N14148

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 50,183 hrs · 33,008 cycles

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

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,372 hrs · 32,205 cycles

LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: DISPLAY — FAILED (ZONE 200) · airframe 48,790 hrs · 31,660 cycles

DURING FLIGHT CAPT MFD FAILED TO BLACK SCREEN FOLLOWED BY SMOKE IN THE COCKPIT. REMOVED AND REPLACED CAPT MFD AND OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. NO MEDICAL ATTENTION OR INJURIES REPORTED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,415 hrs · 31,282 cycles

EMERGENCY LIGHTS ON CEILING PANELS AT SEATS 3, 18, AND 23 INOPERATIVE. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMPS. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 100) · airframe 48,392 hrs · 31,254 cycles

LH FWD LOWER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH FWD LOWER FAIRING EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 47,935 hrs · 30,820 cycles

OVERWING EMERGENCY LIGHT LAMP INOPERATIVE AT BOTH SEATS. REMOVED AND REPLACED BOTH EMERGENCY LIGHT LAMPS. OPS CHECK SAT

Part: WIRE HARNESS — INOPERATIVE (NR 2 ENGINE) · airframe 47,761 hrs · 30,663 cycles

#2 ENG OIL TEMP REACHED 132 DEGREES DURING CLIMB. OIL TEMP STABILIZED AT 122 DEGREES. REMOVED AND REPLACED RH ENG OIL TEMP/PRESS SENSOR. DID NOT FIX. REMOVED AND REPLACED ENGINE EXTERNAL INDICATING HARNESS. OPS CHECK SAT.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 47,617 hrs · 30,516 cycles

RT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH EXT EMERGENCY LIGHT LAMP AND ASSY. NO FIX. VERIFIED CONTINUITY FROM P0782 PIN 7 TO GROUND GS8524, NO DEFECTS NOTED, EWIS GOOD ON EXTERNAL FUSELAGE. NO VOLTAGE AT J0782 PIN 7 TO GROUND. SWAPPED BATTERY CHARGER ASSEMBLY, INVERT ASSEMBLY AND EMERGENCY BATT 2 FOR TROUBLESHOOTING. NO FIXES. FOUND BROKEN WIRE BETWEEN SPLICES SP9032 AND SP8924 - REPAIRED WIRE. OPS CHECK SAT AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 47,522 hrs · 30,433 cycles

RH FWD WING EMERGENCY LIGHT OUT. FOUND RH FWD WING, SERVICE DOOR EXIT SIGN, AND FWD LWR RH EMERGENCY EXIT SIGN DIMMING UNTIL OFF. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,259 hrs · 30,171 cycles

EMERGENCY LIGHT ON MCD INOPERATIVE. REMOVED AND REPLACED MCD LAMP. OPS CHECK FAIL REMOVED MCD LINER. FOUND GROUNDING WIRE NOT ATTACHED TO EMERGENCY LIGHT HOUSING. REMOVED HOUSING SCREW. INSTALLED GROUNDING WIRE ONTO HOUSING SCREW. INSTALLED SCREW. INSTALLED MCD LINER. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 47,145 hrs · 30,056 cycles

FOUND FWD CABIN EMERGENCY LIGHT TOP AND BOTTOM ENTRY WAY AND ABOVE FLIGHT ATT SEAT OUT. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT. NO DEFECTS NOTED AT THIS TIME

Part: LAMP — INOPERATIVE · airframe 46,253 hrs · 29,240 cycles

AISLE EMERGENCY LIGHTS 3, 4 AND 18CD INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS. OPS CHECK SAT

Part: UNKNOWN — ODOR (CABIN) · airframe 46,048 hrs · 29,066 cycles

SMELL IN CABIN POSSIBLY PAC. PERFORMED CABIN VISUAL INSPECTION, RE-RUN PACK AND NO SMELL DETECTED. OPS CHECK SAT

Part: LIGHT — INTERMITTENT (CABIN) · airframe 13,034 hrs · 29,052 cycles

EMERGENCY LIGHTS NOT ARMED EICAS INTERMITTENTLY DISPLAYED. PERFORMED ELECTRICAL RESET AND OPS TEST FOR EMERGENCY LIGHTING. OPS CHECKED GOOD.

