Crash of a Lockheed P-3B-75-LO Orion at Lemoore-Reeves Field AFB: 6 killed

Date & Time: Mar 6, 1969
Type of aircraft:
Operator:
Registration:
152765
Flight Type:
Survivors:
No
Schedule:
Lemoore - Lemoore
MSN:
185-5210
YOM:
1966
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The P-3 Orion aircraft was on a practice GCA approach to Lemoore-NAS/Reeves Field, CA (NLC). The aircraft nosed down at the approach end of the runway then flared nose high with an excessive sink rate. It touched down on the port main landing gear, then the starboard main landing gear, followed by the fuselage section just forward of the mad boom striking the runway. The port wing broke inboard of the #2 engine on or shortly after touchdown and separated from the fuselage. The fuselage slid down the runway and came to rest off the left side of the runway approximately 1100 feet from the approach end. The port wing continued approximately 300 feet beyond the fuselage. Both parts were engulfed in flame. All six occupants were killed.
Source: ASN
Probable cause:
The power levers were at the flight idle position at impact. Investigation concluded that an attempt was made to decrease the sink rate by establishing a nose high attitude prior to impact and the aircraft was in a stalled or near stalled condition with minimum power set.

Crash of a Douglas C-49J near Lone Pine: 35 killed

Date & Time: Feb 18, 1969 at 0510 LT
Type of aircraft:
Operator:
Registration:
N15570
Flight Phase:
Survivors:
No
Site:
Schedule:
Hawthorne - Burbank - Long Beach
MSN:
6320
YOM:
1943
Flight number:
HNA708
Crew on board:
3
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
35
Captain / Total flying hours:
16348
Captain / Total hours on type:
6000.00
Copilot / Total flying hours:
3445
Copilot / Total hours on type:
967
Aircraft flight hours:
48274
Circumstances:
While cruising by night under VFR mode, the crew changed his route from 170° to 195° direction Palmdale as they thought flying over the valley. Shortly later, the airplane struck a ridge and crashed down the slope of Mt Whitney (11,770 feet high) located about 12,5 miles west of Lone Pine. SAR operations were quickly conducted but eventually suspended few days later as no trace of the aircraft nor the 35 occupants was found. The wreckage was located in a very hazardous area on August 8, 1969 and was not detectable till this date due to snow accumulation on the ground. The accident was unsurvivable.
Probable cause:
The deviation from the prescribed route of flight, as authorized in the company's FAA-approved operations specifications, resulting in the aircraft being operated under IFR weather conditions, in high mountainous terrain, in an area where there was a lack of radio navigation aids.
Final Report:

Crash of a Lockheed SP-2E Neptune near El Toro MCAS: 7 killed

Date & Time: Feb 11, 1969 at 2023 LT
Type of aircraft:
Operator:
Registration:
131487
Flight Type:
Survivors:
No
Site:
Schedule:
El Toro - El Toro
MSN:
426-5368
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was completing a local training mission at El Toro MCAS. On approach by night, the crew failed to realize his altitude was too low when the right wing struck the top of ridge. The airplane crashed in the Harding Canyon located 7 miles northwest of the airbase. All seven crew members were killed.

Crash of a Boeing 727-22C off Los Angeles: 38 killed

Date & Time: Jan 18, 1969 at 1821 LT
Type of aircraft:
Operator:
Registration:
N7434U
Flight Phase:
Survivors:
No
Schedule:
Los Angeles – Denver – Milwaukee
MSN:
19891/631
YOM:
1968
Flight number:
UA266
Crew on board:
6
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
38
Captain / Total flying hours:
13665
Captain / Total hours on type:
1908.00
Copilot / Total flying hours:
6642
Copilot / Total hours on type:
1842
Aircraft flight hours:
1036
Circumstances:
Boeing 727-22C N7434U operated Flight 266 from Los Angeles to Denver, CO and Milwaukee, WI. The aircraft had been operating since January 15, 1969, with the No. 3 generator inoperative. This was allowed because according to the Minimum Equipment List, the aircraft is airworthy with only two generators operable provided certain procedures are followed and electrical loads are monitored during flight. Flight 266 was scheduled to depart the gate at 17:55, but was delayed until 18:07 because of the inclement weather and loading problems. The flight commenced its takeoff roll on runway 24 at approximately 18:17. At 18:18:30 the sound of an engine fire warning bell was heard in the cockpit. The crew reported a no. 1 engine fire warning and stated that they wanted to return to the airport. Shortly after shutdown of the No. 1 engine, electrical power from the remaining generator (No. 2) was lost. Following loss of all generator power, the standby electrical system either was not activated or failed to function. Electrical power at a voltage level of approximately 50 volts was restored approximately a minute and a half after loss of the No. 2 generator. The duration of this power restoration was just 9 to 15 seconds. The Boeing descended and struck the sea 11.3 miles west of the airport. The ocean depth at this point is approximately 950 feet.
Probable cause:
The loss of attitude orientation during a night, instrument departure in which all attitude instruments were disabled by loss of electrical power. The Board has been unable to determine (a) why all generator power was lost or (b) why the standby electrical power system either was not activated or failed to function.
Final Report:

Crash of a Rockwell Aero Commander 720 Alti Cruiser in Klamath River: 1 killed

Date & Time: Jan 18, 1969 at 1805 LT
Registration:
N4831C
Flight Phase:
Survivors:
No
Schedule:
Fresno - Eugene
MSN:
720-760-10
YOM:
1959
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
695
Captain / Total hours on type:
154.00
Circumstances:
While cruising by night in marginal weather conditions (rain and fog), the pilot informed ATC about an engine failure. Shortly later, the airplane went out of control, entered a dive and crashed near Klamath River, north of California. The wreckage was found a day later and the pilot, sole on board, was killed.
Probable cause:
It was determined that the probable cause of the accident was that the carburetor on one engine failed after encountering icing conditions. It was reported that the aircraft was not equipped with de-icing equipments.

