N12160

Part: COMPUTER — CORRODED (ZONE 200) · corrosion level 2 · airframe 48,344 hrs · 32,994 cycles

DURING REMOVAL OF NAVIGATION UNIT FOR FOM, CORROSION WAS FOUND ON DIFFERENT POINTS OF THE COMPUTER. REPLACEMENT WAS PERFORMED. PERFORM VOR/ILS TEST. OPS CHECK SAT.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 48,344 hrs · 32,994 cycles

PROFILE SPLICE FOUND WITH CORROSION IN BATHROOM UNDER FLOOR AREA LOCATION FR 60-61 (STA X=20793.0) STGR 17L. REMOVED AND REPLACED STGR SPLICE 17L BETWEEN FR 60-61

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 48,026 hrs · 32,697 cycles

RH OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND LIGHT ASSEMBLY NUTPLATE TO BE BROKEN. REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 47,068 hrs · 31,752 cycles

RH EMERGENCY EXIT ROW AFT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT MARKING ASSEMBLY. OPS CHECK FAILED. REINSTALLED ORIGINAL ASSEMBLY AND REMOVED AND REPLACED #5. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 45,283 hrs · 30,041 cycles

RH WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH WING EMERGENCY LIGHT. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 45,271 hrs · 30,029 cycles

EMERGENCY LIGHT BATTERIES DEAD. REMOVED AND REPLACED #1 AND #2 EMERGENCY BATTERY, RECHARGED #3 AND #4 EMERGENCY BATTERIES WITH 28V ESS DC BUSS AND OPS CHECKED. OPS CHECK SAT. POSITION 1: PN: ABS-2013-1A SN 51991 TSN 4196.26 CSN 3717

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 45,260 hrs · 30,017 cycles

LH EXTERIOR FWD EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED LH EXTERIOR FWD EMERGENCY LIGHT. OPS CHECK SAT

Part: PUMP — INOPERATIVE · airframe 44,557 hrs · 29,396 cycles

HYD 1 SYSTEM LOW QUANTITY ON EICAS THEN 10-15 MINUTES LATER HYD 1 SYSTEM FAIL ON EICAS. REMOVED AND REPLACED HYDRAULIC SYSTEM #1 ELECTRIC MOTOR DRIVEN PUMP. BLED AIR FROM HYDRAULIC SYSTEM 1. OPS CHECK SAT. REMOVED AND REPLACED LH ENGINE DRIVEN HYDRAULIC PUMP. PERFORMED ENGINE LEAK TEST, NO LEAKS NOTED

Part: DUCT — LEAKING (BLEED SYS) · airframe 44,188 hrs · 29,005 cycles

BLEED 1 LEAK IN FLIGHT. INSPECTED AND FOUND BLEED LEAK AT DUCT BETWEEN PRECOOLER AND BLEED VALVE, R/R DUCT AND Y DUCT L/H PYLON. PERFORMED HIGH POWER RUNS FOR ENG LEAK CHECKS, NO BLD 1 LEAK CHECK NOTED , OPS CHECK SAT LEAK CHECK SAT

Part: NONE — NONE · airframe 43,427 hrs · 28,371 cycles

UPPER AFT FUSELAGE EXTERIOR - FUSELAGE SKIN CRACKED STARTING AT 2 EA FASTENER HOELS ON FR75 STGR 2R. REPAIRED CRACK UPPER AFT FUSELAGE EXTERIOR SKIN AT FR75 BETWEEN STGR 2R.

