Crash of a Lockheed P-3A-10-LO Orion into the Atlantic Ocean: 14 killed

Date & Time: Jan 30, 1963 at 0200 LT
Type of aircraft:
Operator:
Registration:
149672
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Patuxent River - Patuxent River
MSN:
5013
YOM:
1962
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
The crew departed Patuxent River NAS on a night exercise with a US Marine Ship. While cruising at an altitude of 500 feet, the airplane nosed down and crashed into the Atlantic Ocean, some 231 miles east of Atlantic City, New Jersey. Few debris and the dead body of the captain were found floating on water. No trace of the rest of the crew was found.
Probable cause:
Due to lack of evidence, it was not possible to determine the exact cause of the accident. Nevertheless, altimeters oscillations could occur in flight and may ba a contributing factor.

Crash of a Boeing B-52C-40-BO Stratofortress in Greenville: 7 killed

Date & Time: Jan 24, 1963 at 1452 LT
Type of aircraft:
Operator:
Registration:
53-0406
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Westover - Westover
MSN:
16886
YOM:
1953
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was engaged in a training flight out from Westover AFB. While cruising at low height, control was lost. Three crew members were able to bail out before the aircraft crashed in the Elephant Mountain Range located near Greenville. Seven crew members were killed while two survived.
Crew (99th BS):
Lt Col Dante Bulli, pilot,
Maj Robert J. Morrison, copilot, †
Cpt Gerald Adler, navigator,
Lt Col Joe R. Simpson Jr., †
Maj William W. Gabriel, †
Maj Robert J. Hill, †
Cpt Herbert L. Hansen, †
T/Sgt Michael F. O'Keefe, †
Cpt Charles G. Leuchter. †
Probable cause:
Failure of the stabilizer shaft broke during a low level exercise.

Crash of a Fairchild F27 in Salt Lake City: 3 killed

Date & Time: Jan 17, 1963 at 1553 LT
Type of aircraft:
Operator:
Registration:
N2703
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Salt Lake City - Salt Lake City
MSN:
6
YOM:
1958
Flight number:
WC703
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
14460
Captain / Total hours on type:
10.00
Copilot / Total flying hours:
15509
Copilot / Total hours on type:
578
Aircraft flight hours:
11708
Circumstances:
This flight was designated by West Coast Airlines, Inc., (WCA) as Pilot Training Flight No. 703. It was for the purpose of rating a company DC-3 captain for F-27 aircraft. N 2703 arrived at Salt Lake City Municipal Airport January 17, 1963, at 1431 1 as West Coast Flight 752 from Seattle, Washington, with stops at Yakima, Pasco, Walla Walla, all in Washington; Lewiston, Montana; and Boise and Twin Falls, both in Idaho. The flight had been uneventful and there were no carryover discrepancies entered in the aircraft's flight log. After completion of turnaround servicing, N 2703 departed the West Coast Airlines ramp at approximately 1506 with Company Cheek Pilot Instructor William Harvey Lockwood, Trainee Captain Elmer J. Cook, and FAA Carrier Inspector Buell Z. Davis aboard. A flight plan was prepared and signed by Captain Lockwood. It listed Elmer J. Cook as the first officer, FAA Inspector Buell Z. Davis as a crew member, and specified that the flight would be in the local area, under VFR conditions, and of 1 hour and 30 minutes duration. At departure Captain Cook occupied the left pilot seat, Captain Lockwood the right pilot seat, and Inspector Davis the observer's (jump) seat. The aircraft carried approximately 3,500 pounds of fuel which was ample for the intended flight. The aircraft's computed gross weight was 28,310 pounds, approximately 7,000 pounds less than maximum allowable for takeoff, and the center of gravity was within prescribed limit. Flight 703 took of f at 1510 and remained in the traffic pattern for a practice landing which was made at 1517. At 1522, Flight 703 made a second takeoff and was last observed three miles south of the airport by the local controller in the tower. The tower clearance for this takeoff was the last radio contact with the flight. The next known sighting of Flight 703 was from the air by the crew of Western Airlines Flight No. 38. At 1531 they observed it at an estimated altitude of 8,000 feet mean sea level (m.s.l.) descending to an estimated altitude of 7,000 feet m.s.l. with the left propeller feathered. It was headed southeasterly, and in the vicinity of the southern tip of Antelope Island in Great Salt Lake, some 10 miles west-northwest of the airport. Several minutes later, the ground controller in the Salt Lake City Tower observed Flight 703 for a few minutes. He saw it approaching the airport from the west at an estimated altitude of 8,000 feet above the ground. It appeared to be flying level as it came approximately over him, continuing a few miles to the east and over Salt Lake City. It then made a right turn to a west-northwesterly heading and continued in that direction until the controller discontinued watching it at a point approximately five miles west of the airport. He did not notice anything unusual about the aircraft's appearance or performance. The next observation of Flight 703 was by a motorist near the southeastern shore of the Great Salt Lake who saw it at an estimated 3,000 feet above the ground descending. He estimated the time of his initial observation to be 1550. The aircraft appeared to be on a northwesterly heading making a normal descent considerate west of the Salt Lake City Airport and continued descent until it appeared "to actually go into the lake itself." He did not see any splash; his position was about six miles from where the wreckage was later found. The official U.S. Weather Bureau observation at Salt Lake City Municipal Airport at 1555 on the day of the accident was: Ceiling estimated 12,000 feet broken, high overcast, visibility 12 miles, temperature 34 degrees F., dewpoint 2 degrees F., wind from south-southwest at 5 knots, altimeter setting 30.05, smoky, snow showers of unknown intensity east. Weather conditions were not appreciably different an hour earlier nor an hour later. At 1700, the Salt Lake City Flight Service Station (FSS) received a request from the Salt Lake City Air Route Traffic Control Center (ARTCC) to initiate a call to Flight 703 on all available frequencies. There was no reply from Flight 703 to these calls. At 1758 the Salt Lake City FSS received information from the Salt Lake City ARTCC that West Coast Flight 703 was overdue and unreported. On January 18, 1963, at approximately 1140, one body and aircraft debris was seen floating in Great Salt Lake. This floating debris was 10.4 nautical miles to the Salt Lake City Very High Frequency Omni Directional Range (VOR) or the 248 de radial. Early next morning the other two bodies were sighted and all three were recovered from the lake.
Probable cause:
The probable cause of the accident was the crew's lack of vigilance, for undetermined reasons, in not checking a simulated emergency descent before striking the water.
Final Report:

Crash of a De Havilland DH.104 Devon at Wigram AFB

Date & Time: Jan 8, 1963 at 1500 LT
Type of aircraft:
Operator:
Registration:
NZ1830
Flight Type:
Survivors:
Yes
Schedule:
Wigram - Wigram
MSN:
04428
YOM:
1953
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The pilot, sole on board, was completing a local training flight at Wigram AFB. On final approach, an engine caught fire. The pilot lost control of the aircraft that stalled and crashed short of runway. While the pilot was uninjured, the aircraft was damaged beyond repair.
Probable cause:
Engine fire on final approach.

Crash of a Vickers 828 Viscount in Nagoya: 4 killed

Date & Time: Nov 19, 1962
Type of aircraft:
Operator:
Registration:
JA8202
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Nagoya - Nagoya
MSN:
444
YOM:
1961
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The crew was engaged in a local training flight at Nagoya-Komaki Airport. While cruising at an altitude of 3,500 feet, the pilot-in-command made a 360 turn when control was lost. The airplane dove into the ground and crashed in a field located few km from the airport. All four crew members were killed. It is believed that the aircraft stalled during the last turn due to an insufficient speed.

Crash of a Douglas C-54D-10-DC Skymaster near Suárez: 5 killed

Date & Time: Nov 16, 1962 at 2212 LT
Type of aircraft:
Operator:
Registration:
FAC-693
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Bogotá - Bogotá
MSN:
10183
YOM:
1944
Location:
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The crew departed Bogotá-El Dorado Airport in the evening for a night training mission. En route, the four engine aircraft struck the slope of Mt Guayatama located near Suárez, about 100 km southwest of its departure point. The aircraft was destroyed and all five crew members were killed.

Crash of a Fokker F27 Friendship 100 in Manila: 3 killed

Date & Time: Oct 12, 1962
Type of aircraft:
Operator:
Registration:
PI-C503
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Manila - Manila
MSN:
10191
YOM:
1961
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
2186
Aircraft flight cycles:
1264
Circumstances:
Shortly after takeoff from Manila-Intl Airport, while climbing, the airplane went out of control and crashed in the suburb of Parañaque located south of the airfield. The aircraft was destroyed and all three crew members were killed while there were no casualties on the ground. The crew was involved in a local training flight at the time of the accident.
Probable cause:
It would be inconclusive for the Board to advance any definitive cause(s) of this accident. The airplane was in emergency a few seconds before it crash-landed. It is, however, deduced that the emergency landing was in all probability attributed to the error on the part of the crew, in that the attempt to relight the left engine, presumable during the process thereof, the right engine was instead, and unintentionally taken for granted. Factors contributing to the accident were the very short time and the relatively low altitude.

Crash of a Lockheed VC-60A LodeStar in Campo de Marte AFB

Date & Time: Oct 6, 1962
Type of aircraft:
Operator:
Registration:
2003
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Campo de Marte - Belém
MSN:
2365
YOM:
1943
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Campo de Marte AFB, while on a training flight to Belém, control was lost and the twin engine airplane crashed in flames. All three crew members were injured while the aircraft was destroyed.

Crash of a Vickers 607 Valetta T.3 near Chippenham: 3 killed

Date & Time: Aug 28, 1962
Type of aircraft:
Operator:
Registration:
WJ480
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lyneham - Lyneham
MSN:
605
YOM:
11
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The crew was performing a local training flight at RAF Lyneham, consisting of takeoff and landings with one engine inoperative. Following a low pass over RAF Lyneham, the crew continued to the northwest when control was lost. The airplane dove into the ground and crashed in a field located five miles northwest of Chippenham. Two crew members were killed while the third occupant was seriously injured. He died from his injuries eight days later.
Probable cause:
The crew voluntarily shut down the right engine to simulate a failure and switched off the fuel system. While climbing, the crew elected to restart the right engine but forgot to switch the fuel system on. Due to insufficient speed, the airplane lost height, stalled and eventually crashed.

Crash of a Martin 404 in Wilmington

Date & Time: Aug 22, 1962 at 0748 LT
Type of aircraft:
Operator:
Registration:
N40401
Flight Type:
Survivors:
Yes
Schedule:
Wilmington - Wilmington
MSN:
14101
YOM:
1952
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4492
Captain / Total hours on type:
125.00
Aircraft flight hours:
20260
Circumstances:
The crew was completing a local training flight at Wilmington-New Hanover County Airport. After touchdown, the airplane went out of control, veered off runway and came to rest. While all three crew members were uninjured, the aircraft was damaged beyond repair.
Probable cause:
The accident was the consequence of an unwanted propeller reversal during a critical phase of landing caused by malfunction of the propeller low pitch stop lever assembly, resulting from foreign matter in the servo valve control.