Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JBXA000315Powerplant · overtemp#1 ENGINE OVERTEMPERATURE/860 DEGREE'S FARENHEIT. CORRECTIVE ACTION: PERFORMED TAY SB 77-1454 IAW TAY 77-1454. CHANGE RESISTOR AFROM CM TO CK. PERFORMED ACCEL AND DECELL CHECKS AND IGV SCHEDULING CHECK IAW TAY 71-00-00.SDR JBXA000297Engine · malfunctionedHIGH EGT APPROACHING REDLINE DURING TOGA TAKEOFF RDU. PEAK TGT 850 FOR 1 SECOND. PERFORMED OPS CHECK OF NR 1 ENGINE TOGA EGT IAW AMM 71-00-00, NO FAULTS NOTED EGT WITHIN LIMITS. OPS CHECK GOOD.SDR JBXA000291Autothrust Sys · malfunctionedFLT 555 RDU/LGA AUTOTHROTTLE NR 1 AND 2 FAULTED ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. RESET FCC AND FAC NR 1 AND 2 AUTOTHROTTLE, OPS CHECK GOOD IAW F-100 MM 22-11-00.SDR JBXA000279Outflow Valve · failedCABIN PRESSURE CONTROL FAULT CAME ON AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. PLACED CONTROL SWITCH TO MANUAL CABIN STILL WOULD NOT PRESSURIZE. RETURNED TO RDU. REMOVED AND REPLACED SECONDARY OUTFLOW VALVE IAW F-100 AMM 21-31-04. PERFORMED OPERATIONAL TESDR JBXA00267Controller · malfunctionedCABIN WILL NOT PRESSURIZE AFTER TAKEOFF. COULD NOT CONTROL MANUALLY. PULLED AND RESET C/B FOR CABIN PRESSURE CONTROLLER. PERFORMED OPERATIONAL CHECK OF CABIN PRESSURE CONTROLLER IAW F-100 AMM 21-31-02. ALL OPERATIONAL CHECKS GOOD AT THIS TIME.SDR JBXA000249Transducer · failedLIFT DUMPER FAULTED ON TAKEOFF ROLL 80-90 KNOTS. FOUND RIGHT OUTBOARD WHEEL SPEED TRANSDUCER FAULTING. REMOVED AND REPLACED NR 4 WHEEL SPEED TRANSDUCER IAW AMM 32-45-02, OPS CHECK GOOD.SDR JBXA000248Brake Assy · failedGATE RETURN. BRAKES RELEASED WITH BRAKE APPLICATION SEVERAL TIMES. SET PARKING BRAKE, PUSHED ANTI-SKID TEST, BRAKES RELEASED WITH AIRCRAFT MOVEMENT. TOWED AIRCRAFT TO GATE. BLEED BRAKE SYSTEM IAW F100 AMM 32-44-00, SERVICED HYDRAULIC SYTEM 1 AND 2 IAW F100SDR JBXA000235Warning Light · illuminatedLIFT DUMPER FAULT MESSAGE DISPLAYED INTERMITTENTLY. ABORTED TAKEOFF. CLEARED FAULT, AIRCRAFT DEPARTED NORMALLY, NO FURTHER FAULTS.SDR JBXA970014Press Switches · failedRDU - FLT 443 - AT 10,000 FEET AS A/C ACCELERATED RUD1 AND RUD2 FAULTED WITH YAW DAMP 1 AND 2 AND ALSO STAB TRIM FAULTS 1 AND 2. BOTH RUDDER FAULTS RESET AT 3,000 FEET. SLOWED TO 210 KTS AND RETURNED TO RDU. ONCE ON THE GROUND IN RDU THE LOW AND HIGH ACTIVESDR JBXA970013Fcc · failedRDU - FLT 771 - AIR RETURN DUE TO RUDDER FAULT 1 AND 2, STABILIZER TRIM 1 AND 2 AND YAW DAMPER 1 AND 2 FAULTS ALSO, HAD AFCAS MX REQUIRED MESSAGE. REMOVED AND REPLACED FLT CONTROL COMPUTER NR 1 (FCC NR 1). OPS CHECK GOOD IAW AMM 22-11-01. OPS CHECK OF RUDDESDR JBXA00029Autothrottle · malfunctionedRDU - FLT 771 - BOTH AUTOTHROTTLES FAULTED PRIOR TO 80 KNOTS, ABORTED TAKEOFF. CORRECTIVE ACTION: PERFORMED AFCAS MAINTENANCE, SHOWED TOGA SWITCH, FCC1, FCC2. RESET TOGA SWITCH, PERFORMED FCC1, FCC2 TEST AND FAC1, 2 TEST ON AFCAS. MAINTENANCE TEST DONE IA
Other aircraft with N110ML · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N110ML now.