Crash of a Douglas C-47A-30-DK into the Atlantic Ocean: 2 killed

Date & Time: May 5, 1948
Operator:
Registration:
NC17645
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Gander – Shannon
MSN:
13978/25423
YOM:
1944
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Crashed into the Atlantic Ocean in unclear circumstances. As the aircraft failed to arrive in Shannon, SAR operations were conducted but eventually suspended five days later, on May 10, as no trace of the aircraft nor both crew members was found.

Crash of a Lockheed L-049-51-26 Constellation in Shannon: 30 killed

Date & Time: Apr 15, 1948 at 0234 LT
Operator:
Registration:
NC88858
Survivors:
Yes
Schedule:
Calcutta – Damascus – Istanbul – Brussels – London – Shannon – Gander – New York
MSN:
2058
YOM:
1946
Flight number:
PA110
Location:
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
21
Pax fatalities:
Other fatalities:
Total fatalities:
30
Captain / Total flying hours:
6230
Captain / Total hours on type:
1564.00
Copilot / Total flying hours:
3310
Copilot / Total hours on type:
956
Aircraft flight hours:
3861
Circumstances:
Pan American's Flight 1-10, originating in San Francisco, California, April 10, 1948, was scheduled to fly around the world to New York, New York. In accordance with company practice the flight changed to a different aircraft, NC-88858, at the Pan American Airways' base in Calcutta, India. The flight took off from Calcutta, April 13, 1948, and continued without incident via Damascus, Syria, and Istanbul, Turkey, to Brussels, Belgium. During a night landing approach at Brussels the fluorescent lighting on the left or pilot side of the cockpit went out. Since the only other lighting immediately available was a chart light which was focused on the automatic direction finder indicator, the flight instruments could not be read, and the remainder of the landing approach was accomplished without visual reference to the flight instruments. An examination was made of the fluorescent lights after the landing. They appeared to operate normally, so the flight departed from Brussels, continuing without difficulty until on the final landing approach into London. When the power was reduced the same pilot's fluorescent lights again went out. This time the chart light was focused on the airspeed indicator. The approach was continued, and the landing was accomplished without incident. A faulty rheostat switch was found to be the cause of the fluorescent light failure, but since a spare switch could not be located, it was not changed at London. An entry describing the defect was placed in the aircraft's Form C, the airplane flight log, and the captain and the flight engineer of the new crew were informed by the company's maintenance supervisor of the condition. Though no actual maintenance was accomplished, the lights again appeared to be operating normally, so the captain, F. C. Jakel, decided to take-off, departing from London at 0035, April 15, 1948, for Shannon. At this time available weather forecasts indicated that at the estimated time of the flight's arrival at Shannon the ceiling there would be 700 feet with a higher cloud layer at 1,000 feet, and visibility 4 miles. At 0159, April 15, 1948, the flight reported being at an altitude of 4,500 feet, contact, over the Limerick Junction fan marker, located 25 statute miles southeast from the Shannon Airport, and requested permission to make a practice approach to the field with the use of the instrument landing system. Shannon Tower cleared the flight for this approach. The tower advised that 3 hours previously the instrument landing system equipment on the airport had been reported faulty, but that it had since been serviced and was operating normally according to its monitoring board, though not flight-checked. At 0210, the flight reported that it was proceeding to the outer marker, 5.2 statute miles northeast of the Shannon Airport, and also made a report, routine for Pan American flights, "mechanical condition okay." In response Shannon Tower advised the flight that the weather over the field was "fog patches, 3 miles visibility, cloud base 400 feet, sky 6/10 covered, wind from 325 degrees at 4 miles per hour." The flight was instructed to land on runway 23, the runway for which the instrument landing system was projected. It was also requested to report when making the 180 degree procedure turn for the inbound instrument approach to the field, and when over the outer marker. The requested position reports were not received by the tower, but at 0220 the flight did report a "missed approach," 2 and advised that it was going around for a second approach. At this time the flight was observed through a break in the clouds by the Shannon Tower, which was the first time that the aircraft had been seen in the vicinity of the Shannon Airport. The aircraft was reported as 500 feet above the ground, over, and in line with runway 23. Power was heard being increased, and the aircraft was observed turning left. On the second approach, at 0227, the flight reported making its 180 degree procedure turn and was cleared for landing by the tower. One minute later, weather conditions at the field were transmitted to the flight as "fog patches, visibility 2 1/2 miles, 6/10 cloud base 400 feet, 4/10 cloud base 300 feet, wind 325 degrees, 3 miles per hour, altimeter 30.29." The flight reported approaching the outer marker at 0231 at which time the tower advised that another flight which had just taken off had reported a ceiling of 500 feet when northwest of the field. Flight 1-10 acknowledged this information, which was the last communication received The aircraft was not observed at any time during the second approach until after it struck the ground. The aircraft struck the ground 2,380 feet northeast of the approach end of runway 23, and directly in line with that runway. Flames followed immediately after impact, and consumed a great portion of the wreckage. A passenger survived while 30 other occupants were killed.
Probable cause:
The Board determines that the probable cause of this accident was the continuation of an instrument approach to an altitude insufficient to clear the terrain. A contributing factor may have been the failure of the pilot's instrument fluorescent light.
Final Report:

