N12172

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,663 hrs · 27,818 cycles

CENTER CEILING EMERGENCY EXIT SIGN BETWEEN SEATS 18A AND 18C IS INOPERATIVE ON FWD SIDE. REMOVED CEILING LIGHT LENS COVER AT SEATS 18A. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK SAT. REINSTALLED LIGHT LENS COVER. OPS CHECK SAT.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 42,612 hrs · 27,765 cycles

SUPPLEMENTAL (NEW) INFORMATION: REMOVED AND REPLACED #1 PACK HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED HEPA FILTERS 1 AND 2. INSTALLED FLOOR PANELS 251FF AND 251HF. REMOVED AND REPLACED NO.0 CARBON SEAL ASSEMBLY. INSTALLED FAN SPANNER - LOCK NUT PLUG. INSTALLED FAN WHEEL ASSEMBLY. INSTALLED BACK FAN SPINNER. INSTALLED BACK THE FAN BLADE FORWARD RETAINER ASSEMBLY. INSTALLED BACK THE FAN BLADES. PERFORMED OPS AND LEAK CHECK OF NO.0 CARBON SEAL. LEAK CHECK FAILED. REMOVED AND REPLACED LH ENGINE.

Part: NONE — NONE · airframe 42,571 hrs · 27,727 cycles

STRONG HYDRAULIC SMELL IN COCKPIT/CABIN. RAN ENGINES FOR 30 MINUTES. NO SMELL NOTED. OPERATED PACKS. OPS CHECK GOOD.

Part: NONE — NONE · airframe 42,472 hrs · 27,633 cycles

FWD EMERGENCY LIGHT INOP. R&R FWD CABIN CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD

Part: SKIN — DENTED (LT AILERON) · airframe 40,297 hrs · 25,710 cycles

LH AILERON LEADING EDGE HAS PROTRUDING DENTS. EVAL DENT AT AILERON LH (SPARS) FOUND TO BE OUT OF LIMITS. LH AILERON LEADING EDGE

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,297 hrs · 25,710 cycles

SERVICE DOOR FLOOR HAS SIGNS OF CORROSION. UPON REMOVED CORROSION AND EVALUATED FLOOR SILL SERVICE DOOR, FOUND TO BE OUT OF LIMITS. FLOOR SILL SERVICE DOOR WERE REMOVED AND INSTALLED. NEW FLOOR SILL SERVICE DOOR.

Part: PIN — CORRODED (EMERGENCY EXIT) · airframe 40,297 hrs · 25,710 cycles

LH AND RH EMERGENCY OVER WING EXIT DOORS HAVE SIGNS OF CORROSION ON THE BOTTOM ALIGNMENT PINS. ALIGNMENT PINS CORROSION WAS OUT OF LIMITS. REMOVED AND INSTALLED PINS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,059 hrs · 25,496 cycles

GALLEY EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED GALLEY EMERGENCY LIGHT LAMP. OPERATIONS TESTED SATISFACTORY.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,633 hrs · 25,088 cycles

EMERGENCY LIGHT ABOVE FWD FA SEAT INOPERATIVE. R&R EMERGENCY LIGHT BATTERY PACK IN POSITION #1. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,531 hrs · 25,001 cycles

RH OVERWING EMERGENCY LIGHT INOPERATIVE. R&R RH OVERWING EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LIGHT — OUT OF POSITION · airframe 39,400 hrs · 24,882 cycles

EMERGENCY LIGHTING STRIP MIS-CONFIGURED. INSTALLED PHOTO LUMINESCENT STRIP.

Part: CHARGER — SHORTED (EMERGENCY LIGHTS) · airframe 39,186 hrs · 24,714 cycles

BOTH LH AND RH OVER WING EMERGENCY LIGHTS INOPERATIVE. R&R RH OVER WING EMERGENCY LIGHT ASSEMBLY DUE TO SHORTED ASSEMBLY. R&R #4 EMERGENCY BATTERY AND CRADLE. OPS CHECK FAILED. R&R #4 EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,036 hrs · 24,593 cycles

LEFT AND RIGHT HAND AFT OVER WING EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT OVER WING EMERGENCY LIGHTS AND FOUND #4 BATTERY CHARGER ASSEMBLY INOPERATIVE. R&R #4 CHARGER ASSEMBLY. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,318 hrs · 23,923 cycles

OVER WING EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY POWER SUPPLY 4 BATTERY PACKS. OPS CHECK SAT.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 38,153 hrs · 23,767 cycles

ELECTRICAL SMOKE SMELL JUST AFTER DEPARTURE #1 MFD BLANKED AFTER SMOKE SMELL WAS DETECTED. TROUBLESHOOT AND FOUND #1 MFD CB POPPED. R&R #1 MFD UNIT. OPS CHECK SAT. NO ELECTRICAL SMOKE NOTED IN THE COCKPIT. NO MFD CB POPPED AT THIS TIME. INSPECTED WIRING TO #1 MFD WITH NO FAULTS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 38,135 hrs · 23,746 cycles

EXIT SIGN ASSEMBLY FWD CABIN BULKHEAD INOPERATIVE. REMOVED ELECTRO-LUMINESCENT LAMP FOUND ELECTRICAL CONNECTION LOOSE. REATTACHED ELECTRO-LUMINESCENT LAMP. OPS CHECK SAT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 38,089 hrs · 23,700 cycles

BOTH OVER WING EMERGENCY LIGHT INOPERATIVE, TWO AFT CEILING EMERGENCY LIGHTS INOPERATIVE, AND FWD AISLE EMERGENCY SIGN INOPERATIVE. R&R AFT CEILING #4 EMERGENCY BATTERY. OPS CHECK SAT.

Part: CONTACTOR — LOOSE (EXTERIOR LIGHT) · airframe 37,791 hrs · 23,439 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXT EMERGENCY LIGHT. OPS CHECK FAILED. AFTER FURTHER TROUBLESHOOTING FOUND CONTACTOR ON THE LIGHT ASSY LOOSE. LIGHT ASSY REQUIRES REPLACEMENT. REMOVED LIGHT ASSY TO FOM. REPLACED SERVICE DOOR EXTERNAL EMERGENCY LIGHT ASSY. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,791 hrs · 23,439 cycles

LT LOWER FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R LT FWD LOWER FAIRING EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 37,678 hrs · 23,369 cycles

DURING MX INSPECTION THE NR 3 CEILING EMERGENCY LIGHT WAS INOP. CHARGED NR 3 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,678 hrs · 23,369 cycles

DURING MX INSPECTION THE NR 4 CEILING EMERGENCY LIGHT WAS INOP. REMOVED + REPLACED NR 4 BATTERY PACK ASSEMBLY IAW AMM 33-50-04. OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,678 hrs · 23,369 cycles

DURING MX INSPECTION THE LEFT SIDE OVER THE WING EMERGENCY LIGHT WAS INOP. REMOVED + REPLACED NR 4 BATTERY PACK ASSEMBLY IAW AMM 33-50-04. OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,960 hrs · 22,872 cycles

TYS A/C WAS FOUND TO HAVE SEVERAL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 2 BATTERY IAW AMM 33-50-04; IPC REFERENCE 33-50-04 FIG 01 ITEM 30. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,254 hrs · 22,371 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A DENT IN FUSELAGE AT FRAME 4 FWD OF THE BATTERY COMPARTMENT. MAINTENANCE REPAIRED AREA IAW EC/TC 2018-070057. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,254 hrs · 22,371 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND A DENT IN THE FUSELAGE SKIN AT FRAME 2 RIGHT SIDE. MAINTENANCE REPAIRED AREA IAW CARD ETD 2018-145-070081. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 36,254 hrs · 22,371 cycles

AREAS OF CORROSION ON CENTER OMEGA BEAM AT FRAMES 58 AND 61. CUTOUT DAMAGE TO CENTER OMEGA BEAM AT FRAMES 58 AND 61. FABRICATED DOUBLERS AND INSTALLED IN ACCORDANCE WITH SRM 53-24-10.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,990 hrs · 19,127 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND A CRACK PROTRUDING FROM A RIVET AT FRAME 79 AND STRINGER 4R. MAINTENANCE INSTALLED A REPAIR BUSHING AT FRAME 79,STRINGER 4R IAW SRM 53-32-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,990 hrs · 19,127 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK PROTRUDING FROM A RIVET AT FRAME 79 AND STRINGER 7L. MAINTENANCE INSTALLED A REPAIR BUSHING AT FRAME 79 AND STRINGER 7L IAW SRM 53-32-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,990 hrs · 19,127 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK PROTRUDING FROM A RIVET AT FRAME 78 AND STRINGER 7L. MAINTENANCE PERFORMED A REPAIR BUSHING IAW SRM 53-32-01. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FITTING — CRACKED (LT ENGINE) · airframe 30,990 hrs · 19,127 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND THE LEFT HAND ENGINE FWD LOWER YOLK FITTING CRACKED. MAINTENANCE R&R THE FITTING IAW CARD NUMBER EAZ6-2014-063. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,990 hrs · 19,127 cycles

TYS A/C IS IN FOR A C-CHECK WHEN INSPECTION FOUND A CRACK ON THE LEFT AFT FUSELAGE AT FRAME 75 AND STRINGER 2L. MAINTENANCE PERFORMED A REPAIR OF SKIN CRACK AT FRAME 75, STRINGER 2L IAW SRM 53-31-01. REFER TO 602 1290900 FOR PRESSURIZATION. PRESSURIZATION C/W AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FRAME — CRACKED (FUSELAGE) · airframe 36,254 hrs · 22,371 cycles

FRAME 25 IS CRACKED AT RT FLOOR SILL (BACKSIDE) BETWEEN STRINGER 15 AND 16L. PERFORMED REPAIR OF FRAME 25 AT FLOOR SILL IAW SRM 53-00-04, REPAIR 14.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,474 hrs · 21,809 cycles

DURING A MAINTENANCE INSPECTION, THE GALLEY SERVICE DOOR LOWER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,028 hrs · 19,371 cycles

DURING MX INSPECTION , THE EMERGENCY EXIT SIGN ON THE BULKHEAD AT SEAT 3CD FOUND INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY EXIT SIGN AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 31,079 hrs · 18,869 cycles

ACFT WAS FOUND WITH A DENT ON THE FORWARD FUSELAGE JUST AFT OF MAIN CABIN DOOR. MAINTENANCE REPAIRED DENT IAW EC-5320-02088. ALL WORK ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · airframe 30,926 hrs · 18,559 cycles

DURING C-CHECK, BAGGAGE DOOR CUTOUT LOWER BEAM HAS CORROSION FRAME 65-68. R & R BAGGAGE DOOR CUTOUT LOWER BEAM FRAME 65-68 IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN SPLICE — CORRODED (FRAMES 13-14) · airframe 30,926 hrs · 18,559 cycles

DURING C-CK. SKIN SPLICE AT FRAME 13-14, STR 21R-19R IS CORRODED. R & R DAMAGED PORTION OF SKIN SPLICE IAW SRM 53-00-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,526 hrs · 18,262 cycles

ACFT IN FOR AN A-CHECK WHEN INSPECTION FOUND THE LT WING FRONT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED THE NR 1 LIGHT BATTERY AND CRADLE REFERENCING AMM 33-50-04 AND IPC 33-50-04, FIG 1 ITEM 30 AND 60. OPS CHECK GOOD AND WAS RELEASED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,298 hrs · 15,438 cycles

DURING MX INSPECTION THE EXIT ROW AT SEATS 12 OVERHEAD AFT FACING EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX R & R NR 3 EMERGENCY LIGHT BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FRAME 47) · airframe 25,365 hrs · 14,846 cycles

RT OMEGA BEAM SUPPORT CRACKED AT FRAME 47. R & R OMEGA BEAM SUPPORT.

Part: FLOOR SUPPORT — CRACKED (FRAME 47) · airframe 25,365 hrs · 14,846 cycles

LT OMEGA BEAM SUPPORT CRACKED AT FRAME 47. R & R BEAM SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

RT OMEGA BEAM CORRODED BEYOND LIMITS AFTER BLEND-OUT. INSTALLED DOUBLER.

Part: FRAME — CORRODED (65) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

FRAME 65 IS CORRODED BEYOND LIMITS AFTER BLEND-OUT, WHERE STRIKER PLATE ATTACHES BETWEEN STRINGER 14L AND 15L. FABRICATED AND INSTALLED DOUBLER.

Part: SHEAR TIE — CORRODED (FRAME 51) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

SHEAR TIE CORRODED BEYOND LIMITS. R & R SHEAR TIE.

Part: FLOOR SUPPORT — CRACKED (FRAME 47) · airframe 25,365 hrs · 14,846 cycles

RT OMEGA BEAM SUPPORT CRACKED AT FRAME 47. R & R RT OMEGA BEAM SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R RT FLOOR SUPPORT.

Part: FRAME — CORRODED (CARGO DOOR TRACK) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

CARGO DOOR FORWARD TRACK FRAME HAS CORROSION BEYOND LIMITS AFTER BLEND-OUT AT LOWER END. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED A FILLER AND DOUBLER.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

LEFT SIDE FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

LEFT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

LT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 25,365 hrs · 14,846 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 25,366 hrs · 14,846 cycles

DURING C-CHECK, INSPECTION FOUND THE CENTER OMEGA BEAM CAP CORRODED AT FRAME 59. MAINTENANCE R & R THE CENTER OMEGA BEAM IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 41-48) · airframe 25,366 hrs · 14,846 cycles

C-CHECK, INSPECTION FOUND THE RT FLOOR SUPPORT CORRODED AT FRAME 41 THRU 48. MAINTENANCE R & R THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 60) · airframe 25,366 hrs · 14,846 cycles

DURING C-CHECK INSPECTION, FOUND THE LT OMEGA BEAM CAP CORRODED AT FRAME 60. MAINTENANCE R & R THE OMEGA BEAM CAP IAW SRM 51-40-02.

Part: SILL — CORRODED (ZONE 800) · airframe 25,366 hrs · 14,846 cycles

C-CHECK, INSPECTION FOUND THE CARGO DOOR LOWER SILL FRAME HAD A CORRODED NUT PLATE. MAINTENANCE R & R THE CARGO DOOR SILL IAW SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: DOUBLER — CORRODED (FLOOR SUPPORT) · airframe 25,366 hrs · 14,846 cycles

DURING C-CHECK, FOUND WALL DOUBLER AT FRAMES 23 - 24 CENTER OMEGA BEAM CORRODED. MX R & R THE WALL DOUBLER IAE SRM 51-40-02.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,636 hrs · 12,390 cycles

DURING MX INSPECTION, THE PILOTS AND GALLEY OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND NOT TO ILLUMINATE. MX R & R THE INVERTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AUDIO PANEL — FAILED (ZONE 100) · airframe 21,055 hrs · 12,010 cycles

CREW REPORTED ELECTRICAL SMOKE COMING FROM F/O'S GLARESHIELD. MX INSPECTED COCKPIT PANELS AND FOUND BURNING ODOR COMING FROM F/O'S AUDIO CONTROL PANEL. R & R F/O'S CONTROL PANEL IAW AMM 23-51-01 OPS CHECKED SUCCESSFUL. ACFT RETURNED TO SERVICE.

Part: LIGHT — SMOKE (CHART HOLDER) · airframe 20,070 hrs · 11,449 cycles

THE CAPTAIN REPORTED SMOKE COMING FROM THE CAPTAIN'S CHART HOLDER LIGHT. MX REPLACED THE CAPTAIN'S CHART HOLDER, OPS TESTED THE LIGHT AND CLEARED THE DISCREPANCY.

Part: DAMPER — WORN (RT AILERON) · airframe 19,610 hrs · 11,173 cycles

SHV - DURING C-CHECK RT AILERON DAMPING HINGE O/B HAT BUSHING IS MIGRATED. MAINTENANCE REPLACED RT AILERON DAMPED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROFILE — CORRODED (MAIN DOOR) · corrosion level 2 · airframe 19,610 hrs · 11,173 cycles

SHV - DURING C-CHECK CORROSION AROUND MAIN DOOR LOWER FRAME AFT SCREW HOLE. MAINTENANCE REMOVED CORROSION AND PERFORMED REPAIR FROM AROUND MAIN DOOR LOWER FRAME AFT SCREW HOLE IAW EC5210-01154 REV A AND IAW EMB-145XR CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,610 hrs · 11,173 cycles

SHV - DURING C-CHECK FWD CARGO TRIANGLE AT FRAME 65 CORRODED AROUND SCREW HOLE. MAINTENANCE PERFORMED REPAIR ON FWD CARGO TRIANGLE BRACKET (RIB) AT FRAME 65 IAW EC5320-01479. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROJECTOR — DEFECTIVE (COCKPIT) · airframe 18,592 hrs · 10,587 cycles

FLIGHT 2949 - EWR - FLIGHT CREW REPORTED SMOKE APPEARED BETWEEN THE GLARESHIELD AND THE TOP OF AUTO-PILOT. EWR MX REMOVED AND REPLACED FLOOD LIGHT PROJECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 16,260 hrs · 9,050 cycles

DURING ROUTINE MAINTENANCE THE LEFT WING EMERGENCY LIGHT AND THE COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,173 hrs · 9,004 cycles

DURING ROUTINE MAINTENANCE THE OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,703 hrs · 8,213 cycles

PANEL 191 LT EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,964 hrs · 7,810 cycles

EWR MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT ON EXIT ROW 12 INOPERATIVE. MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 13,620 hrs · 7,615 cycles

CLE - FLT 2311 - THE CREW REPORTED A BURNING SMELL THAT SEEMED TO BE COMING FROM THE NR 1 PACK. MAINTENANCE INSPECTED AND FOUND A BIRD STRIKE ON THE NR 1 ENGINE. NO DAMAGE WAS FOUND AND BIRD STRIKE INSPECTION WAS PERFORMED.

Part: UNKNOWN — SMOKE (CABIN) · airframe 13,618 hrs · 7,614 cycles

MHT FLT 2958 - THE CREW REPORTED A BURNING SMELL ON SHORT FINAL INTO MHT AND THE F/A NOTICED A SMALL AMOUNT OF SMOKE IN THE CABIN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE CABIN LIGHTING SYSTEMS FOR ANY DEFECTS AND NO DEFECTS WERE FOUND. UNABLE TO DUPLICATE THE DISCREPANCY.

Part: UNKNOWN — ODOR (DE-ICE SYSTEM) · airframe 13,547 hrs · 7,577 cycles

IAH - FLIGHT 2801 - THE CREW REPORTED THAT DURING THE AIRBORNE PORTION OF "B" ICE TEST THE CREW RECEIVED AN EXTREME BURNING ODOR IN THE CABIN AND COCKPIT THAT LASTED ABOUT 30-40 SECONDS AFTER COMPLETION OF THE TEST. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED THE ICE TEST "B" WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — FAULTY (COCKPIT) · airframe 13,424 hrs · 7,506 cycles

EWR FLT 2609 - THE CREW REPORTED ENGINE NR 1 DEFAULTS TO T/O THRUST. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE THRUST RATING PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: SENSE LINE — LEAKING (BLEED AIR SYS) · airframe 12,547 hrs · 7,059 cycles

FLIGHT 2914 - EWR - FLIGHT CREW REPORTED THAT ON CLIMB PASSING THROUGH 13,000FT, BLEED 1 OVERTEMP AND BLEED 2 OVERTEMP WARNINGS ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 LOW TEMP FAN AIR THERMOSTAT SENSE LINE AND PERFORMED OPERATIONAL AND LEAK CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 11,975 hrs · 6,723 cycles

FLIGHT 2438 - EWR - FLIGHT CREW REPORTED THAT AFTER TAKEOFF, WHEN ATTEMPTING TO SELECT THE GEAR HANDLE TO THE UP POSITION, THE GEAR HANDLE WOULDN’T MOVE. PER THE QRH THE HANDLE WAS ABLE TO MOVE BY PRESSING THE DOWNLOCK REL. THE GEAR RETRACTED BUT THE NOSE GEAR DOOR REMAINED OPEN. ALSO CIRCUIT BREAKER E21 DOOR CMD WAS NOTICED POPPED. EWR MX REMOVED AND REPLACED NLG UP PROX SWITCH NR 3, PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW EMB 145 AMM 32-30-00. OPS CHECK GOOD. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,596 hrs · 6,523 cycles

THE CREW REPORTED THAT THE FWD WHITE AISLE PATH LIGHT WAS INOPERATIVE. MX INSPECTED THE ACFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SLEEVE — BLOWN (A/C BAY) · airframe 11,198 hrs · 6,309 cycles