Part: ACM — LOCKED · airframe 45,956 hrs · 28,980 cycles

FOUL ODOR ON CLIMB/DESCENT BETWEEN 5000` AND 14000` PERFORMED ROLLS ROYCE FIM. COMPLIED WITH #1 ENGINE  BORESCOPE INSPECTION ENGINE FLOWPATH AREA, NO OIL POOLING, NO WET OIL FOUND ON OR NEAR THE BOLT HEADS,  JUST SOME DUST OR DAMP GRIME. #1 PACK ACM LOCKED UP DURING RUNS. R & R #1 PACK ACM. OPS CHECK SAT . NO FOUL ODOR NOTED.

Part: NONE — INOPERATIVE · airframe 45,073 hrs · 28,211 cycles

ALL BATTERY 1 EMERGENCY LIGHTS ARE INOPERATIVE. TESTED BATTERY 1. BATTERY VOLTAGE WITHIN LIMITS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER #1. OPS CHECK SAT

Part: NONE — UNKNOWN · airframe 44,977 hrs · 28,124 cycles

BRAKE DEGRADE MESSAGE ON EICAS. REMOVED AND REPLACED INBD RH BRAKE CONTROL VALVE. OPS AND LEAK CHECK SAT. PERFORMED TAXI CHECK OF AIRCRAFT. NO DEFECTS NOTED DURING TAXI

Part: LAMP — INOPERATIVE · airframe 44,909 hrs · 28,062 cycles

OVERWING EMERGENCY LIGHT AT SEAT 18CD INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT AT SEAT 18CD. OPS CHECK SAT

Part: NOT REPORTED — NOT REPORTED · airframe 44,768 hrs · 27,943 cycles

SCRATCH ON RH WING L/E #2 SKIN AT 56" FROM INBD EDGE & 12.5" FROM LOWER EDGE. SCRATCH ON RH WING LE #2 AT 56" FROM INBD EDGE & 12.5" FROM LOWER EDGE FOUND OUT OF LIMITS. RH WING LEADING EDGE #2 REPAIRED WITH A FLUSH PATCH

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 44,768 hrs · 27,943 cycles

AT CF 4 AREA, CORROSION FOUND ON CENTER OMEGA BEAM FLOOR STRUCTURE BTW FR 59 TO FR 60. CORROSION ON CENTER OMEGA BEAM BTW FR 59 TO 60 FOUND OUT OF LIMITS. CUT-OUT ON OMEGA BEAM PERFORMED. CENTER OMEGA BEAM BTW FR 59-60 REPAIRED WITH DOUBLER

Part: ARMREST — CRACKED (SEAT 4A) · airframe 43,628 hrs · 26,923 cycles

SEAT 23A, 5A, 4A, 3A, 2A ARMREST STRUCTURE IS CRACKED. REMOVED AND REPLACED SEAT ASSEMBLY 23A, 5A, 4A, 3A, 2A

Part: SENSOR — MALFUNCTIONED (NR 2 ENGINE OIL) · airframe 42,866 hrs · 26,221 cycles

NR 2 HIGH OIL TEMP INDICATION MAX TEMP NOTED 171 / PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. NO ABNORMAL OIL QUANTITY, PRESSURE, OR ITT. NO EMERGENCY DECLARED, NO INDICATION OF FIRE @ APPROX 16000 FT, THROTTLE AT THE ECLIMB AFTER ENGINE SHUT DOWN TEMP RETURNED TO NORMAL. OIL QUANTITY E1 10 QT E2 11 QT. PERFORMED CMC DOWNLOAD. EXAM 4 FUEL FLOW CHIP DETECTORS. R&R OIL TEMP PRESSURE NR 2 SENSOR. OPS CHECK SAT. LEAK CHECK SAT. NO DEFECTS NOTED. PERFORMED E2 HIGH POWER RUN. OPS CHECK, LEAK CHECK SAT. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LEVER — BENT (SERVICE DOOR) · airframe 42,710 hrs · 26,060 cycles

SERVICE DOOR OPEN RED EICAS INDICATION. FOUND TOP RIGHT MICRO SWITCH LEVER TO BE BENT AND LOOSE. R&R MICRO SWITCH LEVER. OPS CHECK SAT. NO DEFECTS AT THIS TIME. PERFORMED PRESSURIZATION CHECK OF SERVICE DOOR. OPS/LEAK CHECK SAT. NO DEFECTS NOTED AT THIS TIME.

Part: CONTROL VALVE — FAULTY (BRAKE SYSTEM) · airframe 40,887 hrs · 24,534 cycles

PILOT REPORTED BRAKE DEGRADED AFTER TAXING INTO POSITION ON RUNWAY. A/C RETURN TO GATE. MX REMOVED AND REPLACED THE INBOARD BRAKE CONTROL VALVE WITH OPERATIONAL AND LEAK CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 40,437 hrs · 24,198 cycles

DURING C CHECK INSPECTION FOUND REAR FUSELAGE I SKIN CRACKED AT FRAME 75 BETWEEN STR 2R AND 3R. MAINTENANCE REPAIRED I/A/W SRM 53-31-01.

Part: CHANNEL — CRACKED (FRAME 10) · airframe 40,437 hrs · 24,198 cycles

DURING C CHECK INSPECTION FOUND FRAME 10 CHANNEL BRACKET LHS CRACKED BELOW CAPTAINS DV WINDOW. MAINTENANCE REPLACED FRAME 10 CHANNEL BRACKET ON LEFT SIDE.

Part: BRACKET — CRACKED (AILERON DAMPER) · airframe 40,437 hrs · 24,198 cycles

DURING C CHECK INSPECTION FOUND LEFT AILERON DAMPER BRACKET CRACKED. MAINTENANCE REPLACED THE AILERON DAMPER BRACKET.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 40,437 hrs · 36,517 cycles

LAV CENTER FLOOR BEAM BETWEEN FRAMES 59 AND 61 CORRODED AROUND SCREW HOLES. MAINTENANCE REPLACED LAV FLOOR BEAM BETWEEN FRAME 59 AND 61.

Part: SKIN — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 40,437 hrs · 36,517 cycles

DURING HEAVY CHECK INSPECTION CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT THE RADIO ALTIMETER II LOCATION. FRAME 65 TO FRAME 66.MAINTENANCE REPAIRED I/A/W EMBRAER ETD2018-145-124281 AND SRM 53-00-23

Part: BRACKET — CRACKED (COCKPIT WINDOW) · airframe 40,437 hrs · 24,198 cycles

DURING C CHECK INSPECTION THE FLIGHT COMPARTMENT WINDOW STRUCTURE SUPPORTING THE FORWARD FUSELAGE II DOME SKIN WAS FOUND CRACKED. MAINTENANCE PERFORMED SPLICE REPAIR I/A/W ETD2018-145-122287 AND EXPRESSJET EC/TC.

Part: SKIN — CRACKED (RIGHT WING) · airframe 40,437 hrs · 36,517 cycles

DURING C CHECK INSPECTION FOUND CRACK ON RIGHT WING LOWER SKIN SURFACE ADACENT TO RIB 9. MAINTENANCE REPAIRED I/A/W ETD2018-145-131015.

Part: RIB — CRACKED (RT WING) · airframe 40,437 hrs · 36,517 cycles

DURING C CHECK INSPECTION FOUND CRACK ON RIGHT WING RIB 21. REPAIRED RIB 21 ON RIGHT WING I/A/W SRM 57-20-07 AND ETD 2018-145-131536

Part: ACTUATOR — FAILED (HORIZONTAL STAB) · airframe 40,365 hrs · 36,418 cycles

THE CREW REPORTED A MAIN PITCH TRIM FAILURE IN CRUISE FLIGHT. MAINTENANCE REPLACED THE HORIZONTAL STABILIZER ACTUATOR. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,298 hrs · 19,886 cycles

OVERHEAD EXIT LOCATOR SIGN INOPERATIVE. R & R THE OVERWING EMERGENCY EXIT LOCATOR SIGN AND THE EMERGENCY LIGHT AC/DC INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED FOR SERVICE.

Part: FIRE DETECTOR — FALSE INDICATION (APU BAY) · airframe 32,884 hrs · 18,904 cycles

THE CREW REPORTED AN APU FIRE INDICATION IN FLIGHT, TRANSIENT MESSAGE. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT, FOUND NO INDICATION OF APU FIRE, OPERATIOPNALLY TESTED THE FIRE DETECTION SYSTEM WITH NO DEFECTS NOTED, OPERATIONALLY TESTED THE APU WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 32,279 hrs · 18,465 cycles

THE CREW REPORTED RECEIVING A LAVATORY SMOKE WARNING DURING CLIMB. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, PERFORMED ENGINE RUNS AND VERIFIED NORMAL OPERATION OF LAVATORY SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — WORN (ZONE 500) · airframe 29,386 hrs · 16,625 cycles

AFTER TAKEOFF FLUID WAS WITNESSED TREAMING FROM THE LT WING. THE CREW ELECTED TO RETURN TO THE AIRPORT WHERE THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE FOUND THE LT WING RIB 19 FLAPPER VALVE TO BE THE CAUSE OF THE LEAK. THE VALVE WAS REPLACED AND THE DISCREPANCY CLEARED.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,371 hrs · 15,971 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE FROM THE F/A PANEL. MX R & R THE AFFECTED PANEL, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,546 hrs · 14,783 cycles

DURING MX INSPECTION THE COCKPIT OVERHEAD AND FRONT AISLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX R & R NR 1 EMERGENCY LIGHT BATERY CHARGER ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — FALSE ACTIVATION (APU BAY) · airframe 24,306 hrs · 13,326 cycles

THE CREW REPORTED AN APU FIRE IN FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MX INSPECTED THE ACFT WITH NO EVIDENCE OF, OR INDICATION OF FIRE. REMOVED AND REPLACED THE APU FIRE LOOP, OPERATIONALLY TESTED WIH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 24,303 hrs · 13,322 cycles

THE CREW REPORTED A LAVATORY SMOKE MESSAGE ON EICAS. MX R & R THE LAVATORY SMOKE DETECTOR, OPERATIONALLY TESTED WIH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 23,391 hrs · 12,756 cycles

FLT 4614 STL-EWR. CREW REPORTED LAV SMOKE WARNING DURING FLIGHT WITH NO SMELL OR SIGN OF FIRE OR SMOKE. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB145XR AMM 26-14-01 AND RAN ENGINES WITH OPERATIONAL CHECKS SUCCESSFUL AND NO SMOKE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 21,643 hrs · 11,607 cycles

MCI - FLIGHT 6208, THE CREW REPORTED THE F/O'S PITCH TRIM SWITCH WAS INOPERATIVE. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S PITCH TRIM SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LINE — DAMAGED (BLEED AIR SYS) · airframe 21,639 hrs · 11,604 cycles

SHV - BLEED 1 OVERTEMP MESSAGE ON EICAS. REMOVED AND REPLACED FLEXIBLE REFERNCE LINE ON AFT BLEED 1 THERMOSTAT IAW EMB 145 AMM 20-10-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 20,359 hrs · 10,859 cycles

THE CREW REPORTED A "PITCH TRIM BACKUP" INOP MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 20,330 hrs · 10,841 cycles

FLIGHT 2968 - BOS - FLIGHT CREW REPORTED MAIN AND BACK UP TRIM INOPERATIVE AT FL350, AND NOSE PITCHED UP 3 DEG. EWR MX REMOVED AND REPLACED PITCH TRIM ACTUATOR AND HORIZONTAL STABILIZER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. PITCH TRIM ACTUATOR INFO REPORTED ON SDR C2XA10RI113, AND CONTROL UNIT INFO REPORTED ON SDR C2XA10RI114.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 20,332 hrs · 10,843 cycles

FLIGHT 2968 - BOS - FLIGHT CREW REPORTED MAIN AND BACK UP TRIM INOPERATIVE AT FL350, AND NOSE PITCHED UP 3 DEG. EWR MX REMOVED AND REPLACED PITCH TRIM ACTUATOR AND HORIZONTAL STABILIZER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. PITCH TRIM ACTUATOR INFO REPORTED ON SDR C2XA10RI113, AND CONTROL UNIT INFO REPORTED ON SDR C2XA10RI114.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 19,685 hrs · 10,474 cycles

FLIGHT 2753 - EWR - FLIGHT CREW REPORTED BLEED 1 & 2 OVERTEMP IN ICING CONDITION ON EICAS. CREW PERFORMED AIR RETURN SUCCESSFULLY. EWR MX REMOVED AND REPLACED NR 1 FAN AIR VALVE AND SENSING LINE LEADING TO NR 2 FAN AIR VALVE. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. FAN AIR VALVE INFO REPORTED IN SDR C2XA10RI088. SENSING LINE INFO REPORTED IN SDR C2XA10RI089.

