N23139

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 48,721 hrs · 31,429 cycles

RH LATERAL WING-TO-FUSELAGE FAIRING EMERGENCY LIGHT INOPERATIVE. RH SIDE CENTER FAIRING EXTERNAL EMERGENCY LIGHT ACCESS PANEL HAS 4 STRIPPED SCREWS. REMOVED AND REPLACED RH LATERAL WTF FAIRING EMERGENCY LIGHT LAMP. OPS CHECK FAIL. FOUND A PIN MISSING ON ELECTRICAL CONNECTOR OF EMERGENCY LIGHT ASSEMBLY. VERIFIED THAT TWO PINS ARE INSTALLED IN CONNECTOR AND IS NOT MISSING A PIN. SWAPPED BATTERY POWER SUPPLY. OPS CHECK FAILED. REINSTALLED ORIGINAL COMPONENT. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT AND REINSTALLED FAIRING LIGHT ASSEMBLY.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 48,592 hrs · 31,313 cycles

OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BPS #4. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 48,592 hrs · 31,313 cycles

SEVERAL GALLEY AREA EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BPS #2. OPS CHECK GOOD.

Part: LIGHT — MISINSTALLED (ZONE 200) · airframe 47,717 hrs · 30,462 cycles

RH OVERWING EMERGENCY EXIT LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT LIGHT HOUSING.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 47,664 hrs · 30,413 cycles

EMERGENCY EXIT LIGHTS AT ROW 18 INOPERATIVE AND EMERGENCY CEILING LIGHTS AT 18. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FOR ROW 18. OPS CHECK GOOD.

Part: CONTROL UNIT — INOPERATIVE (UNKNOWN) · airframe 47,505 hrs · 30,260 cycles

NO BRAKES ON LANDING BRAKE INB INOPERATIVE MESSAGE FLASHED ON EICAS. REMOVED AND REPLACED #2 & 3 BRAKES. REMOVED AND REPLACED BCU. OPS CHECK SAT. BOTH LEFT AND RIGHT INB TIRES BLOWN. REMOVED AND REPLACED #1, 2, 3, AND 4 MLG TIRES. TAXI CHECK SAT.

Part: BATTERY PACK — INOPERATIVE · airframe 46,103 hrs · 28,958 cycles

EMERGENCY LIGHTS AT EMERGENCY EXIT DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES #3 AND #4. OPS CHECK SAT #3 - ABS-2013-1A SN 53157 TSN 31901.12 - CSN 23546 - TIME SINCE INSPECTION 30302.01

Part: NONE — NONE · corrosion level 2 · airframe 45,409 hrs · 28,334 cycles

CORROSION FOUND ON LOWER SKIN UNDER RAD ALT ANTENNA #2 AFT SUPPORT BTW FR 68-69 IN REAR FUSE I AREA. RAD ALT #2 ANTENNA, SUPPORT, SUPPORT ASSEMBLY AND FAIRING REMOVED FOR ACCESS. ANTENNA SUPPORT AND SUPPORT ASSY BLENDED OUT OF LIMITS. AFTER INVESTIGATION SKIN UNDER RAD ALT FOUND CRACKED. PERFORMED CUT-OUT ON LOWER SKIN UNDER RAD ALT ANTENNA. REPAIRED LOWER SKIN UNDER RAD ALT ANTENNA. REPALCED WITH NEW PART ANTENNA SUPPORT AND BASE SUPPORT. REPROTECTION APPLIED. CORROSION LEVEL II

Part: NONE — NONE · airframe 45,409 hrs · 28,334 cycles

DENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CF II AREA. DENT FOUND ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R IN CFII AREA. CUT-OUT PERFORMED ON RH SKIN BTW FR 25-26 AND BTW STR 13R-12R SKIN REPAIRED. REPROTECTION COVERED.

