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ACCIDENT & INCIDENT REPORTS - DETAIL

Preliminary Report
 

Occurrence Number: 200203671
Release Date: 09-Sep-02
Occurrence Type: Serious-Incident
Location: 6 km N Sydney, Aero.
State: New South Wales (NSW)
Occurrence Date: 10-Aug-02
Time/Zone: 1507 hours EST
Highest Injury Level: None
Investigation Category: 3
Injuries: Fatal Serious Minor None Total
Crew 0 0 0 0 0
Passenger 0 0 0 0 0
Ground 0 0 0 0 0
Total 0 0 0 0 0
Aircraft Details
Aircraft Manufacturer: Boeing Co
Aircraft Model: 747-436
Aircraft Registration: G-BNLK
Serial Number:  
Type of Operation: Air Transport, Scheduled
Damage to Aircraft: Minor (Damage to the forward cargo bay and heat affected fuselage structure)
Departure Time: 1500 hours EST
Departure Point: Sydney, NSW
Destination: Singapore
Crew Details: Role Class of Licence Hours on Type Hours Total
         


FACTUAL INFORMATION

Shortly after departing Sydney, the flight crew became aware of the smell of smoke in the flight deck. Approximately one minute later, the forward cargo fire warning message was displayed on the engine indicating and crew alerting system (EICAS) screen. At this time, the Cabin Service Director called the flight crew and reported smoke mist visible in the passenger cabin. The flight crew reported that they actioned the appropriate check list, activated the fire suppression system, and transmitted a MAYDAY. The crew subsequently returned the aircraft to Sydney, conducting an overweight landing on runway 34L.

While on final approach, the fire warning ceased. Cabin crew reported that there was no longer smoke in the cabin, but the smell was still evident. After landing, the aircraft was stopped on the runway where the emergency services were able to confirm that no fire was visible. The passengers were then disembarked via mobile stairs placed at the front left door.

An inspection of the forward cargo bay found signs of heat damage to a section of the sidewall lining adjacent to the main deck galley chiller boost fan. On removal of the lining, the fuselage insulation blanket between body stations BS880 and BS900 was found burnt, with the fuselage skin, stringers and frame structure also showing signs of being heat affected.

The boost fan was found to have a hole burned in its housing adjacent to the electrical connector, with four of the seven electrical wires burned through. All of the fan impeller blades were also found to have failed.

The investigation is continuing.


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 Page updated:  08-Aug-2002  [Help] [Search] [Subscribe] [Newsroom] [Copyright©] [Privacy] [Webmaster
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