Crash of a Douglas DC-7B at Long Beach

Date & Time: Mar 10, 1958
Type of aircraft:
Operator:
Registration:
N846D
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Long Beach - Long Beach
MSN:
45452
YOM:
1958
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances at Long Beach Airport while performing a test flight prior to its delivery to Eastern Airlines. There were no casualties.

Crash of a Convair CV-240-0 at New Haven

Date & Time: Mar 1, 1958 at 1024 LT
Type of aircraft:
Operator:
Registration:
N94213
Flight Phase:
Survivors:
Yes
Schedule:
Boston – New Haven – Bridgeport – New York
MSN:
23
YOM:
1948
Flight number:
AA535
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7453
Captain / Total hours on type:
4660.00
Copilot / Total flying hours:
5300
Copilot / Total hours on type:
3205
Aircraft flight hours:
20857
Circumstances:
This was scheduled passenger flight 535 of March 1 from Boston, Massachusetts, to New York, New York, with stops planned at New Haven and Bridgeport, Connecticut. The crew, consisting of Captain Edward W. Johnson, First Officer Norman A. Paquette, and Stewardess Marian Sullivan, reported to company operations at Boston well ahead of scheduled departure time. Departure from Boston at 0927 was on time and was in accordance with an TFR clearance to cruise at 6,000 feet via airways to New Haven. The flight was routine and on schedule to New Haven. The aircraft was not refueled during the five-minute stop at New Haven, during which time both engines were stopped. The flight departed the terminal with five passengers and 1460 gallons of fuel. Gross weight of the aircraft was well under the maximum allowable and its center of gravity was located within prescribed limits. The wind was calm and runway 14 (4,116 feet), one of two macadam runways, was selected for takeoff. There is no air traffic control tower at New Haven. After completion of the takeoff checklist, the aircraft moved onto the runway and takeoff was initiated from a tan start without delay. This segment of the flight was being flown by First Officer Paquette who occupied the right seat. Captain Johnson, on the left, maintained directional control during the initial acceleration of the aircraft. Before the aircraft reached the intersection of runways 14 and 19, the landing gear was retracted. The aircraft then skidded clown runway 14 near its center and cane to rest 1,050 feet from the far end. Captain Johnson, Stewardess Sullivan, and three passengers left through the right emergency escape hatch over the wing. First Officer Paquette and the two remaining passengers left through the partially opened front entrance door. Fire, around the left engine and the left outboard wing area, caused considerable damage and was extinguished by the local fire department.
Probable cause:
The Board determines that the probable cause of this accident was the improper technique of the captain resulting in the unintentional retraction of the landing gear prior to V 1 speed, which was made possible by a malfunctioning left gear safety switch. A contributing factor was inadequate inspection by the carrier. The following findings were reported:
- The first officer made the takeoff with the captain performing the duties of copilot from his left seat,
- The aircraft operated normally up to 85 knots in the takeoff roll,
- The captain prematurely applied upward pressure on the landing gear selector handle,
- A defective landing gear safety switch allowed the landing gear selector handle to be unlocked during ground operation of the aircraft, and permitted the landing gear to retract,
- Fire did not develop in the left nacelle and fuel tank area until the aircraft skidded to a stop on the runway,
- The company’s inspection of the safety switch was inadequate.
Final Report:

Crash of a Lockheed 18-56-23 LodeStar off Chicago

Date & Time: Feb 24, 1958
Type of aircraft:
Operator:
Registration:
N9050
Flight Phase:
Survivors:
Yes
Schedule:
Chicago – White Plains
MSN:
2563
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Chicago-Merrill C. Meigs Airport, while in initial climb, the twin engine aircraft stalled and crashed into the Lake Michigan, about 50 feet from the shore. All seven occupants were rescued while the aircraft was lost. Owned by Cluett Peabody & Company, the airplane was on its way to White Plains, New York.

Crash of a Convair CV-240-1 in Palm Springs

Date & Time: Feb 13, 1958 at 1345 LT
Type of aircraft:
Operator:
Registration:
N8405H
Flight Phase:
Survivors:
Yes
Schedule:
Las Vegas – Palm Springs – San Diego
MSN:
22
YOM:
1948
Flight number:
WA019
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
9845
Captain / Total hours on type:
3547.00
Copilot / Total flying hours:
5240
Copilot / Total hours on type:
785
Aircraft flight hours:
22516
Circumstances:
About 1342 Flight 19 took off from runway 31. The takeoff appeared normal, and the aircraft climbed to approximately 500 feet above the ground. At this time several ground witnesses saw two or more silvery pieces separate from the aircraft. Most witnesses said the pieces seemingly separated from the area of the right wing. Almost simultaneously the aircraft was observed to nose down sharply and descend at a steep angle. As it neared the ground it leveled off considerably but continued to descend. It contacted the ground raising a large cloud of dust and then disappeared from the view of the observers behind intervening higher terrain. Seconds later large columns of smoke were seen rising from the accident site. During the ground roll the aircraft struck large boulders in its path and fire occurred which consumed the major portion of the aircraft. There were no fatalities but serious injuries resulted to 5 of the 18 passengers and minor injuries to most of the others. The crew of three received minor or slight injuries.
Probable cause:
The Board determines that the probable cause of this accident was the failure of a mechanic to secure properly the right wing leading edge section as a result of which the unit separated in flight. This improper installation was undetected because of inadequate inspection. The following findings were reported:
- During the departure from Palm Springs the right wing leading edge separated in flight,
- Separation of the component resulted in severe control difficulty and buffeting of the aircraft,
- A gear-down emergency landing was made in the boulder-strewn desert about four miles north-northwest of the airport,
- During the ground roll impacts with the boulders caused severe damage and breakup of the aircraft, and a fire in the left wing spread rapidly and destroyed the aircraft,
- N8405H received a No. 3, areas 1 and 3, heavy maintenance check about two hours of flying time before the accident,
- During the maintenance a mechanic assigned to close and secure the right leading edge forgot to install the retaining screws,
- The gap straps were properly installed,
- An inadequate inspection of the aircraft by the lead mechanic resulted in his failure to detect the omission,
- The gap straps held the leading edge in place until the Palm Springs departure when they failed from loads beyond their design strength.
Final Report:

Crash of a Boeing B-52D-75-DO Stratofortress at Ellsworth AFB: 5 killed

Date & Time: Feb 11, 1958
Type of aircraft:
Operator:
Registration:
56-0610
Flight Type:
Survivors:
Yes
Schedule:
Ellsworth - Ellsworth
MSN:
17293
YOM:
1956
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
On final approach to Ellsworth AFB, while completing a local training sortie, all eight engine lost power. The aircraft stalled and crashed onto a building containing the equipment for the instrument landing approach system and located short of runway. Two crew members were killed while six others were injured. Three people working in the building were killed as well.
Crew:
Cpt Melvin J. Rudd, pilot,
Sgt Richard Gilbert, navigator,
Cpt Verle Rusk, navigator,
1st Lt Leonard R. Scotty, electronic countermeasures officer,
T/Sgt Oscar Orrs, gunner, 1,
Cpt John O'Connell Jr., navigator, †
1st Lt Kenneth B. Kaeppler, radar navigator. †
Those killed on ground were:
A1c Ronald R. Mitchell,
A1 James E. Ferrell,
Mr. Glen M. Allen.
Probable cause:
The accident was the result of a fuel pump screen iced over, leading to a total power loss on all engines.

Crash of a Lockheed P2V-5F Neptune in Norwalk: 6 killed

Date & Time: Feb 1, 1958 at 1913 LT
Type of aircraft:
Operator:
Registration:
127723
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Los Alamitos - Los Alamitos
MSN:
426-5054
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The aircraft departed Los Alamitos AAF for a local training flight with eight crew members on board. While cruising at an altitude of 3,000 feet, the airplane collided with a USAF Douglas C-118A Liftmaster. Registered 53-3277, it left Long Beach Airport five minutes earlier bound for McGuire AFB, New Jersey, with 35 passengers and a crew of six on board. Following the collision, both aircraft went out of control, dove into the ground and crashed in Norwalk. The Liftmaster crashed on several building and a fuel station, killing all 41 occupants and one woman on the ground. The Neptune crashed in a stone-pit located about 2.5 miles north of the C-118 crash site. Six crew members were killed while two others were seriously injured. The accident occurred by night but in good weather conditions with a visibility above 15 miles.
Probable cause:
It was determined that the collision occurred in an uncontrolled area. Both crews were considered as co-responsible of the accident as they failed to take the appropriate measures to avoid each other and to pay attention to potential traffic. The crew of the C-118 was blamed not giving the priority to the Neptune which was flying to his right.

Crash of a Douglas C-118A Liftmaster in Norwalk: 42 killed

Date & Time: Feb 1, 1958 at 1913 LT
Type of aircraft:
Operator:
Registration:
53-3277
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Long Beach – McGuire
MSN:
44648
YOM:
1955
Flight number:
USAF30W/02
Crew on board:
6
Crew fatalities:
Pax on board:
35
Pax fatalities:
Other fatalities:
Total fatalities:
42
Captain / Total flying hours:
7819
Captain / Total hours on type:
1448.00
Copilot / Total flying hours:
701
Copilot / Total hours on type:
439
Circumstances:
The four engine aircraft departed Long Beach Airport at 1908LT bound for McGuire AFB, New Jersey, with 35 passengers and a crew of six on board. Shortly after takeoff, the pilot was cleared to climb to the assigned altitude of 17,000 feet. About five minutes later, while climbing to an altitude of 3,000 feet, the airplane collided with a USN Lockheed P2V-5F Neptune registered 127723. Carrying eight crew members, the Neptune has taken off from Los Alamitos NAS and was completing a local training mission. Following the collision, both aircraft went out of control, dove into the ground and crashed in Norwalk. The Liftmaster crashed on several building and a fuel station, killing all 41 occupants and one woman on the ground. The Neptune crashed in a stone-pit located about 2.5 miles north of the C-118 crash site. Six crew members were killed while two others were seriously injured. The accident occurred by night but in good weather conditions with a visibility above 15 miles.
Probable cause:
It was determined that the collision occurred in an uncontrolled area. Both crews were considered as co-responsible of the accident as they failed to take the appropriate measures to avoid each other and to pay attention to potential traffic. The crew of the C-118 was blamed not giving the priority to the Neptune which was flying to his right.

