Subic Bay International Airport
Aircraft Accident/Incident Report

Subic Bay
Sunday, June 2, 2002 16:00 UTC

NTSB Narrative Summary Released at Completion of Accident

As the MD-11F airplane was on final approach to landing, the flight crew selected flaps 50 (full extension) and continued to approach the runway. About one minute later, the flight crew heard a loud bang and felt the airplane shudder. The airplane then began to roll to the left, and nearly full right control wheel input was required to counter the left roll. The flight crew performed a missed approach, declared an emergency, and diverted to another airport. During the landing, the airplane experienced a tailstrike. The flight control malfunction was initiated by the failure of the bolt assemblies securing the left inboard flap outboard hinge to the wing trailing edge. The lower outboard nut failed first due to stress corrosion cracking. The lower inboard bolt failure was initiated by fatigue and was completed by overload following the failure of the nut on the lower outboard bolt. The two upper bolts failed by overload following the failure of both lower bolt assemblies. The failure of all four bolt assemblies allowed the flap hinge to pull free from the wing trailing edge, drop and jam the left, inboard flap at the fully extended position. The separating flap hinge pulled the components of the left hand spoiler system from their original position resulting in the deployment of spoilers L1, L4, and L5. The deployment of three of the five left-hand spoilers caused the uncommanded left roll of the aircraft. Hydraulic system no. 3 was also damaged when the flap hinge separated allowing the hydraulic fluid to drain out of the system. Once the hydraulic quantity is depleted, the number three spoilers on each wing will not operate. According to Boeing engineers, the loss of the R3 spoiler would affect the ability of the right wing flight controls to counter the left roll of the aircraft. The airplane was originally used as a manufacturer flight test airplane. The impact of the flight-testing of the airplane to the overall fatigue life of the flap hinge bolts could not be determined. Prior to the accident, there were no requirements for the inspection of the flap hinge bolt assemblies on MD-11 aircraft. The manufacturer issued a service bulletin after the accident recommending inspection and/or replacement of the flap hinge, lower bolt assemblies. The bulletin recommends changing from alloy steel bolts and nuts to Inconel. Inconel is a nickel-based alloy that is highly resistant to general corrosion and stress corrosion cracking, which can occur in low alloy, high strength steel. The FAA issued an Airworthiness Directive mandating the Service Bulletin.

NTSB Probable Cause Narrative

The failure of the lower outboard nut and bolt assembly of the left inboard flap's outboard hinge that resulted from stress corrosion cracking and fatigue. Factors contributing to the accident were the inadequate materials specification of the bolt, and inadequate inspection requirements for the assembly.

Event Information

Type of Event Accident
Event Date 6/2/2002
Event Day of the Week Sunday
Time of Event 1600
Event Time Zone Coordinated Universal Time? Same as GMT
Event City Subic Bay
Event State --
Event Country --
Zipcode of the event site --
Event Date Year 2002
Event Date Month 6
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude --
Event Location Longitude --
Event Location Airport Subic Bay International
Event Location Nearest Airport ID SFS
Indicates whether the acc/inc occurred off or on an airport Off Airport/Airstrip
Distance from airport in statute miles 1
Degrees magnetic from airport --
Airport Elevation --
Weather Briefing Completeness Full
Investigator's weather source Witness
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 Not Gusting
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 2
Injury Total Serious --
Injury Total All --
Investigating Agency NTSB
NTSB Docket Number (internal use) 19074
NTSB Notification Source NTSB Comm. Center
NTSB Notification Date Jun 16 2002 12:00AM
NTSB Notification Time 1200
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Dec 20 2005 6:27AM
User who most recently changed record NTSB\JOHB
Basic weather conditions Visual Meteorological Cond
FAA District Office AAI-100 (FAA HQ)

Aircraft Involved

Aircraft #1

Aircraft Registration Number N601FE
NTSB Number DCA02MA042
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 121: Air Carrier
Type of Flight Plan filed IFR
Flight plan Was Activated? Yes
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name McDonnell Douglas
Aircraft Model MD-11F
Aircraft Series Identifier --
Aircraft Serial Number 48401
Certified Max Gross Weight 632000
Aircraft Category Airplane
Aircraft Registration Class U.S. Registered/Foreign Soil
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 5
Number of Engines 3
Fixed gear or retractable gear Retractable
Aircraft, Type of Last Inspection Continuous Airworthiness
Date of Last Inspection Jun 10 2002 12:00AM
Airframe hours since last inspection 88
Airframe Hours 37443
ELT Installed Unknown
ELT Activated Unknown
ELT Aided Location of Event Site Unknown
ELT Type --
Aircraft Owner Name Wilmington Trust Company
Aircraft Owner Street Address Rodney Square North
Aircraft Owner City Wilmington
Aircraft Owner State DE
Aircraft Owner Country USA
Aircraft Owner Zipcode --
Operator is an individual? No
Operator Name FEDERAL EXPRESS CORP
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address --
Operator City Memphis
Operator State TN
Operator Country USA
Operator Zip code 38118
Operator Code FDEA
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 BKK
Departure City Bangkok
Departure State --
Departure Country TH
Departure Time 1930
Departure Time Zone UTC
Destination Same as Local Flt --
Destination Airport Code SFS
Destination City Subic Bay
Destination State --
Destination Country RP
Specific Phase of Flight Approach - VFR pattern - final approach
Report sent to ICAO? Yes
Evacuation occurred No
Date of most recent change to record --
User who most recently changed record --
Since inspection or accident Time of Accident
Event Location Runway Number and Location NA
Runway Length --
Runway Width --
Sight Seeing flight No
Air Medical Flight No
Medical Flight --