Incident Overview

Date: Friday 3 December 1948
Aircraft Type: Douglas DC-6
Owner/operator: American Airlines
Registration Number: NC90733
Location: near Cambray, NM – ÿ United States of America
Phase of Flight: En route
Status: Minor, repaired
Casualties: Fatalities: 0 / Occupants:
Component Affected: Propeller bladePropeller blade
Investigating Agency: CABCAB
Category: Accident
An aircraft incident occurred when a propeller blade experienced a catastrophic failure, resulting in a fire and subsequent emergency landing. The engine failure triggered a significant jolt, leading to the nacelle fire. Despite limited assessment of the damage, the crew initiated an emergency landing at a nearby auxiliary field.An aircraft incident occurred when a propeller blade experienced a catastrophic failure, resulting in a fire and subsequent emergency landing. The engine failure triggered a significant jolt, leading to the nacelle fire. Despite limited assessment of the damage, the crew initiated an emergency landing at a nearby auxiliary field.

Description

The airplane departed Dallas for Tucson at 16:56 to cruise at 18,000 feet. After reaching cruising altitude, the flight proceeded in a routine manner until approximately 19:50, at which time the crew felt a severe jolt when the no. 4 engine separated from its mountings. The nacelle caught fire which was quickly extinguished. Unable to determine the extent of the damage in the nacelle, the crew elected to make an emergency landing at the nearest field, which was at the CAA Auxiliary Field, Columbus, New Mexico. This was accomplished without further incident at 20:10. PROBABLE CAUSE: “Fatigue failure of the propeller blade resulting from circumferential indentation induced on the inside surface of the blade shank during manufacture.”

Primary Cause

Fatigue failure of the propeller blade resulting from circumferential indentation induced on the inside surface of the blade shank during manufacture.Fatigue failure of the propeller blade resulting from circumferential indentation induced on the inside surface of the blade shank during manufacture.

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