Part: NONE — NONE · airframe 45,409 hrs · 28,334 cycles

DENTS FOUND ON LH SKIN BTW FR 19-21 AND BTW STR 11L-12L IN CF I AREA. LH SKIN BTW FR19-21 AND BTW STR 11L-12L IN CF! AREA, PATCH REMOVED FOR INVESTIGATION. 3 DENTS CUT OUT. LH SKIN BTW FR 19-21 AND BTW STR 11L-12L SKIN REPAIRED

Part: NONE — NONE · airframe 45,409 hrs · 28,334 cycles

VENTRAL TANK FRONTAL FACE LIP TO ATTACH THE PANELS IS BARE METAL. CUTOUT DONE ON VENTRAL TANK FWD FACE LIP AND PART FABRICATED. VENTRAL TANK FRONTAL FACE LIP REPAIRED

Part: NONE — NONE · airframe 45,409 hrs · 28,334 cycles

DAMAGE FOUND ON RH OUTBD OMEGA BEAM AT FR 48 IN FLOOR STRUCTURE CF III AREA. ON RH OUTBD OMEGA BEAM AT FR48 IN FLOOR STRUCTURE CF3 AREA, DAMAGE CUTOUT ON RH OMEGA BEAM AT FR 48 IN FLOOR STRUCTURE REPAIR PERFORMED

Part: NONE — NONE · corrosion level 2 · airframe 45,409 hrs · 28,334 cycles

CORROSION FOUND ON LOWER SKIN BTW FR 20-21 AND BTW STR 21L-21R IN CF1 DOOR STRUCTURE AREA. SKIN AT FR20-21 BTW 21L-21R CORROSION BLENDED FOR ENGINEERING REVIEW. IN CF1 FLOOR STRUCTURE AREA. BTW FR20-21 AND BTW STR 21L-21R, LOWER SKIN REPAIRED WITH DOUBLER AND FILLER. INSTALLED WITH SOLID RIVETS. CORROSION LEVEL II

Part: NONE — NONE · airframe 45,409 hrs · 28,334 cycles

LH OMEGA BEAM FOUND CRACKED AT FR 24, AND FR 25 AND BOTTOM FLANG FOUND CORRODED. REPLACED WITH NEW PART LH OMEGA BEAM BTW FR 23-29

Part: LIGHT — MISSING (CABIN) · airframe 45,069 hrs · 28,030 cycles

EMERGENCY FLOOR STRIP AT 1A MISSING. INSTALLED EMERGENCY FLOOR STRIP.

Part: CONNECTOR — BURNED (EMERGENCY LIGHT) · airframe 44,741 hrs · 27,727 cycles

ON DEPARTURE, SMOKE WAS COMING FROM FWD ENTRANCE COMPARTMENT AND THE LIGHT ABOVE THE FWD ENTRANCE COMPARTMENT. FOUND LH FWD PAX CABIN CEILING LIGHT BULB CONNECTION BURNED/MELTED/ R&R CEILING LIGHT ASSEMBLY AT 1A.

Part: BATTERY PACK — INOPERATIVE · airframe 45,594 hrs · 28,490 cycles

FWD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT

Part: LIGHT — INOPERATIVE · airframe 44,443 hrs · 27,454 cycles

BOTH LH SIDE EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R LH SIDE EXTERNAL EMERGENCY LIGHTS. OPS CHECK SAT.

Part: SEAT FRAME — CRACKED (SEAT 22A) · airframe 44,443 hrs · 27,454 cycles

SEATS 22A, 10A & 9A AISLE SIDE FRAME CRACKED. REMOVED AND REPLACED SEATS 10A, 9A & 22A.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 44,206 hrs · 27,240 cycles

NR 1 HYD PUMP FAIL ADVISORY AFTER GEAR EXTENSION. INVESTIGATION FOUND HYD LEAK ON RT GEAR ACTUATOR LINES. R & R ACTUATOR LINE. RII ON GEAR SWINGS, INSTALL PER GMM. LEAK CHECK OPERATIONS CHECK SAT. FOUND HYD LINE ENGINE PUMP LEAKING. R & R HP HYD LINE. LEAK CHECK SAT. R & R NR 1 ENGINE HYD PUMP AND FILTER. LEAK AND OPERATIONS CHECK SAT.