Crash of a Douglas DC-8-62 off Los Angeles: 15 killed

Date & Time: Jan 13, 1969 at 1921 LT
Type of aircraft:
Operator:
Registration:
LN-MOO
Survivors:
Yes
Schedule:
Copenhagen – Seattle – Los Angeles
MSN:
45822/272
YOM:
1967
Flight number:
SK933
Crew on board:
9
Crew fatalities:
Pax on board:
36
Pax fatalities:
Other fatalities:
Total fatalities:
15
Captain / Total flying hours:
11135
Captain / Total hours on type:
900.00
Copilot / Total flying hours:
5814
Copilot / Total hours on type:
973
Aircraft flight hours:
6948
Circumstances:
The aircraft crashed in Santa Monica Bay, approximately 6 nautical miles west at 1921LT. The aircraft was operating as flight SK933 from Seattle, Washington, to Los Angeles, following a flight from Copenhagen, Denmark. A scheduled crew change occurred at Seattle for the flight to Los Angeles. The accident occurred in the waters of Santa Monica Bay while the crew attempting an instrument approach to runway O7R at Los Angeles International Airport. Of the 45 persons aboard the aircraft, 3 passengers and one cabin attendant drowned, 9 passengers and 2 cabin attendants are missing and presumed dead; 11 passengers and 6 crew members including the captain, the second pilot, and the systems operator, were injured in varying degrees; and 13 passengers escaped without reported injury. The aircraft was destroyed by impact. The fuselage broke into three pieces, two of which sank approximately 350 feet of water. The third section including the wings, the forward cabin and the cockpit, floated for about 20 hours before being towed into shallow water where it sank. This section was later recovered and removed from the water. The weather at Los Angeles International Airport was generally: 1,700 feet broken, 3,500 feet overcast; visibility 4 miles in light rain and fog, wind 060° at 10 knots; and the altimeter setting was 29.87 inches of mercury. The weather in the accident area was reported to be similar.
Probable cause:
The lack of crew coordination and the inadequate monitoring of the aircraft position in space during a critical phase of an instrument approach which resulted in an unplanned descent into the water. Contributing to this unplanned descent was an apparent unsafe landing gear condition induced by the design of the landing gear indicator lights, and the omission of the minimum crossing altitude at an approach fix depicted on the approach chart.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 200 in Santa Ana: 9 killed

Date & Time: Nov 23, 1968 at 1959 LT
Operator:
Registration:
N7666
Survivors:
No
Schedule:
Los Angeles - Santa Ana
MSN:
148
YOM:
1968
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
12276
Captain / Total hours on type:
234.00
Circumstances:
Following an uneventful flight from Los Angeles, the crew started the descent to Santa Ana Airport when he encountered poor visibility due low clouds and fog. On short final, the crew failed to realize his altitude was insufficient when the airplane struck a 30 feet steel light pole located along the Costa Mesa Freeway. Out of control, the airplane dove into the ground and crashed in flames 1,8 mile short of runway 20R threshold. The aircraft was totally destroyed and none of the nine occupants survived the crash.
Probable cause:
The accident was probably caused by the combination of the following factors:
- Improper IFR operation,
- The pilot-in-command misjudged altitude,
- Low ceiling and foggy conditions,
- Visibility limited to 3/4 mile or less.
Final Report:

Crash of a Convair CV-580 in Santa Barbara

Date & Time: Nov 12, 1968 at 1728 LT
Type of aircraft:
Registration:
N73135
Flight Type:
Survivors:
Yes
Schedule:
Santa Barbara - Santa Barbara
MSN:
85
YOM:
1968
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4741
Captain / Total hours on type:
866.00
Circumstances:
Following an uneventful training flight in the region of Santa Barbara Airport, the aircraft belly landed, slid for few dozen yards and came to rest on the runway. All four occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The accident was caused by the combination of the following factors:
- The student pilot failed to extend the landing gear on approach,
- Inadequate supervision of flight on part of the pilot-in-command,
- The crew failed to use the approach checklist,
- The landing gear warning horn was inoperative for undetermined reason.
Final Report:

Crash of a Grumman G-21A Goose off Avalon: 1 killed

Date & Time: Sep 29, 1968 at 1400 LT
Type of aircraft:
Registration:
N325
Flight Phase:
Flight Type:
Survivors:
No
MSN:
B127
YOM:
1945
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
14000
Captain / Total hours on type:
3000.00
Circumstances:
While flying at low height, the pilot lost control of the seaplane that crashed into the sea few dozen yards off Avalon. Few debris were found floating on water but the pilot's body was never found.
Probable cause:
Due to lack of evidences, the cause of the accident could not be determined.
Final Report:

Crash of a Lockheed L-1649A Starliner in Stockton

Date & Time: Sep 28, 1968 at 1613 LT
Type of aircraft:
Registration:
N8081H
Flight Type:
Survivors:
Yes
Schedule:
Stockton - Stockton
MSN:
1026
YOM:
1958
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training flight at Stockton Airport, California. Following several uneventful circuits, the crew initiated a new approach. On final, the crew failed to realize his altitude was too low when the right main gear struck a blast pad located 102 feet short of the runway threshold and was torn off. The airplane partially belly landed and slid for dozen yards before coming to rest. While all 11 occupants escaped uninjured, the aircraft was damaged beyond repair.
Probable cause:
The student pilot misjudged the distance and altitude on final and the pilot-in-command failed to supervise the flight adequately.
Final Report: