Crash of a Rockwell Aero Commander 520 in Gary

Date & Time: Aug 14, 1966 at 1545 LT
Operator:
Registration:
N1914
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Gary - Gary
MSN:
520-122
YOM:
1953
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was engaged in a local training flight in Gary, Indiana, simulating engine failure. En route, one of the pilot voluntarily cut one of the engine to simulate a failure. After few seconds, he was unable to restart the engine nor to raise the gear and due to an insufficient speed, the airplane stalled and crashed in a gravel pit. The aircraft was destroyed and all three occupants were injured.
Probable cause:
The crew failed to follow the approved procedures. Improper emergency procedures.
Final Report:

Crash of a BAc 111-203AE in Falls City: 42 killed

Date & Time: Aug 6, 1966 at 2312 LT
Type of aircraft:
Operator:
Registration:
N1553
Flight Phase:
Survivors:
No
Schedule:
New Orleans – Shreveport – Fort Smith – Tulsa – Kansas City – Omaha – Minneapolis
MSN:
70
YOM:
1965
Flight number:
BN250
Crew on board:
5
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
42
Captain / Total flying hours:
20767
Captain / Total hours on type:
549.00
Copilot / Total flying hours:
9296
Copilot / Total hours on type:
685
Aircraft flight hours:
2307
Aircraft flight cycles:
2922
Circumstances:
Flight 250 was a scheduled domestic passenger/cargo flight from New Orleans, Louisiana, to Minneapolis, Minnesota, with intermediate stops at Shreveport, Louisiana, Fort Smith, Arkansas, Tulsa, Oklahoma, Kansas City, Missouri, and Omaha, Nebraska. The flight departed from New Orleans at 1835 hours CST and arrived at Kansas City without reported incident. It departed from Kansas City at 2255 hours on an IFR clearance to Omaha via Jet Route 41 at FL 200. Just prior to take-off, the flight was restricted to 5 000 ft due to conflicting traffic. When the flight was about 12 miles north of Kansas City, control of the aircraft was transferred to the Kansas City Air Route Traffic Control Centre (ARTCC). Radar contact was confirmed and the flight was cleared to climb to and maintain FL 200. After some discussion with ARTCC about the weather the flight crew advised that they would like to maintain 5 000 ft to Omaha. They reported they were at 6 000 ft and ARTCC cleared the flight to maintain that altitude until 5 000 ft was available. At 2303 hours the Kansas City ARTCC initiated a transfer of control of the flight to the Chicago ARTCC but before the transfer could be accomplished the flight requested and received permission from the Kansas City controller to deviate to the left of course. At 2306 hours the Kansas City controller cleared the flight to descend to and maintain 5 000 ft and contact the Chicago ARTCC. After some discussion of the weather as it was displayed on the Chicago controller's radar, the flight was advised that another Braniff flight, Flight 255, was on the same frequency and was at 10 000 ft climbing to 17 000 ft after departing Omaha. The crews of the two aircraft exchanged weather information and the crew of Flight 255 advised that they had encountered light to moderate turbulence from about 15 miles southeast of the Omaha airport and that it appeared they would be out of it in another 10 miles based on their radar observations. Flight 250 terminated this conversation at approximately 2308:30 hours. This was the last transmission received from the flight. Ground witnesses stated that they observed the aircraft approach and either fly into or over a shelf of clouds preceding a line of thunderstorms that was approaching frbm the north and northwest, and that shortly thereafter they saw an explosion in the sky followed by a fireball falling out of the clouds. The aircraft crashed at approximately 2312 hours, 7.6 statute miles on a true bearing of 024.50 from Falls City, Nebraska, at an elevation of 1 078 ft AMSL. All 42 occupants have been killed.
Probable cause:
The Board determined that the probable cause of this accident was in-flight structural failure caused by extreme turbulence during operation of the aircraft in an area of avoidable hazardous weather. The following findings were reported:
The aircraft was confronted with a severe squall line which was oriented across its intended flight route. This system was adequately forecast and reported by the Weather Bureau; however, the company forecast was somewhat inaccurate with respect to the number and intensity of thunderstorms and the intensity of the associated turbulence in the system. The crew was aware of the forecast weather and was aware that the system could have been circumnavigated to the west. This was, in fact, suggested by the co-pilot.
Because the company forecast did not predict a solid line of thunderstorms, the company dispatcher did not take any action to delay or to reroute the flight. However, the dispatcher did not relay to the crew information which might have persuaded the pilot- in-command to avoid the storm system. In fact, when the dispatcher was informed of the efforts of other aircraft to avoid the squall line, he should have recommended avoidance action to Flight 250.
In spite of his apparent concern were the en-route weather and his knowledge that the squall line was quite solid, the pilot-in-command elected to penetrate the line using his airborne weather radar to select a "light" area.
Flight 250 never reached the main squall line. Instead, the aircraft broke up in a roll cloud approximately 5 miles from the nearest radar weather echo. At this ti= the aircraft was at the proper configuration and airspeed for flight in turbulence and the autopilot was engaged.
Flight 250 encountered extreme turbulence generated by the strong horizontal and vertical wind shears associated with the outflow of cold air from the approaching squall line. This turbulence probably caused a large angled gust of very short duration with components in the lateral, vertical, and longitudinal planes.
The forces and accelerations produced by this encounter caused the fin and right tailplane to reach their ultimate loads, with near-simultaneous failures resulting. The aircraft then pitched downward until the right wing reached its negative ultimate load. The loss of these components rendered the aircraft uncontrollable and shortly afterward it probably began a random tumbling motion which stabilized some time before impact into a flat-spinning attitude.
Final Report:

Crash of a Beechcraft C18S Expeditor in San Jose

Date & Time: Aug 4, 1966 at 0545 LT
Type of aircraft:
Registration:
N7385C
Survivors:
Yes
MSN:
6801
YOM:
1944
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5039
Captain / Total hours on type:
167.00
Circumstances:
On final approach to San Jose Airport, both engines failed simultaneously. The airplane stalled, hit tree tops and crashed in a wooded area located few miles short of runway. All nine occupants were injured and the aircraft was destroyed.
Probable cause:
Inadequate preflight preparation on part of the pilot. Double engine failure caused by a fuel exhaustion. Inattentive fuel supply during flight. Auxiliary tanks purposely left empty to remain below gross weight. No enroute refueling accomplished.
Final Report:

Crash of a Grumman G-44 Widgeon in Kendallville

Date & Time: Jul 31, 1966 at 1500 LT
Type of aircraft:
Operator:
Registration:
N132X
Flight Type:
Survivors:
Yes
Schedule:
Kendallville - Kendallville
MSN:
1210
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
862
Captain / Total hours on type:
101.00
Circumstances:
The airplane was engaged in a local pleasure flight in the region of Kendallville. Following an uneventful flight, the pilot returned to Kendallville when, on touchdown, the airplane bounced, stalled and crashed. All five occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Improper level off and improper recovery from bounced landing on part of the pilot.
Final Report:

Crash of a Curtiss C-46A-45-CU Commando in Newark

Date & Time: Jul 28, 1966 at 0850 LT
Type of aircraft:
Operator:
Registration:
N9905F
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
30316
YOM:
1944
Flight number:
VK7990
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
17491
Captain / Total hours on type:
6191.00
Circumstances:
Shortly after takeoff from runway 22 at Newark Airport, while climbing to a height of 200 feet, the left engine failed. The crew immediately reduced his altitude and completed an emergency belly landing in a field. The airplane slid for several yards before coming to rest. Both pilots were slightly injured while the aircraft was damaged beyond repair.
Probable cause:
Failure of the left engine during initial climb after the master and connecting rods and piston rings failed. At the time of the accident, the total weight of the airplane was 9,114 pounds above the MTOW. Poor supervision on part of the operational personnel of the company who dispatched an overloaded aircraft.
Final Report:

Crash of a Douglas C-47A-10-DK in Gallup

Date & Time: Jul 27, 1966 at 1453 LT
Operator:
Registration:
N4994E
Flight Phase:
Survivors:
Yes
Schedule:
Gallup – Albuquerque
MSN:
12442
YOM:
1944
Flight number:
FL188
Crew on board:
3
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8502
Captain / Total hours on type:
4160.00
Circumstances:
During the takeoff roll at Gallup-Senator Clark Airport, control was lost. The aircraft veered off runway and came to rest in flames in a ditch. Three passengers were injured while 13 other occupants were unhurt. The aircraft was written off.
Probable cause:
Improper operation of brakes and/or flight controls during takeoff on part of the PIC. Inadequate supervision of flight on part of the PIC who failed to maintain directional control and failed to abort takeoff.
Final Report:

Crash of a Fairchild C-123 off Cape Lisburne: 9 killed

Date & Time: Jul 16, 1966
Type of aircraft:
Operator:
Flight Type:
Survivors:
No
Schedule:
Elmendorf – Nome – Cape Lisburne
Crew on board:
5
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
The aircraft was engaged in a supply mission from Elmendorf AFB to Cape Lisburne with an intermediate stop in Nome, carrying supply for the local weather station. On approach, the crew encountered poor weather conditions with low clouds and winds gusting up to 28 knots. Control was lost and the airplane crashed into the Chukchi Sea, about 150 feet offshore. All nine occupants were killed, among them two civilians.

Crash of a Fairchild C-119 Flying Boxcar in Jacksonville

Date & Time: Jul 16, 1966
Operator:
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Jacksonville - Jacksonville
Crew on board:
4
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Jacksonville-Towers Field NAS, while climbing, the crew informed ATC about the failure of the left engine and was cleared to return for an emergency landing. Smoke spread in the cockpit and the cabin so it was decided to abandon the aircraft. All 34 occupants bailed out and the airplane crashed in a field and was destroyed. There were no casualties.
Probable cause:
Failure of the left engine after takeoff.

Crash of a De Havilland DH.104 Dove 6A in Hideaway Park: 3 killed

Date & Time: Jul 11, 1966 at 2050 LT
Type of aircraft:
Operator:
Registration:
N1563V
Flight Phase:
Survivors:
No
Site:
MSN:
04449
YOM:
1954
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
9830
Captain / Total hours on type:
10.00
Circumstances:
While in cruising altitude in poor weather conditions, the airplane struck the slope of a mountain in slight flat attitude near Hideaway Park. The aircraft was destroyed and all three occupants were killed. At the time of the accident, weather conditions were poor with low ceiling, rain showers, thunderstorm activity and turbulences.
Probable cause:
The crew continued under VFR mode in adverse weather conditions.
Final Report:

Crash of a Rockwell Aero Commander 560E in Parsippany: 2 killed

Date & Time: Jul 10, 1966 at 1252 LT
Registration:
N3804C
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Morristown - Morristown
MSN:
560-732
YOM:
1959
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2500
Captain / Total hours on type:
500.00
Circumstances:
The crew was completing a local training flight from Morristown Airport when, while in cruising altitude, control was lost. The airplane went into a dive and eventually crashed in an open field located near Parsippany. The aircraft was destroyed and both occupants were killed.
Probable cause:
Loss of control in flight after the right wing spar failed because the pilot was doing steep, low altitude maneuvers. Forces exceeded the designed stress limits of the aircraft. Overload failure.
Final Report: