Crash of a Douglas C-47 in the Sandia Mountains: 9 killed

Date & Time: Apr 26, 1963
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Andrews - March
Crew on board:
4
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was performing a secret mission from Andrews AFB to March AFB. While overflying New Mexico, he encountered severe icing conditions. A wing fell off and the aircraft crashed in the Sandia Mountain Range located northeast of Albuquerque. All nine occupants were killed and the aircraft was destroyed. All USAF C-47's were grounded following this accident, until the struts had been replaced.
Probable cause:
Investigations revealed that a wing's guy broke in flight, probably when the airplane was flying in an area subject to severe icing.

Crash of a Douglas C-133B-DL Cargomaster at Travis AFB: 9 killed

Date & Time: Apr 10, 1963 at 1612 LT
Type of aircraft:
Operator:
Registration:
59-0523
Flight Type:
Survivors:
No
Schedule:
Travis - Travis
MSN:
45574
YOM:
1959
Crew on board:
9
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew was completing a local training flight at Travis AFB. After few circuits, the pilot-in-command started a new approach to runway 21L in poor weather conditions when control was lost. The airplane crashed in a huge explosion 0,8 mile short of runway threshold and was destroyed. All nine crew members were killed.

Crash of a Douglas R4D-8 in Millington

Date & Time: Mar 15, 1963 at 2040 LT
Operator:
Registration:
17158
Flight Type:
Survivors:
Yes
Schedule:
Saint Louis – Millington
MSN:
43368
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The approach to Millington was completed by night and in poor weather conditions. On final, the pilot declared an emergency as an engine failed. As the aircraft was not properly aligned with the runway, the crew elected to make a go around. A second attempt to land was completed in thunderstorm activity when the airplane stalled, hit a pecan tree and crashed in Hill Street, just near some houses. On ground, it lost its right wing and came to rest in flames. All 33 occupants evacuated safely while the aircraft was destroyed by fire.
Probable cause:
Engine failure on final.

Crash of a Boeing KC-135A-BN Stratotanker at Eielson AFB: 9 killed

Date & Time: Feb 27, 1963
Type of aircraft:
Operator:
Registration:
56-3597
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Eielson - Eielson
MSN:
17346
YOM:
1958
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The crew departed Eielson AFB, engaged in a routine refueling mission. Just after liftoff, while in initial climb, the engine number one failed. The airplane banked left and crashed in a huge explosion onto several buildings. All seven crew members and two people on the ground were killed. The aircraft and two buildings (the crew rest house and a guard local) were destroyed.
Probable cause:
Failure of the engine number one at takeoff.

Crash of a Curtiss C-46F-1-CU Commando at Thun Field AFB

Date & Time: Feb 16, 1963 at 1826 LT
Type of aircraft:
Operator:
Registration:
N616Z
Flight Type:
Survivors:
Yes
Schedule:
Ogden-Hill – Malmstrom – McChord – Portland – Ogden-Hill
MSN:
22590
YOM:
1942
Flight number:
VK060
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7003
Captain / Total hours on type:
1133.00
Copilot / Total flying hours:
2133
Copilot / Total hours on type:
300
Aircraft flight hours:
17683
Circumstances:
Zantop Air Transport, Inc., LOGAIR Flight 60-16 (VK060), a Curtiss C-40F, N616Z, crashed following an attempt to land on runway 17 at Thun Field, near Puyallup, Washington, at 1826 P.s.t., February 16, 1963. Both crew members survived the crash but were severely injured. There were no other occupants. The aircraft was destroyed by the impact and post-impact fire. An engine malfunction seven minutes after takeoff from McChord AFB, Washington, was followed by an unsuccessful attempt to feather the propeller and by intermittent overspeeding. During an attempted go-around from the landing approach the pilot lost control of the aircraft and crashed in a pasture approximately one-half tile northeast of Thun Field.
Probable cause:
The Board determines that the probable cause of this accident was the improper handling of an emergency situation, precipitated by a mechanical malfunction, which resulted in an unsuccessful single engine go-around. A contributing factor was the failure of Radar Approach Control to provide complete, accurate airfield data to the pilot.
Final Report:

