Estado: | Accident investigation report completed and information captured |
Fecha: | martes 22 septiembre 1981 |
Hora: | 16:48 |
Tipo: |  McDonnell Douglas DC-10-30CF |
Operador: | Air Florida |
Registración: | N101TV |
Numéro de série: | 46800/96 |
Año de Construcción: | 1973-03-27 (8 years 6 months) |
Horas Totales de la Célula: | 25824 |
Ciclos: | 6214 |
Motores: | 3 General Electric CF6-50C2 |
Tripulación: | Fatalidades: 0 / Ocupantes: 15 |
Pasajeros: | Fatalidades: 0 / Ocupantes: 56 |
Total: | Fatalidades: 0 / Ocupantes: 71 |
Daños en la Aeronave: | Considerable |
Consecuencias: | Repaired |
Ubicación: | Miami International Airport, FL (MIA) ( Estados Unidos de América)
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Fase: | Despegue (TOF) |
Naturaleza: | Vuelo Doméstico Programado |
Aeropuerto de Salida: | Miami International Airport, FL (MIA/KMIA), Estados Unidos de América |
Aeropuerto de Llegada: | Fort Lauderdale International Airport, FL (FLL/KFLL), Estados Unidos de América |
Número de Vuelo: | 2198 |
Descripción:Air Florida Airlines, Flight 2198, a DC-10-30CF sustained an uncontained failure of its right underwing engine (No. 3) during the takeoff roll at Miami International Airport, Florida. The engine failure occurred at about 90 knots indicated airspeed. The pilot rejected the takeoff and stopped the aircraft safely.
The aircraft was damaged by the release of high energy engine debris. The resultant damage caused an uncommanded retraction of the right wing outboard leading edge slat. Components of the No. 3 engine control system and fire protection system, the electrical system, and the Nos. 1 and 3 hydraulic systems were also damaged by engine debris.
Probable Cause:
PROBABLE CAUSE: "The failure of quality control inspections to detect the presence of foreign material in the low pressure turbine cavity during the reassembly of the low pressure turbine module after installation of the stage 1 low pressure turbine rotor disk. The foreign material in the low pressure turbine cavity damaged the bolt holding the stage 1 low pressure turbine rotor disk and stage 2 low pressure turbine rotor disk together. The bolts failed at high engine thrust and the stage 3 low pressure turbine disk separated from the low pressure turbine rotor assembly, oversped, and burst."
Accident investigation:
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Investigating agency: | NTSB  |
Status: | Investigation completed |
Duration: | 196 days (7 months) | Accident number: | NTSB-AAR-82-3 | Download report: | Final report
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Subsiguiente / acciones de seguridad
NTSB issued 2 Safety Recommendations
Issued: 06-APR-1982 | To: FAA | A-82-38 |
EXPEDITE THE PUBLICATION OF GUIDANCE MATERIAL FOR ACCEPTABLE MEANS OF COMPLIANCE WITH 14 CFR 25.903(D)(1), WHICH INCLUDES COMPLIANCE DOCUMENTATION BY FAILURE MODE AND EFFECT ANALYSIS, PROVIDES FOR ROTOR FRAGMENT ENERGY LEVELS AND PATHS BASED ON CASES OF SEVERE IN-SERVICE DAMAGE, AND REFLECTS ADVANCES IN ANALYTICAL TECHNIQUES AND CONCEPTS WHICH HAVE TAKEN PLACE SINCE CERTIFICATION PROGRAMS OF THE EARLY 1970\'S. (Closed - Acceptable Action) |
Issued: 06-APR-1982 | To: FAA | A-82-39 |
ACTIVELY ENCOURAGE RESEARCH AND DEVELOPMENT IN CONTAINMENT TECHNOLOGY AND ENGINE RELIABILITY, INCLUDING BASIC DESIGN CONCEPTS, MANUFACTURING PROCESSES, AND MAINTENANCE FACTORS TO DETECT AND PREVENT IMPENDING FAILURES. (Closed - Acceptable Action) |
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Fotos
Map
This map shows the airport of departure and the intended destination of the flight. The line between the airports does
not display the exact flight path.
Distance from Miami International Airport, FL to Fort Lauderdale International Airport, FL as the crow flies is 34 km (21 miles).
This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.