Aviation Accident Summaries

Aviation Accident Summary DCA88MA052

SEATTLE, WA, USA

Aircraft #1

N819PH

de Havilland DHC-8

Analysis

SHORTLY AFTER TKOF FROM SEATTLE-TACOMA INTL AIRPORT, THE CREW NOTED A RT ENG POWER LOSS AND DECIDED TO RETURN FOR A PRECAUTIONARY LNDG. AFTER LOWERING THE LNDG GEAR, A MASSIVE FIRE WAS DISCOVERED IN THE RT ENG NACELLE. AFTER LNDG, DIRECTIONAL CONTROL AND ALL BRAKING WAS LOST. THE ACFT DEPARTED THE LEFT SIDE OF THE RWY 16L AFTER THE LEFT POWER LEVER WAS MOVED TO FLT IDLE. THE F/O ADVISED TWR THAT THE ACFT WAS OUT OF CONTROL. THE ACFT ROLLED ONTO THE RAMP AREA WHERE IT STRUCK A RWY DESIGNATOR SIGN, GROUND EQUIPMENT, AND JETWAYS B7 AND B9. THE ACFT WAS SUBSEQUENTLY DESTROYED BY FIRE. INVESTIGATION REVEALED THAT DURING OVERHAUL THE HIGH PRESSURE FUEL FILTER COVER WAS IMPROPERLY INSTALLED ON THE ENG AND THE IMPROPER INSTALLATION WAS NOT DISCOVERED DRG COMPANY INSTALLATION OF THE ENG ON THE ACFT. THIS LED TO A MASSIVE FUELLEAK AND THE NACELLE FIRE. THE FIRE/EXPLOSION CAUSED THE LOSS OF THE ENG PANELS, REDUCING THE EFFECTIVENESS OF THE FIRE SUPPRESSION SYSTEM AND ALLOWING OTHER SYSTEMS TO BE DAMAGED. (FOR FURTHER INFORMATION-SEE NTSB/AAR-89/02.)

 

Source: NTSB Aviation Accident Database

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