Serious incident Boeing 747-422 N175UA,
ASN logo
ASN Wikibase Occurrence # 370413
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Tuesday 1 April 2003
Time:12:15 LT
Type:Silhouette image of generic B744 model; specific model in this crash may look slightly different    
Boeing 747-422
Owner/operator:United Airlines
Registration: N175UA
MSN: 24382/806
Year of manufacture:1990
Total airframe hrs:50293 hours
Engine model:Pratt & Whitney PW4056
Fatalities:Fatalities: 0 / Occupants: 319
Aircraft damage: None
Category:Serious incident
Location:Chicago, IL -   United States of America
Phase: En route
Nature:Passenger - Scheduled
Departure airport:Hong Kong (KHKG)
Destination airport:Chicago-O'Hare International Airport, IL (ORD/KORD)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
While in normal cruise flight, the crew experienced lateral control problems. An emergency was declared. The aircraft landed safely at the intended destination. Evidence of a water leak was identified by the cabin crew approximately 5 hours from the destination. Efforts to control the leak were effective, however it was not completely stopped. Water was reported coming from the upper deck and flowing through the main deck ceiling. The flight was subsequently directed by air traffic control to make an enroute course change. However, when this command was entered in the Flight Management Computer (FMC) the aircraft began a shallow left turn instead of a right turn as required. Initial attempts to disconnect the autopilot were not successful and the autopilot was manually overridden. The relief first officer at the controls stated the controls "felt unusual" and "stiff." The captain reported elevator and rudder were normal, but bank angle was limited. The landing was accomplished smoothly and safely according to the captain, and the aircraft was taxied to the gate without incident. After landing, the captain noted the controls felt normal. Ramp personnel reported a significant amount of water draining from the fuselage and the drain masts at the gate. A post-incident examination of the aircraft revealed that areas of the main deck carpeting was saturated. The canted pressure deck overboard drains were not obstructed. A 6-inch long by 0.125-inch wide gap was located along the outboard edge of the canted pressure bulkhead on the right side of the aircraft. The seam was not sealed as required. Immediately aft of the canted pressure bulkhead were aileron and flight spoiler control cables. Four (4) circuit breakers common to the external drain line heaters were found open. The external drain lines route wastewater from the cabin overboard. The breakers were pulled in conjunction with routine cleaning of the drain lines prior to departure. Ground functional testing of the aileron controls, the aileron trim and the autopilot did not find any anomalies. A flight test was completed to verify in-flight operation of the flight controls and potable water system. No anomalies were noted. Airline procedures related to the routine inspection and cleaning of the external drains were reviewed. Resetting of the drain heater circuit breakers was the last item. A service bulletin had been issued which recommended testing, cleaning and inspection of the canted pressure deck drainage system (overboard drains), general visual inspection of the deck structure a pressurization test. Service bulletin instructions included a visual inspection for loose, missing or cracked sealant. The airline was in the process of incorporating the service bulletin into its maintenance program. As a result, the initial service bulletin procedures had not been completed prior to the incident. An airworthiness directive (AD) which required cleaning of "the cavity aft of the wing center section" and verification that all drains were open and clean was in effect at the time of the incident and had been complied with. A new AD was issued following the incident which mandated full compliance with the existing service bulletin.

Probable Cause: Failure of company maintenance personnel to fully comply with published maintenance/inspection procedures, as well as the resulting inoperative drain heaters and restricted movement of the aileron control cables. Contributing factors were the impeded waste water drain system due to the inoperative heaters and the reduced aileron control due to restricted movement of the control cables.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CHI03IA097
Status: Investigation completed
Duration: 6 months
Download report: Final report

Sources:

NTSB CHI03IA097

History of this aircraft

Other occurrences involving this aircraft
14 September 1997 N175UA United Airlines 0 Grand Forks, ND non

Location

Revision history:

Date/timeContributorUpdates
25-Mar-2024 10:27 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org