Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JBXA000211Connector · dirtyFLT 7 RDU/BOS - NR 1 ENG TGT INDICATES LARGE FLUCTUATIONS IN ALL PHASES OF FLIGHT. FUEL FLOW ON NR 1 INDICATES 300 - 400 LBS HIGHER THAN NR 2 ON HIGH POWER SETTINGS. CLEANED TGT TEST PORT CANNON PLUG IAW F100 MM 77-45-00. PERFORMED ENGINE POWER RUN IAW F1SDR JBXA0000194Engine · overtempABORTED TAKEOFF FLL, NR 2 ENGINE TGT WARNING TEMP WAS APPROX 875 PULLED BACK THRUST LEVERS TO 1.5 EPR TO ALLOW TGT TO DECREASE TO BELOW 735. PERFORMED OVER TEMPERATURE INSPECTION OF NR 2 ENGINE IAW AMM 71-00-00, NO DEFECTS NOTED.SDR JBXA0000148Thrust Reverser · malfunctionedENGINE NR 1 REVERSER MESSAGE ON CLIMB-OUT THROUGH 240. PERFORMED OPERATIONAL CHECK OF NR 1 THRUST REVERSER IAW AMM 78-30-00, OPS CHECK GOOD.SDR JBXA9900099Computer · malfunctionedFLT 79 RDU/LGA- ON CLIMBOUT HAD STALL COMPUTER WARNING ASSOCIATED WITH MULTIPLE FAULTS ON RT MFDU. AIR RETURN TO RDU. PERFORMED OPERATIONAL CHECK OF STALL WARNING SYSTEM IAW 27-35-00. NO FAULTS NOTED. UPON ARRIVAL TO AICRAFT NO FAULTS INDICATIED.SDR JBXA9900093Engine · vibrationAFTER LIFTOFF IN RDU CREW GOT A VIBRATION HIGH ENG. NR 2 INDICATION ON INNER TAPE (N2). OCCURRED WITH VIBRATION SWITCH IN BOTH NORMAL AND ALTERNATE POSITIONS. CREW REDUCED POWER TO CLIMB POWER AND VIBRATION WARNING CLEARED, BUT WAS STILL IN THE HIGH IN THE SDR JBXA9900070Pitot Head · inoperativeFLT 112 RDU TO LGA, AFTER TAKEOFF PITOT NR 3 HEAT WARNING LMFDU. PITOT NR 3 HEAT FAULT WOULD NOT RESET. RETURNED TO RDU. REMOVED AND REPLACED NR 3 PITOT HEAD. OPS AND LEAK CHECKS GOOD IAW F-100 MM 34-11-01.SDR JBXA9900068Door · missingON WALK AROUND, FOUND APU SERVICE PANEL MISSING. REPLACED APU SERVICE PANEL IAW AMM 52-44-00.SDR JBXA9900066Bulb · failedAFTER SELECTING LANDING GEAR UP ON TAKEOFF THE NOSE GEAR INDICATOR INDICATED THAT IT WAS STILL DOWN AND LOCKED. THE LANDING GEAR WAS CYCLED DOWN AND THEN UP TWICE WITH THE SAME RESULTING INDICATIONS. ALL OTHER (SECONDARY) INDICATIONS INDICATED THE GEAR WAS USDR JBXA980052Union · crackedINFLIGHT, HYDRAULIC SYSTEM NR 1 QUANTITY DOWN TO 34 PERCENT. AIRCRAFT DIVERTED TO EWR. TROUBLE SHOOTING, FOUND NR 1 SYSTEM LEAKING AT T-FITTING MLG HYDRAULIC TUNNEL. REMOVED AND REPLACED T-FITTING, SERVICED AND LEAKED CHECKED SYSTEM, AND PRESSURE TESTED FITSDR JBXA980034Controller · malfunctionedRDU - FLT 304 - LT WINDOW HEAT FAULTED WHEN POWER APPLIED FOR TAKEOFF. CORRECTIVE ACTION: INSPECTED LT WINDSHIELD AND SIDE WINDOWS. NO DEFECTS NOTED. PERFORMED BITE TEST OF CONTROLLER. ALL ELEMENTS TESTED GOOD AND SENSORS TESTED GOOD. REMOVED AND REPLACESDR JBXA970019Hydraulic Pump · failedNUMBER 1 HYDRAULIC SYSTEM LOW QUANTITY. CREW PREFORMED MANUAL GEAR EXTENTION DUE TO LOSS OF HYDRAULIC SYSTEM NUMBER 1. BOTH MAIN LANDING GEAR DOORS WHERE DAMAGED ON LANDING IN RDU. MAINTENANCE FOUND ENGINE NR 2 HYD SYS NR 1 PUMP WITH A BLOWN SEAL. REMOVED SDR JBXA970005Fuel Flow Reg · malfunctionedAFTER TAKEOFF PARTIAL THORTTLE ONLY ON RIGHT ENGINE RETURN TO RDU PARTIAL POWER. REMOVED AND REPLACED RIGHT ENGINE FUEL FLOW REGULATOR IAW F-100 MM 73-21-01. PERFORMED LEAK CHECK, NO LEAKS NOTED. (M)SDR JBXA00033Auto Throttle · malfunctionedBDL - FLT 222 - NO AUTO THROTTLE ON FMA, ABORTED TAKEOFF AT BDL. PERFORMED AUTO THROTTLE SERVO TEST PER MM 22-31-01 AND AFCAS PANEL PROCEDURES PER MM 22-41-00. ALL CHECKS NORMAL. OPS CHECK OK. (M)SDR JBXA00031Auto Throttle · malfunctionedBOS - FLT 552 - DURING TAKEOFF ROLL, ABORTED TAKEOFF DUE TO AUTO THROTTLE FAULT 1 AND 2 THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE PERFORMED THRUST REVERSER TEST. T/R OPERATING NORMALLY. AFCAS FAULTED FAC MAINTENANCE PERFORMED AFACS TEST OPS CHECK G
Other aircraft with N104ML · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N104ML now.