Crash of a Lockheed L-049 Constellation in Shannon: 9 killed

Date & Time: Dec 28, 1946 at 0209 LT
Operator:
Registration:
NC86505
Survivors:
Yes
Schedule:
Paris – Shannon – Gander – New York
MSN:
2026
YOM:
1945
Flight number:
TW6963
Location:
Country:
Region:
Crew on board:
9
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
2964
Captain / Total hours on type:
114.00
Copilot / Total flying hours:
1978
Copilot / Total hours on type:
70
Aircraft flight hours:
1098
Circumstances:
At 0135 the flight transmitted a report to Shannon Radio indicating its position as over the Irish coast at 7,000 feet. At this time the flight was cleared to cross the Limerick marker at 5,000 feet. Shortly thereafter Shannon Radio advised the flight of the Shannon weather. Visibility 2 miles, 10/10 cloud cover at 900 feet, 3/10 at 500 feet, wind 160 degrees, 5 knots, altimeter setting 30 04 inches. At 0153 the flight reported over the Shannon radio range station at 5,000 feet and was given clearance to descend on the SE leg. While in the procedure turn at 0200 the flight transmitted a position report to Shannon Radio and, in acknowledgement, received a later Shannon weather report. Rain and drizzle, visibility 2 miles, 10/10 cloud cover at 900 feet, 6/10 at 400 feet, wind 120 degrees, 5 knots, altimeter setting 30 04. Receipt of this weather retort was acknowledged and the Shannon control tower cleared the aircraft for approach to Runway 14. At 0206 the flight reported over the range station at 1,200 feet at which time Shannon Tower advised Aircraft 505 that Shannon was reporting 10/10 cloud cover at 400 feet, 4/10 at 250 feet, visibility 1 mile, wind 120 degrees, 5 knots. Upon receiving acknowledgement from the flight Shannon Tower requested the pilot to make a ceiling check. This request was also acknowledged by the flight. At approximately 0208 personnel at Shannon Airport observed Aircraft 505 approach the field on a heading parallel to Runway 32. The aircraft appeared to continue on this heading until over the airport at which time it turned to the right to a heading of approximately north. Shortly thereafter the aircraft disappeared from sight. At approximately 0209 these observers saw a brilliant flash WNW of the airport and heard a loud noise. Realizing that Aircraft 505 had crashed, tower personnel immediately initiated rescue operations and dispatched emergency crews to the scene of the accident.
Probable cause:
The board determines that the probable cause of this accident was an error in altimeter indication, the primary reason for which was the reversal of the primary and alternative static source lines which leg the pilot to conduct his approach, to the airport at a dangerously low altitude. A contributing factor was the negligence of maintenance personnel in certifying to the satisfactory functioning of the static system although the tests required to determine such a condition were not accomplished. A further contributing factor was the restriction of vision from the cockpit resulting from fogging of the unheated windshield panels.
Final Report:

Crash of an Avro 652 Anson I into the Shannon River

Date & Time: Nov 19, 1946
Type of aircraft:
Operator:
Registration:
MG902
Flight Phase:
Flight Type:
Survivors:
Yes
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a training sortie when he lost his orientation due to the deterioration of the weather conditions, and was unable to locate his position. Due to fuel shortage, the captain decided to attempt an emergency landing and eventually tried to ditch the airplane off Shannon Airport. The twin engine aircraft crash landed in the Shannon River and sank. All three crew members were quickly rescued.

Crash of a Douglas C-54E-5-DO Skymaster near Stephenville: 39 killed

Date & Time: Oct 3, 1946 at 0503 LT
Type of aircraft:
Operator:
Registration:
N90904
Flight Phase:
Survivors:
No
Site:
Schedule:
New York – Gander – Shannon – London – Berlin
MSN:
27290
YOM:
1945
Country:
Crew on board:
8
Crew fatalities:
Pax on board:
31
Pax fatalities:
Other fatalities:
Total fatalities:
39
Captain / Total flying hours:
3926
Captain / Total hours on type:
1561.00
Copilot / Total flying hours:
1707
Copilot / Total hours on type:
805
Aircraft flight hours:
3731
Circumstances:
The four engine aircraft left New York-La Guardia Airport at 1214LT bound for Berlin, Germany, with intermediate stops in Gander, Shannon and London. While descending over Newfoundland, the crew encountered poor weather conditions and was forced to divert to Stephenville-Ernest Harmon Airport where he landed at 1630LT. For operation reasons, the crew should have a 12 hours rest time and the next departure was then scheduled at 0445LT the following morning. By night, the crew started the takeoff roll from runway 07 and after rotation, continued straight ahead when few minutes later, at an altitude of 1,160 feet, the aircraft hit the slope of a mountain and crashed in a dense wooded area located 7 miles northeast of the airfield. The aircraft christened 'Flagship New England' disintegrated on impact and all 39 occupants were killed. At the time of accident, weather conditions were considered as good with a ceiling at 5,000 feet (overcast) and a visibility above 10 miles.
Crew:
William A. Westerfield, pilot,
Robert Beckman Lehr, copilot,
John B. Tierney Jr., navigator,
James M. Barry, radio officer,
Mark Spelar, flight engineer,
Herbert B. Ewing, purser,
Jerome Lewis, navigator,
Margaret Ann Burleigh, stewardess.
Probable cause:
It was determined that the pilot in command continued in a straight ahead direction after rotation instead of turning to the right to avoid the rising terrain. Unfortunately, it was not possible to ascertain the reason why the crew decided to follow such wrong procedure. In conclusion, on the basic of the foregoing, the Board determined that the probable cause of this accident was the action of the pilot in maintaining the direction of takeoff toward higher terrain over which adequate clearance could not be gained.
Final Report:

Crash of a Lockheed L-049 Constellation in Shannon

Date & Time: Sep 24, 1946
Operator:
Registration:
NC88831
Survivors:
Yes
Schedule:
New York – Shannon – London
MSN:
2031
YOM:
1945
Location:
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from New York-La Guardia, the crew completed the approach and landed properly. After touchdown, the captain requested the copilot for flaps up when the aircraft sank on its belly, skidded for several yards and came to rest, broken in two. All 36 occupants were evacuated safely while the aircraft was written off.
Probable cause:
It was determined that the accident was caused by a misinterpretation from the copilot that raised the landing gear instead of the flaps, causing the aircraft to fail on its belly.

Crash of a Douglas DC-4-1009 near Gander: 27 killed

Date & Time: Sep 18, 1946 at 0242 LT
Type of aircraft:
Operator:
Registration:
OO-CBG
Survivors:
Yes
Schedule:
Brussels – Shannon – Gander – New York
MSN:
42986
YOM:
1946
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
27
Circumstances:
Following an uneventful flight from Shannon, the crew started the descent to Gander Airport by night and in poor weather conditions. Most probably in a way to establish a visual contact with the ground, the captain reduced his altitude and passed below the minimum safe altitude when the aircraft hit trees and crashed in flames in a dense wooded area located 35 km from the airport. A crew member and 16 passengers were rescued while 27 other occupants were killed.
Probable cause:
The pilot continued the approach at an insufficient altitude and thus failed to follow the published approach procedures.

Crash of a Douglas DC-3-268B in Shannon

Date & Time: Jun 18, 1946 at 2100 LT
Type of aircraft:
Operator:
Registration:
EI-ACA
Flight Phase:
Survivors:
Yes
MSN:
2178
YOM:
1940
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Shannon Airport, while climbing, the crew reported to ATC that the left engine caught fire. The captain elected to return but as he realized this would not be possible, he decided to attempt an emergency landing. The aircraft crash landed in a marshland near the airport and came to rest. Ten occupants were injured while nine others were unhurt. The aircraft was written off.
Probable cause:
Fire on left engine.

Crash of a De Havilland DH.91 Albatross in Shannon

Date & Time: Jul 6, 1943
Operator:
Registration:
G-AFDK
Survivors:
Yes
Schedule:
Bristol – Shannon
MSN:
6804
YOM:
1938
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On touchdown at Shannon-Rinneanna Airport, the aircraft went out of control, veered off runway and came to rest. While all 14 occupants escaped uninjured, the aircraft was damaged beyond repair.
Crew:
Geoffrey Palliser Moss, pilot,
D. M. Revell, radio operator,
C. Caseley, flight engineer,
R. Gilmour,
A. H. Wigmore.
Passengers:
Neil Richardson,
Simon Marks,
Pauline Gower,
Gerard d'Erlanger,
John Marchbank,
David Smillie Smith MacDowall,
Grahame Temple Meller,
Keith Granville,
Piers John Barnes Wimbush.