Lajes – Hamilton – Charleston
Flight / Schedule
Lajes – Hamilton – Charleston
Aircraft
Douglas C-124 Globemaster IIRegistration
53-0033
MSN
44328
Year of Manufacture
1953
Operator
United States Air Force - USAFDate
October 3, 1956 at 07:21 AM
Type
CRASHFlight Type
Military
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Crash Location
Charleston-Intl South Carolina
Region
North America • United States of America
Coordinates
32.8803°, -80.0386°
Crash Cause
Human factor
Narrative Report
On October 3, 1956 at 07:21 AM, Lajes – Hamilton – Charleston experienced a crash involving Douglas C-124 Globemaster II, operated by United States Air Force - USAF, with the event recorded near Charleston-Intl South Carolina.
The flight was categorized as military and the reported phase was landing (descent or approach) at a airport (less than 10 km from airport) crash site.
10 people were known to be on board, 3 fatalities were recorded, 7 survivors were identified or estimated. This corresponds to an estimated fatality rate of 30.0%.
Crew on board: 9, crew fatalities: 2, passengers on board: 1, passenger fatalities: 1, other fatalities: 0.
The listed crash cause is human factor. The Douglas C-124 transport plane departed Lajes AFB, Azores on a flight across the Atlantic Ocean to Bermuda-Kindley Field (NWU). The airplane remained on the ground at Bermuda for two hours. It took off again at 01:50 EST, bound for Charleston AFB, SC (CHS). Over the Azalea intersection the pilot checked and was advised that Charleston weather had deteriorated rapidly, presently 15,000 ft broken, visibility 1/4 mile with ground fog. The captain decided enter a holding pattern over Charleston to wait for the sun to burn off the fog. At approximately 06:30 visibility had slightly increased to 1/2 mile in ground fog. Five minutes later a Delta Air Lines flight landed following an ILS approach. The captain decided to carry out a GCA approach and was cleared for this at 06:35. The descent and final approach were normal until just prior to or reaching GCA minimums. At this time the aircraft got too low and clipped the tops of trees that stood about 68 feet above the ground. This caused a fast torque drop and subsequent loss of the no. 3 engine. The co-pilot then declared an emergency. The propeller of engine no.3 was feathered, the flaps were retracted, and an attempt as made to raise the landing gear. Indications were that the right main gear did not retract, and there was damage to the underside of the aircraft. Prior to the emergency the navigator had been asleep (the crew had been on duty for nearly 20 hours). Thus, he had not been monitoring the approach with radar. Also, he made no attempt to assist with dead reckoning, or in any other way to prevent the pilot from becoming lost. At 06:48, the crew became uncertain of their position. They flew for the next 33 minutes in the vicinity of Charleston AFB, at an altitude of only 800 to 1000 feet, because the aircraft would climb no higher even with max power. The aircraft was lost from GCA search radar, apparently due to the low altitude. The passenger and two crew members were killed while seven other occupants were injured.
Aircraft reference details include registration 53-0033, MSN 44328, year of manufacture 1953.
Geospatial coordinates for this crash are approximately 32.8803°, -80.0386°.
Fatalities
Total
3
Crew
2
Passengers
1
Other
0
Crash Summary
The Douglas C-124 transport plane departed Lajes AFB, Azores on a flight across the Atlantic Ocean to Bermuda-Kindley Field (NWU). The airplane remained on the ground at Bermuda for two hours. It took off again at 01:50 EST, bound for Charleston AFB, SC (CHS). Over the Azalea intersection the pilot checked and was advised that Charleston weather had deteriorated rapidly, presently 15,000 ft broken, visibility 1/4 mile with ground fog. The captain decided enter a holding pattern over Charleston to wait for the sun to burn off the fog. At approximately 06:30 visibility had slightly increased to 1/2 mile in ground fog. Five minutes later a Delta Air Lines flight landed following an ILS approach. The captain decided to carry out a GCA approach and was cleared for this at 06:35. The descent and final approach were normal until just prior to or reaching GCA minimums. At this time the aircraft got too low and clipped the tops of trees that stood about 68 feet above the ground. This caused a fast torque drop and subsequent loss of the no. 3 engine. The co-pilot then declared an emergency. The propeller of engine no.3 was feathered, the flaps were retracted, and an attempt as made to raise the landing gear. Indications were that the right main gear did not retract, and there was damage to the underside of the aircraft. Prior to the emergency the navigator had been asleep (the crew had been on duty for nearly 20 hours). Thus, he had not been monitoring the approach with radar. Also, he made no attempt to assist with dead reckoning, or in any other way to prevent the pilot from becoming lost. At 06:48, the crew became uncertain of their position. They flew for the next 33 minutes in the vicinity of Charleston AFB, at an altitude of only 800 to 1000 feet, because the aircraft would climb no higher even with max power. The aircraft was lost from GCA search radar, apparently due to the low altitude. The passenger and two crew members were killed while seven other occupants were injured.
Cause: Human factor
Occupants & Outcome
Crew On Board
9
Passengers On Board
1
Estimated Survivors
7
Fatality Rate
30.0%
Known people on board: 10
Operational Details
Schedule / Flight
Lajes – Hamilton – Charleston
Operator
United States Air Force - USAFFlight Type
Military
Flight Phase
Landing (descent or approach)
Crash Site
Airport (less than 10 km from airport)
Region / Country
North America • United States of America
Aircraft Details
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