Ted Stevens International Airport
Aircraft Accident/Incident Report

Anchorage, Alaska 99502
Wednesday, October 9, 2002 17:40 AKD

NTSB Narrative Summary Released at Completion of Accident

The instrument flight rules scheduled international flight was in cruise flight at FL350 with the autopilot engaged, when it abruptly rolled into a 30 to 40 degree left bank. There were indications that the lower rudder moved to the left blowdown limit, and remained there. Emergency procedures failed to correct the problem, and the flight diverted to the nearest airport for an emergency landing. As the airspeed decreased during the approach, the lower rudder deflected further to the left. The flightcrew used asymmetric engine thrust to maintain heading. After landing, the lower rudder remained deflected fully to the left, and could not be repositioned until the hydraulic pressure was relieved. An inspection of the forged aluminum manifold of the lower rudder power control module (PCM) revealed the end portion which houses the yaw damper actuator had fractured off from the main portion of the manifold. The lower rudder PCM and the flight data recorder (FDR) were sent to the NTSB laboratory. The data retrieved from the FDR showed an initial lower rudder deflection of 17.5 degrees left, and a subsequent increase to 32 degrees (full) left. The incident airplane has two independently supported and operated rudders, which provide yaw control. Typically, the upper and lower rudders operate in unison. The hydraulic actuators for the lower and upper rudders are controlled by independent power control modules. The power control modules for both the upper and lower rudders are virtually identical. The fractured power control module was disassembled and inspected. The yaw damper piston was protruding from the fracture, and precluded functional testing of the module. The individual components of the power control module were tested, and no anomalies were found. Dimensional checks showed no discrepancies, and metallurgical testing showed the manifold material was consistent with the manufacturer's specifications. Metallurgical examination revealed a mode of crack initiation and growth consistent with fatigue. A non-destructive inspection process was developed, and a group of similar power control modules were inspected. The group contained power control modules with higher and lower use cycles than the incident airplane's power control module. No similar fractures were found. As a result of this incident, the airplane's manufacturer has issued an Alert Service Bulletin which recommends operators perform an ultrasonic inspection on pertinent high-time lower and upper rudder power control modules. The Federal Aviation Administration has issued a Notice of Proposed Rule Making for a airworthiness directive which would make the ultrasonic inspection mandatory for all affected airplanes.

NTSB Probable Cause Narrative

The fatigue fracture of the lower rudder power control module manifold, which resulted in a lower rudder hardover.

Event Information

Type of Event Incident
Event Date 10/9/2002
Event Day of the Week Wednesday
Time of Event 1740
Event Time Zone --
Event City Anchorage
Event State ALASKA
Event Country --
Zipcode of the event site 99502
Event Date Year 2002
Event Date Month 10
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 611028N
Event Location Longitude 1495947W
Event Location Airport Ted Stevens International
Event Location Nearest Airport ID PANC
Indicates whether the acc/inc occurred off or on an airport On Airport
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness Full
Investigator's weather source Pilot
Time of the weather observation
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID --
Elevation of weather observation facility --
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation --
Lighting Conditions Night
Lowest Ceiling Height --
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) --
Air Temperature at event time (in degrees celsius) --
Dew Point at event time (in degress fahrenheit) --
Wind Direction (degrees magnetic) --
Variable Wind Indicator --
Wind Speed (knots) --
Wind Velocity Indicator --
Wind Gust Indicator Unknown
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) --
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury None
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor --
Injury Total None 404
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 14693
NTSB Notification Source FAA Anchorage, ROC
NTSB Notification Date Oct 9 2002 12:00AM
NTSB Notification Time 1744
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Jun 29 2004 8:02AM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office Anchorage FSDO-03

Aircraft Involved

Aircraft #1

Aircraft Registration Number N661US
NTSB Number ANC03IA001
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 121: Air Carrier
Type of Flight Plan filed IFR
Flight plan Was Activated? Yes
Damage None
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Boeing
Aircraft Model 747-400
Aircraft Series Identifier --
Aircraft Serial Number 23719
Certified Max Gross Weight 873000
Aircraft Category Airplane
Aircraft Registration Class U.S. Registered/U.S. Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 429
Number of Engines 4
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Conditional
Date of Last Inspection Aug 30 2001 12:00AM
Airframe hours since last inspection 5209
Airframe Hours 50090
ELT Installed No
ELT Activated No
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name State Street Bank and Trust Company Trustee
Aircraft Owner Street Address PO Box 778
Aircraft Owner City Boston
Aircraft Owner State MA
Aircraft Owner Country USA
Aircraft Owner Zipcode 02102
Operator is an individual? No
Operator Name NORTHWEST AIRLINES INC
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address 6300 Boeing Ave.
Operator City Anchorage
Operator State AK
Operator Country USA
Operator Zip code 99502
Operator Code NWAA
Owner has at least one certificate --
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not Scheduled
Indicates Domestic or International Flight International
Operator carrying Pax/Cargo/Mail Passenger Only
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board Yes
Departure Point Same as Event No
Departure Airport Code DTW
Departure City Detroit
Departure State MI
Departure Country USA
Departure Time 1403
Departure Time Zone EDT
Destination Same as Local Flt --
Destination Airport Code NRT
Destination City Narita
Destination State --
Destination Country JA
Specific Phase of Flight Cruise - normal
Report sent to ICAO? Yes
Evacuation occurred No
Date of most recent change to record Nov 26 2003 1:19PM
User who most recently changed record PETL
Since inspection or accident Last Inspection
Event Location Runway Number and Location --
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --