Charlotte, NC, USA
N809DE
McDonnell Douglas MD-11
The captain stated he was the pilot flying and the takeoff and climb to the cruise altitude of 33,000 feet was conducted within normal parameters. After level off the relief pilot left the cockpit to begin his rest period. Within a few minutes he observed that the number 2 engine master warning light was illuminated, as well as a level 3 alert on the Engine and Alert Display and a red light on the number 2 fire handle and fuel shutoff lever. The fire bell did not activate. He and the first officer performed the memory and initial action items on the hard card checklists for an engine fire and shutdown the No. 2 engine. In addition, the captain discharged an engine fire bottle. The engine fire light continued to illuminate. The captain then fired a second engine fire bottle. The engine fire light continued to be illuminated. The captain requested that the relief pilot return to the cockpit. He then contacted Air Traffic Control (ATC) and told them that their No. 2 engine was on fire and that they intended to land at the nearest suitable field. ATC responded that Charlotte was 35 miles away with a 10,000 foot runway. He asked for radar vectors and an immediate descent into Charlotte. They were given a lower altitude. The first officer initiated fuel dumping. The relief pilot returned to the cockpit and he asked the relief pilot and the first officer to run the checklists. As they descended the aircraft encountered heavy rain, light hail, and moderate turbulence. In addition, they observed a bright flash to the left of the nose, which might have been a lightning strike. As they completed the descent and approach checklists he told the crew to expect an emergency evacuation upon landing and directed the first officer to so inform the flight attendants. The aircraft was configured for an engine out approach and they reviewed the loss of a second engine procedure. The remainder of the approach, touchdown and landing roll occurred within normal parameters. He brought the airplane to a stop on the runway. The engine fire indication remained illuminated. The relief pilot stated they did not terminate fuel dumping prior to landing. They completed the items on the evacuation checklist. He then ordered an evacuation of the airplane. According to Delta Air Lines representatives, examination of the No. 2 engine by company maintenance personnel found one fire loop chafed through an adjacent cable, an integrated drive generator (IDG) feeder cable, inside the No. 2 engine cowling This allowed a direct 115 volt AC connection between the IDG and the fire detection control unit. The result was an electrical short and complete failure of the detection control unit that was indicated in the cockpit as a fire warning. There was no evidence of fire in the No. 2 engine. Boeing Service Bullettin MD11-71-086 was issued on May 21, 1996. The subject of the service bulletin was "Power Plant - Electrical Harness - Replace/Modify Integrated Drive Generator (IDG) Wire Harness Support Brackets". On May 21, 2001, Boeing elevated the service bulletin to the "Alert" level. Boeing recommended that aircraft operators accomplish the service bulletin within 1 year. According to Delta Air Lines personnel, in November 2001, Delta Air Lines Aircraft Engineering issued a Engineering Order to comply with Alert Service Bulletin MD11-71A086. The Engineering Order stated that all engines should be inspected and modified by November 2002. All three engines on the accident aircraft were inspected and modified in accordance with the Engineering Order on March 3, 2002. On March 28, 2002, the No. 2 engine was changed and the engine installed had not been modified by the Engineering Order.The Delta Airlines descent, approach, and before landing checklists dated June 30, 2000, and which were in use at the time of the accident, required the pilots to check the Engine and Alert Display. When fuel dumping is activated, a message is displayed on the Engine and Alert Display.
HISTORY OF FLIGHT On March 31, 2002, about 1945 eastern standard time, a McDonnell Douglas MD-11, N809DE, registered to Delta Air Lines, Inc., operating as a Title 14 CFR Part 121 scheduled international passenger flight, Delta flight number 12, executed an emergency landing and passenger evacuation at the Charlotte/Douglas International Airport, Charlotte, North Carolina. Instrument meteorological conditions prevailed and an international instrument flight plan was filed. The aircraft received minor damage, and three flightcrew, 11 cabincrew and 215 passengers were not injured. Eleven passengers received minor injuries and five passengers sustained serious injuries. The flight departed Atlanta for London's Gatwick Airport at 1902. The captain stated that he was the pilot flying and also he was acting as a Line Check Airman providing operating experience training to the first officer. This was the first officer's first operating experience segment as an MD-11 first officer. The takeoff and climb to the cruise altitude of 33,000 feet was conducted within normal parameters. After level off the relief pilot left the cockpit to begin his rest period. Within a few minutes he observed that the number 2 engine master warning light was illuminated, as well as a level 3 alert on the EAD (Engine and Alert Display) and a red light on the number 2 fire handle and fuel shutoff lever. The fire bell did not activate. He and the first officer performed the memory and initial action items on the hard card checklists for an engine fire. In addition, the captain discharged an engine fire bottle. The engine fire light continued to illuminate. The captain then fired a second engine fire bottle. The engine fire light continued to be illuminated. The captain requested that the relief pilot return to the cockpit. He then contacted ATC (Air Traffic Control) and told them that their No. 2 engine was on fire and that they intended to land at the nearest suitable field. ATC responded that Charlotte was 35 miles away with a 10,000-foot runway. He asked for radar vectors and an immediate descent into Charlotte. They were given a lower altitude. The relief pilot returned to the cockpit and he asked the relief pilot and the first officer to run the checklists. As they descended the aircraft encountered heavy rain, light hail, and moderate turbulence. In addition, they observed a bright flash to the left of the nose, which might have been a lightning strike. As they completed the descent and approach checklists he told the crew to expect an emergency evacuation upon landing and directed the first officer to so inform the flight attendants. The aircraft was configured for an engine out approach and they reviewed the loss of a second engine procedure. The remainder of the approach, touchdown and landing roll occurred within normal parameters. He brought the airplane to a stop on the runway. The engine fire indication remained illuminated. They completed the items on the evacuation checklist. He then ordered an evacuation of the airplane. The first officer stated that the captain was the flying pilot. The takeoff roll and climbout from Atlanta were conducted within normal parameters. When the aircraft leveled at flight level 330, the relief pilot left the cockpit to begin his rest period. Within a few minutes , he observed a flashing red warning light, a level 3 alert on the EAD and a red light on the No. 2 engine fire handle and fuel shutoff lever. The captain began an immediate descent into Charlotte and requested that the relief pilot return to the cockpit. The first officer began to run the engine fire/severe damage checklist. He stopped to provide the relief pilot access to the cockpit. He then completed the items on the checklist with the assistance of the relief pilot. As they descended the captain called for fuel dump. The first officer accomplished the items on the fuel dump checklist. The aircraft was encountering heavy rain, light hail, and moderate turbulence. There were no strong echoes indicated on weather radar. In addition, they observed a bright flash to the left of the nose. The captain remarked that they had been struck by lightning. The first officer initiated and accomplished the descent checklist after changing the destination and setting up the landing runway in the flight management system. The relief pilot assisted him in the completion of the approach checklist. As they became established on the glideslope for runway 18 at Charlotte, the captain told then to expect an emergency evacuation upon landing and instructed the relief pilot to so inform the flight attendants. The airplane was configured for an engine out approach. While on final approach, the first officer announced and read the loss of second engine checklist. At 840 feet agl, he initiated and completed the before landing checklist. The captain brought the airplane to a stop on the runway and then called for the emergency evacuation checklist, which the relief pilot read and performed. The captain made a public address announcement and the first officer activated the evacuation horn. The relief pilot stated that he sat on the cockpit jumpseat during the takeoff roll and climbout from Atlanta. When the aircraft leveled at flight level 330, he left the cockpit to begin his rest period. Within a few minutes a flight attendant informed him that the captain had requested that he return to the cockpit immediately. Upon entering the cockpit he observed that the fire handle light for the No. 2 engine was illuminated and that the captain and first officer were in the process of running the engine fire checklist. The captain asked him to run the checklists with the first officer so that he could focus his attention on the operation of the aircraft and communications with ATC. As they completed the checklists the captain began an emergency descent into Charlotte. The engine fire light remained illuminated after completion of checklist items. As they descended, the aircraft encountered heavy rain, light hail, and moderate turbulence. In addition, they observed a bright flash to the left of the nose. The captain remarked that they had been struck by lightning. As they completed the descent and approach checklists and became established on the glideslope for runway 18 at Charlotte, the captain said to expect an emergency evacuation upon landing and directed the relief pilot to so inform the flight attendants. The aircraft was configured for an engine out approach. In addition, the flight crew reviewed the loss of second engine procedure. The remainder of the approach, touchdown and landing roll occurred within normal parameters. The captain brought the airplane to a stop on the runway. They then completed the items on the evacuation checklist. The relief pilot stated in interview with NTSB that they did not terminate the fuel dumping prior to landing. The flight attendant positioned at the 1R door stated that about 10 minute after takeoff the flight attendants were given the 10,000-foot signal, but the seat belt sign was left on due to light turbulence. They began cabin service. A while later the pilots called back and told the flight attendants to take their seats. About 30 seconds later the pilots asked that they send the relief pilot to the cockpit, that they had a problem and needed him right away. The aircraft began descending and they stowed the carts. The aircraft continued the descent at a steep angle. The flight attendant positioned at the 1L door, who was the onboard leader, talked to the pilots and the pilots told her they had a fire in No. 2 engine and would be landing in Charlotte. The pilot also told her to prepare the cabin for an emergency landing and that he did not think they would have to evacuate the aircraft, but to review their emergency procedures. She passed this information to the other flight attendants. They completed the preparation for landing and took their seats. About 30 seconds from landing the onboard leader made an announcement to the passengers reminding them of the emergency lights. The landing was smooth and the aircraft stopped. The power went off and the emergency lights came on. The evacuation horn sounded. The onboard leader yelled through the cockpit door to confirmed the evacuation signal with the pilots, and someone yelled yes. He went to the 1R door, assessed the conditions outside, confirmed the door was armed, and opened the door. He saw the door move up into the ceiling and the slide/raft come out of the bottom of the door. As he reached for the assist handle near the door, the slide began to inflate. He could hear the rush of compressed air from the inflation bottle and the slide began to fill the doorway, pushing him against the windscreen in front of the row one seats. The slide inflated up to the ceiling from the floor, then bent and came into the aisle, then hit the floor, and bent back up to the ceiling and wrapped around the windscreen. It completely filled the doorway and into the aisle and the area near the cockpit door. He pulled himself out of the way of the slide and became worried that the slide might explode, because the inflation tubes were completely inflated. It was drum tight. He immediately blocked the exit and looked to the 1L door. The door was open and he began directing passengers to that door. As A zone emptied he moved to the 2R door. The flight attendant at the 1L door stated a cockpit crewmember exited the cockpit and deflated the slide at the 1R door with a crash axe. The flight attendant at the 4R door stated that when the evacuation signal activated, he initially thought it was the lavatory smoke detectors activating and he checked the lavatory for smoke. He then realized it was the evacuation signal and initiated evacuation through the 4R door. The Charlotte/Douglas International Airport, Aircraft Rescue and Fire Fighting (ARFF) chief on duty at the time of the accident stated to NTSB personnel that the fire station was notified by air traffic controllers at 1942, of a MD-11 landing with a possible No. 2 engine fire. The ARFF equipment was pre-positioned near runway 18R. When the airplane landed it was followed by ARFF vehicles. The ARFF Chief radioed his vehicles to use caution because of the reduced visibility in the heavy rain and also because fuel was being sprayed on the vehicle's windshields from the airplane. He cautioned also that the runway was slippery from the rain-fuel mixture. He did not see fuel coming from the fuel dump pipes on the wings. PERSONNEL INFORMATION The captain held an airline transport pilot certificate for airplane multiengine land, type rated on the Boeing 737, 757, 767, Lockheed L1011, and the McDonnell Douglas MD-11. The date of his most recent proficiency check on the MD-11 was October 4, 2001. He was designated a company line check airman on the MD-11 on January 25, 2002. Company records indicate that at the time of the accident, he had accumulated 20,120 total flight hours with 1,647 hours in the MD-11 type aircraft. His most recent Federal Aviation Administration, (FAA) first-class medical certificate was issued on February 2, 2002, with no limitations or waivers. On this particular flight he was serving as a check airman for the purpose of providing the newly rated first officer with operating experience. The first officer held an airline transport certificate for airplane multiengine land, type rated on the McDonnell Douglas MD-11. The date of his initial type-rating check ride was March 20, 2002. Company records indicate that at the time of the accident, he had accumulated 8,363 total flight hours with 5 hours in the MD-11 aircraft. His most recent FAA first-class medical certificate was issued on December 5, 2001, with no limitations or waivers. This particular segment of the flight was his first exposure to MD-11 crew operating experience. His most recent previous position with the company was as a B-727 captain. The relief pilot held an airline transport certificate for airplane multiengine land, type rated on the McDonnell Douglas MD-11. Company records indicate that at the time of the accident, he had accumulated 11,500 total flight hours with 1,268 hours on the MD-11 aircraft. His most recent company proficiency check on the MD-11 was during February, 2002. His most recent FAA first-class medical certificate was issued on March 3, 2002, with no limitations or waivers. His most recent previous position with the company was as a B-767 first officer. Eleven flight attendants were assigned to Flight 12. All flight attendants were qualified on the MD-11 aircraft. AIRCRAFT INFORMATION The cockpit warning for an engine fire on the MD-11 aircraft consists of an aural and visual warning. A continuous bell rings and is automatically inhibited on landing from 100 feet radar altitude to 80 knots airspeed. The visual indications are a MASTER WARNING light on the cockpit glare shield as well as the CRTs [displayed by the EAD, (engine and alert display) feature of the EIS (electronic instrument alerting system)] and a red "ENG FIRE, (1, 2, or 3)" in the engine fire handle and the engine fuel switch. The fire warning system consists of dual detection loops that require either, (1) detection of an overheat or fire by both loops or, (2) a failure of one loop and a fire detection of the other loop. An inflatable evacuation slide/raft is installed in a slide stowage container, mounted on the inside, bottom of every cabin door. Opening the door, when the arming lever adjacent to the door is in the SLIDE ARMED position, will automatically inflate and deploy the slide/raft. A manual inflation handle is installed in the slide/raft assembly and becomes visible when the slide is deployed. If the automatic inflation feature malfunctions, the manual handle can be pulled to inflate the slide/raft. METEOROLOGICAL INFORMATION The 1851 observed weather for the Charlotte airport was reported as: winds from 360 degrees at 7 knots, 2 statute miles visibility in light drizzle and mist, ceiling was overcast at 300 feet, ambient temperature and dew point both 55 degrees F, altimeter setting 29.87 inHg., with a remark that surface visibility was 5 statue miles. While the flight was on final approach, Charlotte tower relayed surface winds of 010 degrees at 10 knots, visibility of 2 miles in mist. FLIGHT RECORDERS The airplane was equipped with a L-3 Communications model FA2100 digital solid state, 2-hour, cockpit voice recorder (CVR). The CVR was taken to the NTSB Vehicle Recorders Laboratory, Washington, D.C., for readout. A transcript of the final 17 minutes and 20 seconds of the recording was prepared. See NTSB CVR Specialist's Factual Report. The airplane was equipped with a Loral Fairchild Model F-1000 digital flight data recorder (DFDR). The DFDR was taken to the NTSB Vehicle Recorders Laboratory for readout. The data indicated the No. 2 engine fire warning activated at 1928:41, when the aircraft was in cruise flight at 33,000 feet. At 1928:51, the No. 2 engine was shutdown. Fuel quantity began decreasing rapidly at about 1934 and continued to decrease rapidly until the recording ended at 1945, shortly after the airplane landed. See NTSB Specialist's Factual Report of Investigation, Digital Flight Data Recorder. WRECKAGE AND IMPACT INFORMATION According to Delta Air Lines representatives, examination of the No. 2 engine by company maintenance personnel found one fire loop chafed through an adjacent cable, an integrated drive generator (IDG) feeder cable, inside the No. 2 engine cowling. This allowed a direct 115 volt AC connection between the IDG and the fire detection control unit. The result was an electrical short and complete failure of the detection control unit that was indicated in the cockpit as a fire warning. There was no evidence of fire in the No. 2 engine. Examination of the 1R slide/raft by NTSB and representatives of Air Cruisers, the manufacturer of the slide/raft, Boeing, and Delta Airlines showed that the manual inflation handle was fully stowed. The inflation valve was found one ratchet notch from the fully open position. According to the manufacturer, this condition typically occurs when the valve is opened slowly instead of quic
The failure of the aircraft operator to comply with, in a timely manner, on the No. 2 engine, Boeing Alert Service Bulletin MD11-71A086, resulting in the integrated drive generator feeder cable chaffing through a fire warning loop and failure of the fire warning system due to electrical damage. This resulted in a continuous indication in the cockpit of a No. 2 engine fire, an emergency descent and landing, and injuries to passengers during the subsequent emergency evacuation of the airplane.
Source: NTSB Aviation Accident Database
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