N11189

Part: SUPPORT — CORRODED (WASTE VALVE) · corrosion level 2 · airframe 42,708 hrs · 28,318 cycles

TOILET WASTE VALVE SUPPORT HAS CORRODED HARDWARE. REMOVED 1 AFT RINSE NIPPLE SCREW. REPLACED AND INSTALLED 1 AFT RINSE NIPPLE SCREW. REMOVED 4 AFT WASTE DRAIN VALVE SCREWS. REPLACED AND INSTALLED 4 AFT WASTE DRAIN VALVE SCREWS

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,708 hrs · 28,318 cycles

FLOOR SILL ASSEMBLY AT STR 16R FR20 FWD GALLEY CORRODED AROUND N/P HOLE. BLENDED CORROSION ON FLOOR SILL ASSEMBLY AT STR 16R FR20 UNDER FWD GALLEY AT N/P HOLE. PERFORMED REQUIRED 30X DVI ON BLEND REPAIR AT STR 16R FR20. PRE-TREATED AND PRIMED AREA.

Part: DOOR — UNSECURE (ZONE 800) · airframe 42,627 hrs · 28,242 cycles

RAMP AGENT REPORTS MCD WILL NOT FULLY CLOSE. INSPECTED, AND PERFORMED OPS CHECK OF MCD. OPS CHECK SAT. NO DEFECTS NOTED.

Part: VALVE — INOPERATIVE · airframe 42,602 hrs · 28,218 cycles

BLEED 1/2 OVER TEMP IN ICING. REMOVED AND REPLACED LOW TEMP AIR THERMOSTAT. OPS CHECK SAT. PERFORMED TI AND AGAIN BLEED 2 ARROW TURN AND WENT INTO RED. NO EICAS MESSAGE WAS GIVEN. REMOVED AND REPLACED BLEED 2 OUTLET TEMP SENSOR. PERFORMED BLOCK 1, 2, AND 3 OPS CHECK. BLEED 2 LOW TEMP OCCURRED FOR 2 MINUTES WITH BOTH ENGINES IDLE AND BOTH BLEEDS AND PACKS ON. PERFORMED FIRST HIGH POWER FOR 4 MINUTES WITH NO CARROT IN THE RED AND NO EICAS MESSAGES, PERFORMED SECOND 4 MINUTE RUN WITH SAME RESULTS. BLEED 2 TEMP CARROT RODE THE LINE BETWEEN RED AND GREEN WHILE BLEED 1 STAYED IN THE MIDDLE OF THE GREEN. CAPPED BOTH FAVS AND PERFORMED INITIAL ENGINE RUNS, BLEED 2 TEMP SLOWLY MOVED TO THE MIDDLE OF THE WHITE WHILE BLEED 1 DID NOT MOVE, RH FAV OPENED AT HIGH POWER. PERFORMED CHECK OF E2 PRE COOLER EXHAUST. NO SIGNS OF EXCESSIVE HOT AIR. FOUND RIGID LINE FROM E2 FAV SENSE LINE AT VALVE CHAFFED BUT NOT ALL THE WAY THROUGH. PRESSURIZED THE LINE BETWEEN THE FAV SENSE LINE AND THE THERMOSTATS. NO LEAK FOUND. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE. OPS AND LEAK CHECK SAT. PERFORMED OPS TEST OF THE ENGINE AIR BLEED SYS 1 AND 2. OPS CHECK GOOD.

Part: TIRE — FAILED (ZONE 700) · airframe 42,087 hrs · 27,753 cycles

AIRCRAFT JARRING AT VR. COMPLIED WITH LANDING GEAR TIRE BUST OR TIRE TREAD FAILURE INSPECTION. NO DAMAGE OR DEFECTS NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 41,853 hrs · 27,525 cycles

SERVICE DOOR EXIT SIGN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED INVERTER 2. OPS CHECK SAT.

Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 41,294 hrs · 27,024 cycles

MFD FLICKERING ON/OFF WHEN RADAR TURNED ON AND BURNING ODOR. REMOVED AND REPLACED CAS MFD DISPLAY UNIT WITH NEW. OPS CHECK GOOD. NO SMELL OR ODOR NOTED.