Part: SKIN — CRACKED (RT WING LE) · airframe 43,808 hrs · 26,875 cycles

SUSPECTED CRACKS ON RH L/E III COMING FROM OUTBOARD TWO VORTILONS AND EXTENDING UPWARD. R&R #3 RH WING LEADING EDGE. OPS CHECK LEAK CHECK SAT AT THIS TIME

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,671 hrs · 26,726 cycles

BOTH OVER WING EMERGENCY LIGHTS ARE INOPERATIVE. R&R EMERGENCY LIGHT BATTERY #4. OPS CHECK SAT.

Part: LIGHT — MISINSTALLED (EXTERIROR) · airframe 42,327 hrs · 25,525 cycles

RH OVER WING EXTERNAL EMERGENCY LIGHT UPSIDE DOWN. RE POSITIONED RH OVER WING EXTERNAL EMERGENCY LIGHT.

Part: GROUND WIRE — FAILED (EMERGENCY LIGHTS) · airframe 42,017 hrs · 25,228 cycles

MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. DISASSEMBLE AND TESTING REVEALS BAD GROUND. CORRECT CIRCUIT WIRES. OPS CHECK SAT.

Part: RIB — CRACKED (FUSELAGE) · airframe 42,014 hrs · 25,227 cycles

IAH - DURING MAINTENANCE INSPECTION CRACKS WERE DETECTED AROUND THE NUT PLATE HOLES FOR THE GRAB HANDLE IN THE COCKPIT ON OVERHEAD RIB. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH SRM 53-12-16 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — CRACKED (COCKPIT) · airframe 42,014 hrs · 25,227 cycles

IAH - DURING MAINTENANCE INSPECTION THE RT OVERHEAD PANEL IN THE COCKPIT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH TECHNICAL DISPOSITION ETD 2019-145-067895 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (NOTE: THERE IS NO FRAME OR STRINGER LOCATION FOR THIS PART REF SRM 53-12-16 FIG 1)

Part: STRAKE — DENTED (FUSELAGE) · airframe 42,013 hrs · 25,226 cycles

HOB- DURING PREFLIGHT INSPECTION THE CREW REPORTED A DENT IN THE LEFT HAND REAR STRAKE BETWEEN FRAMES 9 & 10. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA AND THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · corrosion level 2 · airframe 40,806 hrs · 24,338 cycles

DURING A C CHECK INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT AT FRAME 61. MAINTENANCE REPLACED THE LEFT FLOOR SUPPORT IAW SRM 51-40-02.

Part: SKIN SPLICE — CORRODED (FRAMES 23-24) · corrosion level 2 · airframe 40,806 hrs · 24,338 cycles

DURING A C CHECK INSPECTION, THE SKIN SPLICE BETWEEN FRAMES 23 - 24, STRINGERS 18R AND 19R WAS CORRODED. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-02.

Part: DOUBLER — CORRODED (FRAME 61) · corrosion level 2 · airframe 40,806 hrs · 24,338 cycles

DURING A C CHECK INSPECTION, FOUND CORROSION AT FRAME 61, STRINGER 16L. MAINTENANCE REPLACED CARBON CROSSBEAM PARTITION SUPPORT DOUBLER IAW SRM 51-40-02

Part: SKIN — CRACKED (FRAME 75) · airframe 40,806 hrs · 24,338 cycles

DURING A C CHECK INSPECTION, FOUND THE FUSEALGE SKIN CRACKED AT FRAME 75, STRINGER 2L. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-31-01, ITEM 5.

Part: RIB — CRACKED (LEFT WING) · airframe 40,806 hrs · 24,338 cycles

DURING A C CHECK INSPECTION, FOUND CRACK ON LEFT WING RIB 21 AROUND RIVET HOLE .250 LENGTH. MAINTENANCE PERFORMED REPAIR IA/W SRM 1142 57-20-07 AND ETD 2018-145-080654.

Part: LIGHT — BURNED (ROW 7A) · airframe 38,124 hrs · 22,435 cycles

BURNING ELECTRICAL ODOR FORWARD FRONT OF CABIN. FOUND ROW 7A SIDE WALL LIGHT RETAINER TO BE BURNING. REMOVED THE LIGHT IAW AMM 33-21-06.

