N14143

Part: UNKNOWN — ODOR (CABIN) · airframe 46,605 hrs · 30,300 cycles

BURNING RUBBER SMELL AFTER TAKE OFF ON CLIMB. PERFORMED FIM PROCEDURES. PERFORMED HIGH POWER ENGINE RUNS. NO SMOKE OR ODOR PRESENT. ALL INDICATIONS NORMAL.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 46,397 hrs · 30,104 cycles

WEIRD CHEMICAL SMELL COMING FROM COCKPIT ON DESCENT. PERFORMED WITH ENGINE BLEED 1 AND 2. OC SAT. RAN PACK SYSTEM DURING HIGH POWER RUN ON FULL HOT AND FULL COLD. ENGINES AND PACKS WERE ON TOTAL TIME OF 40 MINUTES. NO DEFECTS OR SMELL WERE NOTED.

Part: LAMP — INOPERATIVE (ZONE 200 EXT) · airframe 46,098 hrs · 29,816 cycles

RIGHT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EXTEIOR FWD EMERGENCY LIGHT. OPS CHECK SAT

Part: A/C PACK — ODOR (NR 1) · airframe 45,949 hrs · 29,468 cycles

DIRTY SOCK SMELL ON DECENT FROM PACK 1. FOLLOWED FIM. DIRTY SOCK SMELL ODOR WAS NOT PRESENT AT THIS TIME. PERFORMED GVI INSPECTION OF THE #1 PACK SYSTEM, NO DEFECTS NOTED. HIGH POWER ENG RUNS PERFORMED. DIRTY SOCK SMELL NOT PRESENT. PERFORMED BORESCOPE INSPECTION OF ENG 1 COMPRESSOR INLET. NO INDICATION OF OIL RESIDUE FOUND AT THIS TIME.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 45,706 hrs · 29,407 cycles

CRACK ALONG INTERNAL FUEL TANK DOUBLER UNDER RH WING RIB 9 FOUND CRACK TO BE MIGRATING ACROSS DOUBLER THROUGH 3 HIGH LOCK (FWD) HOLES. REMOVED HILOCK COLLARS FROM SPLICE ON OUTBD SIDE OF RIB 9 AND REMOVED FILLET SEALANT. REMOVED SPLICE BELOW RIB 9. FOUND RH WING SPLICE TO BE CRACKED. DRILLED NEW DOUBLER FOR RIB 9 UNDER RH WING READY FOR INSTALL. COMPLETED INSTALL OF DOUBLER PLATE AT RH WING AT RIB 9. COMPLIED WITH ETD 2023-145-008902 AT RH WING RIB 9 SPLICE PLATE. INSTALLED FUEL PANELS 631DB AND 641AB. PERFORME DLEAK CHECK. LEAK CHECK FOUND TO BE SAT. NO LEAKS NOTED.

Part: LAMP — INOPERATIVE · airframe 44,532 hrs · 28,343 cycles

LH FORWARD EXTERNAL EMERGENCY LIGHT INOP. R/R LH FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT

Part: NONE — INOPERATIVE · airframe 44,439 hrs · 28,258 cycles

SMOKE SMELL FROM COCKPIT DURING DEP CLIMB OUT. REMOVED AND REPLACED SLEEVES BETWEEN DUAL TEMP CONTROL VALVE AND Y-DUCT ON #2 PACK VALVE. REMOVED AND REPLACED #2 ACM. O-RING BETWEEN TURBINE OUTLET DUCT AND ACM STILL NEEDS TO BE INSTALLED. INSTALLED O-RING. OPS/LEAK CHECK SAT. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE · airframe 44,079 hrs · 27,933 cycles

EMERGENCY CEILING LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IN COCKPIT. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN · airframe 43,644 hrs · 27,567 cycles

RH FWD FUSELAGE I, TWO LIGHTING STRIKES SUSPECTED BTW FR 1A & 2 AND ABOVE STR 13R. DURING LIGHTING STRIKE INVESTIGATION MULTIPLE STRIKE SPOTS BLENDED WITHIN LIMITS, SOME ACCEPTED AS IS AND 2 BLEND OUT FOUN OUT OF LIMITS AND NEED A EXTERNAL DOUBLER REPAIR. FIRST REPAIR (BLEND #4) PERFORMED AT FR2 STR 13R AND SECOND (BLEND #7) AT FR4 STR 13R

Part: UNKNOWN — UNKNOWN · airframe 43,644 hrs · 27,567 cycles

MULTIPLE DENTS FOUND ON EXTERNAL SKIN OF MAIN DOOR BTW STR 06L AND STR 08L, STR 12L AND STR 15L. MULTIPLE DENTS ON EXT SIGN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L STRIPPED FOR INVESTIGATION ON EXT SKIN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L DENTS 1, 2, 3, 4 AND 9 FOUND WITHIN LIMITS AND DENTS #5, 6, 7, AND 8 FOUND BEYOND LIMITS ON EXT SKIN OF MAIN DOOR BTW STR 12L-14L DENTS REPAIRED

Part: NONE — NONE · airframe 43,644 hrs · 27,567 cycles

CF1, SKIN FOUND WITH EXISTING BLEND BTW FR 20-21 STR 11-12L. CF1, SKIN BTW FR 20-21 AND STR 11-12L FOUND BLENDED OUT OF LIMITS. REPAIR WAS MADE.

Part: SKIN — DAMAGED (FRM 3 S1-13R) · airframe 43,644 hrs · 27,567 cycles

FWD FUSELAGE 1 RH SKIN AT FR 3 BTW STR 01R-13R SEVERAL RIVETS NOT PROPERLY INSTALLED. PAINT STRIPPED ON FWD FUSELAGE I RH, STR 01R-13R FOR INVESTIGATION ON FWD FUSELAGE I RH SKIN AT FR3 BTW STR 01R-13R IMPROPERLY INSTALLED RIVETS REMOVED. RIVETS HOLES FOUND TO BE ELONGATED, REPAIR LAYED OUT FOR SUBMISSION TO ENGINEERING STRINGER C/O ATS STR 1, 4, 9, 11 REMOVED AND FRAME SPLICE AT STR12. RH SKIN AT FR3 BTW STR 1 AND 13R REPAIRED. STR C/OUT AND FRAME SPLICE REINSTALLED.

Part: UNKNOWN — UNKNOWN · airframe 43,644 hrs · 27,567 cycles

RIVET FOUND ON LEADING EDGE II RH. DENT AT RIVET LOCATION OF LEADING EDGE II RH FOUND OUT OF LIMITS AND NEEDS REPAIR PARTS FOR REPAIR SPLICE AND FILLER FABRICATED. REPAIR SPLICE AND FILLER INSTALLED

Part: DOUBLER — CORRODED (FRM 65-66 S21L-R) · airframe 43,644 hrs · 27,567 cycles

CORROSION FOUND ON ANTENNA INNER DOUBLER BTW FR 65-66 AND STR 21LH + STR 21RH. REMOVED R. ALT ANTENNA FOR ACCESS, REMOVED INNER AND OTHER DOUBLER FOR INVESTIGATION. AFTER FURTHER INVESTIGATION FOUND OUTER SKIN CRACK OUT OF LIMITS AT R. ALT ANTENNA LOCATION. PERFORMED CUT OUT ON OUTER SKIN AT R ALT ANTENNA LOCATION. REPAIRED OUTER SKIN AT R.ALT ANTENNA LOCATION. INNER DOUBLER BLENDED OUT OF LIMITS AND REPLACED WITH NEW PART.

Part: NONE — NONE · airframe 43,644 hrs · 27,567 cycles

CENTER FUSE II, FRAME 25 CRACKED BTW STR 16R-15R. FRAME REPAIRED

Part: NONE — NONE · airframe 43,644 hrs · 27,567 cycles

CRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. FRAME REPAIRED

Part: SKIN — DENTED (FRMS 8-9 S18-20L) · airframe 43,644 hrs · 27,567 cycles

LH FWD FUSELAGE II, DENT FOUND ON EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. DENT REMOVED BY CUT OUT ON LH FWD FUSE II EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. PATCH DOUBLER LOCALLY FABRICATED. AT LH FWD FUSELAGE II, EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L DENT REPAIRED.

Part: NONE — NONE · airframe 43,644 hrs · 27,567 cycles

CF1 FLOOR STRUCTURE PROFILE OMEGA BTW FR 20-23 LH CORRODED. AFTER FURTHER INVESTIGATION OMEGA BEAM FOUND CRACKED AT FASTENERS LOCATION. CF1 FLOOR STRUCTURE, OMEGA BEAM REPLACED.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 43,333 hrs · 27,307 cycles

PHOTOLUMINESCENT STRIP CRACKED AT SEAT 1A. R/R PHOTOLUMINECENT STRIP

Part: SEAT FRAME — CRACKED (CABIN) · airframe 42,726 hrs · 26,783 cycles

FOUND SEATS 23A, 22A, 24A, 21A, 7A, 5A HAVE A CRACK BELOW ARMREST ON STRUCTURE. R&R 23A, 22A, 24A, 21A, 7A, 5A SEATS. OPS CHECK SAT. NO DEFECTS NOTED.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 42,009 hrs · 26,108 cycles

LG AIR GROUND FAIL EICAS MESSAGE IMMEDIATELY AFTER TAKE OFF. ADJUST NLG TORQUE LINK TARGET. PERFORM GEAR SWINGS FAIL. TROUBLESHOT TO LGEU. R&R LGEU AND GEAR SWINGS 5 TIMES. OPS CHECK SAT. NO OTHER DEFECTS NOTED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 41,978 hrs · 26,083 cycles

FORWARD EXTERNAL EMERGENCY LIGHTS FWD OF WING INOPERATIVE. REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED BURNT OUT BULBS. OPS CHECK SAT.

Part: FASTENER — LOOSE (EMERGENCY EXIT) · airframe 41,978 hrs · 26,083 cycles

RIGHT PASSENGER CABIN, ESCAPE HATCH DOOR TOOK SEVERAL MINUTES TO REMOVE DOOR TO FOM. FOUND FASTENERS THAT ATTACH SIDEWALL PANEL TO EMERGENCY EXIT DOOR FRAME LOOSE CAUSING DOOR TO JAM ON FASTENERS. RESECURED FASTENERS. OPS CHECK SAT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 41,852 hrs · 25,962 cycles

LG LEVER DISAGREE ON TAKE-OFF. PERFORMED GVI OF NLG, MLG, AND WHEEL WELLS WITH NO DEFECTS. CHECKED CMC WITH NO FAULTS. PERFORMED GEAR SWINGS. FOUND TO BE TRANSITORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG LEVER) · airframe 41,630 hrs · 25,766 cycles

LG LEVER DISAGREE MASTER WARNING ON TAKE OFF. CHECKED FOR PROPER UP LOCK HOOK POSITIONS. NO FAULTS FOUND. CHECKED PROX SWITCHES FOR CONDITION AND SECURITY. NO DEFECTS FOUND. PERFORMED MULTIPLE EXTENSION AND RETRACTION TESTS. OPS CHECK SAT. NO DEFECTS NOTED. NO ABNORMAL EICAS MESSAGES

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,616 hrs · 25,753 cycles

BOTH OVER WING EMERGENCY LIGHTS INOPERATIVE. R&R #4 EMERGENCY LIGHT BATTERY. OPS CHECK FAILED. R&R BATTERY CHARGER ASSEMBLY. OPS CHECK SAT. ORIGINAL BATTERY STILL INSTALLED.

Part: UNKNOWN — NOISY (EMERGENCY EXIT) · airframe 41,087 hrs · 25,283 cycles

LEFT OVER WING EMERGENCY EXIT WHISTLES. REMOVED AND REINSTALLED EMERGENCY EXIT AND THEN PERFORMED PRESSURIZATION PROCEDURE. NO DEFECTS NOTED AND LEAK CHECK SAT AT THIS TIME.

Part: ELECTRONIC UNIT — FAULTY (MLG) · airframe 40,978 hrs · 25,182 cycles

ON APU START SEVERAL EICAS MESSAGES APPEARED AND REMAIN ON. R&R AC STATIC INVERTER. OPS CHECK SAT. ONLY FOR THE MESSAGE 115 VAC BUS OFF. OPS CHECK FAIL FOR ALL OTHER MESSAGES. FOUND FAULTY LGEU. R&R LGEU. OPS CHECK SAT. ALL EICAS FAULTS CLEARED. NO DEFECTS NOTED WITH GUST LOCK OPERATION.

Part: ELECTRONIC UNIT — INOPERATIVE (MLG) · airframe 40,927 hrs · 25,134 cycles

LANDING GEAR AIR/GROUND FAIL ON ROTATION, GEAR WILL NOT RETRACT. R&R LEGU. JACKED AND SWUNG GEAR MULTIPLE TIMES. OPS CHECK SAT. NO OTHER DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 40,231 hrs · 24,503 cycles

CABIN WILL NOT MAINTAIN PRESSURIZATION OPERATING ON ONE PACK. PERFORMED AIRCRAFT PRESSURIZATION WITH BOTH PACKS OPERATIVE. NO PRESSURE LOSS NOTED. OPS CHECK SAT.

Part: SENSOR — INOPERATIVE (SMOKE DETECTOR) · airframe 40,071 hrs · 24,385 cycles

ON DECENT FROM 8-6000 FEET CREW HAD AURAL AND EICAS MESSAGE. LAV SMOKE WARNING IN FLIGHT PROCEDURE PER QRH PULLED C/B E9 AND E10. NO APU RUNNING. NO SMOKE NOTED AND NO ODOR NOTED. R&R LAV SMOKE DETECTOR SENSOR. OPS CHECK SAT. PERFORMED HIGH POWER RUNS WITH NO DEFECTS NOTED AND INSPECTED WIRING WITH NO FAULTS. UPON FURTHER TROUBLESHOOTING OF THE LAV DETECTION, FOUND GASPER LINE FILTER DAMAGED. R&R GASPER LINE FILTER. NO OTHER DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,876 hrs · 23,264 cycles

CENTER FLOORBEAM IS CORRODED AT FR 50-61. FABRICATED AND INSTALLED REPAIR DOUBLER ONTO CENTER FLOORBEAM AT FR 59-61. HFEC INSPECTION FOUND NOTED NO DEFECTS IN CUT OUT OF FLOORBEAM.

Part: LIGHT — DEFECTIVE (EXTERIOR) · airframe 38,499 hrs · 22,888 cycles

EXTERNAL EMERGENCY LIGHT AT MAIN DOOR INOP. TROUBLE SHOT TO BAD CONTACT ASSY. R&R MAIN CABIN DOOR LIGHT ASSY. OPS CK SAT MEL CLEARED.

Part: WIRE — BROKEN (CABIN) · airframe 38,499 hrs · 22,888 cycles

EXTERNAL EMERGENCY LIGHT AT LT FORWARD LOWER FAIRING INOP. REMOVED AND REPLACED NR 1 BATTERY CHARGER ASSY FOR EMERGENCY LIGHTS. OPS CHECK FAILED. FOUND BROKEN/CHAFFED WIRE. REPAIRED BY SPLICING. OPS CHECK SAT.

Part: BUTTON — FAILED (WINDOW HEAT) · airframe 36,918 hrs · 21,530 cycles

THE CREW REPORTED WINDSHIELD HEAT NR 1 FAILED IN FLIGHT AND HAD ELECTRICAL BURNING ODOR. MAINTENANCE REPLACED THE WINDSHIELD HEAT SYSTEM PUSH BUTTON. OPS CHECKED GOOD.

Part: VALVE — FAULTY (CABIN PRESSURE) · airframe 35,340 hrs · 20,430 cycles

PILOT REPORTED LOST PRESSURIZATION GOING THROUGH 10,000 FT. MAINTENANCE R & R AIR DISTRIBUTION GROUND CONNECTION VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · airframe 35,245 hrs · 20,366 cycles

DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 35,245 hrs · 20,366 cycles

DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 79, STR 5-6L. REPAIRED RIVET AREA ON FUSELAGE AROUND RIVET FROM 79, STR 5L-6L IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 35,245 hrs · 20,366 cycles

DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 78, STR 5-6R. REPAIRED AREA ON FUSELAGE AROUND RIVET FROM 78 IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (NR 1 PYLON) · airframe 33,545 hrs · 19,214 cycles

DURING ROUTINE MAINTENANCE THE NR 1 PYLON FOWARD YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE YOKE FITTING IAW STS EA 26-2014-063.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,221 hrs · 18,358 cycles

DURING MAINTENANCE INSPECTION, THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TIRE — FAILED (NR 2) · airframe 32,215 hrs · 18,352 cycles

DURING TAKEOFF, NR 2 TIRE BLEW FROM FOD DAMAGE CAUSING MULTIPLE DAMAGES TO THE RT GEAR AUX DOOR. MAINTENANCE R & R THE RT MLG AUX DOOR IAW AMM 32-10-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF CHECKS.

Part: ENGINE — FOD (NR 2) · airframe 32,215 hrs · 18,352 cycles

WHILE ON TAKEOFF THE NR 2 TIRE BLEW APART IMBEDDING PART OF TIRE IN THE NR 2 ENGINE AND DAMAGING THE FLAP. THE NR 2 ENGINE WILL BE CHANGED AND THE FLAP TEMPORARY REPAIRED FOR A FERRY FLIGHT TO REPAIR THE SMALL DAMAGE TO THE FLAP. ALL WORK WILL BE ACCOMPLISHED IAW WITH RR MANUAL 72-00-00. AFTER BLEED LEAKS AND OIL LEAKS ARE VERIFIED GOOD THE ACFT WILL BE RELEASED FOR A FERRY FLIGHT TO FURTHER EVALUATE DAMAGES AND REPAIR THE FLAP.

Part: LIGHT — BURNED (CABIN) · airframe 30,447 hrs · 17,241 cycles

CREW REPORTED SMOKE COMING FROM CABIN OVERHEAD LIGHTS AT SEAT 23A. MX INSPECTED AND FOUND LIGHT RECEPTACLE BURNED. R & R SIDEWALL LIGHT ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (LT WING AILERON) · airframe 29,726 hrs · 16,792 cycles

DURING C-CHECK, THE LT WING AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 29,726 hrs · 16,792 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 28,729 hrs · 16,159 cycles

LEFT OMEGA BEAM, RT AND LT SPLICE BETWEEN FRAMES 16 AND 17 CRACKED. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 28,729 hrs · 16,159 cycles

CENTER OMEGA BEAM SPLICE BETWEEN FRAMES 16 AND 17 CRACKED ON LT SIDE. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.

Part: WINDSHIELD — CRACKED (COCKPIT)

THE CREW REPORTED THE F/O WINDSHIELD CRACKED INTO SPIDER WEB FORM AT 13,000. ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE F/O`S WINDSHIELD. OPS CHECKS WERE GOOD.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 23,869 hrs · 13,019 cycles

SHV - DURING C-CHECK FRAME 65 SHEAR CLIP HAS CORROSION STRINGER 16L-17L. MAINTENANCE PERFORMED REPAIR AT FRAME 65 SHEAR CLIP STRINGER 16L-17L IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (HORIZ STAB) · airframe 23,869 hrs · 13,019 cycles

SHV - DURING C-CHECK THE RT HORIZONTAL STABILIZER FITTING WAS FOUND TO BE WORN CAUSING THE BUSHING TO MIGRATE. MAINTENANCE PERFORMED A REAMING AND OVERSIZE BUSHING REPAIR TO THE FITTING IAW EMB 145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (HORIZ STAB) · airframe 23,869 hrs · 13,019 cycles

SHV - DURING C-CHECK THE LT HORIZONTAL STABILIZER FITTING WAS FOUND TO BE WORN CAUSING THE BUSHING TO MIGRATE. MAINTENANCE PERFORMED A REAMING AND OVERSIZE BUSHING REPAIR TO THE FITTING IAW EMB 145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 19,779 hrs · 10,469 cycles

FLIGHT 2415 - EWR - FLIGHT CREW REPORTED SMOKE SMELL AROUND EXIT ROW. EWR MX FOUND EXIT SIDE WALL LAMP END BROKEN. REMOVED AND REPLACED EXIT SIDE WALL LAMP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PRECOOLER — CRACKED (BLEED AIR SYS) · airframe 19,593 hrs · 10,364 cycles

CLE FLT 2359 THE CREW REPORTED A BLEED 1 & 2 OVERTEMP MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PRECOOLER. ALSO REPLACED THE NR 2 FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,931 hrs · 10,008 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 17,239 hrs · 9,096 cycles