Part: DAU — INOPERATIVE (FUEL SYSTEM) · airframe 41,207 hrs · 26,940 cycles

FUEL TRANSFER INOPERATIVE IN FLIGHT. REMOVED AND REPLACED DAU #1. OPS CHECK SAT. PERFORMED A FUEL TRANSFER OPS CHECK. OPS CHECK SAT. NO REPEAT FAULT CODES FOUND. REMOVED AND REPLACED VENTRAL PUMP A. OPS/LEAK CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,942 hrs · 26,725 cycles

LOWER SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LOWER SERVICE DOOR EMERGENCY LIGHT. OPS CHECK SAT

Part: CONNECTOR — CORRODED (CALL LIGHT) · airframe 40,860 hrs · 26,654 cycles

EMERGENCY CALL LIGHT ALWAYS ON IN THE COCKPIT. INSPECTED FA'S HANDSET CONNECTORS, PERFORMED WIRE CHECKS BETWEEN HANDSETS AND PA AMP AND PERFORMED OPS CHECK. NO DEFECTS NOTED. FOUND CORROSION AT P8100, CLEANED CORROSION AND OPS CHECK GOOD. INSPECTED FA'S HANDSET CONNECTORS, PERFORMED WIRE CHECKS BETWEEN HANDSETS AND PA AMP, AND PERFORMED OPS CHECKS, NO DEFECTS NOTED. FOUND CORROSION AT P8100, CLEANED CORROSION AND OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 40,630 hrs · 26,452 cycles

WING TO FUSELAGE FRONT FAIRING LH EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT HOUSING. OPS CHECK SAT.

Part: LAMP — NONE (UNKNOWN) · airframe 39,843 hrs · 25,687 cycles

LH EMERGENCY EXIT OVERHEAD LIGHT INOP R/R LH EMERGENCY EXIT OVERHEAD LIGHT BULB. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,652 hrs · 25,503 cycles

MAIN CABIN DOOR HARD TO OPEN/CLOSE. APPLIED DRY LUBRICATION TO MAIN CABIN DOOR HINGE AND DOOR SEAL. OPS CHECK GOOD.

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

CF3, LH OMEGA BEAM #5 CRACKS SUSPECTED FOUND BTW FRAME 41 AND 42 ON FLOOR STRUCTURE. CF3, LH OMEGA BEAM #5 HAS CRACKS SUSPECTED FOUND AT FRAME 41 AND 42 ON FLOOR STRUCTURE. 1 CRACK FOUND AT FR41. BEAM REPAIRED WITH A DOUBLER

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

CF3, LH OMEGA BEAM #6 CRACK SUSPECTED FOUND AT FRAME 51 ON FLOOR STRUCTURE. CF3, LH OMEGA BEAM #6 CRACK FOUND AT FRAME 51 ON FLOOR STRUCTURE. BEAM REPAIRED WITH A DOUBLER.

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

CF2, CORROSION AND (3X) SUSPECTED CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BETWEEN FR 24-30. CF2, CORROSION (LEVEL 1) AND 3 CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 24-30. BEAM IS REPAIRED WITH 3 DOUBLERS

Part: NONE — NONE · corrosion level 2 · airframe 39,387 hrs · 25,263 cycles

CORROSION FOUND ON L GUSSET IN TOILET AREA BTW FR 59-61. CF4, CORROSION FOUND ON LH GUSSET IN TOILET AREA BTW FR 59-61. AFTER INVESTIGATION, CORROSION FOUND ON OMEGA BEAM AT FR 59 & 61. BEAM REPAIRED WITH 2 DOUBLERS

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

CF2, CORROSION AND (3X) SUSPECTED CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BETWEEN FR 29-36. CF2, CORROSION (LEVEL 1) AND 3 CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 29-36. BEAM IS REPAIRED WITH 3 DOUBLERS

Part: NONE — NONE · corrosion level 2 · airframe 39,387 hrs · 25,263 cycles

CORROSION ON REAR FUSE 2 LOWER SKIN, BTW FR 80-81 AND BTW STR 19L-21L. CORROSION ON REAR FUSE 2 LOWER SKIN BTW FR 80-81 AND BTW STR 19L-21L. SKIN IS REPAIRED WITH A DOUBLER.

Part: NONE — NONE · corrosion level 2 · airframe 39,387 hrs · 25,263 cycles

AT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-69. AT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-69, SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN · airframe 39,387 hrs · 25,263 cycles

RF1, LH FR68 REINFORCEMENT BRACKET CARGO DOOR HOLDER FOUND CRACKED. AFTER INVESTIGATION, A CRACK IS FOUND ON Z FRAME. Z FRAME SPLICED

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

CRACKS SUSPECTED (14X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. CRACKS SUSPECTED ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 4 CRACKS FOUND. INSTALLED REPAIR DOUBLER AT FR 78 AND BTW STR 5L-7L.

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

REPAIR DOUBLER TO REWORK ON CENTER FUSE 4 UPPER SKIN, BTW FR 56-57 AND BTW STR 2L-1R. REPAIR DOUBLER ON CENTER FUSE 4 UPPER SKIN, BTW FR 56-57 AND BTW STR 2L-1R

Part: NONE — NONE · airframe 39,387 hrs · 25,263 cycles

DENTS ON CENTER FUSE I LOWER SKIN, BTW FR 17-19 AND BTW STR 21L-21R. ON CENTER FUSE I, LOWER SKIN, BTW STR 21L-21R DENT FOUND OUT OF LIMIT. ON CENTER FUSE 1, LOWER SKIN BTW FR 17-19 AND BTW STR 21L-21R DENT REPAIRED WITH A DOUBLER. SURFACE REPROTECTION COVERED.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · corrosion level 2 · airframe 39,387 hrs · 25,263 cycles

CF1, CORROSION FOUND ON RH OMEGA BEAM AT FR 23 ON FLOOR STRUCTURE AREA. CORROSION ON RH OMEGA BEAM AT FR 23 AROUND NUTPLATE BLENDED OUT OF LIMTIS. RH OMEGA BEAM AT FR 23 ON FLOOR STRUCTURE REPAIRED

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 39,387 hrs · 25,263 cycles

DENT ON LH CENTER FUSE 1 SKIN, BTW FR 22-23 AND BTW STR 12L-13L. ON LH CENTER FUSE 1, DENT BTW FR 22-23 AND BTW STR 12L-13L FOUND OUT OF LIMITS. LH CENTER FUSE, BTW FR 22-23 AND STR 12L-13L EXTERNAL SKIN, DENT REPAIRED WITH A DOUBLER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,911 hrs · 24,835 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT BPS1. LIGHTS ONLY MOMENTARILY CAME ON. REMOVED AND REPLACED NEWLY INSTALLED POWER SUPPLY AT BPS1. OPS CHECK GOOD

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,911 hrs · 24,835 cycles

AFT OVERWING EMERGENCY EXIT PLACARD INOPERATIVE. REMOVED AND REPLACED INVERTER #4. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,911 hrs · 24,835 cycles

FWD & MIDDLE AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT BPS1. LIGHTS ONLY MOMENTARILY CAME ON. REMOVED AND REPLACED NEWLY INSTALLED POWER SUPPLY AT BPS1. OPS CHECK GOOD

Part: LAMP — INOPERATIVE · airframe 38,318 hrs · 24,294 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: NONE — NONE · airframe 36,669 hrs · 22,820 cycles

EXISTING DOUBLER BETWEEN FRAMES 15 AND 16 BETWEEN STRINGERS 10R AND 11R. REPAIR WAS ACCOMPLISHED

Part: NONE — NONE · airframe 36,669 hrs · 22,820 cycles

CIRCULAR REPAIR DOUBLER INCORRECTLY INSTALLED ON FORWARD FUSELAGE PRESSURE BULKHEAD. INSTALLED DOUBLER ON FWD BULKHEAD AFT SIDE.

Part: NONE — NONE · airframe 36,669 hrs · 22,820 cycles

FUSELAGE EXISTING REPAIR LOCATED BETWEEN FRAMES 19-20 STGR 2-4R. REMOVED DOUBLER AND REPAIRED CENTER FUSELAGE I SKIN AT FR 19-20 AND STGR 2-4R.

Part: NONE — NONE · airframe 36,669 hrs · 22,820 cycles

EXISTING DOUBLER BETWEEN FRAMES 70-72 + AND BETWEEN STRINGER 11-14L. REMOVED DOUBLER AND REPAIRED REAR FUSELAGE SKIN BETWEEN FRAMES 70-72 AND STRINGERS 11L-14L.

Part: NONE — NONE · airframe 36,669 hrs · 22,820 cycles

RECOMPLY WITH EC5310-01446 IN FORWARD AVIONICS BAY. RECOMPLIED WITH EC5310-01446 IN FORWARD AVIONICS BAY

Part: CONTROL MODULE — SMOKE (CABIN LIGHTS) · airframe 36,650 hrs · 22,805 cycles

IAH FLIGHT 3907. THE CREW REPORTED AN ELECTRICAL SMOKE ODOR IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,293 hrs · 22,462 cycles

RH FLOOR SILL CORRODED FROM FRAME 29-35. REMOVED AND REPLACED RH FLOOR SILL FRAME 29-35 IAW EMB SRM 51-40-02.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,293 hrs · 22,462 cycles

FRAME #2 DAMAGED AT STRINGER 14L-16L. REMOVED AND REPLACED FRAME #2 AT STRINGER 14L-16L IAW EMB 145XR SRM 51-40-02 & 51-20-03.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 36,293 hrs · 22,462 cycles

FRAME #3 DAMAGED AT STRINGER 14L-16L. REMOVED AND REPLACED FRAME #3 AT STRINGER 14L-16L IAW EMB 145XR SRM 51-40-02 & 51-20-03.

Part: WIRE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,922 hrs · 22,245 cycles

DURING ROUTINE MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE.MAINTENANCE REPAIRED SERVICE DOOR LIGHT WIRING. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,300 hrs · 20,965 cycles

PILOT REPORTED "EMERGENCY LIGHT OVER FA JUMPSEAT NOT WORKING". MX REMOVED AND REPLACED EMERGENCY EXIT WARNING SIGN OVER FA JUMPSEAT. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — DEFECTIVE (SPOILER) · airframe 27,489 hrs · 16,186 cycles

SPOILER FAIL ILLUMINATED ON DECENT WITH THRUST LEVERS AT IDLE. R & R SPOILER CONTROL UNIT IAW EMB 145 27-63-02. OPS CK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · corrosion level 2 · airframe 24,379 hrs · 14,108 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01950. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 24,379 hrs · 14,108 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: FLOOR SUPPORT — CORRODED (FRAME 59) · corrosion level 2 · airframe 24,379 hrs · 14,108 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01950. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-24) · corrosion level 2 · airframe 24,379 hrs · 14,108 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23-24. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01785. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 23,991 hrs · 13,867 cycles

CREW REPORTED THAT THE NR 1 PFD BLANKED OUT TRIPPING THE CIRCUIT BREAKER. CAUTIONS WERE CHECKED AND A STRONG ELECTRICAL ODOR WAS DETECTED. MAINTENANCE R & R THE AFFECTED PFD, OPS TESTED WITH NO DEFECTS. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,210 hrs · 13,386 cycles

CREW REPORTED EMERGENCY LIGHT IN CABIN DOES NOT WORK. MAINTENANCE INSPECTED THE ACFT, RESET THE EMERGENCY LIGHTS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 22,116 hrs · 12,660 cycles

