Narrative:During the descent between FL200 and FL190 the crew received a No 2 engine generator electrical fault warning, followed by a duct overheat warning in "J" zone. An attendant reported flames below the floor and behind the wall lining aft of L3 door. The attendant discharged a portable fire extinguisher and reported the fire extinguished. A fire warning was then received on No 2 engine. Cockpit and cabin began to fill with smoke. The crew shut down No 2 engine and donned oxygen masks. The pilot landed safely.
The fire originated in the left aft underfloor area of the airplane's fuselage, aft of the C-3 cargo compartment and forward of the rear pressure bulkhead.
Classification:
Inflight fire
Forced landing on runway
Sources:
» NTSB
Follow-up / safety actions
NTSB issued 4 Safety Recommendations
Issued: 27-NOV-1985 | To: FAA | A-85-129 |
REQUIRE THAT A REVISED FUNCTIONAL TEST BE PREPARED AND ISSUE AN AIRWORTHINESS DIRECTIVE TO IMMEDIATELY EVALUATE THE CONDITION OF ALL COMPONENTS OF THE PASSENGER OXYGEN SYSTEM ON LOCKHEED L-1011 AIRCRAFT TO ENSURE OPERATION BOTH DURING AUTOMATIC ACTIVATION AND WHEN ACTIVATED FROM THE FLIGHT ENGINEER\'S STATION. (Closed - Acceptable Action) |
Issued: 27-NOV-1985 | To: FAA | A-85-130 |
REVIEW THE DESIGN OF THE LOCKHEED L-1011 PASSENGER OXYGEN SYSTEM, AND REQUIRE CHANGES AS NEEDED SO THAT THERE IS NO POTENTIAL FOR FAULTS WHICH CAN DISABLE THE SYSTEM AND REMAIN UNDETECTED. (Closed - Acceptable Action) |
Issued: 27-NOV-1985 | To: FAA | A-85-131 |
REVIEW THE DESIGN OF THE LOCKHEED L-1011 CABIN DOOR OPENING MECHANISM TO ENSURE THAT THE MECHANISM WILL OPERATE PROPERLY WHEN EXPOSED TO OVERHEAT CONDITIONS WHICH COULD OCCUR DURING SURVIVABLE IN-FLIGHT AND POSTCRASH FIRE EMERGENCIES, AND REQUIRE MODIFICATION TO PRECLUDE CABIN DOOR OPENING PROBLEMS. (Closed - Acceptable Action) |
Issued: 27-NOV-1985 | To: FAA | A-85-132 |
ISSUE A TELEGRAPHIC AIRWORTHINESS DIRECTIVE TO REQUIRE AN IMMEDIATE ONE-TIME INSPECTION OF ALL CABIN DOORS ON LOCKHEED L-1011 AIRPLANES TO DETERMINE WHETHER THEY WILL OPEN THE MANUAL MODE WITH PRESCRIBED TIME LIMITS USING ENERGY STORED IN THE COUNTERBALANCE MECHANISM. REQUIRE THAT ACTIONS ARE TAKEN BEFORE FURTHER FLIGHT TO CORRECT DEFECTS WHICH CAN AFFECT ADVERSELY THE OPERATION OF A DOOR DURING AN EMERGENCY EVACUATION. (Closed - Acceptable Action) |
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Photos
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 Abu Dhabi International Airport to Singapore-Changi International Airport as the crow flies is 5850 km (3656 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.