Accident McDonnell Douglas MD-11C I-DUPA,
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ASN Wikibase Occurrence # 147061
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Date:Tuesday 14 January 2003
Type:Silhouette image of generic MD11 model; specific model in this crash may look slightly different    
McDonnell Douglas MD-11C
Registration: I-DUPA
MSN: 48426/468
Year of manufacture:1992
Engine model:General Electric CF6-80C2D1F
Fatalities:Fatalities: 0 / Occupants: 142
Aircraft damage: None
Location:New York-John F. Kennedy International Airport, NY (JFK/KJFK) -   United States of America
Phase: Landing
Nature:Passenger - Scheduled
Departure airport:Milano, (LIMC)
Destination airport:New York-John F. Kennedy International Airport, NY (JFK/KJFK)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
The flight was at cruise altitude when the flight crew discovered that they were unable to move the control wheel for lateral (aileron) control. The rudder and elevator flight controls remained free for movement. As the flight neared its destination, the crew tried to extend with wing flaps. The leading edge slats extended, but they were unable to extend the trailing edge wing flaps. The flight landed in that condition. Post flight examination of the airplane revealed ice accumulations in all three wheel wells. The ice had accumulated on the aileron control cables, and flap extension cables, and prevented cable movement. The ice was traced to a water leak in the potable water system where a rubber hose attached to a water line fitting, under the floorboard, near the 3R door. When the floorboard in the area was lifted, upward movement of the floorboard was restricted by the rubber hose water line that was attached to the underside of the floor board. Water was observed misting from the line where it attached to the fitting. When the floorboard was lifted further, the water line pulled loose from the fitting, and water flowed out. Examination of the rubber water hose revealed it failure was due to excessive load applied to the crimped joint between the flexible hose and it end fitting. The airplane manufacturer had attached water lines to the underside of the floorboards. The airplane maintenance manuals did not contain any information about how to know if a water line was connected to the underside of a floorboard, or for disconnecting water lines attached to the underside of the floorboards prior to lifting them. There was no jammed flight control checklist in effect at the time of the incident. QAR data revealed the pilots had limited movement with the of the ailerons with the auto-pilot engaged or disengaged through roll control wheel steering (RCWS), a customer selected option for the airplane.
Probable Cause: A leak of potable water onto the lateral (aileron) flight control cables, and flap extension cables, which subsequently froze them in place. An additional cause was the improper procedures used by mechanics for floorboard removal which stretched the rubber hose, and led to the leak, all due to the manufacturer's lack of guidance in the maintenance manuals on floorboard removal.

Accident investigation:
Investigating agency: NTSB
Report number: NYC03IA042
Status: Investigation completed
Download report: Final report



History of this aircraft

Other occurrences involving this aircraft
29 November 2017 N986AR Centurion Air Cargo 0 Sacramento-Mather Airport, CA (MHR/KMHR) min
Wingtip, pod strike


Revision history:

26-Jul-2012 07:20 harro Added
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
09-Dec-2017 18:05 ASN Update Bot Updated [Cn, Operator, Departure airport, Destination airport, Source, Narrative]

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