Crash of a Douglas B-26B in Union City: 4 killed

Date & Time: Oct 3, 1955 at 2117 LT
Type of aircraft:
Operator:
Registration:
N67148
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Bridgeport – White Plains – LaGuardia – Tulsa
MSN:
29229
YOM:
1944
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
The aircraft departed Bridgeport, Connecticut, for California at 1245LT carrying two crew members. Two stops were then made at White Plains,N. Y. and at LaGuardia Field where 2 passengers boarded the aircraft. At 1346 the flight left La Guardia for Tulsa, Oklahoma, under Visual Flight Rules and no flight plan was filed. At Tulsa the aircraft was refueled with 906 gallons of gasoline which filled to capacity both main tanks, the nose tank and the rear fuselage tank. After the pilots were briefed by the Tulsa U.S. Weather Bureau Office, an Instrument Flight Rules flight plan was filed with the Air Route Traffic Centre. At 2114LT Oklahoma City Airway Communications Station received a call from the flight on 126.7 mcs requesting cancellation of the IFR flight plan and asking for a landing clearance at Oklahoma City. The flight was given the special 2100LT weather as 10,000 feet overcast, sky partially obscured, fog. visibility 1-1/2 miles, and was advised to contact RAPCON (Radar Approach Control) on 119.3 mcs for a clearance to land as IFR conditions prevailed. The crew advised that it desired clearance for Will Rogers Field. This was the last radio contact with the aircraft. It crashed at 2117LT 2 3/8 miles northwest of Union City, Oklahoma, and 23 miles west of Will Rogers Field, Oklahoma City. Two explosions were heard in the air prior to the crash and portions of the empennage and fuselage were found along the last 3 miles of the flight path. All four occupants were killed, among them George Skakel Sr., founder of Great Lakes Carbon Corporation and his wife Ann.
Probable cause:
The probable cause of this accident was the loss of the aircraft's empennage as a result of an in-flight fuel explosion in the aft section of the fuselage. Investigation recent A-26 accident indicates possible fire and explosion hazard in rear fuselage area. For all A-26-B and A-26-C aircraft having rear fuselage tank installed in same compartment with electrical components liable to sparking the following restriction is mandatory until further notice. Rear fuselage fuel tank shall be drained, purged, and marked to prohibit use. Placard cockpit fuel controls and filler cap for information pilot and servicing personnel.
Final Report:

Crash of a Douglas SC-47D in Burns: 7 killed

Date & Time: Sep 24, 1955
Operator:
Registration:
43-16145
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Selfridge - Reno
MSN:
20611
YOM:
1944
Location:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
Enroute from Selfridge AFB, Michigan, to Reno-Stead Airport, the crew encountered poor weather conditions and lost control of the airplane that crash near Burns. All seven crew members were killed.

Crash of a Boeing KC-97F-17-BO Stratotanker at Dow AFB

Date & Time: Sep 20, 1955
Type of aircraft:
Operator:
Registration:
51-0373
Flight Type:
Survivors:
Yes
MSN:
16440
YOM:
1951
Location:
Crew on board:
12
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On touchdown, the airplane went out of control and burst into flames. While all 12 crew members were evacuated safely, the aircraft was destroyed by fire.

Crash of a North American TB-25N Mitchell at Mitchel AFB: 6 killed

Date & Time: Sep 13, 1955 at 0830 LT
Operator:
Registration:
45-8822
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Mitchel – Wright-Patterson
MSN:
108-47673
YOM:
1945
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Shortly after takeoff from Mitchel AFB, while climbing to a height of about 300 feet, the crew informed ground about the failure of the right engine. The crew elected to make an emergency landing when the aircraft crashed in a cemetery in Uniondale, bursting into flames. All six occupants were killed.
Crew:
Maj James D. Judy, pilot,
Cpt Richard E. Hall.
Passengers:
Lt Col Morris I. Fass,
S/Sgt John I. Jackson Jr.,
Lee Rogow,
Larry J. Rubrecht.
Probable cause:
Failure of the right engine for unknown reasons.

Crash of a Douglas DC-3C in Burbank: 3 killed

Date & Time: Sep 8, 1955 at 0757 LT
Type of aircraft:
Registration:
N74663
Survivors:
Yes
Schedule:
Burbank – Oakland
MSN:
6257
YOM:
1943
Flight number:
CRR024
Crew on board:
3
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4500
Captain / Total hours on type:
1200.00
Copilot / Total flying hours:
2880
Copilot / Total hours on type:
120
Aircraft flight hours:
9849
Circumstances:
This was a nonscheduled flight originating at Burbank, California, for Oakland, California. There were 30 passengers and a crew consisting of Captain Joseph A. Bradsher, Copilot Keith C. Dutson, and Stewardess Utta Jorgensen. Company records indicated that takeoff gross weight was 26,089 pounds (authorized maximum was 26,200 pounds), and the center of gravity of the aircraft was located within prescribed limits. A Defense Visual Flight Rules flight plan was filed; the plane was loaded, taxied to the end of the runway, and its engines were run up. At 0751 the flight was cleared for takeoff from runway 15, to climb westward on top of haze and smoke. It executed a takeoff and climbed in a normal manner into smoke haze, which was more dense toward the south., and in which it was lost to view of observers at the airport. Approximately one minute 2 after takeoff (0752) Flight 24 called the tower and requested an emergency landing clearance. This was granted; runway 7 was suggested by the tower and accepted by the pilot. The airport was cleared of traffic and emergency equipment alerted. At 0755 the tower called repeatedly as the flight had not been sighted. At 0756 the flight called the tower and stated its intent to land on runway "31." Lockheed Air Terminal has no runway 31 but has a runway 33. About this time Flight 24 was sighted by the control tower operator an estimated one mile to the southwest proceeding in a nose-high attitude toward the airport but not aligned with any runway. Across the approach track being used was a powerline about 500 feet short of the airport boundary. As this line approached the nose-high attitude increased and immediately after passing this powerline the aircraft executed a slight left turn, banked 10 to 12 degrees. The left wing then struck a service powerline at the airport boundary. The aircraft stalled, its left wing collided with two parked Air Force C-54's, it cartwheeled, slid across the apron and struck Lockheed Service hangar No. 24, coming to rest in the open doorway of that hangar. The fuselage broke open at a point behind the wing and most of the survivors escaped or were rescued through this opening. Small fires started by the crash were quickly extinguished by personnel of Lockheed's plant protection organization, who also rescued survivors and rendered first aid most efficiently. This organization also guarded the scene and wreckage.
Probable cause:
On the basis of all available evidence the Board determines that the probable cause of this accident was the captain's irrevocable commitment to a landing without radio or visual confirmation of his runway alignment following engine failure immediately after takeoff. A contributing factor was engine malfunction immediately after takeoff in near minimum visibility. The following findings were reported:
- Overheating of the right engine's rear master rod and loss of much of its bearing metal constituted a failure which foretold imminent internal destruction of that engine,
- Feathering of the right propeller was not accomplished and that propeller continued to rotate (windmill),
- The aircraft when observed approaching the airport had its gear extended, its attitude was excessively nose-high, and it was not aligned with any runway,
- The left wing of the aircraft struck a powerline,
- Forward motion continued; the aircraft stalled and collided successively with two parked Air Force aircraft, the apron, and Lockheed Service Hangar No. 24.
Final Report:

Crash of a Kaiser-Frazer C-119J Flying Boxcar in Alexandria: 3 killed

Date & Time: Sep 6, 1955
Operator:
Registration:
51-8142
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
145
YOM:
1952
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
During initial climb, the aircraft suffered an engine failure, stalled and crashed 3 miles north of Alexandria Airport. Three crew members were killed and three others were injured.
Probable cause:
Engine failure shortly after takeoff.

Crash of a Douglas C-124C Globemaster II at Kirtland AFB: 1 killed

Date & Time: Sep 6, 1955
Operator:
Registration:
50-0097
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Kirtland - March
MSN:
43235
YOM:
1950
Crew on board:
9
Crew fatalities:
Pax on board:
60
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The takeoff was attempted in strong cross winds. During the takeoff roll, the aircraft deviated from the runway centerline. Despite corrections on part of the flying crew, the four engine aircraft veered off runway and came to rest. A passenger was killed while few others were injured.

Crash of a Douglas VC-47D in Skwentna: 12 killed

Date & Time: Sep 1, 1955
Operator:
Registration:
45-0893
Flight Type:
Survivors:
No
Schedule:
Elmendorf – Nome
MSN:
16896/34153
YOM:
1945
Location:
Crew on board:
5
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
12
Circumstances:
Enroute from Elmendorf AFB to Nome, the crew encountered engine problems and decided to divert to Skwentna Airport for an emergency landing. On short final, the airplane went out of control and crashed one mile short of runway. All 12 occupants were killed in the crash.
Probable cause:
Engine problems.

Crash of a De Havilland L-20A Beaver near Safford: 1 killed

Date & Time: Aug 25, 1955
Type of aircraft:
Operator:
Registration:
52-6100
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
473
YOM:
1953
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
Crashed in unknown circumstances in a mountainous area located about 13 miles north of Safford. The pilot Wilfred P. Champlain, sole on board, was killed.

Crash of a Kaiser-Frazer C-119F Flying Boxcar in Charleston: 9 killed

Date & Time: Aug 23, 1955 at 0200 LT
Operator:
Registration:
51-8165
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Charleston - Charleston
MSN:
168
YOM:
1952
Crew on board:
11
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
Shortly after a night takeoff at Charleston Airport, while climbing, one of the engine caught fire and exploded. The airplane lost height and crashed in flames onto several houses located in a residential area, some 1,7 mile from the airfield. Six crew members were seriously injured while five others were killed. Four people in the houses were killed as well.
Probable cause:
Engine explosion during initial climb for unknown reason.