Part: LIGHT — DISCHARGED (CABIN) · airframe 37,530 hrs · 22,034 cycles

THE FLIGHT CREW REPORTED THAT THE EMERGENCY LIGHT STRIPS AT SEATS 18 A & D WERE NOT ILLUMINATING. MAINTENANCE CHARGED THE EMERGENCY LIGHT STRIOS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 36,051 hrs · 20,962 cycles

DURING MAINTENANCE INSPECTION THE LT AND RT AFT OVER THE WINGS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (EMERGENCY LIGHTS) · airframe 31,419 hrs · 17,843 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR AT 11A. MAINTENANCE INSPECTED THE ACFT AND R & R THE LIGHT HARNESS FOR SEAT 11A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 31,373 hrs · 17,814 cycles

DURING MX INSPECTION THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01505. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK, CRACKS WERE FOUND AROUND FASTENERS ON THE LT AFT SKIN FROM FRAMES 77-79 AND STRINGERS 5-7L. MX REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02830. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK, THE SHEAR TIE AT FRAME 68 BETWEEN STRINGERS 15-16L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01494, REVA. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 800) · corrosion level 2 · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK. THE MAIN DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5210-01154. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 5-7R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02830. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 29,945 hrs · 16,902 cycles

DURING C-CHECK THE FRAME 10 SEGMENT BETWEEN STRINGERS 9-10L WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FRAME SEGMENT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 2 ENGINE) · airframe 29,886 hrs · 16,866 cycles

NR 2 ENGINE MOUNT YOKE LOWER, FWD EAR AFT FITTING IS CRACKED. R & R NR 2 ENGINE MOUNT YOKE. ACFT RELEASED AND RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (CABIN LIGHTS) · airframe 28,205 hrs · 15,813 cycles

THE CREW REPORTED A BURN LIKE ODOR IN THE CABIN - COCKPIT. THE ACFT WAS INSPECTED AND THE FORWARD LIGHT BALLAST WAS DEACTIVATED. MX R & R THE FIRST CEILING LIGHT HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,904 hrs · 14,951 cycles

DURING MX INSPECTION, EMERGENCY LIGHT ABOVE SEAT 12A WAS FOUND INOPERATIVE. MX R & R 12A EMERGENCY LIGHT LAMP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 26,143 hrs · 14,444 cycles

ON CLIMBOUT, ODOR OF BURNED OIL IN COCKPIT, ACFT RETURNED TO DEPARTURE. LT SIDE ENGINE R & R. WORK WAS DONE IAW RR 72-00-00 . ACFT RELEASED TO SERVICE AFTER LEAK AND OPS CHECKED.

Part: RELAY — FAULTY (LANDING GEAR)

MCI- IAH CREW REPORTED ON DESCENT INTO IAH LANDING GEAR AIR/GROUND FAIL MESSAGE INFLIGHT - INTERMITTENT ACCOMPANIED BY "TAKEOFF TRIM" AND "TAKEOFF FLAPS" CONFIGURATION WARNING INDICATIONS. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE IDENTIFIED FAULTY RELAY "K0024" REFERENCE EMB145 AMM 20-13-02. JACKED AIRCRAFT AND REIDENTIFIED AND REPRODUCED FAULT REFERENCE EMB145 AMM 32-32-00. REMOVED AND REPLACED RELAY IAW EMB 145 AMM 20-13-02. AIRCRAFT OPS CHECKED GOOD AND RETURNED TO SERVICE.

Part: SKIN — DENTED (CARGO DOOR) · airframe 23,157 hrs · 12,501 cycles

TYS - A/C CAME IN ON A DMI FOR A BAGGAGE DOOR DENT. MAINTENANCE CUTOUT DAMAGE, RECONTOURED DENT, PERFORMED A NDT, NO CRACKS FOUND IAW ETD 2011-145/05532 AND NDT ET-01. INSTALLED A REPAIR PATCH AND A FILLER IAW EMB 145XR SRM 51-40-02. PRIMED PAINTED IAW 135/145 CPM 51-21-03. PRESSURIZATION PERFORMED AND NO LEAKS NOTED IAW 145 AMM21-31-00. A/C RELEASED TO SERVICE.

