N190JB

Part: SENSOR — FAILED (SLAT SYSTEM) · airframe 36,180 hrs · 23,019 cycles

FLT 1262, PBI-LGA. DIVERTED TO JFK. EMERGENCY DECLARED. FLAP FAIL MSG ANNUNCIATED DURING APPROACH. FLAP FAIL QRH (7-3) ACCOMPLISHED DURING DELAY VECTORS; R & R RIGHT WING POSITION SENSOR PER AMM 27-53-04 UP TO SUB TASK 420-007-A

Part: SEAL — CRACKED (LT PYLON) · airframe 35,710 hrs · 22,699 cycles

FLT 440, CLE-BOS. DURING AN ENGINE CHANGE AT BOS, WAS REPORTED WITH TWO CRACKS AT THE LT PYLON SUPPORT INBOARD SEAL (PN 190-03266-004) MEASURING 9MM LONG AND OUTBOARD SEAL (190-03266-003) MEASURING 21MM LONG. THERE ARE NO ALLOWABLES IN THE SRM AND CONTACTED INSTRUCTING TO PERFORM A STOP-DRILL TO THE CRACKS, FABRICATE AND INSTALL A TEMPORARY REPAIR DOUBLER. THIS EC E18-647-01 EMBODIES TEMPORARY REPAIR INSTRUCTIONS PER REF /1/ ETD VALID FOR 5000FH. EC E18-647-02 EMBODIES PERMANENT REPAIR INSTRUCTIONS DETAILING SEALS REPLACEMENT WITHIN 5000FH; APPROVED THIS REPAIR PER REF /1/ ETD AND IS CLASSIFIED AS MAJOR.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 34,454 hrs · 21,797 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. FOLLOWED FIM 33-50-00-810-813-A. FOUND THE POWER SUPPLY INOPERATIVE. R & R THE POWER IAW AMM 33-50-01. OPS NORMAL.

Part: SEAT TRACK — CORRODED (FRAME 17) · corrosion level 2 · airframe 33,050 hrs · 20,833 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT SEAT TRACK AT FRAME 17, RBL 11. THE SEAT TRACK WAS REPAIRED IAW SRM 53-10-10, REP 51, REV 35.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 30,495 hrs · 19,089 cycles

EMERGENCY LIGHT BATTERY FAULT APPEARS ON EICAS, WHEN EMERGENCY LIGHTS ARE ACTIVATED. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER UNIT BATTERY IAW AMM 33-50-01. OPS CHECK PERFORMED. OPS CHECKED NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG) · airframe 29,695 hrs · 18,517 cycles

DIVERTED, DECLARED EMERGENCY DURING FLIGHT, PILOT RECEIVED WARNINGS, LG WOW SYS FAIL , BRAKE CONTROL FAULT, AND 3 DOORS OPEN MESSAGE- DOOR CARGO AFT OPEN, SERVICE DOOR AFT OPEN, DOOR PASSENGER AFT OPEN. IN COMPLYING WITH THE QRH, PILOT DIVERTED TO THE NEAREST SUITABLE AIRPORT. MAINTENANCE PERFORMED A POWER DOWN. RESET PSEM NR 2 IAW FIM 32-61-00, NO FURTHER FAULTS. ALL WARNING MESSAGES WENT AWAY. CONSIDERED TRANSITORY CONDITION OF THE PSEM NR 2, ACFT OK FOR SERVICE AT THIS TIME. NO FURTHER ANOMALIES.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 25,928 hrs · 16,045 cycles

DURING HEAVY MAINTENANCE CHECK FOUND UNDERSIDE OF VERTICAL STABILIZER RIB 12 CRACKED IN 2 LOCATIONS. TRIMMED OUT AFFECTED FLANGES, PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED THE REQUIRED SHEAR CLIPS. ALL WORK ACCOMPLISHED IAW EC E15-242-01.

Part: BEAM — CORRODED (FRAMES 85-87) · corrosion level 2 · airframe 25,928 hrs · 16,045 cycles

DURING A HEAVY MAINTENANCE CHECK, FOUND THE AFT PASSENGER DOOR LOWER MACHINED BEAM CORRODED FRAMES 85-87, LBL 42-44. R & R THE MACHINED BEAM IAW SRM 51-41-02, 51-43-03 AND 51-43-04.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 25,928 hrs · 16,045 cycles

DURING A HEAVY MAINTENANCE CHECK, FOUND CORROSION IN FWD CABIN OTBD OF RT FLOORBEAM AT FRAME 17, RBL 25-33. REMOVED CORROSION ON THE FLOORBEAM IAW SRM 51-12-01 AND 51-10-03. CUTOUT THE AFFECTED AREAS AND INSTALLED FILLER USING LEFT ANGLE SUPPORT IAW EA 15-226-01.

Part: SENSOR — FAILED (SLATS) · airframe 23,402 hrs · 14,426 cycles

AIR RETURN TO DEPARTURE DUE TO SLAT FAIL EICAS ON TAKEOFF. CREW ATTEMPTED QRH RESET BUT UNSUCCESSFUL. TROUBLESHOT IAW FIM TASK 27-81-00-810-805-A. R & R LT SLAT SKEW SENSOR, OPS CHECKED NORMAL. SLATS AND FLAPS OPS OK.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 22,291 hrs · 13,734 cycles

DURING MAINTENANCE CHECK, FOUND EMERGENCY BATTERY FAULT ECAM APPEARED DURING EXTERIOR EMERGENCY LIGHT TEST. TROUBLESHOT IAW FIM 33-50-00-810-813-A. R & R MID EMERGENCY LIGHT BATTERY ASSY. CHECKED NORMAL IAW AMM 33-50-01. AIRCRAFT OK FOR SERVICE.

Part: FLOAT — DISLODGED (FUEL QTY) · airframe 21,066 hrs · 12,864 cycles

AIR RETURN DUE TO FUEL 1 LOW LEVEL EICAS MESSAGE ON CLIMB OUT. CREW EXECUTED QRH, NORMAL LANDING. FOUND MAGNETIC LEVEL INDICATOR FLOAT STOP CAME OFF AND WAS STUCK AT OTBD SCAVENGE EJECTOR. R & R MAGNETIC LEVEL INDICATOR IAW AMM 28-42-01. OPS CHECKED GOOD.

Part: CONDITIONER — FAILED (FUEL SYSTEM) · airframe 21,006 hrs · 12,814 cycles

AIR TURN BACK, DUE TO FUEL 1 LOW LEVEL ON EICAS. NO OTHER INDICATION BESIDES EICAS MESSAGE. ALL FUEL QUANTITY INDICATION WERE NORMAL, ONCE AC FUEL PUMP 1 WAS SELECTED ON FUEL 1 LOW LEVEL EICAS WAS REMOVED FROM EICAS. FUEL 1(2) LO LEVEL WARNING EICAS MESSAGE, 1 INOP. R & R FCU IAW AMM 28-41-03, OPS CHECK OK.

Part: FAN — FAILED (COCKPIT) · airframe 18,665 hrs · 11,331 cycles

FLT 6102 IAD-BOS DIVERTED TO JFK, ELECTRICAL SMOKE RE-APPEARED DURING FLIGHT. NO SYSTEM FAILURE NOTED. FOUND ODOR COMING FROM RECIRCULATING FAN VENTS IN COCKPIT. REMOVED AND REPLACED RECIRCULATING FAN PER AMM 21-24-01. OPS CHECK OK.

Part: FAN — FAILED (COCKPIT) · airframe 18,665 hrs · 11,331 cycles

FLT 6102 IAD-BOS DIVERTED TO JFK, ELECTRICAL SMOKE RE-APPEARED DURING FLIGHT. NO SYSTEM FAILURE NOTED. FOUND ODOR COMING FROM THE RECIRCULATING FAN VENTS IN THE COCKPIT. REMOVED AND REPLACED RECIRCULATING FAN PER AMM 21-24-01. OPS CHECK OK.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,664 hrs · 11,330 cycles

FLT 1253 BOS-IAD, AN ELECTRICAL SMOKE SMELL WAS OBSERVED BY THE F/O AND F/A DURING FLIGHT. PERFORMED INSPECTION AS PER FIM 25-30-00-810-801-A. ALL CHECKS NORMAL.

Part: PRECOOLER — CRACKED (BLEED AIR SYS) · airframe 14,633 hrs · 8,863 cycles

FLT 136 RSW-JFK, A/C DIVERTED TO MCO DUE TO BLEED LEAK 1 ON CLIMBOUT FOLLOWED BY BLEED LEAK 2. TECHNICIAN FOUND PRECOOLER ON NR 1 ENGINE CRACKED. REMOVED AND REPLACED NR 1 ENGINE PRECOOLER. PERFORMED ENGINE PNEUMATIC BLEED TEST IAW 36-11-00, OPS CHECK GOOD.

Part: WIRE HARNESS — SHORTED (LE SLAT) · airframe 14,337 hrs · 8,703 cycles

FLT 1732 BDA-JFK, CREW DECLARED EMERGENCY DUE EICAS SLAT FAIL WITH NO ACTION ON SLAT/FLAP LEVER. FOUND SHORT ON SLAT HARNESS 2/3 RT SIDE. REPLACED HARNESS 2/3 RT SIDE AND OPS CHECK GOOD.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 11,851 hrs · 7,215 cycles

FLT 1124 - FLL-CLT FLT CREW DECLARED EMERGENCY LANDING DUE TO STEER FAIL DISPLAYED ON EICAS UPON LG NSW STEERING DOES NOT FUNCTION. RESET A/C IAW AMM TASK 24-23-00-810-806-A. ALL MESSAGES CLEARED. A/C OK TO CONTINUE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 11,676 hrs · 7,106 cycles

FLT JB1329 BOS-BWI STEERING FAIL EICAS MESSAGE UPON PUTTING GEAR DOWN GOING INTO BWI. PERFORMED GO AROUND AND QRH AND MESSAGE REOCCURRED ON SECOND GEAR DOWN CYCLE. UPON LANDING NO NOSE STEERING TOWED TO THE GATE. MX INTERROGATED CMC FOUND FAULT CODE 45452175CMC T/S IAW FIM 45-45-00-810-973-A, RESET NWS C/B'S FAULT CLEARED. NO FURTHER FAULTS PRESENT TRANSITORY CONDITION OF NWS PER FIM. AIRCRAFT RETURNED TO SERVICE.

Part: COFFEEMAKER — SHORTED (FWD GALLEY) · airframe 10,103 hrs · 6,141 cycles

FLT 1761, FLL-SJU, AIR RETURN TO FLL DUE SMOKE FROM FWD GALLEY, RT COFFEE POT SHORTED. FOUND EVIDENCE OF BURNT WIRE NEXT TO WATER HEATER RT COFFEEMAKER. REMOVED AND REPLACED BOTH COFFEEMAKERS, LT REMOVED COFFEEMAKER PRECAUTIONARY PER AMM 25-37-03, OPS CHECK NORMAL. ALSO PERFORMED VISUAL INSPECTION OF SURROUNDING AREAS WITHIN THE COMPARTMENT HOUSING THE COFFEEMAKERS AND NO EVIDENCE OF ANY DAMAGE RELATING TO ARCING OR BURNING NOTED. ALL A/C SIDE WIRING, INSULATION, CONNECTORS AND TERMINALS APPEAR SERVICEABLE AT THIS TIME. AS A PRECAUTION, ALSO PERFORMED VISUAL INSPECTION OF AFT GALLEY COFFEEMAKERS AND ADJACENT AREAS, ALL OPS CHECK NORMAL.

Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 9,455 hrs · 5,787 cycles

FLT 1401, FLL-AUS, SLAT FAIL AFTER TAKEOFF, RETURN TO FLL. TROUBLESHOT PER FIM 27-81-00-810-807-A, FOUND DEFECTIVE AND REPLACED SLAT SKEW SENSORS, RT 2/3 & RT 3/4 OUTBOARDS PER AMM 27-83-01. CLEARED INHIBITS AND CYCLED FLAPS/SLATS NORMALLY. SLAT FAIL MESSAGE CLEARED. A/C IS OK FOR SERVICE.

