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Maui, HI
The Safety Board's full report on this investigation is provided as Aviation Accident Report number AAR-89/03. To obtain a copy of this report, or to view the executive summary online, please see the Web site at http://www.ntsb.gov/publictn/publictn.htm FLT 243 EXPERIENCED AN EXPLOSIVE DECOMPRESSION AND STRUCTURAL FAILURE AT FL240 WHILE ENROUTE FROM HILO, HI, TO HONOLULU, HI. APRX 18 FT OF CABIN SKIN AND STRUCTURE AFT OF THE CABIN ENTRANCE DOOR AND ABOVE THE PASSENGER FLOORLINE SEPARATED FROM THE ACFT. ONE FLT ATTENDANT WHO WAS STANDING IN THE AISLE WAS SWEPT OVERBOARD. THE FLT DIVERTED TO MAUI AND A LANDING WAS ACCOMPLISHED. EXAMINATION OF THE ACFT REVEALED DISBONDING AND FATIGUE DAMAGE WHICH LED TO THE FAILURE OF THE LAP JOINT AT S-10L AND THE SEPARATION OF THE FUSELAGE UPPER SKIN BETWEEN STATIONS 360 AND 540. (SEE NTSB/AAR-89/03)
The Safety Board's full report on this investigation is provided as Aviation Accident Report number AAR-89/03. To obtain a copy of this report, or to view the executive summary online, please see the Web site at http://www.ntsb.gov/publictn/publictn.htm FLT 243 EXPERIENCED AN EXPLOSIVE DECOMPRESSION AND STRUCTURAL FAILURE AT FL240 WHILE ENROUTE FROM HILO, HI, TO HONOLULU, HI. APRX 18 FT OF CABIN SKIN AND STRUCTURE AFT OF THE CABIN ENTRANCE DOOR AND ABOVE THE PASSENGER FLOORLINE SEPARATED FROM THE ACFT. ONE FLT ATTENDANT WHO WAS STANDING IN THE AISLE WAS SWEPT OVERBOARD. THE FLT DIVERTED TO MAUI AND A LANDING WAS ACCOMPLISHED. EXAMINATION OF THE ACFT REVEALED DISBONDING AND FATIGUE DAMAGE WHICH LED TO THE FAILURE OF THE LAP JOINT AT S-10L AND THE SEPARATION OF THE FUSELAGE UPPER SKIN BETWEEN STATIONS 360 AND 540. (SEE NTSB/AAR-89/03)