IAH - FLIGHT 2962, THE CREW REPORTED A BLEED 1 CLOSED EICAS MESSAGE FOLLOWED BY PACK 1 CLOSED EICAS MESSAGE APPEARING REPEATEDLY, THE APU WAS USED FOR PRESSURIZATION, AND A CABIN HIGH ALT WARNING WAS RECEIVED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED A SLEEVE ON THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 9,778 hrs · 5,398 cycles

SHV - DURING C-CHECK THE RIGHT HAND BUTTSTRAP WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 65 AND 66. MAINTENANCE REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5320-01405. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — GOUGED (AILERON) · airframe 9,778 hrs · 5,398 cycles

SHV - DURING C-CHECK THE LEFT HAND DAMPER BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,778 hrs · 5,398 cycles

SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5320-01404. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 9,778 hrs · 5,398 cycles

SHV - DURING C-CHECK THE MAIN DOOR WAS FOUND TO HAVE CORROSION ON THE BOTTOM FRAME AROUND THE FORWARD NUT PLATE HOLE. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — MISSING (CUSTOMER AIR) · airframe 9,407 hrs · 5,362 cycles

FLT 7765 - LAX TO LAX - DURING CLIMB FLIGHT CREW REPORTED E1 HIGH ITT. AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. MX PERSONNEL FOUND COSTOMER SERVICE DISCHARGE TUBE CLAMP MISSING CAUSING GASKET ALSO MISSING. MX INSTALLED A NEW CLAMP AND GASKET OPERATIONALLY CHECKED HIGH POWER RUNS SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: ACTUATOR — DAMAGED (T/E FLAP) · airframe 7,935 hrs · 4,240 cycles

FLT 7782 - SJC TO ONT - FLIGHT CREW REPORTED FLAP FAIL ON LANDING AT 33 DEGREES, ATTEMP TO RESET AS PER MX INSTRUCTIONS AND IT GOT STUCK AT 11 DEGREES. MX SET ALL FLAPS AT 9 DEGREES AND THE OPERATING LIMITATIONS WERE NOT TO EXCEED 200 KNOTS AND RELEASED THE AIRCRAFT ON A FERRY PERMIT TO ONT WERE MX PERSONNEL REMOVED BOTH RIGHT I/B FLAP O/B P/N 885500-1003, S/N 00262 TSN 7932 CSN 4237 TSO 7932 AND I/B P/N 885500-1001, S/N 00258 TSN 7935 CSN 4240 TSO 7935 ACTUATORS AND REPLACED THEM. OPERATIONALLY CHECK WITH NO DEFECTS AND THE A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 7,299 hrs · 3,832 cycles

CLE FLIGHT 2488 - THE CREW REPORTED A LAV SMOKE WARNING INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. THE PRIMARY FAILURE/REASON FOR REMOVAL WAS OIL LEAKING PAST NR 4 CARBON SEAL ASSEMBLY ALLOWING OIL TO ENTER THE CORE FLOWPATH AND CAUSE OIL SMELL IN THE CABIN.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 7,154 hrs · 3,752 cycles

FLT 2761 - RIC TO EWR - DURING CLIMB, CREW HAD WARNING OF LAV SMOKE. EWR MX REMOVED AND REPLACED LAV SMOKE SENSOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 6,921 hrs · 3,622 cycles

IAH - FLIGHT 2152, THE CREW REPORTED THAT THE EMERGENCY LIGHTS CAME ON DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY LIGHT SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 6,262 hrs · 3,292 cycles

MCI - FLIGHT 2018, DURING TAKEOFF ROLL, THE CREW REPORTED SMOKE IN THE CABIN & THE CAPTAIN ABORTED THE TAKEOFF. MCI MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS WITH BLEED AIR AND PACKS SELECTED ON WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,076 hrs · 3,194 cycles

GRR - FLIGHT 2114, THE CREW REPORTED THAT THE FLAPS FAILED ON APPROACH. THE CREW DECLARED AN EMERGENCY LANDING, AND LANDED AT GRR WITHOUT INCIDENT. MAINTENANCE RESET THE FLAPS CIRCUIT BREAKER, AND FLAP SWITCH AT THE MAINTENANCE PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 5,701 hrs · 2,994 cycles

CREW REPORTED, LAV SMOKE WARNING ON EICAS AND AUDIBLE ALARM, RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB 145XR AMM #26-14-01. OPS CHECKED GOOD.