Part: NONE — NONE · corrosion level 2 · airframe 43,427 hrs · 28,371 cycles

MAIN CABIN AFT WET AREA CENTER OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FR59-FR60 Y=0. REPAIRED CORROSION AROUND 2 EACH NUTPLATE HOLES BY CUTOUT AND INSTALL OF 2 EA DOUBLERS AT DAMAGED AREA CENTER OMEGA BEAM AT FR59-FR60 AT Y=0

Part: NONE — NONE · corrosion level 2 · airframe 43,427 hrs · 28,371 cycles

CORROSION ON RH GUSSET BETWEEN FR22-FR23 Y.00. REMOVED AND REPLACED RH GUSSET BETWEEN FR 19 - FR23 Y.00

Part: PUMP — INOPERATIVE · airframe 42,921 hrs · 27,926 cycles

E1 HYD PUMP FAIL ON EICAS AFTER ROTATION. REMOVED AND REPLACED E1 HYD PUMP. DURING BLEED FOUND BAD O-RING ON HYD PRESSURE LINE FROM SYS 1 ELE HYD PUMP. REMOVED AND REPLACED O-RING. NO LEAKS NOTED. OPS AND LEAK CHECK SAT.

Part: BATTERY PACK — INOPERATIVE · airframe 42,637 hrs · 27,664 cycles

INTERIOR EMERGENCY EXIT LIGHTS OVER BOTH WINGS INOPERATIVE. REMOVED AND REPLACED #3 BATT POWER SUPPLY. OPS CHECK SAT.

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 41,895 hrs · 27,029 cycles

ROW 18A EXIT PANEL OVER TOP HANDLE LOOSE. RESECURED OVER WING EXIT DOOR OPEN AND CLOSE HANDLE ACCESS PANEL APPLIED NEW VELCRO. NO FURTHER DEFECTS NOTED.

Part: ARMREST — CRACKED (SEAT 8A) · airframe 41,782 hrs · 26,925 cycles

CRACK FOUND ON PAX SEAT ARMREST AT 3A, 5A, 8A, 9A AND 21A. REMOVED AND REPLACED SEAT 3A, 5A, 8A, 9A, AND 21A

Part: LIGHT — INOPERATIVE (EXTERIOR EMER) · airframe 41,530 hrs · 26,700 cycles

RT FWD WING TO FUSELAGE EMERGENCY LIGHT INOPERATIVE. R &R RT FWD WING TO FUSELAGE EMERGENCY LIGHT. OPERATIONS CHECK SATISFACTORY.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,361 hrs · 26,552 cycles

EXTERNAL LEFT HAND FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT HAND FWD EMERGENCY LIGHT. OPERATIONS CHECK SATISFACTORY.

Part: COVER — DISLODGED (EMERGENCY EXIT) · airframe 41,214 hrs · 26,416 cycles

EMERGENCY EXIT COVER HANDLE AT 18A HANGING DOWN. RE-SECURED VELCRO FOR EMERGENCY EXIT COVER HANDLE.

Part: TRIM PANEL — UNSECURE (ROW 18A WINDOW) · airframe 41,212 hrs · 26,414 cycles

EXIT ROW 18A WINDOW TRIM NOT SECURE. RE-SECURED TRIM ON THE LT OVER WING ESCAPE HATCH, NO DEFECTS NOTED.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 39,573 hrs · 24,925 cycles

PRESSURIZATION FAILED IN AUTO MODE DURING CLIMB OUT, PRESS MANUAL MODE WORKED FINE. R&R PNEUMATIC OUTFLOW VALVE. OPS CHECK FAILED (PN 2099L011100 SN 02211)R&R ELECTROPNEUMATIC OUTFLOW VALE (PN 2097K011100 SN 00407). OPS CHECK FAILED. R&R DIGITAL AUTO CONTROLLER. OPS CHECK SAT.

Part: SLEEVE — DISCONNECTED (NR 2 ACM DUCT) · airframe 39,111 hrs · 24,517 cycles

CABIN PRESSURIZATION LEAK IN FLIGHT - AIRCRAFT DEPRESSURIZED. FOUND PACK 2 ACM DUCT SLEEVE DISCONNECTED & TORN, R&R SLEEVE. PERFORMED OPS/LEAK CHECK OF COOLING PACK SYSTEM & PRESSURIZATION CONTROL SYSTEM. OPS AND LEAK CHECK SAT.

Part: ANGLE — CRACKED (NLG) · airframe 38,682 hrs · 24,131 cycles

NLG UP-LOCK LEFT AND RIGHT ANGLE CORNERS CRACKED. REMOVED AND REPLACED NLG UP-LOCK LEFT AND RIGHT ANGLES.

Part: DOOR — CRACKED (THRUST REVERSER) · airframe 38,682 hrs · 24,131 cycles

LT UPPER THRUST REVERSER DOOR FORWARD FLANGE CRACKED. REPAIRED LT UPPER THRUST REVERSER DOOR FORWARD FLANGE.

Part: CROSSBEAM — CRACKED (NLG) · airframe 38,682 hrs · 24,131 cycles

NLG UP-LOCK CROSSBEAM CRACKED. REMOVED AND INSTALLED NEW NLG UP-LOCK CROSSBEAM.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,682 hrs · 24,131 cycles

PERFORM PERMANENT REPAIR OF DENT AFTER 5,000 FLIGHT CYCLES AT AREA BETWEEN FR 19 AND 20 AND STR 11L AND 12L. PERFORMED PERMANENT REPAIR OF THE 2 EA DENTS ON THE LT EXTERNAL SKIN AT FRAME 19-20 STR 11L-12L

Part: CROSSBEAM — CRACKED (NLG) · airframe 38,682 hrs · 24,131 cycles

NLG UP-LOCK AFT CROSSBEAM CRACKED. REMOVED AND REPLACED NLG UP-LOCK AFT CROSSBEAM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 38,682 hrs · 24,131 cycles

SERVICE DOOR THRESHOLD BEAM CORRODED AS MARKED. INSTALLED NEW SERVICE DOOR THRESHOLD BEAM.

Part: STRUCTURE — CRACKED (LT WING) · airframe 38,682 hrs · 24,131 cycles

NR 1 LT LEADING EDGE ATTACH FLANGE IS CRACKED. MARKED. TRIMMED AND REMOVED DAMAGE ON NR 1 LEADING EDGE ATTACH FLANGE. PERFORMED HFEC INSPECTION ON NR 1 LT LEADING EDGE ATTACH FLANGE BLENDED AREA. NO DEFECTS FOUND. TREATED AND PRIMED BLENDED AREA ON NR 1 LT LEADING EDGE ATTACH FLANGE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,682 hrs · 24,131 cycles

FR 62 STR 6-7 SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR CLIP ON FR 62 STR 6-7R.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 38,682 hrs · 24,131 cycles

RT FLOOR SILL AFTER 48 TO FR 52 CORRODED AS MARKED. INSTALLED RT FLOOR SILL AT FR 48 TO FR 52.

Part: RIB — CRACKED (LT MLG WW) · airframe 38,682 hrs · 24,131 cycles

LT GEAR WALL AFT LOWER RIB CRACKED. REMOVED AND REPLACED LT GEAR WALL AFT LOWER RIB.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,682 hrs · 24,131 cycles

FR 60 STRG 4-5 R TORSION BAR BRACKET IS CRACKED. REMOVED AND REPLACED TORSION BAR BRACKET FROM FR 60 BETWEEN STR4R - STR5R.

Part: ACTUATOR — INOPERATIVE (PITCH TRIM) · airframe 38,573 hrs · 24,044 cycles

MAIN PITCH TRIM INOPERATIVE. R&R HORIZONTAL STAB ACTUATOR. OPS CHECK SAT. INSTALLED AND SEALED PANELS 324EL, 321EL, 325LR, 321DR, 321CL, 333DC, 321AL. NO DEFECTS NOTED AT THIS TIME.

Part: TRIM PANEL — OUT OF ADJUST (CABIN) · airframe 38,084 hrs · 23,615 cycles

CAPTAIN SIDE OVER WING EMERGENACY EXIT APPEARS UNSEATED. ADJUSTED SIDE WALL TRIM. NO DEFECTS NOTED AT THIS TIME. CAPT EMERGENCY WINDOW SECURED

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 33,623 hrs · 19,858 cycles

DURING MAINTENANCE INSPECTION THE COCKPIT EMERGENCY LIGHT AND FWD EMERGENCY LIGHT MARKER WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (RIGHT WING) · airframe 28,316 hrs · 16,337 cycles

THE CREW REPORTED FUEL LEAK IN RT WING FUEL VENT. LONG VAPOR TRAILS SPOTTED BY TOWER AND PASSENGER WHILE THE ACFT WAS IN CLIMB ATTITUDE. MAINTENANCE INSPECTED AND REPLACED THE RT WING FUEL CHECK VALVE. LEAK CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 27,385 hrs · 15,779 cycles

DURING A-CHECK INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED FRAME 77 JUST ABOVE STRINGER 6L. MX REMOVED THE DAMAGE AND INSTALLED AN OVERSIZED RIVET, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 26,920 hrs · 15,491 cycles

DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR 77, BELOW STR 3R. MX WAS ABLE TO REMOVE THE CRACK AND INSTALL AN OVERSIZED RIVET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 26,920 hrs · 15,491 cycles

DURING 2A INSPECTION, AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FR 78 BELOW STR06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW APPROVED TECH DISPOSITION ETD2013-145-038298, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 26,920 hrs · 15,491 cycles

DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR78 BELOW STR 6R. MX REMOVED THE DAMAGE, AND PERFORMED A BUSHING REPAIR IAW APPROVED TECHNICAL DISPOSITION ETD2013-145-038298, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 25,609 hrs · 14,655 cycles

DURING MX INSPECTION THE AFT SIDE OF EMERGENCY LIGHT AT ROW 12 WAS FOUND INOPERATIVE. MX FOUND AND REPAIRED LOOSE CONNECTION WITH OPS CHECKS SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,106 hrs · 13,019 cycles

DURING MX INSPECTION THE AFT EXIT ROW CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 21,721 hrs · 12,054 cycles

FLT 4379 EWR CREW REPORTED SMOKE IN COCKPIT DURING TAXI ASSOCIATED WITH ADVANCEMENT OF THRUST ON ENGINE NR 2 AND PERFORMED GATE RETURN. EWR MX PERFORMED ENGINE RUNS WITH PACKS OPERATING AND NO SMOKE OR SMELL NOTED. EWR MX SUSPECTS DE-ICE FLUID MAY HAVE CAUSED SMOKE/SMELL SINCE DE-ICING WAS PERFORMED PRIOR TO TAXI. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FMU — MALFUNCTIONED (LT ENGINE) · airframe 21,531 hrs · 11,940 cycles

RAP - FLIGHT 6158, ON APPROACH TO RAP FROM DEN THE CREW REPORTED A NUMBER ONE ENGINE UNCOMMANDED SHUTDOWN. THE AIRCRAFT LANDED AT RAP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE FPMU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: METERING UNIT — INOPERATIVE (NR 1 ENGINE) · airframe 21,532 hrs · 11,940 cycles

ACFT HAD ENGINE NR 1 UNCOMMANDED SHUTDOWN ON APPROACH. MAINTENANCE REMOVED AND REPLACED NR 1 FPMU. OPS AND LEAK CHECKED GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,566 hrs · 11,278 cycles

DURING ROUTINE MAINTENANCE THE LOWER FORWARD EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 19,748 hrs · 10,662 cycles

EWR - FLT 2370 THE CREW REPORTED A CABIN ALTITUDE AMBER INDICATION 8400-8500 AT FL370. NO CHANGE IN MANUAL MODE. DESCENT IN AUTO MODE WAS NORMAL. MAINTENANCE INSPECTED AND REPLACED THE OUTFLOW VALVE AND OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — DEFECTIVE (CABIN PRESSURE) · airframe 19,695 hrs · 10,630 cycles

FLIGHT 2575 - EWR - FLIGHT CREW REPORTED AUTO PRESS ERRATIC. EWR MX REMOVED AND REPLACED CPAM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FITTING — CORRODED (CARGO BAY) · corrosion level 2 · airframe 18,020 hrs · 9,691 cycles

SHV - DURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15-16L WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CUP — CORRODED (CABIN) · corrosion level 2 · airframe 18,020 hrs · 9,691 cycles

SHV - DURING C-CHECK THE WASTE DRAIN CUP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CUP IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OUTFLOW VALVE — FAULTY (CABIN PRESSURE) · airframe 17,333 hrs · 9,319 cycles

FLIGHT 2717 - EWR - FLIGHT CREW REPORTED PRESSURIZATION RATE OF CLIMB ERRATIC. EWR MX REMOVED AND REPLACED OUTFLOW ELECTRO PNEUMATIC VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRANSPONDER — INOPERATIVE (COCKPIT) · airframe 15,943 hrs · 8,561 cycles

IAH - FLIGHT 2738, THE CREW REPORTED THAT THE CAPTAINS BOOM, HAND, AND O2 MASK MICROPHONES WORK INTERMITTENTLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE COMM/XPNDR UNIT (RCZ), OPERATIONALLY TESTED WITH NO DEFECTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 15,775 hrs · 8,445 cycles

TYS - A/C EN ROUTE FROM EWR TO MSY WHEN ICIAS MESSAGE INDICATED SMOKE IN THE BAGGAGE COMPARTMENT. PILOTS OPEN FIRE BOTTLES AND DIVERTED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED BOTH SMOKE DETECTORS AND REPLACED THE FIRE BOTTLES. A/C RELEASED TO SERVICE ALL WORK ACCOMPLISHED IAW AMM 26-15-01. OPS CHECK GOOD.

Part: DETECTION SYS — MALFUNCTIONED (CARGO BAY) · airframe 15,726 hrs · 8,416 cycles

MEM - FLIGHT 2859 - THE CREW REPORTED A BAGGAGE SMOKE INDICATION IN FLIGHT. THE CREW DISCHARGED THE BAGGAGE FIRE BOTTLES AS A PRECAUTION. PERFORMED AN EMERGENCY DESCENT, AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF FIRE OR SMOKE. REMOVED AND REPLACED THE BAGGAGE FIRE BOTTLES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 15,459 hrs · 8,259 cycles

FLIGHT 2403 - EWR - FLIGHT CREW REPORTED BAGG SMOKE WARNING ON EICAS. CREW PERFORMED SYSTEM RESET SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO DOOR)

SHV - DURING C-CHECK BAGGAGE DOOR INNER LOWER FRAME HAS CORROSION. MX REPAIRED BAGGAGE DOOR INNER LOWER FRAME IAW EC 5230-01194. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FITTING — DAMAGED (AILERON PCA)

SHV - DURING C-CHECK LT AILERON PCA ATTACHMENT HAS MIGRATED BUSHING. MX REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MX R&R THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV DURING C CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5320-01228. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

SHV DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT FRAME 65-68. MX R&R THE AFFECTED BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DEFECTIVE (EMERGENCY LIGHTS) · airframe 12,018 hrs · 6,374 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND MULTIPLE EMERGENCY LIGHT DIMMED. MX REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (COCKPIT) · airframe 10,944 hrs · 5,812 cycles

IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED RELAY K0021, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — DEFECTIVE (COCKPIT) · airframe 10,944 hrs · 5,812 cycles

IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY ELECTRICAL PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (COCKPIT) · airframe 10,944 hrs · 5,812 cycles

IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED RELAY K0097, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 10,637 hrs · 5,652 cycles

IAH - FLIGHT 2186, THE CREW REPORTED BAGGAGE WARNING LIGHT ILLUMINATED IN FLIGHT WITH NO INDICATIONS IN EICAS. THE AIRCRAFT LANDED IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.