Crash of a Boeing 720-051B in the Everglades National Park: 43 killed

Date & Time: Feb 12, 1963 at 1350 LT
Type of aircraft:
Operator:
Registration:
N724US
Flight Phase:
Survivors:
No
Schedule:
Miami – Chicago – Spokane – Seattle – Portland
MSN:
18354
YOM:
1961
Flight number:
NW705
Crew on board:
8
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
43
Captain / Total flying hours:
17835
Captain / Total hours on type:
150.00
Copilot / Total flying hours:
11799
Copilot / Total hours on type:
1093
Aircraft flight hours:
4684
Circumstances:
The aircraft arrived in Miami at 1240, following a routine flight from Chicago, Illinois The captain of the inbound flight reported that the only mechanical discrepancy was, "the outflow valves being a little sticky merely made it a little difficult to maintain the pressurization in a smooth manner. "These valves were cleaned, and a leaking rivet at the No. 4 reserve fuel tank was plugged when it was noticed by the mechanic. This was the only maintenance performed during the "turnaround". Flight 705 is regularly scheduled from Miami. to Portland, Oregon, with intermediate stops at Chicago, Illinois and Spokane and Seattle, Washington. The computed takeoff gross weight of 175,784 pounds, and center of gravity (e.g.) of 25 percent mean aerodynamic chord (MAC) were both well within the allowable limits. Prior to departing the ramp at 1325, the crew asked the ground controller about the departure routes being utilized, and he replied that most flights were departing ". . either through a southwest climb or a southeast climb and then back over the top of it. . . "The flight departed Miami with an Instrument Flight Rules (IFR) clearance at 1335 In accordance with the pilot's request for a". . . southeast vector "a left turn was rude after takeoff from runway 27L and circuitous routing was utilized in conjunction with radar vectors from Miami Departure Control, to avoid *** of anticipated turbulence associated with thunderstorm activity (See Attachment A). A similar departure pattern had been previously flown by another flight Subsequently, while maintaining 5,000 feet and a heading of 300 degrees, Flight 705 requested clearance to climb to a higher altitude. Following a discussion between the flight and the Federal Aviation Agency (FAA) radar departure controller about the storm activity, and while clearance to climb was being coordinated with the Miami Air Route Traffic Control Center (ARTCC), the flight advised "Ah-h we're in the clear now. We can see it out ahead . . . looks pretty bad." At 1343, Flight 705 was cleared to climb to flight level 2/ 250 (FL250). They responded, "OK ahhh, we'll make a left turn about thirty degrees here and climb. . "The controller asked of 270 degree was their selected climbout heading, and they replied that this would take them". . . out in the open again". . Accordingly, clearance was granted. Following some discussion about the severity of the turbulence, which was described as moderate to heavy, the flight advised, "OK, you better run the rest of them off the other way then." At 1345 radar service was terminated and control of Flight 705 was transferred to Miami ARTCC. When the flight did not establish radio communication with ARTCC on the initial frequency, Departure Control provided a secondary frequency, and instructed the flight to turn to a heading of 360 degrees which was acknowledged. When Miami ARTCC requested position and altitude, the flight replied, "We're just out of seventeen five (17,500 feet) and standby on the DME one." This transmission ended at 1348, and was the last known communication with Flight 705 The voice transmissions emanating from the flight were made by the first officer. Witnesses in the area reported that a loud explosion had occurred in the air, and several felt a subsequent ground tremor. They also reported that heavy rain had been failing in the area. One witness, in company with five other persons, was seven miles south of the main wreckage site She heard the sound of an explosion which had no echo. When she looked in that direction she saw an orange ball of flame in the edge of a cloud. As she directed the attention of her companions toward this flame, it dropped straight down, becoming a streak, and disappeared behind trees. Shortly after the disappearance a second sound was heard. Statements were received from the crews of four other flights operating in the Miami area at the approximate time of the accident. The first, in a large jet which approached Miami from the west at 7,000 feet, reported the weather as ". . . in and out of broken clouds and light rain showers with light turbulence. Darker heavy shower activity was observed to the (south) of course. We observed no small cells on our radar scope. . only a broad rain area. . . "Another crew, in a four-engine aircraft, departed Miami at 1318, via a departure pattern similar to that which Flight 705 later followed. They described the worst turbulence as". medium to moderate . . . "from west of the airport to north of the Miami VORTAC .3/ They were maintaining 5,000 feet at the time. A third crew in a 720B was folding southeast of Miami at 13,000 feet. They observed numerous rain cells on radar in the Miami area and encountered light ice at this altitude. The fourth crew, also flying a large jet, taxied out shortly after Flight 705 but delayed takeoff for nearly an hour because of the weather. The weather in the Miami area at the time of the accident was characterized by a pre-frontal squall line approximately 250 miles in length, oriented on a northeast-southwest line immediately northwest of Miami (See Attachment A). The U. S. Weather Bureau (USWB) radar observation at Miami at 1344 indicated a broken area of thunderstorms associated with this line, with cells two to twenty miles in diameter, and tops of detectable moisture at 30,000 feet. The line was moving southeast at eight knots, and moderate rain showers were occurring at the station. The 0600 and 1800 Miami radiosonde ascents showed the freezing level to have been at 11,100 and 12,400 feet m.s.1., respectively. SIGMET 4/ No. 3 prepared by the USWB at Miami, valid from 0900-1300, forecast moderate to severe turbulence 5/ in thunderstorms, with a chance of extreme turbulence in heavier thunderstorms. This advisory was called to the attention of the crew of Flight 705 by the operations agent at Miami, and was attached to their dispatch papers. SIGMET No. 4, valid from 1300-1700, was not received until approximately 1315, after the crew of Flight 705 had left the operations office. It forecast moderate to severe turbulence, but deleted the reference to extreme turbulence indicated in SIGMET No 3. Since the dispatcher for this flight is stationed in Minneapolis, the physical Limitations involved made it difficult to apprise the crew of this latest advisory prior to their taxi time of 1325. The aircraft was completely destroyed by impact forces and all 43 occupants have been killed.
Probable cause:
The Board determines that the probable cause of this accident was toe unfavorable interaction of severe vertical air drafts and large longitudinal control displacements resulting in a longitudinal "upset" from which a successful recovered was not made.
Final Report:

Crash of a Convair C-131E at Ogden-Hill AFB: 1 killed

Date & Time: Feb 4, 1963
Operator:
Registration:
55-4758
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Ogen-Hill - Norton
MSN:
345
YOM:
1956
Crew on board:
2
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Shortly after rotation, while in initial climb, one of the engine failed. The crew feathered the propeller and the captain decided to make an emergency landing. The aircraft belly landed and slid for several before coming to rest in flames in a gully located 4 miles southeast of the airfield. A passenger died while 19 other occupants were rescued. The aircraft was destroyed.
Probable cause:
Engine failure during initial climb.

Crash of a Lockheed L-1049H Super Constellation in San Francisco: 4 killed

Date & Time: Feb 3, 1963 at 1207 LT
Operator:
Registration:
N9740Z
Flight Type:
Survivors:
Yes
Schedule:
Norfolk – Dallas – China Lake
MSN:
4851
YOM:
1958
Flight number:
SL40Z
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
18000
Captain / Total hours on type:
882.00
Copilot / Total flying hours:
18600
Copilot / Total hours on type:
232
Aircraft flight hours:
4257
Circumstances:
A Slick Airways Lockheed 1049H, N9740Z, crashed and burned during an ILS approach to runway 28R at the San Francisco International Airport at approximately 1207 P.s.t., February 3, 1963. Due to an inoperative glide slope receiver, the crew was listening radar advisories on the localizer receiver for altitude information. The aircraft struck approach lights 1,170 feet from the runway threshold, climbed to about 200 feet and then crashed approximately 1,900 feet beyond the threshold and on the left edge of runway 28L. Of the three crew members and five passengers aboard, the captain, first officer, and two passengers received fatal injuries. The remaining persons aboard received serious injuries. The aircraft was destroyed by subsequent fire.
Probable cause:
The Board determines the probable cause of this accident was the continuation of an instrument approach after adequate visual reference was lost below authorized minimums. Inadequate monitoring of the instrument approach by the PAR controller was a contributing factor.
Final Report:

Crash of a Boeing B-52E-90-BO Stratofortress near Mora: 2 killed

Date & Time: Jan 30, 1963 at 0500 LT
Type of aircraft:
Operator:
Registration:
57-0018
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Walker - Walker
MSN:
17412
YOM:
1957
Location:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a training mission our from Walker AFB by night when the tail broke off in turbulence. Four crew members ejected before the aircraft crashed into the Sangre de Christo Mountain Range, some 10 miles northwest of Mora. Two crew members were killed.
Crew:
Four crew survived:
Lt Col Donald Hayes, pilot,
Maj Thomas J. McBride, copilot,
Maj Emil Goldbeck, navigator,
Lt Col Nicholas Horangic, radar operator,
Maj George Szabo, weapons systems operator, †
M/Sgt Harvey Burl Dean, tail gunner. †

Crash of a Vickers 812 Viscount in Kansas City: 8 killed

Date & Time: Jan 29, 1963 at 2244 LT
Type of aircraft:
Operator:
Registration:
N242V
Survivors:
No
Schedule:
Midland – Lubbock – Wichita Falls – Lawton – Oklahoma City – Tulsa – Kansas City
MSN:
356
YOM:
1958
Flight number:
CO290
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
18611
Captain / Total hours on type:
3409.00
Copilot / Total flying hours:
5761
Copilot / Total hours on type:
2648
Aircraft flight hours:
12860
Circumstances:
Continental Air Lines Flight 290, a Viscount 812, N242V, a regularly flight from Midland, Texas, crashed at the Kansas City Municipal Airport, Kansas City, Missouri, at 2244 c. s. t., January 29, 1963. All the occupants, three crew members and five passengers, received fatal injuries and the aircraft was destroyed by impact and subsequent fire. After making a straight-in approach to land on runway 18, in visual flight conditions, the aircraft continued to fly over the runway in a nose-up attitude without touching down. Near the south end of the runway, from an altitude of approximately 90 feet, the aircraft nosed over sharply, wings level, and dived into the ground. The main wreckage came to rest 680 feet beyond the end of the runway.
Probable cause:
The Board determines that the probable cause of this accident was an undetected accretion of ice on the horizontal stabilizer which, in conjunction with a Specific airspeed and aircraft configuration, caused a loss of pitch control.
Final Report: