Accident Details
Probable Cause and Findings
the overstress fracture of the airplane's refueling adapter ring that resulted from the abnormal angular force applied to it. The applied angular force occurred due to the ground refueler inadequately positioning the hydrant fuel truck (in relation to the airplane), and his inattentiveness while lowering the refueling lift platform, thus permitting the refueling hose to become snagged and pulled at an angle. The fracture of the adapter ring during the refueling led to the ignition of the pressurized (mist producing) spilled fuel and subsequent fire.
Aircraft Information
Analysis
HISTORY OF FLIGHT
On September 5, 2001, at 1714 mountain daylight time, a Boeing 777-236, British registration G-VIIK, was substantially damaged during a ground fire at Denver International Airport, Denver, Colorado. The fire started when the airplane was parked at the gate unloading passengers and being refueled. The captain, first officer, a third pilot, 13 cabin crewmembers, and 10 passengers who were on board at the time of the accident, were not injured; however, the ground service refueler was fatally injured. British Airways was operating the airplane, Flight 2019 (call sign BAW91F), under Title 14 CFR Part 129. Visual meteorological conditions prevailed for the 9 hour 38 minute cross-country flight that originated from London, United Kingdom.
The airplane departed Gatwick International Airport, London, United Kingdom, at 0713 with 256 passengers, and was cleared to land on runway 16 at Denver International Airport (DEN) Denver, Colorado, at 1646 (the scheduled arrival time was 1615). Federal Aviation Administration (FAA) Air Traffic Control (Denver tower) instructed BAW91F to contact Denver ramp control, for taxi instructions, at 1656. BAW91F was cleared to taxi to gate A37, and its flight data recorder indicates that its auxiliary power unit (APU) was started at 1658 and its engines were shut down at 1706. A British Airways Senior Air Safety Investigator stated that the airline's Boeing 777's APU is normally started during taxi-in, and the airplane's electrical load is transferred from the main engines to the APU automatically via "no-break" technology when the engines are in idle, or during shut down. The captain for the flight said that during short time turn around, ground power is not used. He said that at the time of the accident, the airplane's electrical power supply was being generated by its APU.
The refueling hydrant truck was parked under the airplane's left wing, facing aft, and outboard of the left engine. Videos taken from DEN firefighting equipment showed that the hydrant truck had been chocked, and the hydrant truck's hydrant coupler had been attached to the airport's subsurface pit hydrant. The DEN fire department's video and a United Airline's maintenance-engineer also confirmed that the refueler had grounded the truck to the pit hydrant, and bonded the truck to the airplane's left main landing gear.
The maintenance-engineer said the refueler had raised the lift platform and had attached two hoses to the airplane's left wing refueling manifold system. As the maintenance-engineer approached the hydrant truck, he noted that refueling of the airplane had already started. He further stated that he frequently saw refuelers lower their lift platforms for head clearance comfort (during the refueling), and/or to receive their refueling requirements from a maintenance-engineer. He did not remember seeing the lift platform move on this occasion.
The maintenance-engineer said he positioned himself between the airplane's left engine and the hydrant truck to tell the refueler what fuel load should be put on the airplane. He said the refueler turned towards him and leaned down, with his back to the refueling hoses, to give him the amount of fuel that remained from the previous flight. He said the refueler had the dead-man fuel control (shut off device) in his left hand, and the hydrant truck's fuel flow meter was beginning to rotate rapidly. The last reading he remembered seeing on the fuel flow meter was 60 gallons. He further noted that the hydrant truck's turbo-diesel engine was running.
As the maintenance-engineer looked up at the refueler, he observed the inboard fuel hose separate sideways (forward, in relationship to the truck) from the airplane, and flap around "violently spraying fuel in all directions." He yelled at the refueler that the "hose was loose." The maintenance-engineer was immediately soaked with fuel and even swallowed some. He said the flames propagated up from the bottom of the truck, through the open lattice of the lift platform floor, and "engulfed the fueler." He immediately ran for a large fire-extinguishing bottle.
A second maintenance-engineer was standing inboard of the left engine when he "felt the heat and turned and looked to see a huge fire had broken out at the fuel truck [hydrant truck]." The airplane's captain was standing inside the airplane near the door to the jetway. He said that a flight attendant was the first crewmember to notice the fire; her alarm motivated him to move to a jetway window to view aft. He said that he observed a "fire near [the] left engine," and he ordered all remaining persons to immediately evacuate the airplane.
A pilot standing nearby said that a large ball of fire enveloped the hydrant truck and much of the airplane's left wing; he said the heat was very intense. He yelled to another person to call the fire department. He ran to assist a maintenance-engineer in retrieving a large fire extinguisher bottle. The fire department received the call at 1714, arrived at the scene at 1717, and immediately extinguished the fire.
Several civilian witnesses, inside the concourse, made the following observations: the first witness observed "men refueling [the airplane]. I saw the hose fly up and a spray covered the vehicle (looked like a jet of water). I then saw a small fire followed by a large ball of fire engulf the vehicle. Various people were running away from the vehicle as the fire continued to grow." She said she then thought there was some "smoke" or vapor before the fire started. She recalled the fire starting from the truck, but could not be specific whether it was from the basket or the body of the vehicle. A second witness "noticed that there was a spray of clear fluid coming from around where the people were refueling the jet. I thought it could be water, but noticed a number of the people running away and then thought it must be fuel. Shortly afterwards (1 second?) I saw the fuel explode and engulf the truck and engine of the plane." During a second interview in England, this witness recalled, "seeing the fire first in the basket, then down onto the truck. The fireball then enveloped the fuel truck, then the refueler, then up below the wing to the engine with an orange flame."
A third witness said, "I was watching the servicing of British Airlines Flight 2019, when suddenly [I] saw a huge fountain of liquid (presume jet fuel) in the air followed by a huge ball of flame. As they were refueling the aircraft, I would think either the hose ruptured or the coupling failed." A fourth witness said, "I saw a flash, followed by an expanding fireball. After taking cover, it appeared the refueling stand behind [the] port wing was on fire." A fifth witness said, "[the] fire started ground."
Additional witnesses said, "I saw that [the] engine explode, fire was coming from the engine." Another said, "explosion either from the engine or right in front of the engine. The fire was surrounding the engine and wing. The fire was also spreading on the ground." Another said, "I saw what appeared to be smoke coming from the engine whilst the re-fueling truck was re-fueling. There was a sudden flash and the truck [and the] engine was engulfed in flames." Another said, the fire started from the top of the wing and came down. Another said, "I looked up to see flames that looked like they were coming from the engine on the right side. Then it looked like a truck or something behind the engine was also on fire." And one more said, "The left outboard engine was suddenly engulfed in flames. Could see a fuel truck behind this engine. Flame appeared to spread over more of the A.C in the vicinity of the left outboard engine. Fuel was burning on the ground."
According to a British Airways representative, the 26 individuals still on-board the airplane at the time of the accident were evacuated through the jetway without incident.
PERSONNEL INFORMATION
Aircraft Service International Group (ASIG) hired the refueler on October 14, 1997. ASIG records indicate that he had received training and was qualified to refuel 17 different aircraft for 10 different airlines (he was qualified on the Boeing 777 on April 27, 1999; it was not determined how many Boeing 777s he had actually fueled). He had refueled one previous airplane (a Lufthansa A340-313X), on the afternoon of the accident, using hydrant truck number 9417. He completed that refueling approximately 30 minutes before the accident. At the time of the accident, the refueler was wearing a cotton shirt, and pants made of 65 percent polyester and 35 percent cotton.
The first maintenance-engineer (with 24 years of aviation maintenance experience) said, in a Denver Police Department interview, regarding the ASIG fueler, "He is generally not the one assigned to that plane, I believe." The second maintenance-engineer (with approximately 30 years of aviation maintenance experience) said regarding the fueler, "He wasn't one of the normal guys; I haven't seen him very often."
According to the Denver Police Department, the refueler was 5 feet 11 inches tall, and weighed 160 pounds. The refueler died from his injuries on September 11, 2001. He was 24 years old.
AIRCRAFT/VEHICLE INFORMATION
General Information about the Airplane
The airplane, a Boeing 777-236, was a twin engine, turbofan aircraft with a maximum gross takeoff weight of 590,000 pounds, and was manufactured in 1998. At the time of the accident, there were 359 similar aircraft in use worldwide, of which British Airways operated 44. The airplane's flight deck seats four, and an additional 14 cabin crew positions were located in the cabin area along with seats for a maximum of 267 passengers. Two General Electric Model GE-90 engines powered the airplane with a maximum takeoff thrust at Denver, Colorado, of 90,000 pounds each. The GE-90 engines were suspe...
Data Source
Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN01FA157