Crash of a Convair B-36B-1-CF Peacemaker at Fairchild AFB: 7 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
44-92032
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Fairchild - Fairchild
MSN:
29
YOM:
1946
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The crew was completing a local training mission at Fairchild AFB. During an aborted takeoff, the airplane crashed in unclear circumstances. Seven crew members were killed and three others were injured.

Crash of a Fairchild C-119F-FA Flying Boxcar in Lothian: 18 killed

Date & Time:
Operator:
Registration:
51-7993
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oklahoma City – Bolling – Mitchel
MSN:
10732
YOM:
1951
Crew on board:
6
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
18
Circumstances:
While cruising under VFR in poor weather conditions, the crew contacted ATC and requested the permission to continue under IFR. Awaiting the permission, the pilot-in-command lost control of the airplane that dove into the ground and crashed in Lothian, about 14 miles east of Andrews AFB. All 18 occupants were killed.
Probable cause:
It was determined that weather conditions were poor at the time of the accident and that the crew should never start the flight under VFR rules. While cruising under VFR rules in IFR conditions, the crew lost control of the aircraft.

Crash of a Convair CV-340-35 in Midland

Date & Time:
Type of aircraft:
Operator:
Registration:
N90853
Flight Phase:
Survivors:
Yes
Schedule:
El Paso – Midland – Kansas City
MSN:
44
YOM:
1953
Flight number:
CO046
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11038
Captain / Total hours on type:
620.00
Copilot / Total flying hours:
2742
Copilot / Total hours on type:
659
Aircraft flight hours:
3099
Circumstances:
At 0833 Trip 46 was cleared to Runway 10 for takeoff. At this time the aircraft carried 585 gallons of fuel and was loaded to a gross takeoff weight of 36,345 pounds which was 10,655 pounds less than the maximum allowable. The load was properly distributed so that the center of gravity of the aircraft was within the approved limits. A pre-takeoff check was conducted adjacent to Runway 10 at which time the propellers, engines and instruments gave normal Indications. A part of this check included moving the control column fore and aft and turning the wheel left and right in order to check the control system for freedom of movement and full travel. At 0838 the flight was cleared for takeoff which was made using normal takeoff power. Immediately after becoming airborne the crew noted a slight vibration which was attributed to an unbalanced condition of the spinning main landing gear wheels. Captain Persing applied brakes during the landing gear retraction to eliminate this vibration; however, it not only continued but rapidly increased in severity. The aircraft reached an altitude of approximately 75 feet, the highest attained, and was near the airport boundary when the vibration stopped with a sudden jolt and the aircraft assumed a nose-down attitude. The first officer immediately sensing the situation joined the captain and both exerted their entire strength applying back pressure to their respective control columns to keep the aircraft from plunging into the ground. The captain quickly reduced power; however, the nose-down pressure could not be completely overcome. The first officer used nose-up trim control in an effort to relieve the nose-down pressure; this action had no appreciable effect and during the last attempt the trim tab control wheel appeared to be stuck. The captain established a shallow left turn with the thought of returning to the airport and continued the turn about 45 degrees from the takeoff heading. As air speed decreased power was momentarily increased whereupon it became evident to the crew that using power sufficient to maintain flight resulted in an insurmountable nose-down pressure. The captain therefore decided to make a wheels-up landing straight ahead. Close to the ground the first officer closed the throttles and the captain pulled the electrical crash bar. Contact with the ground followed with the aircraft in a near-level attitude and at approximately 100 m.p.h. Although the passengers and crew received injuries of varying degrees, they were able to get out of the aircraft unassisted in an orderly manner. The evacuation was mainly through the rear service door (emergency exit) and was accomplished in about 30 seconds. There was no fire.
Probable cause:
The Board determines that the probable cause of this accident was loss of control due to a failure of the right elevator trim tab push-pull rod caused by a reversed installation of the right elevator trim tab idler as a result of the carrier’s reliance on the Manufacturers Illustrated Parts Catalog as a maintenance reference. The following findings were reported:
- Immediately following a normal takeoff the right elevator trim tab push-pull rod failed and the stub end became wedged, holding the trim tab in a full-up or aircraft nose-down position,
- The trim tab position resulted in the crew being unable to control the aircraft and a wheels-up landing resulted,
- The push-pull rod failed as a result of excessive stresses caused by interference resulting from a reversed idler installation,
- The right elevator trim tab assembly as removed, reinstalled, inspected and functionally checked by company maintenance personnel 14:40 flight hours prior to the accident,
- Correct positioning of the right idler component could not be determined from the Maintenance Manual figure, 7.4.101, which the carrier considered appropriate for the installation,
- The Manufacturers Illustrated Parts Catalog was used in accordance with company policy as an installation reference to determine the idler position,
- Under conventional interpretation of the appropriate exploded diagram of the Parts Catalog, the idler was installed in reverse,
- The Illustrated Parts Catalog was not intended and should not have been used as a maintenance reference.
Final Report:

