N1819U

Destroyed
Fatal

MCDONNELL DOUGLAS DC-10-10 S/N: 46618

Summary

On July 19, 1989, a Mcdonnell Douglas DC-10-10 (N1819U) was involved in an accident near Sioux City, IA. The accident resulted in 111 fatal injuries, 47 serious injuries, 125 minor injuries, with 13 people uninjured out of 296 aboard. The aircraft was destroyed.

The National Transportation Safety Board determined the probable cause of this accident to be: THE INADEQUATE CONSIDERATION GIVEN TO HUMAN FACTORS LIMITATIONS IN THE INSPECTION AND QUALITY CONTROL PROCEDURES USED BY UNITED AIRLINES' ENGINE OVERHAUL FACILITY WHICH RESULTED IN THE FAILURE TO DETECT A FATIGUE CRACK ORIGINATING FROM A PREVIOUSLY UNDECTECTED METALLURGICAL DEFECT LOCATED IN A CRITICAL AREA OF THE STAGE 1 FAN DISK THAT WAS MANUFACTURED BY GENERAL ELECTRIC AIRCRAFT ENGINES. THE SUBSEQUENT CATASTROPHIC DISINTEGRATION OF THE DISK RESULTED IN THE LIBERATION OF DEBRIS IN A PATTERN OF DISTRIBUTION AND WITH ENERGY LEVELS THAT EXCEEDED THE LEVEL OF PROTECTION PROVIDED BY DESIGN FEATURES OF THE HYDRAULIC SYSTEMS THAT OPERATED THE DC-10'S FLIGHT CONTROLS.

This accident is documented in NTSB report DCA89MA063. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1819U.

Accident Details

Date
Wednesday, July 19, 1989
NTSB Number
DCA89MA063
Location
SIOUX CITY, IA
Event ID
20001213X28786
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
111
Serious Injuries
47
Minor Injuries
125
Uninjured
13
Total Aboard
296

Probable Cause and Findings

THE INADEQUATE CONSIDERATION GIVEN TO HUMAN FACTORS LIMITATIONS IN THE INSPECTION AND QUALITY CONTROL PROCEDURES USED BY UNITED AIRLINES' ENGINE OVERHAUL FACILITY WHICH RESULTED IN THE FAILURE TO DETECT A FATIGUE CRACK ORIGINATING FROM A PREVIOUSLY UNDECTECTED METALLURGICAL DEFECT LOCATED IN A CRITICAL AREA OF THE STAGE 1 FAN DISK THAT WAS MANUFACTURED BY GENERAL ELECTRIC AIRCRAFT ENGINES. THE SUBSEQUENT CATASTROPHIC DISINTEGRATION OF THE DISK RESULTED IN THE LIBERATION OF DEBRIS IN A PATTERN OF DISTRIBUTION AND WITH ENERGY LEVELS THAT EXCEEDED THE LEVEL OF PROTECTION PROVIDED BY DESIGN FEATURES OF THE HYDRAULIC SYSTEMS THAT OPERATED THE DC-10'S FLIGHT CONTROLS.

Aircraft Information

Registration
Make
MCDONNELL DOUGLAS
Serial Number
46618
Engine Type
Turbo-jet
Model / ICAO
DC-10-10 DC10
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
3

Registered Owner (Historical)

Status
Deregistered
Country
United States

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DCA89MA063