THE CREW REPORTED THAT DURNG CRUISE THE MAIN PITCH TRIM WAS INOP. THE ACFT RETURNED TO DEPARTURE WHERE IT KANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE

Part: ACTUATOR — LEAKING (NLG) · airframe 16,782 hrs · 8,847 cycles

FLIGHT 3096 - EWR - FLIGHT CREW REPORTED LG GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT DURING GEAR EXTENSION, MSG GOES AWAY AFTER 2 SECONDS. EWR MX REMOVED AND REPLACED RT NOSE GEAR DOOR ACTUATOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 15,893 hrs · 8,382 cycles

IAH - FLIGHT 2924, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM BOTH COFFEEMAKERS. MX PLACED THE COFFEEMAKERS ON NEF NR GL01 D CTL NR 160100, AND THE ACFT WAS RETURNED TO SERVICE. ON 12/14/08 THE DISCREPANCY REPEATED AND MX INSPECTED THE COFFEEMAKERS, FOUND THEM TO BE DIRTY ON THE HEATERS, CLEANED THE HEATERS, OPS CHECKED WITH NO DEFECTS, REMOVED THE NEF, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 15,893 hrs · 8,382 cycles

IAH - FLIGHT 2924, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM BOTH COFFEEMAKERS. MX PLACED THE COFFEEMAKERS ON NEF NR GL01 D CTL NR 160100, AND THE ACFT WAS RETURNED TO SERVICE. ON 12/14/08 THE DISCREPANCY REPEATED AND MX INSPECTED THE COFFEEMAKERS, FOUND THEM TO BE DIRTY ON THE HEATERS, CLEANED THE HEATERS, OPS CHECKED WITH NO DEFECTS, REMOVED THE NEF, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 2484 - EWR - FLIGHT CREW REPORTED ELECTRICAL ODOR IN CABIN. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF ELECTRICAL SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY, SYSTEM WORKING PROPERLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: ATTACH BRACKET — WORN (RT AILERON) · airframe 14,074 hrs · 7,413 cycles

RIGHT AILERON PCA ATTACH BRACKET WORN. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177. OPS CHECK GOOD AIRCRAFT STILL IN "C" CHECK.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 10,764 hrs · 5,763 cycles

FLT 2780 - DURING PREFLIGHT INSPECTION THE CEILING EMERGENCY LIGHT AT THE PASSENGER DOOR DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 10,220 hrs · 5,464 cycles

EWR LOG SQUAWK FLT NR 1206, FOUND SEVERAL CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB-145XR AMM 33-50-04. OPS CHECK GOOD CLOSED

Part: CARBON SEAL — FAILED (NR 4) · airframe 8,417 hrs · 4,475 cycles

IN EWR, CREW REPORTED LAV SMOKE AFTER TAKEOFF, NOTICEABLE HAZE AND SMELL IN CABIN, MAINTENANCE FERRY FROM EWR TO TYS. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW EMB-145AMM SEC-2 AND TASK CARD 6271001, OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED TO SERVICE. FAILURE OF THE ENGINE WAS THE NR 4 CARBON SEAL.

Part: BALLAST — BURNED (GALLEY) · airframe 8,226 hrs · 4,369 cycles

IAH - FLIGHT 2866, DURING CLIMB THE CREW REPORTED SMOKE IN THE GALLEY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 7,590 hrs · 4,043 cycles

CRP - FLIGHT 2543, DURING PREFLIGHT INSPECTION, THE EMERGENCY EXIT SIGN ON THE RIGHT HAND EMERGENCY EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 7,590 hrs · 4,043 cycles

CRP - FLIGHT 2543, DURING PREFLIGHT INSPECTION, THE EMERGENCY EXIT SIGN IN THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEVEL GEAR — BROKEN (NR 2 ENGINE) · airframe 4,435 hrs · 2,360 cycles

BTR - FLIGHT 3334, THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN IN FLT. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,239 hrs · 1,178 cycles

IAH - DURING MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE CEILING EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — LOOSE (CABIN) · airframe 3,667 hrs · 1,954 cycles

CLE- FLIGHT 2708, CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHT STRIP BY THE CABIN DOOR WAS DETACHED FROM THE FLOOR. MAINTENANCE INSPECTED AND RESECURED THE AISLE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD.