Crash of a Lockheed 18-56-23 LodeStar in Tallahassee: 4 killed

Date & Time: Jun 8, 1962 at 0756 LT
Type of aircraft:
Operator:
Registration:
N45W
Flight Phase:
Survivors:
No
Schedule:
Montgomery – Jacksonville
MSN:
2477
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
A Lockheed Lodestar 18, registered N45W and owned by Winn-Dixie Stores, Inc, departed Montgomery-Dannelly Field, Alabama, at approximately 07:06 on company business flight to Jacksonville, Florida. En route altitude was 8,000 feet. A Lockheed T-33A-1-LO Shooting Star US Air Force jet trainer, serial 51-4532, departed Moody AFB at approximately 07:13 on a local IFR training flight. The T-33 climbed to 20,000 feet following takeoff from Moody and proceeded to the Tallahassee VOR where it was cleared by Tallahassee Approach Control for penetration and an ILS approach to runway 36 at Tallahassee Airport. While under Tallahassee Approach Control, two ILS approaches were completed followed by two ILS missed approaches. After the second ILS missed approach, the flight was cleared at approximately 07:50 by Tallahassee Approach Control, "...from present position direct to the Tallahassee OMNI, maintain 3,000, anticipate routing Victor 22, Greenville, direct to Valdosta OMNI." After that the T-33 reported VFR on top at 4000 feet. The crew continued VFR and requested a climb to 20.000 feet, direct to Valdosta, which was approved. The two aircraft collided in midair at approximately 8,000 feet altitude, approximately 4.3 miles northwest of the Tallahassee VOR Station. The T-33 climbed up into the Lodestar. The Lodestar's right propeller cut through the forward end of the T-33 right tip tank. The Lodestar's fuselage lower surface scrubbed across the T-33's right wing upper surface just inboard of that tip tank at an angle of 14 degrees leftward from the T-33's longitudinal axis. The various impacts on the T-33's right wing caused it to yaw to the right, with the result that its tail assembly ripped through the Lodestar's left wing at a greater angle than that of initial impact. The Lodestar's left wing was severed from trailing edge to leading edge at this time. The impact severed the T-33's tail assembly causing loss of control. The T-33 entered an inverted flat spin in which it remained until contact with the ground. Both crew members of the T-33 ejected safely. The Lodestar crashed, killing all four on board.
Probable cause:
The Board determines the probable cause of this accident was failure of the T-33 pilots to observe the Lodestar while climbing through its flight altitude. unauthorized deviation from an IFR flight plan was a contributing factor.

Crash of a De Havilland DH.104 Dove in Edinburgh

Date & Time: May 29, 1962
Type of aircraft:
Operator:
Registration:
G-ANDY
Flight Phase:
Survivors:
Yes
MSN:
04441
YOM:
1953
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Edinburgh-Turnhouse Airport, while climbing, an engine failed. The airplane struck power cables, stalled and crashed in a field. Both crew members were evacuated while the aircraft was damaged beyond repair.
Probable cause:
Engine failure after liftoff.

Crash of a Douglas DC-3S in Bluefield

Date & Time: Apr 12, 1961
Type of aircraft:
Operator:
Registration:
N541S
Survivors:
Yes
Schedule:
Pittsburgh – Bluefield
MSN:
43192
YOM:
1937
Crew on board:
3
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was completing a flight from Pittsburgh to Bluefield, carrying a crew of three and one passenger, the vice-president of the United States Steel Corporation. After touchdown, the airplane went out of control, veered off runway and came to rest on an embankment. All four occupants were uninjured while the aircraft was damaged beyond repair.

Crash of a Curtiss C-46A-35-CU Commando in Calderon

Date & Time: Apr 8, 1961
Type of aircraft:
Operator:
Registration:
HK-489E
Survivors:
Yes
MSN:
26778
YOM:
1944
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
27
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed on landing at Calderon. All 29 occupants escaped uninjured while the aircraft was written off.

Crash of a Lockheed 18 LodeStar in Minersville: 6 killed

Date & Time: Jan 13, 1960
Type of aircraft:
Registration:
N672
Flight Phase:
Survivors:
No
Site:
Schedule:
San Francisco – Cedar City
MSN:
2069
YOM:
1941
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
While flying in foggy conditions, the twin engine aircraft struck the slope of a mountain located near Minersville. All six occupants were killed.

Crash of a Lockheed L-1856 LearStar near Woonsocket: 7 killed

Date & Time: Dec 15, 1958 at 0930 LT
Type of aircraft:
Operator:
Registration:
N37500
Flight Phase:
Survivors:
No
Schedule:
Linden – Boston
MSN:
2251
YOM:
1942
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
En route to Boston, the crew encountered poor weather conditions with icing. Both carburetors suffered icing in flight and both engines failed. The airplane went out of control, dove into the ground and crashed in a field located five miles southwest of Woonsocket. The airplane was destroyed upon impact and all seven occupants were killed.
Crew:
Alexander Sable, pilot,
Edward Luidcinaitis, copilot.
Passengers:
Nelson A. Bergstend,
Ferdinand Liot,
Stephen Baksal,
Raymond Buese,
Jesse Hackney.
Probable cause:
The pilot's decision to continue on to his destination in freezing weather after total power loss of one engine from induction icing. Contributing causal factors were the serious deficiency in weather briefing and inadequate information in the Airplane Flight Manual for the most effective use of carburetor anti-icing and deicing.

