What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: on February 6, 1996 at 1152 PST delta flight 1400 landed at Portland, Oregon on runway 28R and blew both right side main landing tires. The runway was closed until delta was able to remove and replace both tires. At the time of the incident both the number 3 engine thrust reverser and the anti-skid system were inoperative, and properly deferred in accordance with the minimum equipment list. The conditions at the time of the incident were heavy rain and standing water. At the time of the incident runway 21 was in use at pdx, the crew related that they could not accept that runway. Runway 28R was offered and accepted. Winds were 190 @ 21 with gusts to 28 knots. Upon landing both right main tires blew. Maintenance at Portland removed and replaced both right main landing gear tires and brake assemblies. In addition they removed and replaced the anti-skid control shield. Subsequent inspection at pdx revealed a crosswired left main landing gear anti-skid harness. Maintenance at pdx rerouted the harness, and ops checked the system. They also removed and replaced #3 thrust reverser pressure switch to clear the dmi on #3 t/r. informed certificate holding district office of findings.
As the FAA filed it
NARRATIVE: ON FEBRUARY 6, 1996 AT 1152 PST DELTA FLIGHT 1400 LANDED AT PORTLAND, OREGON ON RUNWAY 28R AND BLEW BOTH RIGHT SIDE MAIN LANDING TIRES. THE RUNWAY WAS CLOSED UNTIL DELTA WAS ABLE TO REMOVE AND REPLACE BOTH TIRES. AT THE TIME OF THE INCIDENT BOTH THE NUMBER 3 ENGINE THRUST REVERSER AND THE ANTI-SKID SYSTEM WERE INOPERATIVE, AND PROPERLY DEFERRED IN ACCORDANCE WITH THE MINIMUM EQUIPMENT LIST. THE CONDITIONS AT THE TIME OF THE INCIDENT WERE HEAVY RAIN AND STANDING WATER. AT THE TIME OF THE INCIDENT RUNWAY 21 WAS IN USE AT PDX, THE CREW RELATED THAT THEY COULD NOT ACCEPT THAT RUNWAY. RUNWAY 28R WAS OFFERED AND ACCEPTED. WINDS WERE 190 @ 21 WITH GUSTS TO 28 KNOTS. UPON LANDING BOTH RIGHT MAIN TIRES BLEW. MAINTENANCE AT PORTLAND REMOVED AND REPLACED BOTH RIGHT MAIN LANDING GEAR TIRES AND BRAKE ASSEMBLIES. IN ADDITION THEY REMOVED AND REPLACED THE ANTI-SKID CONTROL SHIELD. SUBSEQUENT INSPECTION AT PDX REVEALED A CROSSWIRED LEFT MAIN LANDING GEAR ANTI-SKID HARNESS. MAINTENANCE AT PDX REROUTED THE HARNESS, AND OPS CHECKED THE SYSTEM. THEY ALSO REMOVED AND REPLACED #3 THRUST REVERSER PRESSURE SWITCH TO CLEAR THE DMI ON #3 T/R. INFORMED CERTIFICATE HOLDING DISTRICT OFFICE OF FINDINGS.
Other reports on N830WA · 2
Matched to the same aircraft by N-number and date.