Part: SENSE LINE — LEAKING (BLEED AIR SYS) · airframe 19,685 hrs · 10,474 cycles

FLIGHT 2753 - EWR - FLIGHT CREW REPORTED BLEED 1 & 2 OVERTEMP IN ICING CONDITION ON EICAS. CREW PERFORMED AIR RETURN SUCCESSFULLY. EWR MX REMOVED AND REPLACED NR 1 FAN AIR VALVE AND SENSING LINE LEADING TO NR 2 FAN AIR VALVE. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. FAN AIR VALVE INFO REPORTED IN SDR C2XA10RI088. SENSING LINE INFO REPORTED IN SDR C2XA10RI089.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 19,112 hrs · 10,162 cycles

SHV - DURING FLIGHT BAGGAGE DOOR OPEN INDICATION IN FLIGHT. PERFORMED OPS CHECK OF BAGGAGE DOOR IAW EMB 145 XR AMM 52-70-00. NO FAULTS PRESENT AT THIS TIME. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 19,121 hrs · 10,169 cycles

IAH - FLIGHT 2962, THE CREW REPORTED, RECEIVED A BAGGAGE DOOR INDICATION WITH AN OPEN INDICATOR AND CABIN PRESSURE AT 18000 FT SHOULD HAVE BEEN 1900 FT AND WAS READING 5900 FT AND WAS RISING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,112 hrs · 10,162 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS CORROSION BETWEEN FR 59. REPAIRED OMEGA BEAM IAW EC5310-01473. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,112 hrs · 10,162 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 17,976 hrs · 9,561 cycles

FLIGHT 2370 - EWR - LIGHT CREW PERFORMED AIR RETURN DUE TO LANDING GEAR NOT RETRACTING. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 17,976 hrs · 9,561 cycles

FLIGHT 2370 - EWR - LIGHT CREW PERFORMED AIR RETURN DUE TO LANDING GEAR NOT RETRACTING. CREW LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 17,741 hrs · 9,423 cycles

PBI - FLIGHT 3150, THE CREW REPORTED HAZE AND ODOR IN THE CABIN. THE AIRCRAFT RETURNED TO PBI, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS APPROVED FOR A FERRY FLIGHT TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — MALFUNCTIONED (NR 1 ENGINE) · airframe 17,738 hrs · 9,420 cycles

EWR FLT 2994 - THE CREW REPORTED A LAV SMOKE EICAS MESSAGE DURING CLIMB. LIGHT SMOKE IN THE CABIN AND COCKPIT WAS REPORTED. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 16,853 hrs · 8,943 cycles

TYS FOR IAH - THE MAIN CABIN DOOR WOULD NOT SECURE. MAINTENANCE LUBED THE DOOR AND OPS CHECKED GOOD, REL BY C3052.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 15,286 hrs · 8,091 cycles

IAH - FLIGHT 2574, THE CREW REPORTED A LAV SMOKE DETECTOR WARNING DURING CLIMB. THE AIRCRAFT RETURNED TO IAH 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: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,285 hrs · 6,536 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT SWITCH AT THE FORWARD FLIGHT ATTENDANT STATION WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE ATTENDANT CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: LEG ASSY — UNDERSERVICED (NLG) · airframe 11,448 hrs · 6,089 cycles

IAH - FLIGHT 3095, THE CREW REPORTED AN AIR/GROUND FAILURE DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NLG STRUT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 9,073 hrs · 4,798 cycles

TYS - DURING A 2C INSPECTION DAMAGE WAS FOUND AT FR 60 AT STRINGER 5L. MAINTENANCE CUT OUT THE DAMAGE AREA, FABRICATED A L-SHAPED SPLICE AND INSTALL L-SHAPE SPLICE AND SEALED IAW EMB 145XR SRM 53-00-04 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 2C INSPECTION.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 4,084 hrs · 2,156 cycles

CLE - FLIGHT 3238, THE CREW REPORTED THAT THE GASPER VENTS WERE NOT WORKING, AND AFTER RESETTING THE GASPER FAN CIRCUIT BREAKER A STRONG BURNING ODOR WAS PRESENT. MAINTENANCE MEL'D THE GASPER FAN UNDER MEL 21-23-03 CONTROL NUMBER 053036, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT RON'D AT MCI OFF OF FLIGHT 2608, WHERE MAINTENANCE REMOVED AND REPLACED THE GASPER RECIRCULATING FAN, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 2,385 hrs · 1,247 cycles

SDF - DURING 1A CHECK FOUND GALLEY PHOTOLUMINESCENT LIGHT STRIP COVER CRACKED. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP COVER. AIRCRAFT WAS APPROVED AND RETURNED TO SERVICE.