Part: GCU — INOPERATIVE (APU) · airframe 23,072 hrs · 12,456 cycles

FLIGHT 2808 - EWR - FLIGHT CREW REPORTED THAT ON APU START RECEIVED APU FIRE INDICATION THAT CLEARED ITSELF UPON RE-START - APU RE-STARTED BUT ZERO AMPS. EWR MX PERFORMED FIRE DETECTION ON APU - NO FAULTS FOUND. MX REMOVED AND REPLACED APU GCU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 22,895 hrs · 12,353 cycles

ALB FLT 6021 THE CREW REPORTED PRESSURIZATION ERRATIC IN FLIGHT. COULD NOT CORRECT IN MANUAL MODE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE MANUAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,200 hrs · 11,771 cycles

ORD FLT 5926 THE CREW REPORTED THE AIRCRAFT STOPPED DEPRESSURIZING AT ABOUT 4000 FT ON DESCENT. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL PROCEDURES. MAINTENANCE REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: INDICATOR — ERRATIC (FUEL QTY) · airframe 19,922 hrs · 10,479 cycles

FLIGHT 2140, THE CREW REPORTED THAT THE NR 2 AND TOTAL FUEL QUANTITY INDICATIONS WERE ERRATIC. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE FUEL QUANTITY ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/17/10, IAH MAINTENANCE REVERSED THE DDP PROCEDURES, AND OPERATIONALLY TESTED THE FUEL QUANTITY INDICATING SYSTEM WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,228 hrs · 10,095 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AFT OF FRAME 59. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 59 IAW EMB-145 EC5310-01473 AND EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,228 hrs · 10,095 cycles

SHV - DURING C-CHECK CORRODED (LEVEL 3 LOCAL) ANGLE BRACKET FOR FRAME 65 AT CARGO DOOR CUTOUT STRINGER 14L. MAINTENANCE REPAIRED AND INSTALLED DOUBLER AT ANGLE BRACKET FOR FRAME 65 AT CARGO DOOR CUTOUT STRINGER 14L IAW EMB-145XR SRM 51-40-01 AND EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,487 hrs · 9,693 cycles

MAIN DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED INVERTER IAW EMB AMM 33-50-11.

Part: CONNECTOR — CONTAMINATED (SMOKE DETECTION) · airframe 16,449 hrs · 8,617 cycles

CLE FLIGHT NR 2294 THE CREW REPORTED A BAG SMOKE MSG ON THE EICAS MOMENTARILY. AFTER A MINUTE THE MSG CLEARED. NO LIGHT ON THE OVERHEAD BUTTON WAS NOTED. MX INSPECTED AND REPLACED CONNECTOR P2615. OPS CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — DEFECTIVE (LANDING GEAR) · airframe 15,911 hrs · 8,327 cycles

FLIGHT 2859 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AND ENGINE 1/2 REV DISAGREE AFTER SELECTING GEAR UP. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. MESSAGES DISAPPEARS WHEN SELECTED GEAR DOWN. EWR MX REMOVED AND REPLACED PROXIMITY SWITCH AND SERVICED NOSE LANDING GEAR. MX PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 12,700 hrs · 8,201 cycles

IAH DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOP. MX R&R THE NR 3 BATTERY PACK. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 12,700 hrs · 8,201 cycles

IAH DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOP. MX R&R THE NR 4 BATTERY PACK. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED (EMERGENCY LIGHT)

FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE FOUND EMERGENCY LIGHTS AT ROW 12 INOPERATIVE. RIC MAINTENANCE REMOVED AND REPLACED BURNED BULBS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: RELAY — INOPERATIVE (ELECTRICAL SYS)

FLIGHT 2489 - RIC - AFTER TAKEOFF, FLIGHT CREW REPORTED ELECTRICAL EMERGENCY ABNORMAL MESSAGE ON EICAS AND PERFORMED AIR RETURN. RIC MX REMOVED AND REPLACED RELAY K0021 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: BULB — BURNED (EMERGENCY LIGHTS) · airframe 14,266 hrs · 7,450 cycles

DURING ROUTINE MAINT, MX FOUND MAIN ENTRANCE DOOR EMERGENCY LIGHT (CEILING PANEL) INOPERATIVE. MX REMOVED AND REPLACED THE BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE — CHAFED (FIRE DETECTION) · airframe 12,351 hrs · 6,469 cycles

CLE FLIGHT 2578 THE CREW REPORTED THE NR 1 ENGINE FIRE DETECT CAUTION MESSAGE CAME ON FOR A BRIEF MOMENT ON DESCENT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE W101-1813-24 BETWEEN PO873 AND PO962. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL PANEL — INOPERATIVE (CABIN) · airframe 11,981 hrs · 6,282 cycles

CLE FLIGHT 2320 - THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT TEST FROM THE F/A CONTROL PANEL. ALSO THE CABIN LIGHTS WOULD NOT OPERATE. MAINTENANCE INSPECTED AND REPLACED THE F/A'S CABIN CONTROL PANEL. OPERATIONAL CHECKS OF ALL THE LIGHTS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 11,751 hrs · 6,161 cycles

MCI - FLIGHT 3118, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE OVERWING EMERGENCY EXIT LIGHTS TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — MALFUNCTIONED (CARGO BAY) · airframe 10,159 hrs · 5,314 cycles

IAH - FLT 2239, ON DESCENT THE CREW REPORTED A BAGGAGE SMOKE INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BAGGAGE VENT FAN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 9,384 hrs · 4,901 cycles

IAH - FLIGHT 2324, THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT COMPARTMENT DURING THE PART "B" OF ICE TEST. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED THE ICE TEST IAW EMB-145 AMM 30-00-00 & 71-00-00 WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUEL TANK — CORRODED (VENTRAL) · airframe 9,362 hrs · 4,888 cycles

CORROSION ON FWD SKIN OF VENTRAL TANK UNDERNEATH FLAME ARRESTER ATTACH BRACKET. CUT OUT AFFECTED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER. ALODINED AND PRIMED IAW EC 2810-01027.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHT) · airframe 9,353 hrs · 4,884 cycles

RIC MX - DURING ACFT ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHTS OVERWING WEAK. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 3. OPERATIONAL TEST PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — WEAK (EMERENCY LIGHT) · airframe 4,494 hrs · 2,360 cycles

TYS - DURING A SCHEDULED 4C INSPECTION WHEN THE SERVICE/ROUTINE WAS BEING C/W THE NR 2 EMERGENCY BATTERY WAS FOUND LOW ON CHARGE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AND OPS CHECK WAS GOOD. A/C WILL BE RELEASED WHEN ALL WORK IS C/W.

Part: BATTERY PACK — WEAK (EMERGENCY LIGHT) · airframe 4,494 hrs · 2,360 cycles

TYS - AIRCRAFT WAS IN FOR A 4C INSPECTION AND DURING THE SERVICE ROUTINE, THE NR 1 EMERGENCY LIGHT BATTERY WAS FOUND NOT CHARGED. MAINTENANCE REPLACED THE EMERGENCY BATTERY AND THE OPS CHECK WAS GOOD. A/C WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: WARNING SYSTEM — FALSE ACTIVATION (MLG) · airframe 4,088 hrs · 2,148 cycles

CREW REPORTED A LANDING GEAR DISAGREE AFTER TAKEOFF WITH THE GEAR UP. AIRCRAFT LANDED WITHOUT INCIDENT AND MAINTENANCE PERFORMED MULTIPLE GEAR SWINGS WITH NO DISCREPANCEY NOTED. AIRCRAFT RETURNED TO SERVICE

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 11,427 hrs · 8,580 cycles

MKE - FLIGHT 2843, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE MID CABIN EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN LEAD ON THE LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE EMERGENCY LIGHTING WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT'S LIGHTING CONTROL PANEL, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.