Part: SENSOR — DEFECTIVE (LE SLAT) · airframe 9,455 hrs · 5,787 cycles

FLT 1401, FLL-AUS, SLAT FAIL AFTER TAKEOFF, RETURN TO FLL. TROUBLESHOT PER FIM 27-81-00-810-807-A. FOUND DEFECTIVE AND REPLACED SLAT SKEW SENSORS, RT 2/3 & RT 3/4 OUTBOARDS PER AMM 27-83-01. CLEARED INHIBITS AND CYCLED FLAPS/SLATS NORMALLY. SLAT FAIL MESSAGE CLEARED. A/C IS OK FOR SERVICE.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 6,783 hrs · 4,296 cycles

FLT 907, JFK-ORD, COMPLETE LOSS OF HYDRAULICS SYSTEM NR 2. ACCOMPLISHED MANUAL GEAR EXTENSION PER QRH. FOUND NR 2 EDP LEAKING. REMOVED AND REPLACED NR 2 EDP IAW AMM 29-11-01, OPS CHECK AND LEAK CHECK GOOD. SERVICED HYD RESERVOIR IAW AMM 12-12-01. CHECK OK.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 6,354 hrs · 4,070 cycles

FLT 626, HOU-JFK, FLAP FAIL EICAS MESSAGE ON FLAP/SLAT RETRACTION AFTER TAKEOFF (FLAP 3). PERFORMED QRH PROCEDURE AND LANDED BACK AT HOU (LANDING WEIGHT 92,000 LBS) NORMAL TOUCHDOWN. REMOVED AND REPLACED RIGHT NR 4 FLAP ACTUATOR IAW E190 AMM 27-51-01, OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE.

Part: CONTROL LEVER — FAILED (COCKPIT) · airframe 5,406 hrs · 3,541 cycles

FLT NR 1304, IAD-JFK - SLAT FAIL EICAS MSG SLATS STUCK FULLY EXTENDED. REMOVED AND REPLACED SLAT FLAP CONTROL LEVER IAW 27-53-01. SLAT/SLATS RETRACT AND STOWED NORMALLY.

Part: WIRE HARNESS — DEFECTIVE (L/E SLAT) · airframe 5,298 hrs · 3,481 cycles

SLAT FAIL EICAS MESSAGE AFTER SELECTING FLAPS 1. SLAT POSITION SHOWED LOCKED SOMEWHERE BETWEEN THE 0 AND 1 POSITION WITH - DISPLAYED IN THE SLAT POSITION BOX. FURTHER MOVEMENT OF FLAP HANDLE HAD NO EFFECT ON SLAT POSITION. MESSAGE OCCURED AROUND 210 KTS DURING FIRST MOVEMENT OF HANDLE. REMOVED AND REPLACED RT OLD STANDARD SLAT HARNESSES (W611) AND (W612) PER EO E2707138 PART II, CLEARED SLAT FAIL MESSAGE IAW 27-83-00. ALL EICAS MSG CLEAR.

Part: WARNING SYSTEM — ACTIVATED (T/E FLAP) · airframe 5,261 hrs · 3,459 cycles

WHEN SELECTING FLAPS 1 RECEIVED FLAP FAIL EICAS. RAN QRH. LANDED WITH FLAPS/SLATS 0. PERFORMED FIM TASK 27-51-00-810-802-A, VERIFIED ALL FLAP ACTUATOR TORQUE LIMITERS ARE NOT TRIPPED. FAULT CLEARED. FLAP OPERATIONAL CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 1,364 hrs · 889 cycles

EMERGENCY LIGHT RT CENTER OVERWING SLIDE WOULD NOT ILLUMINATE. ACCOMPLISHED WIRING CHK IAW AWM 33-50-50. WIRES FROM BATTERY PACK NR 4 CONNECTOR (P1895) PIN "H" TO LIGHT CONNECTOR (P3321) PINS A/B CHECK GOOD. FOUND BATTERY PACK NR 4 AT FAULT, REMOVED AND REPLACED PACK NR 4 IAW 33-50-01, ALL OPS CHK NORMAL.

Part: WARNING LIGHT — ILLUMINATED · airframe 886 hrs · 551 cycles

ON TAKEOFF ROLL AT APPROX 70 KTS, AURAL "NO TAKEOFF BRAKES". NO EICAS MESSAGE. REJECTED TAKEOFF MAX SPEED APPROX 90 KTS. ACCOMPLISHED FIM TASK 31-51-00-810-803A. NO EICAS MESSAGES AND NO CMC MESSAGES PRESENT. AIRCRAFT OK FOR CONTINUED SERVICE.