What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Aircraft 213FE, a Boeing 727 operated by federal express was positioned on gate 600 awaiting pushback. Gate 600 pushback requires the tail to be turned east for a west taxi. The tug operator is responsible for aligning the aircraft for departure. As the aircraft approached (push phase) the junction line (intersection of taxiway centerline and gate entrance line), the aircraft was stopped facing, nose southwest. The tug operator initiated the tow process by signaling to her crew that she was ready to pull the aircraft forward to align it with the taxiway centerline. At some point, the shear pins failed between the nose gear attachment head and bar assembly during either the pushback or towing modes of operation, which resulted in the tug and aircraft colliding. Initial contact between the two vehicle and aircraft occurred on the right side of the tug and right side of the aircraft behind the nose landing gear. Damage to the aircraft is substantial between, sta.385 (RH side) and continues to sta. 440 (LH side) with gouges extending 3 to 4 feet aft. Damage was also found on the RH nose landing gear sheel. The tug driver sustained injury to her right shoulder, separated in two places and a fractured jaw.
As the FAA filed it
(-23) AIRCRAFT 213FE, A BOEING 727 OPERATED BY FEDERAL EXPRESS WAS POSITIONED ON GATE 600 AWAITING PUSHBACK. GATE 600 PUSHBACK REQUIRES THE TAIL TO BE TURNED EAST FOR A WEST TAXI. THE TUG OPERATOR IS RESPONSIBLE FOR ALIGNING THE AIRCRAFT FOR DEPARTURE. AS THE AIRCRAFT APPROACHED (PUSH PHASE) THE JUNCTION LINE (INTERSECTION OF TAXIWAY CENTERLINE AND GATE ENTRANCE LINE), THE AIRCRAFT WAS STOPPED FACING, NOSE SOUTHWEST. THE TUG OPERATOR INITIATED THE TOW PROCESS BY SIGNALING TO HER CREW THAT SHE WAS READY TO PULL THE AIRCRAFT FORWARD TO ALIGN IT WITH THE TAXIWAY CENTERLINE. AT SOME POINT, THE SHEAR PINS FAILED BETWEEN THE NOSE GEAR ATTACHMENT HEAD AND BAR ASSEMBLY DURING EITHER THE PUSHBACK OR TOWING MODES OF OPERATION, WHICH RESULTED IN THE TUG AND AIRCRAFT COLLIDING. INITIAL CONTACT BETWEEN THE TWO VEHICLE AND AIRCRAFT OCCURRED ON THE RIGHT SIDE OF THE TUG AND RIGHT SIDE OF THE AIRCRAFT BEHIND THE NOSE LANDING GEAR. DAMAGE TO THE AIRCRAFT IS SUBSTANTIAL BETWEEN, STA.385 (RH SIDE) AND CONTINUES TO STA. 440 (LH SIDE) WITH GOUGES EXTENDING 3 TO 4 FEET AFT. DAMAGE WAS ALSO FOUND ON THE RH NOSE LANDING GEAR SHEEL. THE TUG DRIVER SUSTAINED INJURY TO HER RIGHT SHOULDER, SEPARATED IN TWO PLACES AND A FRACTURED JAW.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N213FE · 2
Matched to the same aircraft by N-number and date.