Crash of a Douglas JD-1 Invader in El Centro: 2 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
77172
Flight Phase:
Flight Type:
Survivors:
No
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was performing a combined exercice with other aircraft. In flight, the Invader collided with a USAF North American F-86 Sabre. Out of control, it dove into the ground and crashed in El Centro, killing both crew members.

Crash of a Fairchild C-119G Flying Boxcar in Huntingdon: 4 killed

Date & Time:
Operator:
Registration:
52-5894
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Fort Benning - Fort Benning
MSN:
11061
YOM:
1952
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
1188
Captain / Total hours on type:
436.00
Copilot / Total flying hours:
444
Copilot / Total hours on type:
104
Circumstances:
The crew left Fort Benning-Lawson AFB in Columbus, Georgia, at 1334LT on a training flight to Maxwell AFB, Montgomery, Alabama. The training program consisted of approaches, touch and goes and landings. After takeoff from Fort Benning, the captain decided to modify his schedule and flew to the northwest to Huntingdon, Tennesse, where he came from. This city is more than 300 miles northwest from Fort Benning. Approaching Huntingdon, the captain reduced his altitude and completed a first low pass over the city. Few minutes later, at a speed of 230 knots, he made a second low pass over the city when the plane hit the roof of a house and disintegrated on a field. All four crew members were killed while nobody on the ground was injured.
Crew:
1st Lt Jack C. Jenkins, pilot,
2nd Lt John C. Peachey, copilot,
A2c Franklin D. Levy, flight engineer,
A2c David A. Probus, flight engineer.
Probable cause:
The aircraft disintegrated as a result of stress applied beyond the designed load limits. Inspection of the engines disclosed no malfunction of the power recovery turbines. The pilot violated several procedures by operating an aircraft in a careless and reckless manner, by flying over a congested area at less than 2,000 feet above the highest obstacle within a radius of 2,000 feet, by disregarding established boundaries of the local flying area and proceeding to a point approximately 170 nautical miles outside of the prescribed flying area while operating on a local flight clearance. In addition, the pilot failed to follow instructions for accomplishing scheduled crew training published by squadron training directive and as briefed by the Squadron Operations Officer. The pilot had made two extremely low and high speed passes over the town of Huntingdon.
Final Report:

Crash of a Convair CV-240-1 near Wright: 9 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
N8407H
Flight Phase:
Survivors:
No
Schedule:
Los Angeles – Las Vegas – Cedar City – Salt Lake City – Casper – Rapid City – Minneapolis
MSN:
37
YOM:
1948
Flight number:
WA034
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
7500
Captain / Total hours on type:
4634.00
Copilot / Total flying hours:
6850
Copilot / Total hours on type:
2300
Aircraft flight hours:
12145
Circumstances:
Western Air Lines' Flight 314 departed Los Angeles, California, on a scheduled flight to Minneapolis, Minnesota, with intermediate stops scheduled at Las Vegas, Nevada; Cedar City and Salt Lake City, Utah; Casper, Wyoming, and Rapid City, South Dakota. The flight was routine to Salt Lake City, where a relief crew consisting of Captain M. R. Cawley, First Officer R. E. Crowther and Stewardess Mary Grace Creagan took over the flight in accordance with company crew assignment schedules. Prior to departure from Salt Lake City the aircraft was refueled to a total of 1,000 gallons, which filled all tanks, Flight 34 departed from the Salt Lake City ramp at 0721, but returned a few minutes later because of a broken nose wheel steering cable. The cable was replaced and Flight 34 was off the ground at 0850. According to company records, at takeoff the gross weight was 36,990 pounds, 2,144 pounds less than the maximum allowable weight of 39,134 pounds; the load was properly distributed so that the center of gravity of the aircraft was within approved limits. There were an passengers. The flight plan filed with Air Route Traffic Control specified Instrument Flight Rules at 15,000 feet via Green 3 and Blue 76 Airways. Eastward from Salt Lake City the Casper weather went below company minimums and Flight 34 elected to overfly this scheduled stop. After being advised of this action by the company Casper radio, Air Route Traffic Control issued a new clearance for the flight to descend to and maintain 13,000 feet to the Rapid City range station via Blue 37 and Red 2 Airways. However, an altitude change to 17,000 feet was requested by the flight and this was authorized by ARTC. At 1010 N8407H reported 17,000 over Casper, estimating the Wright intersection (122 miles west of Rapid City) at 1027. The Flight reported as being over the Wright intersection at 1025, at 17,000 feet, estimating Rapid City at 1050. The Casper company radio operator gave the flight the 0930 en route weather and the 1010 Rapid City Special #2 terminal weather. This, the last radio contact, was acknowledged by the flight at 1027. At 1041 the Rapid City radio operator attempted unsuccessfully to contact the flight to deliver a clearance for an instrument approach to Rapid City. Attempts continued until 1053 and at that time the Denver company dispatcher was advised that contact with the flight had been lost. At 1106 emergency procedures were initiated. Intermittent snows and restricted visibilities hampered intensive air search efforts. The wreckage was sighted by a Western Air Lines pilot the afternoon of February 28, and ground parties reached the scene that night. The aircraft had crashed in an isolated ranch area and all nine occupants had been killed.
Probable cause:
The Board, after intensive study of all evidence, determines that the probable cause of this accident was a sudden emergency of undetermined origin under adverse weather conditions resulting in rapid descent and impact with the ground at high speed. The following findings were reported:
- Weather was a major factor in the accident as heavy to possibly severe turbulence and heavy icing existed in the area,
- The flight was routine until approximately five minutes before the crash,
- A sudden emergency or difficulty of undetermined origin occurred that resulted in rapid descent to the ground; no emergency was declared,
- Both engines were developing power at impact,
- Due to the disintegration of the wreckage it was impossible to definitely determine if structural failure or control malfunctioning had occurred prior to impact.
Final Report:

Ground fire of a Convair B-36B-15-CF Peacemaker at Fairchild AFB

Date & Time:
Type of aircraft:
Operator:
Registration:
44-92069
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Fairchild - Fairchild
MSN:
66
YOM:
1946
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful training mission, the crew was returning to Fairchild AFB. After touchdown, the pilot completed the braking procedure and vacated the runway via a taxiway when one of the main landing gear collapsed. The aircraft came to a halt in flames and while all occupants were able to evacuate safely, the aircraft was completely destroyed by fire. It was reported that one of the undercarriage collapsed and punctured a fuel tank. The fire could not be extinguished in time.
Probable cause:
Undercarriage collapsed during taxi.

Crash of a Fairchild C-82A Packet in Yelm

Date & Time:
Type of aircraft:
Operator:
Registration:
48-0569
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
10204
YOM:
1948
Location:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
An engine failed in flight, forcing the crew to attempt an emergency landing. The airplane belly landed in a field located one mile north of Yelm and came to rest. There were no casualties but the aircraft was written off.
Probable cause:
Engine failure.

Crash of a Douglas C-47D near Curry: 10 killed

Date & Time:
Operator:
Registration:
45-0895
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Fort Wainwright - Elmendorf
MSN:
16898/34155
YOM:
1945
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
While flying in freezing rain, the airplane crashed on the slope of a mountain located about 20 miles north of Curry, in the Denali National Park. Six occupants were rescued while ten others were killed.

Crash of a Lockheed P2V-5 Neptune near Barbers Point NAS: 8 killed

Date & Time:
Type of aircraft:
Operator:
Registration:
124874
Flight Type:
Survivors:
No
Site:
Schedule:
Iwakuni - Barbers Point
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
8
Circumstances:
During a night approach to Barbers Point NAS, the pilot-in-command decided to make a go around for unknown reason. He completed a turn to the left when the airplane hit the slope of Mt Pu'u Kaua (3,127 feet high) located northwest of the Naval Air Station. The airplane was destroyed upon impact and all eight crew members were killed.
Crew:
Lt Walter J. Hanzo Jr., pilot,
Ens Gerald Martin Hazlett, copilot,
Ens Wilbur D. Cooper,
Adc John Robert Staples,
Ad2 Joseph Daniel Beczek,
Am2 Paul Martin Kohler,
At2 Joseph Michael Maksymon,
At3 Richard Knuton Brown.
Probable cause:
Failure of the pilot to follow the published procedure while turning to the left during an attempt to go around instead of turning to the right over the ocean to avoid any obstacle. A reduced visibility caused by night remains a contributory factor.