Crash of a Grumman G-21A Goose in Pointe-Claire

Date & Time: Jun 17, 1958
Type of aircraft:
Registration:
CF-EXA
Survivors:
Yes
Schedule:
Chibougamau - Montreal
MSN:
B050
YOM:
1944
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Dorval Airport, both engines failed. The seaplane stalled and crashed in a prairie located at Pointe-Claire, few dozen yards from the airfield. All six occupants were injured, some of them seriously, and the aircraft was written off.
Probable cause:
On final approach, the pilot mistakenly put the fuel selector in a wrong position (empty tank), causing both engines to stop.

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 Beechcraft C-45F Expeditor near Tanauan: 6 killed

Date & Time: Oct 11, 1957 at 1830 LT
Type of aircraft:
Registration:
PI-C622
Flight Phase:
Survivors:
No
Site:
Schedule:
Ozamis City – Manila
Location:
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
At approximately 0540LT, PI-C622, with 5 passengers and a pilot aboard took off from the Manila International Airport on a charter flight to Ozamis City and return. The aircraft departed Ozamis on the return trip to Manila at approximately 1550LT the same day. At approximately 1830LT, radio contact with the Manila Tower was established and the aircraft reported its position to be over the Province of Batangas, which is about 60 nautical miles SW of Manila and lies on course on the route Ozamis-Manila. On the C-45F Beechcraft it takes about 25 minutes flight time to Manila. The pilot requested information as to the prevailing weather conditions over Manila and vicinity and the weather report as of 1800LT was relayed to and received by the pilot. Further efforts were made by the Tower at 1900LT and 1930LT to contact the aircraft but with negative results. At approximately 2030LT, the Manila Tower received the information from the Rescue Coordinating Centre that the aircraft crashed in a wooded area located on Mt Makiling, in the region of Tanauan, about 45 miles SW of Manila. The aircraft was totally destroyed and all six occupants were killed, among them Carlos P. Romulo, son of the US Ambassador in the Philippines. The pilot founded PADC in 1954.
Crew:
Paul L. Gunn, pilot.
Passengers:
Carlos P. Romulo,
Allen O. Gorman,
Raplh L. Tover,
Zane Duncan,
Harold Broad.
Probable cause:
The Board determined that the probable cause of the accident was the unsuccessful procedure of the pilot in trying to avoid the severe thunderstorm existing over the area at that time. His attempt to fly below the thunderstorm resulted in a ground collision. A contributing factor was the weather over the area which, at the time of the accident, was zero visibility and almost zero ceiling, with a high degree of turbulence, heavy rain and lightning. Also, the Board concluded that even if the right engine of PI-C-622 was feathered at such 1,500-foot altitude over the vicinity of the crash, the aircraft could still have climbed. From evidence gathered by the Board, there was no factual finding either on the airframe or on the engine maintenance that might have contributed to the crash. The Board was more inclined to attach the circumstances surrounding the accident to the weather in that the pilot in all probability flew low to 'get under the overcast'
Final Report:

Crash of a Lockheed 18-56-23 LodeStar near Uniontown: 6 killed

Date & Time: Oct 6, 1957 at 1655 LT
Type of aircraft:
Operator:
Registration:
N80G
Flight Phase:
Survivors:
No
Site:
Schedule:
Cleveland – Hot Springs – Johnstown
MSN:
2351
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
10000
Captain / Total hours on type:
3000.00
Copilot / Total flying hours:
3600
Copilot / Total hours on type:
200
Aircraft flight hours:
4608
Circumstances:
N80G departed Cleveland, Ohio, at approximately 1208LT for Ingalls Field Airport, Hot Springs, Virginia. The crew consisted of Captain Warren F. Noonan and Copilot Theodore O. Krauss. The purpose of the flight was to pick up passengers at Hot Springs, then fly to Johnstown, Pennsylvania, for an additional passenger, and return to Cleveland. The flight landed at Ingalls Field Airport sometime between 1300 and 1400 without incident. No records of aircraft arrival times are kept at this airport. N80G departed Hot Springs at approximately 1545LT with four passengers on board. The aircraft was observed to take off on the northeast runway and to climb to an altitude below the clouds. It was then observed to fly in a northwesterly direction for approximately four or five miles. About 1650, over an hour after takeoff and just before the aircraft struck the mountain, it was heard by a number of persons who lived within a radius of 10 miles of the accident scene; none saw it. The airplane hit trees and crashed in a wooded area, killing all six occupants.
Probable cause:
The Board determines that the probable cause of this accident was the action of the pilot in attempting VFR flight under instrument conditions over mountainous terrain. The following findings were reported:
- The crew was probably briefed by the U. S. Weather Bureau for the trip to Hot Springs and return, prior to departure from Cleveland,
- The VFR flight from Cleveland to Hot Springs was routine,
- The weather conditions north and east of Hot Springs at the time of the return required flight in accord with instrument flight rules; this was not done,
- No telephone or aircraft radio contacts wore made by the crew with any CAA communications station, either to file a flight plan or request weather information,
- The aircraft was heard but not seen flying a northeasterly heading in the overcast near the accident site,
- The aircraft was equipped for instrument flight.
Final Report: