Aircraft Accident/Incident Report

Lake Michigan, --
Wednesday, October 20, 2004 20:29 CDT

NTSB Narrative Summary Released at Completion of Accident

The Boeing 747-132, operated as an unscheduled domestic cargo flight under 14 CFR Part 121, was climbing through 15,000 feet mean sea level when the number one engine separated from its forward and aft engine mounts resulting in substantial damage to the airplane. The flight diverted to an alternate airport where it landed without further incident. Examination of the engine revealed an uncontained separation of an approximately 180-degree arc of the second stage turbine disk rim. The missing section of the rim coincided with circumferential rub marks on the second stage turbine disk that corresponded to rub marks on the rear inner rails of the second stage turbine vanes. The rubbed areas of the disk and vanes did not exhibit heat cracking consistent with a relatively long time period of rubbing relative to a sudden disk-to-vane contact. The fan rotor bearing did not exhibit rotational distress. The engine did not exhibit any evidence of a blade separation, case rupture, or any other uncontainment. The second stage retaining bolts are coated with a baked-on antiseize compound, FelPro C-200, during manufacture. Metallurgical exam of the second stage turbine bolts revealed cracking in the head-to-shank fillet radius and the presence of silver consistent with Silver Goop. Silver Goop is an anti-seize compound not authorized by the engine manufacturer for use in the high-pressure turbine area but is authorized in the low-pressure compressor area due to the catalytic properties of silver with wet FelPro C-200 resulting in a corrosive mixture that can contribute to bolt fractures. The induced loads from the second stage disk rim separation were estimated to have been 3.6 - 6.6 times greater than to those induced by a fan blade separation. The accident operator purchased an engine as-is and that according to maintenance records was not preserved when it was removed from an airplane belonging to another operator about 5 years prior to the accident. The high-pressure turbine (HPT) module was removed from this engine and installed on one of the accident operator's other engines prior to it being removed and then installed on the accident airplane engine. The accident operator's examination of the HPT was limited to a visual inspection that would not have detected a vane shift or ascertained the integrity second stage turbine vane assembly.

NTSB Probable Cause Narrative

The number one engine separated from the airplane during climb due to the uncontained separation of a portion of the second stage turbine disk rim after the second stage turbine vanes contacted the disk. The second stage turbine vanes contacted the second stage turbine disk due to the operator's inadequate inspection of the high pressure turbine module and the improper repair of the module by unknown maintenance personnel.

Event Information

Type of Event Accident
Event Date 10/20/2004
Event Day of the Week Wednesday
Time of Event 2029
Event Time Zone Central Daylight Time
Event City Lake Michigan
Event State --
Event Country --
Zipcode of the event site --
Event Date Year 2004
Event Date Month 10
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 420432N
Event Location Longitude 0865202W
Event Location Airport --
Event Location Nearest Airport ID --
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles --
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness --
Investigator's weather source Weather Observation Facility
Time of the weather observation 1956 Central Daylight Time
Direction of event from weather observation facility (degrees) --
Weather Observation Facility ID ORD
Elevation of weather observation facility 655
Distance of event from weather observation facility (units?) --
Time Zone of the weather observation CDT
Lighting Conditions Night
Lowest Ceiling Height 1700
Lowest Non-Ceiling Height --
Sky/Lowest/Cloud Conditions Clear
Sky Condition for Lowest Ceiling Overcast
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 11
Dew Point at event time (in degress fahrenheit) 8
Wind Direction (degrees magnetic) 10
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) --
Wind Velocity Indicator --
Wind Gust Indicator Unknown
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.12
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 5
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 22316
NTSB Notification Source FAA
NTSB Notification Date Oct 20 2004 12:00AM
NTSB Notification Time 2230
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Nov 29 2007 8:02AM
User who most recently changed record NTSB\johb
Basic weather conditions Visual Meteorological Cond
FAA District Office Detroit FSDO

Aircraft Involved

Aircraft #1

Aircraft Registration Number N709CK
NTSB Number CHI05MA011
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 121: Air Carrier
Type of Flight Plan filed IFR
Flight plan Was Activated? No
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Boeing
Aircraft Model 747-132
Aircraft Series Identifier --
Aircraft Serial Number 20247
Certified Max Gross Weight --
Aircraft Category Airplane
Aircraft Registration Class --
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 7
Number of Engines 4
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Continuous Airworthiness
Date of Last Inspection Oct 1 2004 12:00AM
Airframe hours since last inspection 94.1
Airframe Hours 93548.7
ELT Installed --
ELT Activated --
ELT Aided Location of Event Site --
ELT Type --
Aircraft Owner Name Kalitta Air, LLC
Aircraft Owner Street Address 818 Willow Run Airport
Aircraft Owner City Ypsilanti
Aircraft Owner State MI
Aircraft Owner Country USA
Aircraft Owner Zipcode 48198
Operator is an individual? No
Operator Name --
Operator Same as Owner? Yes
Operator Is Doing Business As --
Operator Address Same as Owner? Yes
Operator Street Address --
Operator City --
Operator State --
Operator Country --
Operator Zip code --
Operator Code KCSA
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 Non-scheduled
Indicates Domestic or International Flight International
Operator carrying Pax/Cargo/Mail Cargo
Type of Flying (Per_Bus / Primary) --
Second Pilot on Board Yes
Departure Point Same as Event No
Departure Airport Code ORD
Departure City CHICAGO
Departure State IL
Departure Country USA
Departure Time 2010
Departure Time Zone CDT
Destination Same as Local Flt --
Destination Airport Code JFK
Destination City NEW YORK
Destination State NY
Destination Country USA
Specific Phase of Flight Climb
Report sent to ICAO? No
Evacuation occurred No
Date of most recent change to record Sep 4 2007 2:04PM
User who most recently changed record DINC
Since inspection or accident --
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --