MD80 CAPTAIN ELECTS TO REJECT TKOF ABOVE 120 KNOTS DUE TO HIGH EGT ON RIGHT ENGINE AND RETURNS TO GATE FOR MAINTENANCE.
Synopsis
MD80 CAPTAIN ELECTS TO REJECT TKOF ABOVE 120 KNOTS DUE TO HIGH EGT ON RIGHT ENGINE AND RETURNS TO GATE FOR MAINTENANCE.
Narrative
AFTER FLYING 2 LEGS IN ACFT; WE TAXIED OFF THE GATE FOR A TKOF ON RWY 12L AT STL. THE ACFT WT WAS APPROX 142000 LBS; FLAPS 8 DEGS WITH AN OAT OF APPROX 90 DEGS. I ELECTED TO MAKE A MAX PWR TKOF. WE STARTED THE R ENG DURING TAXI AND WERE CLRED INTO POS ON RWY 12L. AFTER TKOF CLRNC WAS RECEIVED; THE R ENG WAS SLOW TO SPOOL UP FROM IDLE; TAKING SEVERAL SECONDS LONGER THAN THE L TO REACH 1.4 EPR. THE ACFT WAS STOPPED IN POS DURING THE SPOOL UP DELAY. AT 1.4 EPR; BOTH ENGS ACCELERATED NORMALLY TO MAX TKOF THRUST. AS WE ACCELERATED THROUGH 110 KTS; I NOTICED THE R EGT PASSING 590 DEGS C; AT 120 KTS THE R EGT WAS AT 620 DEGS C AND CLBING. WITH APPROX 6000 FT OF RWY LEFT; I DECIDED TO ABORT THE TKOF; SURE THAT AN ENG FAILURE WAS IMMINENT. I ANNOUNCED WE WERE ABORTING AND APPLIED REVERSE THRUST AND USED MANUAL BRAKES TO STOP AT THE END OF THE RWY AS TO AVOID A BRAKE OVERHEAT EVENT. WE TAXIED TO THE GATE WITHOUT INCIDENT AND ASKED FOR PRECONDITIONED AIR TO BE APPLIED TO THE BRAKES AS THE PAX DISEMBARKED.
Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.