Crash of a Rockwell Aero Commander 500A in Sutter: 1 killed

Date & Time: Feb 6, 1966 at 1330 LT
Operator:
Registration:
N9385R
Flight Phase:
Flight Type:
Survivors:
No
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3500
Captain / Total hours on type:
75.00
Circumstances:
While in cruising altitude, the twin engine aircraft went out of control, entered a dive and crashed in a huge explosion near Sutter, California. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
The exact cause of the accident could not be determined.
Final Report:

Crash of a Learjet 23 near Palm Springs: 8 killed

Date & Time: Nov 14, 1965 at 1721 LT
Type of aircraft:
Registration:
N243F
Flight Phase:
Survivors:
No
Schedule:
Palm Springs – Hollywood
MSN:
23-063
YOM:
1965
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
15100
Captain / Total hours on type:
125.00
Copilot / Total flying hours:
160
Copilot / Total hours on type:
24
Aircraft flight hours:
43
Circumstances:
About 1721 P.s.t., November 14, 1965, Lear Jet Model 23, N243F, operated as a free transportation flight by the Paul Kelly Flying Service, Inc., crashed shortly after a night takeoff from the Palm Springs Airport at Palm Springs, California. The crash was in the Indio Hills approximately 13 miles east of the airport. The six passengers and two crewmembers were fatally injured. The aircraft was destroyed by impact and fire. The flight, which was to transport the passengers to Burbank, California, was observed to depart Runway 13 in a normal manner, commence a low-angle climbout, and accelerate to a relatively high speed. Shortly after takeoff the pilot called the Thermal, California Flight Service Station. Although station personnel responded immediately, there were no other transmissions from the flight. About this time the aircraft was observed to make a left turn beneath a low cloud base of about 3,000 feet, proceed in a northerly direction and then enter a steep dive from horizontal flight, and crash. All eight occupants were killed.


Probable cause:
The Board determines that the probable cause of this accident was spatial disorientation of the pilot, resulting in a loss of control.
Final Report:

Crash of a Boeing EC-97G Stratofreighter at Palmdale AFB

Date & Time: Oct 28, 1965
Operator:
Registration:
53-0358
Flight Type:
Survivors:
Yes
MSN:
17140
YOM:
1953
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For undetermined reason, the four engine aircraft made a wheels-up landing at Palmdale AFB, slid for several yards and came to rest. There were no injuries but the airplane was damaged beyond repair.

Crash of a Lockheed PV-2 Harpoon in Hayward: 2 killed

Date & Time: Sep 7, 1965 at 1624 LT
Type of aircraft:
Registration:
N7671C
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
15-1120
YOM:
1944
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
12000
Circumstances:
After being converted by Oakland Airmotive Centaurus for civil use, the aircraft was engaged in a delivery flight, carrying two passengers and one pilot. Shortly after takeoff from Hayward Airport, while in initial climb, the twin engine aircraft stalled and crashed in flames. The pilot and a passenger were killed while the second passenger was injured. The aircraft was destroyed.
Probable cause:
Improper maintenance, servicing and inspection on part of the maintenance personnel. Inadequate flight preparation on part of the pilot. It was reported that the modification done on the aircraft were not approved by FAA. The aircraft was improperly loaded at the time of the accident, which caused the stall. Errors made in modification work and loading resulted out of limits aft CofG n° 377 filed by FAA.
Final Report:

Crash of a Beechcraft C-45H Expeditor in Long Beach: 8 killed

Date & Time: Aug 7, 1965 at 0209 LT
Type of aircraft:
Operator:
Registration:
N88Q
Flight Phase:
Survivors:
No
MSN:
AF-710
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
7000
Circumstances:
Shortly after takeoff from Long Beach Airport, while climbing by night and a limited visibility due to fog, one of the engine failed. Unable to maintain a safe altitude, the twin engine aircraft struck power cables, stalled and crashed in flames in Lakewood. The airplane was totally destroyed by impact forces and a post crash fire and all 8 occupants were killed.
Probable cause:
Investigations were unable to determined the exact cause of the engine failure.
Final Report:

Crash of a Boeing C-135A-BN Stratotanker at El Toro AFB: 84 killed

Date & Time: Jun 25, 1965 at 0146 LT
Type of aircraft:
Operator:
Registration:
60-0373
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
McGuire - El Toro - Hickam - Kadena
MSN:
18148
YOM:
1961
Crew on board:
12
Crew fatalities:
Pax on board:
72
Pax fatalities:
Other fatalities:
Total fatalities:
84
Circumstances:
The aircraft was on its way from McGuire AFB to Kadena, Okinawa, with intermediate stops at El Toro AFB and Hickam AFB, Honolulu. The departure from El Toro AFB was completed by night and marginal weather conditions. One minute after liftoff, during initial climb at an altitude of about 1,150 feet, the four engine aircraft struck the slope of the Loma Hill located three miles from the airfield. The aircraft struck the hill 150 feet below the summit and disintegrated on impact. None of 84 occupants survived the crash. At the time of the accident, the visibility was limited due to low clouds, light drizzle and night.
Probable cause:
It was determined that the crew performed a straight-in climb after takeoff instead of making a turn to the left as prescribed in the published departure procedures of the El Toro AFB.

Crash of a Beechcraft C18S in Corona del Mar: 9 killed

Date & Time: May 29, 1965 at 0700 LT
Type of aircraft:
Registration:
N9107R
Flight Phase:
Flight Type:
Survivors:
No
MSN:
5660
YOM:
1943
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
835
Captain / Total hours on type:
20.00
Circumstances:
The twin engine aircraft was completing a regional flight on behalf of the Department of Commerce. While cruising in cloudy conditions, the airplane adopted a nose down attitude, started an uncontrolled descent and eventually struck power cables before crashing in Corona del Mar. The airplane was totally destroyed and all nine occupants were killed.
Probable cause:
Uncontrolled descent caused by a miscellaneous instrument failure in flight for undetermined reason.
Final Report:

Crash of a Lockheed L-1049H Super Constellation in San Francisco: 3 killed

Date & Time: Dec 24, 1964 at 0031 LT
Operator:
Registration:
N6915C
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
San Francisco – New York
MSN:
4812
YOM:
1957
Flight number:
FT282
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
14911
Captain / Total hours on type:
3942.00
Copilot / Total flying hours:
4113
Copilot / Total hours on type:
3811
Circumstances:
Flight 282 was a scheduled domestic cargo flight from San Francisco International Airport, California, to John F. Kennedy International Airport, New York. It was originally scheduled to depart at 2100 hours, Pacific Standard Time, on 23 December, but the flight was delayed because of the non-availability of a flight engineer. An engineer obtained from Los Angeles arrived in San Francisco at 2315 hours and the flight departed at 0028 hours on 24 December. At 0015 hours, while taxiing to runway 28L, the flight advised Ground Control that because of a heavy load, they would like to proceed out past the GAP Radio Beacon to the Golden Gate Intersection, and thence via Victor 150 to Sacramento instead of direct to Sacramento as originally filed. The request was coordinated with Oakland Air Route Traffic Control Centre and approval obtained. The crew was then advised that for take-off on runway 28L there would be a 'heavy' left crosswind from 210° at 18 to 25 knots which they acknowledged. After having switched to clearance delivery frequency, the flight was cleared to Kennedy Airport via Victor one fifty Sacramento, Victor six north, and requested to climb out on the San Francisco two eight seven radial for a vector to Golden Gate Intersection to intercept Victor one fifty. This was acknowledged. The Clearance Delivery Controller then stated: " You can disregard the vector, climb outbound San Francisco 287° radial to Golden Gate Intersection, then Victor 150, and, depending on your altitude, they probably will give you a vector to intercept (Victor) 150 before you get to Golden Gate". This was also acknowledged. The Local Controller, who was also Tower Supervisor, noted the time of 0030 on his clock as the aircraft became airborne and passed the tower. An eyewitness observed the landing lights retracting as the aircraft crossed the end of the runway. However, several witnesses along the flight path, including some located at points just prior to the crash, saw both landing lights on. Landing lights of the L-1049H may be retracted flush with the lower wing surface and remain on until switched off. After take-off, witnesses stated the aircraft made a slight turn to the right, then a steeper turn to the left, and then was observed returning to a wings-level attitude as it entered the clouds. At 0030:22, the flight was advised to contact Departure Control and did so immediately. The Departure Controller advised the flight at 0030:57 that he had radar contact with it and requested it to report leaving thousand-foot altitudes. At 0031:05, the crew asked how they were tracking toward the GAP. The Departure Controller switched his radar scope from the 30 to the 10-mile setting and requested the flight's altitude. The crew!replied they were at 900 ft. At 0031:20, the Departure Controller advised that they were left of the San Francisco 287° radial. As he received no acknowledgement he repeated his message. The Departure Controller stated that within seconds after the second transmission, the target stopped, bloomed, and disappeared from the radar scope. Repeated attempts to communicate with the flight after its disappearance from the scope were unsuccessful. At this time, 0032:30, the controller placed a time hack on the communications tape. Ground impact was computed to have occurred at approximately 0031:30. Main impact occurred 860 ft above sea level on Sweeney's Ridge, at approximately 4.3 miles on the 257° radial of the SFO TVOR. The coordinates of the impact area were 122° 28' 00" W longitude and 37° 38' 28" N latitude. The aircraft disintegrated on impact and all three crew members were killed.
Probable cause:
The pilot, for undetermined reasons, deviated from departure course into an area of rising terrain where downdraught activity and turbulence affected the climb capability of the aircraft sufficiently to prevent terrain clearance.
Final Report:

Crash of a Grumman G-21A Goose off Avalon

Date & Time: Jul 13, 1964 at 0740 LT
Type of aircraft:
Operator:
Registration:
N4221A
Flight Phase:
Survivors:
Yes
Schedule:
Avalon – Long Beach
MSN:
1029
YOM:
1939
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7600
Captain / Total hours on type:
4100.00
Circumstances:
Shortly after takeoff from the Bay of Avalon, while climbing, the pilot apparently encountered engine problems. He elected to make an emergency landing but the seaplane was ditched and later sank. All 10 occupants were evacuated safely.
Probable cause:
The cause of the accident was undetermined.
Final Report:

Crash of a Boeing KC-135A-BN Stratotanker in the Death Valley National Park: 4 killed

Date & Time: Jul 8, 1964
Type of aircraft:
Operator:
Registration:
60-0340
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Larson - Larson
MSN:
18115
YOM:
1961
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The KC-135 was engaged in a refueling mission out from Larson AFB, Washington, and was carrying a crew of four. At an altitude of 26,000 feet, following a successful refueling mission of a USAF Republic F-105D-15-RE Thunderchief registered 61-0091, the crew of the KC-135 attempted to leave the area and the pilot-in-command made a turn to the right when the engine number four struck the cockpit window of the Thunderchief. Out of control, both aircraft dove into the ground and crashed in a mountainous area located in the Death Valley National Park. All four crew members on board the KC-135 as well as the pilot of the Thunderchief were killed.
KC-135 crew:
Cpt Thomas F. Dozier, pilot,
1st Lt Erwin W. Boelter Jr., copilot,
1st Lt Ronald D. Williams, navigator,
S/Sgt Robert J. Graves, boom operator.
Thunderchief pilot:
Cpt Leonard F. Reynolds.
Probable cause:
The exact cause of the midair collision remains unclear.