PILOT REPORTED A RT WING FUEL LEAK AND PERFORMED AIR RETURN. MX INSPECTED AND FOUND THE RT WING OUTERMOST FLAP VALVE LEAKING. MX R & R THE RT WING FLAP VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK, STRINGER 21R CORRODED BETWEEN FRAMES 12 AND 13. MX R & R STRINGER 21R SECTION BETWEEN FRAME 9-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK FUSELAGE CRACKED AROUND RIVET AT FRAME 79, STRINGER 5L-6L. MX PERFORMED REPAIR OF FUSELAGE SKIN IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK RT GROUND SPOILER ACTUATOR UPPER ATTACHMENT BRACKET HAS MIGRATING HAT BUSHING. MX R & R RT GROUND SPOILER ACTUATOR UPPER INBD BUSHING IAW EC5750-01415 REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 79, STRINGER 3L-4L. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 79, STRINGER 3L-4L IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK, FUSELAGE CRACKED AROUND RIVET AT FRAME 75, STRINGER 2L-3L. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 75, STRINGER 2L-3L IAW EC5330-02353. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK LAV CENTER OMEGA BEAM BUTTSTRAP CORRODED (LEVEL 1 LOCAL) AROUND NUTPLATE AT FRAME 59. MX R & R LAV CENTER OMEGA BEAM BUTTSTRAP AT FRAME 59 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK LT INTERCOSTAL SUPPORT BETWEEN FRAMES 12 AND 13, STRINGER 20L-21L CORRODED (LOCAL LEVEL 2). MX R & R LT INTERCOSTAL BETWEEN FRAMES 12-13 STRINGER 21L-20L IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LOCAL LEVEL 2) IN RADIUS (2 PLACES) FRAME 20. MX R & R CENTER OMEGA BEAM AT FRAME 20 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK FRAME 65 CLIP AT CARGO DOOR LOWER BEAM CORRODED (LOCAL LEVEL 2). MX R & R FRAME 65 CLIP REPAIR BETWEEN STRINGER 16L-17L IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK, STRINGER 21L HAS LEVEL 2 CORROSION BETWEEN FRAMES 12 AND 13. MX R & R STRINGER 21L SECTION BETWEEN FRAME 29-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK, CARGO FWD TRIANGLE AT FRAME 65 HAS LEVEL 2 CORROSION AROUND NUT PLATE. MX REPAIRED AND REINSTALLED CARGO FWD TRIANGLE AT FRAME 65 IAW EC5320-01479 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

DURING C-CHECK RT INTERCOSTAL SUPPORT BETWEEN FRAME 12-13 STRINGER 20R AND 21R CORRODED (LOCAL LEVEL 2). MX R & R RT INTERCOSTAL BETWEEN FRAMES 12-13 STRINGER 21R-20R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 18,673 hrs · 10,363 cycles

SHV-DURING C-CHECK LAV RT OMEGA BEAM BUTTSTRAP CORRODED (LOCAL LEVEL 2) AROUND RIVETS AND UNDER CARBON CROSS BEAM AT FRAME 61. MX R & R THE LAV RT OMEGA BEAM BUTTSTRAP BETWEEN FRAMES 59-61 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 16,894 hrs · 9,330 cycles

MCI - FLIGHT 6119, DURING CRUISE FLIGHT THE CREW REPORTED A BLEED ONE OVERTEMP WARNING. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE FAN AIR THERMOSTAT, AND FAN AIR VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 16,894 hrs · 9,330 cycles

MCI - FLIGHT 6119, DURING CRUISE FLIGHT THE CREW REPORTED A BLEED ONE OVERTEMP WARNING. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE FAN AIR THERMOSTAT, AND FAN AIR VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 16,761 hrs · 9,221 cycles

MCI - FLIGHT 6176, DURING CRUISE THE CREW REPORTED A HSV1 FAIL MESSAGE. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE HSV, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,188 hrs · 8,759 cycles

MX FOUND ROW 12 CEILING EXIT SIGN NOT ILLUMINATING. REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 16,140 hrs · 8,719 cycles

LAV SMOKE ON TAKEOFF CLIMB. REMOVED AND REPLACED NR 1 ENGINE IAW T/C 6271001. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: DISPLAY — SHORTED (COCKPIT) · airframe 15,235 hrs · 8,200 cycles

IAH - FLIGHT 2123 THE CREW REPORTED THE NR 1 PFD HAS A BURNING SMELL AND IS POPPING THE CIRCUIT BREAKER. MAINTENANCE REMOVED AND REPLACED THE PFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — INOPERATIVE (SMOKE WARNING) · airframe 15,001 hrs · 8,076 cycles

FLIGHT 2224 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION WOULD NOT TEST. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 13,677 hrs · 7,335 cycles

SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS FROM FRAMES 78-79 AND STRINGERS 3-11R. MAINTENANCE REMOVED THE CRACKS BY REAMING AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02194. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (SPOILER) · airframe 13,677 hrs · 7,335 cycles

SHV - DURING C-CHECK THE LT GROUND SPOILER O/B HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE WORN HINGE IAW EMB 145XR AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (EXTINGUISH SYS) · airframe 11,356 hrs · 6,122 cycles

FLIGHT 2052 - EWR - FLIGHT CREW REPORTED BAGG FIRE EXTINGUISHER SYSTEM NO TEST. EWR MX REMOVED AND REPLACED RELAY H18 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRANSPONDER — INOPERATIVE · airframe 10,886 hrs · 5,875 cycles

FLIGHT 3146 - RIC - FLIGHT CREW REPORTED COMM 1 WENT TO DASHES AND INOPERATIVE IN FLIGHT. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFULLY. RIC MX REMOVED AND REPLACED COMM UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SUMP — LEAKING (NR 1 ENGINE) · airframe 9,846 hrs · 5,304 cycles

ECTM WORKSHEET ISSUED BY EXPRESSJET ENGINEERING TO REMOVE AND REPLACE NR 1 ENGINE DUE TO HAZE/ODOR IN THE CABIN. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. TEAR DOWN REPORT FROM ROLLS ROYCE SHOWED LEAKAGE FROM THE COOL FRONT SUMP ON THE NR 1 ENGINE.

Part: CARBON SEAL — MALFUNCTIONED (NR 2 ENGINE) · airframe 9,628 hrs · 5,185 cycles

DURING SCHEDULED MAINTENANCE THE NR 2 ENGINE WAS FOUND TO BE THE SOURCE OF SMOKE ACCUMULATING IN THE PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED THE ENGINE TO CORRECT THE DISCREPANCY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR CLOSED.

Part: CLAMP — MISSING (DUCT) · airframe 9,543 hrs · 5,127 cycles

FLIGHT 2291. FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX FOUND V-BAND COUPLING AND METAL GASKET SEALING ELEMENT MISSING ON LT COMPRESSOR TUBE. MX REPLACED GASKET AND V-BAND COUPLING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 9,450 hrs · 5,079 cycles

PIT - FLIGHT 2529, DURING CLIMB THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE ACFT RETURNED TO PIT WHERE IT LANDED WITHOUT INCIDENT. CONTRACT MX INSPECTED THE ACFT AND RAN THE ENGINES WITH THE CREW AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

FLT MX - ONT - WHILE PERFORMING 1A CHECK AND OPERATIONALLY CHECK EMERGENCY LIGHTS THE FWD EXIT SIGN AT ROW 12 DID NOT FULLY ILLUMINATE. MX REMOVED AND REPLACED FWD EXIT SIGN AT ROW 12. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 6,978 hrs · 3,755 cycles

FLT 0001 - ONT - FLIGHT CREW REPORTED LAV SMOKE INDICATION DURING CLIMB. NO VISIBLE SMOKE. AIRCRAFT RETURNED TO BLOCK WITHOUT INCIDENT, EMERGENCY WAS NOT DECLARED. MX PERSONNEL INSPECTED AND FOUND NO DEFECTS. OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (LAVATORY) · airframe 6,959 hrs · 3,744 cycles

AUS - FLIGHT 1, THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT. THE AIRCRAFT RETURNED TO AUS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT CLAMP — DEFECTIVE (ENGINE) · airframe 6,867 hrs · 3,694 cycles

FLT 22 ONT - FLIGHT CREW REPORTED ON CLIMB FROM ONT-E2 HIGH ITT - CANNOT MAINTAIN POWER. FLIGHT CREW RETURNED TO BLOCK AND DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED 14TH STAGE COMPRESSOR DISCHARGE TUBE V-BAND CLAMP OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 4,024 hrs · 2,144 cycles

IAD - ROUTINE CHECK FOUND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY LIGHT BATTERIES IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.

Part: HANDLE — MALFUNCTIONED (EMERGENCY EXIT) · airframe 2,386 hrs · 1,265 cycles

IAH - FLIGHT 2048, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE CAPTAINS EMERGENCY EXIT RED HANDLE WOULD NOT OPEN. MAINTENANCE INSPECTED THE EMERGENCY EXIT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 1,801 hrs · 956 cycles

IAH - FLIGHT 2623, THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE EN ROUTE TO IAH FOLLOWED BY SMELL OF BURNING WIRES AND CAPT PFD WENT FULL BRIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION, WITH NO DEFECTS NOTED, REMOVED AND REPLACED THE CAPTAINS PFD, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.