On January 20, 2002, at 0715 eastern standard time, a McDonnell Douglas DC-9-32, N837AT, operated by Air Tran Airways as flight 67, was substantially damaged during pushback at Washington Dulles International Airport, Dulles, Virginia. There were no injuries to the 2 certificated airline transport pilots, 3 flight attendants, or 61 passengers. Visual meteorological conditions prevailed. An instrument flight rules (IFR) flight plan had been filed, for the flight that was conducted under 14 CFR Part 121. Use your browsers 'back' function to return to synopsisReturn to Query Page
The flight was destined for Atlanta, Georgia. According to the captain, the ramp was covered with snow and ice, and their gate position required a pushback with a nose swing of about 120 degrees. The airplane had an inoperative APU, and he elected to start both engines at the gate prior to pushback because a single engine crossbleed start would require an N1 of 80 percent on the operative engine. After both engines were started, the pushback was initiated. As the tug neared a 90 degree position to the right side of the nose of the airplane, it started to move forward, and then stopped when it struck the tug, after which the captain set the brakes. The captain added that he had not applied the brakes until after the airplane came to rest.
According to the diagrams on the Air Tran Airways safety report filled out by the captain, the position of the tug was near 90 degrees to the right of the nose of the airplane when the airplane started to move forward.
According to an interview conducted with the tug driver by the Metropolitan Washington Airports Authority, Airport Operations Division, the tug driver reported that he had conducted two earlier pushback with no problems. The tug driver added that with both engines running on the airplane, the airplane felt heavier during the push.
During the pushback, there were two wing walkers, the tug driver, and an additional walker near the nose of the airplane, who was using a headset to remain in communications with the flight crew.
The people who conducted the pushback were contract employees who had been trained in accordance with Air Tran Airways general maintenance manual (GMM). There was no specific requirement to use a headset. However, the Air Tran Airways GMM did state that headset communication was the primary method of communications during pushback and tow. It further stated, "If an interphone/headset is to be used, the tractor operator will man the headset...." The investigation revealed that the tug driver did not wear the headset because the chord had broken, and had been repaired several times, which shortened its overall length.
The tug driver reported that he had already pushed back two airplanes that morning with no problems, and that the initial part of the push was without incident. As the airplane entered an area where the ramp was icy, he turned the nose of the airplane to the west. The nosewheels on the airplane started slipping, and he was unable to communicate this to the cockpit crew. He stopped the tug and the airplane slid into the tug.
The walker on the interphone to the cockpit reported that he was not looking at the airplane when it began to slip. When he became aware that the airplane was slipping, there was insufficient time to tell the flight crew to set the brakes. He did not make any transmission to the pilots prior to impact.
The ramp was reported as icy, and some people reported difficulty in walking.
The tug used for pushback was a Hough T-225, rated to push an airplane up to 225,000 pounds. The tires on the tug were not equipped with chains. The ramp had not been sanded.
Within the preceding 12 hours, the airport had reported periods of freezing rain, followed by light snow.
A toxicological report on the tug driver was negative for drugs or alcohol.
Neither Air Tran Airways, nor the contract operator had any specific training directed to the problems that could be encountered with pushing airplanes on icy ramps, or winter operations in general.
Damage to the airplane consisted of a hole in the right side of the fuselage, located about 3 feet below the bottom of the forward, right side cabin door, and about 4 feet behind the trailing edge of the door. Internally, there was damage to the longerons.