Eight crews were found uninjured while one was killed as his parachute failed to open.
Probable cause:
Engine failure in flight.

Crash of a Douglas C-47B-1-DK near Alamogordo: 7 killed

Date & Time:
Operator:
Registration:
43-48386
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
14202/25647
YOM:
1944
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
Few minutes after its takeoff from Holloman Airport, the aircraft hit a mountain located 10 miles northeast of Alamogordo. All seven crew members were killed.

Crash of a Convair B-36J-5-CF Peacemaker near Sterling City: 15 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
52-2818
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Walker - Walker
MSN:
374
YOM:
1952
Flight number:
Abbott 27
Crew on board:
15
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
15
Circumstances:
While conducting a training mission from Walker AFB, the crew encountered poor weather conditions with thunderstorm activity and turbulences. The airplane lost wing panels, went out of control and crashed in a flat attitude in a desert area located 18,5 miles southwest of Sterling City. All 15 crew members were killed.
Probable cause:
Loss of control caused by heavy turbulences in thunderstorm activity.