N24103

Part: BUSHING — MISSING (SPOILER) · airframe 44,895 hrs · 26,740 cycles

ACTUATOR ATTACH POINT ON R/H GROUND SPOILER HAT BUSHING MISSING. REAMED BOTH BUSHING HOUSINGS, INSTALLED NEW HAT BUSHINGS. AIRCRAFT STILL IN C CHECK.

Part: SUPPORT FRAME — CRACKED (FRAMES 10-11) · airframe 44,895 hrs · 26,740 cycles

TYS- CRACK ON FRAME FWD OF LH COCKPIT CEILING SPEAKER BETWEEN FRAME 10-11. THE CRACKED SECTION WAS REMOVED A SUPPORT AND SPLICE WERE FABRICATED AND INSTALLED IAW ENGINEERING DOCUMENT PROVIDED.

Part: SUPPORT — CRACKED (NLG UPLOCK) · airframe 44,895 hrs · 26,740 cycles

TYS A/C WAS FOUND WITH THE NLG UP LOCK SUPPORT FRAME ON THE AFT SIDE CRACKED. MAINTENANCE REPLACED THE UP LOCK SUPPORT BRACKET IAW EMB 145XR SRM 51-40-02. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 44,082 hrs · 26,124 cycles

THE CREW REPORTED STRONG OIL ODOR DURING DESCENT WHEN THROTTLES WERE AT IDLE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,862 hrs · 25,954 cycles

IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 64-65 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLER / DOUBLER REPAIR. OPERATIONAL CHECKS WERE PERFORMED WITH NO DISCREPANCIES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,862 hrs · 25,954 cycles

IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 68-69 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLER / DOUBLER REPAIR. OPERATIONAL CHECKS WERE PERFORMED WITH NO DISCREPANCIES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,837 hrs · 25,934 cycles

DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18A WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,837 hrs · 25,934 cycles

DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18CD WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 42,630 hrs · 25,042 cycles

FLIGHT 4178, THE CREW REPORTED STRONG OIL FUMES POSSIBLY COMING FROM THE NR 1 PACK. THE AIRCRAFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECKED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 38,987 hrs · 22,559 cycles

DURING C-CK STRINGER 18R CORRODED AT FR 23. REMOVED STRINGER AND SPLICED IN A NEW STRINGER IAW SRM 53-00-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — SHORTED (COCKPIT) · airframe 37,589 hrs · 21,566 cycles

THE CREW REPORTED THAT AT LEVEL CRUISE AT FL360, F/O PFD WENT RED, THEN BLANK AND THEN HAD AN INTENSE SULFUR/ELECTRICAL FIRE ODOR OCCURRED IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE CONTRACT MAINTENANCE PLACED THE F/O PFD ON MEL 34-22-01-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. LATER, MAINTENANCE R & R THE F/O'S PFD, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, CLEARED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (AFT CARGO) · airframe 37,299 hrs · 21,370 cycles

AFT BAGGAGE SMOKE DETECTOR FAILED. R & R SMOKE DETECTOR. ACFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,466 hrs · 20,791 cycles

THE CREW REPORTED EMERGENCY EXIT LIGHT IDENTIFER ABOVE THE F/A JUMPSEAT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: SHEAR TIE — CORRODED (FRAME 13) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, SHEAR TIE CORRODED, AT FRAME 13 BETWEEN STRINGERS 20-21R. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 9) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, SHEAR TIE AT FRAME 9 BETWEEN STRINGER 20-21L CORRODED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: RECEPTACLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, CORROSION ON VENTRAL TANK FWD FACE AROUND THREE CONNECTOR RECEPTACLES. REPAIRED IAW EC5320-01942 REV. ORIG. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN SPLICE — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, SKIN SPLICE CORRODED, BETWEEN FRAMES 13-14 STRINGERS 20R-20L. MAINTENANCE PERFORMED REPAIR ON SKIN SPLICE IAW SRM 53-00-02, FIG 201. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (FUEL TANK) · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK VENTRAL TANK CHAFED ON LT SIDE FRAME 51-52. MAINTENANCE REPAIRED VENTRAL TANK IAW EC5320-01941 REV ORIG. ACFT APPROVED FOR RETURN SERVICE.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, LOWER CENTER FUEL LINE SUPPORT BRACKET ON RIB 1 OF VENTRAL TANK CORRODED. MAINTENANCE R & R SUPPORT BRACKET IAW SRM 53-20-07. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK CORROSION, ON VENTRAL TANK FWD FACE AT SUPPORT BRACKET FOR FUEL LINE. REPAIRED SUPPORT BRACKET IAW EC5320-01942 REV. ORIG. ACFT APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-14. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAMES 11-12) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 11-12 AND STRINGERS 20-21R. MAINTENANCE R & R THE SKIN IAW SRM 51-20-01. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FRAMES 20-22) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 33,066 hrs · 18,566 cycles

DURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-18. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01940. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

CENTER OMEGA BEAM CORRODED BEYOND LIMITS. R & R GUSSET.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 27,459 hrs · 14,950 cycles

R & R OMEGA BEAM SUPPORT CRACKED. R & R SUPPORT.

Part: SILL — CORRODED · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

CORROSION BEYOND LIMITS ON SILL. R & R SILL.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

RT OTBD SILL CORRODED BEYOND LIMITS. R & R SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

RT OMEGA BEAM GUSSET CORRODED BEYOND LIMITS. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

LT OMEGA BEAM CORRODED BEYOND LIMITS. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

LEFT SIDE OMEGA BEAM, FRAME 59 THRU 61 CORRODED BEYOND LIMITS AT NUT PLATES.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,459 hrs · 14,950 cycles

SILL HAS CORROSION BEYOND LIMITS AT FRAME 61 LT SILL.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 25,935 hrs · 13,957 cycles

MASTER WARMING PITCH TRIM INOP ON EICAS. REMOVED AND REPLACED HORZ STAB ACTUATOR IAW EMB 145XR AMM 27-40-02. OPS CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTION) · airframe 25,886 hrs · 13,929 cycles

IAH - FLIGHT 4183, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WENT OFF TWICE WITH NO SIGNS OF FIRE OR SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, AND LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 25,886 hrs · 13,929 cycles

IAH - FLIGHT 4183, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WENT OFF TWICE WITH NO SIGNS OF FIRE OR SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, AND LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 25,426 hrs · 13,671 cycles

TYS - A/C WAS LEAVING BNA ON CLIMBOUT, THE CREW GOT A EICAS MESSAGE OF AIR-GROUND FAIL. A/C RETURN TO BNA WHERE MAINTENANCE ADJUSTED THE PROX SWITCHES AND TARGETS AT THE LT FOWARD, RT FOWARD AND AFT PROX SWITCHES, OPS CHECK GOOD AND WAS RELEASED. NO PARTS INVOLVED, JUST ADJUSTING OF SWITCHES AND TARGETS.

Part: FADEC — INOPERATIVE (E&E BAY) · airframe 24,966 hrs · 13,379 cycles

IAH - FLIGHT 3038, THE CREW REPORTED THAT THE NUMBER TWO ENGINE FADEC WAS COMMANDING THE HIGHEST THRUST RATING AND WOULD NOT STAY SET AT A LOWER RATING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FADEC 2A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LINE — FAILED (BLEED AIR SYS) · airframe 24,889 hrs · 13,338 cycles

EWR FLT 2370 THE CREW REPORTED A BLEED 1 OVERTEMP MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED LINE TO THE LOW TEMPERATURE THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 24,776 hrs · 13,275 cycles

L/G AIR GROUND FAIL MESSAGE ON EICAS ON EXTENSION. REMOVED AND REPLACED RT MLG UPPER PROX SWITCH IAW EMB145 AMM32-63-01 OPS CHECK GOOD IAW EMB 145XR AMM 32-63-05. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: WIRE — BROKEN (FIRE DETECTION) · airframe 24,034 hrs · 12,824 cycles

TYS - ENGINE 2 FIRE DETECT FAIL MESSAGE APPEARED FOR APPROXIMATELY 10 SEC ON SHORT FINAL APPROACH. MAINTENANCE REPAIRED WIRE W407-0012-20 NEAR CONNECTER PO 915 IAW EMB 145 SWPM 2021-00. OPS CHECK GOOD AND WAS THEN RELEASED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,996 hrs · 12,802 cycles

IAH - DURING A-CHECK INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,695 hrs · 11,566 cycles

MCI - DURING MAINTENANCE INSPECTION THE LT OVERWING EXIT UPPER AFT EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FILTER — DIRTY (BLEED AIR SYS) · airframe 20,937 hrs · 11,148 cycles

IAH - FLIGHT 2037, THE CREW REPORTED A BLEED ONE AND TWO OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND TWO FAN AIR VALVE FILTERS, OPERATIONALLY, AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (TAT) · airframe 19,708 hrs · 10,488 cycles

FLIGHT 2463 - EWR - FLIGHT CREW REPORTED "TAT 2 HEAT INOP" INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED TAT CURRENT SENSOR AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: APU — LEAKING · airframe 18,125 hrs · 9,638 cycles

FLT 2602 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL ON T/O IN EWR AND XNA. RIC MX REMOVED AND REPLACED APU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LINE — CRACKED (APU FUEL SYS) · airframe 18,005 hrs · 9,577 cycles

CLE FLIGHT NR 2267 THE CREW REPORTED A FUEL ODOR FOR 2-3 MINUTES AFTER APU SHUTDOWN. MX INSPECTED AND REPLACED THE FORWARD FUEL LINE FROM THE APU FUEL FILTER TO THE FUEL CONTROL UNIT. OPS CHECKS WERE GOOD AND NO FUEL ODOR WAS PRESENT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,005 hrs · 9,577 cycles

CLE FLIGHT NR 2267 THE CREW REPORTED THE GALLEY FLOOR STRIP EMERGENCY LIGHT WAS INOPERATIVE. MX INSPECTED AND REPLACED THE LIGHT STRIP ASSEMBLY. OPS CHECKS WERE GOOD.

Part: FILTER — LOOSE (APU) · airframe 17,978 hrs · 9,560 cycles

FLIGHT 2794, THE CREW REPORTED A STRONG FUEL ODOR ON ROTATION WITH THE APU RUNNING. THE ACFT LANDED AT TUL WITHOUT INCIDENT WHERE THE APU WAS PLACED ON MEL 49-00-00 CAT C, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT RETURNED TO IAH ON FLIGHT 2031, WHERE MX INSPECTED THE APU, TIGHTENED THE APU FUEL FILTER CAP, OPS TESTED WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,945 hrs · 9,541 cycles

IAH - FLIGHT 2114, THE CREW REPORTED A STRONG FUEL SMELL DURING TAKEOFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN WITH APU BLEED ON WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — SHORTED (COCKPIT) · airframe 17,828 hrs · 9,473 cycles

AFTER PARKING, CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT ONLY. MX INSPECTED THE ACFT AND REMOVED AND REPLACED THE OBSERVERS AUDIO CONTROL PANEL, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 17,610 hrs · 9,349 cycles

IAH - FLIGHT 2608 THE CREW REPORTED A FUEL SMELL ON TAKEOFF IN THE CABIN AND COCKPIT THAT LASTED 30-60 SECONDS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BLEED SYSTEM ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,272 hrs · 9,325 cycles

LT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. LT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,572 hrs · 9,325 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 54. MAINTENANCE REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 17,572 hrs · 9,325 cycles

RT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. RT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,572 hrs · 9,325 cycles

CENTER OMEGA BEAM LOWER FLANGE HAS CORROSION AT FR 34. REPAIRED CENTER OMEGA BEAM LOWER FLANGE IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 17,572 hrs · 9,325 cycles

SHV - DURING C-CHECK RT OMEGA BEAM CORRODED AT NUT PLATE AREAS AT FR 59-61. MAINTENANCE REPAIRED RT OMEGA BEAM BETWEEN FR 59-61 IAW EC 5320-01434. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (MLG) · airframe 17,181 hrs · 9,088 cycles

IAH FLIGHT 2245. THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MSG UPON GEAR RETRACTION AFTER TAKE OFF. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MX R&R THE LANDING GEAR ELECTRONIC UNIT. OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — ERRATIC (CABIN PRESSURE) · airframe 15,659 hrs · 8,291 cycles

FLIGHT 1245 - EWR - CREW REPORTED CABIN PRESSURE WOULD NOT DESCENT UNTIL CABIN IS WITHIN 700 FEET OF AIRCRAFT ALTITUDE. CREW TRIED TO USE "MAN" MODE BUT IT DID NOT WORK, "AUTO" MODE DID NOT WORK. THE CABIN PRESSURE DID WHAT IT WANTED REGARDLESS OF CREW INPUT. WHEN CREW SWITCHED TO "MAN" CABIN ALTITUDE INITIALLY CLIMBED AT 3000 FPM. IT THEN BECAME UNRESPONSIVE AND KEPT THE CABIN ALTITUDE 700 FEET BELOW AIRCRAFT ALTITUDE. CREW LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED MANUAL PRESS CONT IAW EMB145XR AMM 21-31-02 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR SEAL — DIRTY (EMERGENCY EXIT) · airframe 14,858 hrs · 7,893 cycles

FLIGHT 2146 DAB TO EWR. CREW REPORTED,: EMERGENCY EXIT LEFT SIDE BY SEAT 12A HAD WHISTLE ON CLIMB TO ALTITUDE. REPAIR EWR MX "CLEANED AND LUBED EMERGENCY EXIT 12A DOOR SEAL IAW EMB 145 AMM 52-21-01." A/C APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 14,585 hrs · 7,757 cycles

BRO - FLIGHT 2196, THE CREW REPORTED BAGGAGE SMOKE INDICATION INTERMITTENTLY DURING FLIGHT, THE CREW DISCHARGED THE BAGGAGE FIRE BOTTLES AND LANDED IN BRO WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO EVIDENCE OF FIRE OR SMOKE FOUND. REPLACED THE FIRE BOTTLES, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,882 hrs · 6,879 cycles

IAH - FLIGHT 2682, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDOW — STUCK (COCKPIT) · airframe 11,540 hrs · 6,146 cycles

IAH FLI9GHT 2598, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE CAPTAINS DV WINDOW WOULD NOT OPEN. MAINTENANCE OPERATIONALLY CHECKED THE WINDOW WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 11,305 hrs · 6,011 cycles

IN EWR LOG SQUAWK STEP EMERGENCY EXIT LIGHT INOP. THE REPAIR WAS REMOVED AND REPLACED COCKPIT STEP EMERGENCY EXIT MARKING SIGN IAW EMB-145XR AMM 33-50-14. OPS CHECK GOOD REF EMB-145XR AMM 33-50-00.

Part: WIRE HARNESS — LOOSE (COCKPIT) · airframe 9,882 hrs · 5,252 cycles

IAH - FLIGHT 3152 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT UNDER THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT, AND RESECURED THE WIRING HARNESS, OPERATIONALLY CHECKED WITH NO DIFFICULTIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (TE FLAPS) · airframe 9,105 hrs · 4,830 cycles

CREW REPORTED, FLAPS FAILED TO OPERATE, DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED FECU IAW EMB145XR AMM 27-53-02, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,031 hrs · 4,783 cycles

DURING ROUTINE MAINTENANCE THE EXIT SIGN AT THE MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EXIT SIGN INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,975 hrs · 4,753 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EXIT ROW EMERGENCY LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,770 hrs · 4,643 cycles

SDF - LEFT FWD WING EXTERIOR EMERGENCY LIGHT INOP. A/C RELEASED IAW MEL 33-50-00 CAT C 063546. 12/22/2005 REMOVED AND REPLACED BATTERY POWER SUPPLY.

Part: VALVE — LEAKING (FUEL VENT) · airframe 8,149 hrs · 4,319 cycles

CLE FLIGHT NR 2693, THE CREW REPORTED A FLUID LEAK FROM THE NR 1 WING. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 WING FUEL VENT VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 6,395 hrs · 3,389 cycles

DURING SERVICE AND ROUTINE CHECKS ON RON MAINTENANCE FOUND THE FORWARD CABIN AISLE EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED FORWARD CABIN AISLE EMERGENCY LIGHT LAMP IAW EMB145XR AMM 33-50-08. OPS CHECKED GOOD.

Part: CONDENSER — DIRTY (NR 1 PACK) · airframe 6,027 hrs · 3,192 cycles

CLE FLIGHT 2484 THE CREW REPORTED THE NR 1 PACK EMITS STRONG ODOR WHEN BLEED OUTPUT IS LOW. MAINTENANCE INSPECTED AND RELEASED A/C IAW MEL 21-51-00/2. MAINTENANCE REPLACED THE MIXER CONDENSOR. OPERATIONAL CHECKS WERE GOOD.