Crash of a Douglas A-26B-25-DL Invader in the Old Dad Mountains: 2 killed

Date & Time: Jan 31, 1958 at 0943 LT
Type of aircraft:
Operator:
Registration:
41-39310
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
George - Winslow - Phoenix - Blythe - George
MSN:
7023
YOM:
1941
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew left George AFB in the early morning on a training flight to Winslow, Phoenix, Blythe and return to George, with four other similar aircraft. While cruising, one of the Invader's crew made an error and left his position, causing his aircraft to struck the top of the Invader registered 41-39310. Out of control, the airplane dove into the ground and crashed in a desert and mountainous area located in the Old Dad Mountains, in the Mojave National Preserve. Both crew members were killed. The other plane was able to land without further incident but with one engine inoperative.
Crew:
1st Lt Alexander Aros,
A1c Patrick W. Hughes.

Crash of a Convair R3Y-2 Tradewind off Alameda NAS

Date & Time: Jan 24, 1958
Type of aircraft:
Operator:
Registration:
128446
Flight Type:
Survivors:
Yes
Schedule:
Honolulu - Alameda
Crew on board:
5
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On a flight from Honolulu (Keehi lagoon) to Alameda NAS, the propeller detached from the engine number one and struck the fuselage, causing vibrations. The crew continued the flight to Alameda NAS and while landing on breakwater, the airplane crash landed and sank. All 21 occupants were rescued but the aircraft was lost.
Probable cause:
Loss of a propeller blade in flight.

Crash of a Lockheed 5C Vega in Tenakee: 1 killed

Date & Time: Jan 15, 1958 at 1600 LT
Type of aircraft:
Operator:
Registration:
N47M
Survivors:
Yes
Schedule:
Juneau – Angoon – Hood Bay – Baranof – Rodgers Point – Tenakee – Juneau
MSN:
99
YOM:
1929
Flight number:
ACA040
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1263
Captain / Total hours on type:
209.00
Aircraft flight hours:
13496
Circumstances:
Alaska Coastal Airlines, a scheduled air carrier, is authorized to conduct operations throughout southeastern Alaska. On January 15, 1958, Captain Fred B. Sheldon departed from Juneau to fly Trip 40. Scheduled stops were planned at Angoon, Hood Bay, Baranof, Rodgers Point, Tenakee, and the flight was to terminate at the point of origin, Juneau. Weather reports for the area indicated conditions to be generally good, enabling the flight to be conducted according to visual flight rules. Ceilings were forecast to be 2,000 to 3,000 feet and winds near the surface were anticipated to be moderate and generally southwesterly. At least one mountain pass over the route was reported closed because of clouds. The gross takeoff weight of the aircraft at Juneau was calculated to be 5,237 pounds, approximately 4 pounds less than the maximum allowable. The load was correctly distributed within the center of gravity limitations. Flight 40 departed Juneau at 1301 and was routine to Angoon. After refueling, the flight continued uneventfully to Hood Bay, Baranof, Rodgers Point; arriving at Rodgers Point about 1520. About 1530, after the takeoff from Rodgers Point, a radio operator there advised the station agent at Tenakee (the next intended en route stop) that flight 40 was off the water and would need 20 gallons of fuel when it arrived. At approximately 1557 the agent at Tenakee heard a distress call from flight 40 over the radio. The pilot called “Mayday” and stated he was trying to make it to the flats in Kadashan Bay. The agent then called Flight 40 by radio asking its position. Sheldon’s final message was “ . . . the flats across from Tenakee.” Immediately thereafter the aircraft crashed. Both passengers were injured while the pilot was killed.
Probable cause:
The Board determines that the probable cause of this accident was the poor flight planning by the pilot and his poor judgment in allowing the aircraft to run out of fuel. A contributing factor was the lack of adequate organization and management of the air carrier’s operations to ensure that all flights were planned and conducted with safety. The following findings were reported:
- With one fuel tank out of use, the aircraft did not comply with the requirements of Bulletin 7A under which it was certificated for passenger-carrying service,
- No evidence of mechanical or structural failure was found,
- The pilot did not plan his flight to provide for an adequate fuel reserve at all times,
- The company did not provide adequate supervision or control over flight planning or clearance of flights,
- A longer alternate route had to be followed by the flight because of unfavorable weather,
- The aircraft exhausted its fuel supply and crashed,
- The air carrier’s operations manual was incomplete and was not maintained current as required by regulations,
- The CAA safety inspection program was ineffective in terms of ensuring that the carrier was conducting operations at a level of safety appropriate for the carrier’s operating certificate and associated operating specifications.
Final Report: