N27962

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,105 hrs · 28,704 cycles

DURING PREFLIGHT, THE CREW REPORTED THAT THE EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,564 hrs · 28,289 cycles

DURING MX INSPECTION, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT SYS BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN LIGHT) · airframe 37,427 hrs · 28,186 cycles

THE CREW REPORTED SIDEWALL LIGHT FIXTURE BURNED AT ROW 9A. MAINTENANCE REPLACED SEAT 9A LIGHT HARNESS. OPS CHECKS WERE GOOD.

Part: TORQUE BOX — DAMAGED (ZONE 500) · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, LT NR 1 UPPER INBD TORQUE BOX BOLT HOLE DAMAGED. REPAIRED IAW EC5710-01202, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, CORROSION AROUND MAIN DOOR LOWER NUTPLATES. REPAIRED IAW EC5210-01154, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, FRAME 65 CORRODED AT NUT PLATES AT STRINGER 14-15L. R & R FRAME 65 DOUBLER IAW SRM 51-40-02 AND EC5310-01505, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, SERVICE DOOR HAS CORROSION AROUND LOWER NUTPLATES. REPAIRED IAW EC5210-01154, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, LT FWD LOWER ENGINE YOKE FWD FITTING CRACKED. REPAIRED IAW EC5450-01071. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CHAFED (ZONE 200) · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, FRAME 60 CHAFED AT STRINGER 5L. REPAIRED IAW EC5310-01695. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 200) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK INTERNAL SKIN CORRODED. FRAMES 13-14, STRINGERS 20L-20R. REPAIRED IAW EC5320-01777. ACFT APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, SERVICE DOOR LOWER AFT CUTOUT CORRODED FRAME 22. MX INSTALLED AND FABRICATED DOUBLER IAW EC5310-01373. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, AFT LOWER CARGO DOOR CUTOUT SHEAR CLIP CORRODED FRAME 68. MX R & R SHEAR CLIP IAW SRM 51-40-02 AND EC5320-01494. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK FWD LOWER CARGO DOOR CUTOUT SHEAR CLIP CORRODED FRAME 65. MX R & R SHEAR CLIP IAW SRM 51-40-02 AND EC5320-01494, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (ZONE 100) · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK, EXTERNAL FUSELAGE DENTED BETWEEN FRAMES 75-76, STRINGERS 17-18R. REPAIRED IAW EC5330-02731, REV A. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 900) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 20-22 AND STRINGERS 15R-16R. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,325 hrs · 25,831 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,735 hrs · 25,374 cycles

DURING MX INSPECTION THE ROW 3 TO 5 FLOOR EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MX R & R THE LIGHT STRIP WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,006 hrs · 24,776 cycles

RT OVERWING EXTERIOR AFT EMERGENCY LIGHT FOUND INOP. MX R & R NR 5 EMERGENCY LIGHT INVERTER WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 31,347 hrs · 23,467 cycles

DURING ROUTINE MX, THE LAST AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MX REPAIRED THE EMERGENCY LIGHT STRIP CONNECTOR. OPS CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — INTERMITTENT (SPOILERS) · airframe 31,182 hrs · 23,323 cycles

DURING FLIGHT THE CREW RECEIVED A SPOILER FAIL MESSAGE AND PERFORMED AN EMERGENCY DESCENT. WHERE THE ACFT LANDED WITHOUT INCIDENT. MX REPLACED A SPOILER PROXIMITY SWITCH, PERFORMED SUCCESSFUL OPS CHECKS AND CLEARED THE DISCREPANCY.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,944 hrs · 23,144 cycles

DURING PREFLIGHT INSPECTION, THE CREW FOUND THE AFT SECTION OF FLOOR PATH LIGHTING TO BE INOPERATIVE. MX REPLACED THE NR 6 EMERGENCY LIGHT INVERTER, PERFORMED A SYS OPS CHECK AND CLEARED THE DISCREPANCY.

Part: CONTROL PANEL — FAULTY (SMOKE DETECTION) · airframe 30,841 hrs · 23,068 cycles

THE CREW REPORTED A LAV SMOKE WARNING MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE SMOKE DETECTOR CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,278 hrs · 22,659 cycles

DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE AT SEAT 8&9. MAINTENANCE REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DIRTY (LANDING GEAR) · airframe 29,366 hrs · 21,974 cycles

TYS POST C-CHECK TEST FLIGHT- AFTER TAKEOFF L/G LEVER WOULD NOT GO UP AND MULTIPLE EICAS MESSAGES. A/C AIR RETURNED WITHOUT INCIDENT. MX REMOVED CLEANED AND RE-INSTALLED WEIGHT ON WHEELS PROX SWITCH CONNECTOR AND OPS CHECKED GOOD. SECOND TEST FLIGHT SATISFACTORY.

Part: BALLAST — OVERHEATED (CABIN) · airframe 28,725 hrs · 21,484 cycles

IAH - FLIGHT 2277, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL IN THE GALLEY AREA. MAINTENANCE REMOVED AND REPLACED THE BALLAST AT SEAT 3BC, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 28,552 hrs · 21,360 cycles

FLIGHT 2734, OMA - IAH, AFTER TAKEOFF THE CREW REPORTED A BLEED ONE LEAK INDICATION AND ELECTED TO DIVERT TO LNK WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING OF THE SYSTEM AND DETERMINED THAT THERE WAS NOT A BLEED LEAK HOWEVER THE AIRCRAFT WAS RELOCATED TO CLE WHERE ADDITIONAL TROUBLESHOOTING COULD BE PERFORMED. IN CLE SYSTEM OPERATIONAL CHECKS WERE PERFORMED HOWEVER THE CONDITION COULD NOT BE DUPLICATED NOR DID THE WARNING INDICATION RE-APPEAR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,665 hrs · 20,690 cycles

FLIGHT 2084 - EWR - DURING ROUTINE INSPECTION, EWR MX FOUND EMERGENCY LIGHT STRIP INOPERATIVE. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UPLOCK — INOPERATIVE (RT MLG) · airframe 27,124 hrs · 20,275 cycles

FLIGHT 2545 - ALB - FLIGHT CREW REPORTED BANGING NOISE WHEN GEAR RETRACTED. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT MLG UPLOCK BOX AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG DOOR) · airframe 26,564 hrs · 19,879 cycles

FLIGHT 2814 - EWR - FLIGHT CREW REPORTED AIR GROUND FAIL INDICATION ON EICAS WHEN LANDING GEAR COMES DOWN. EWR MX REMOVED AND REPLACED NLG DOOR ACTUATOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LANDING GEAR) · airframe 26,459 hrs · 19,801 cycles

FLIGHT 3001 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MSG ON EICAS. EWR MX CLEANED AND RE-SECURED ALL PROX SWITCHES AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 26,325 hrs · 19,701 cycles

FLIGHT 3054 - DTW - FLIGHT CREW REPORTED SMELL SEEMED TO BE COMING FROM 4TH SEAT ROW OVERHEAD, IT DID NOT CHANGE WITH PACK ON OR OFF. MX REMOVED AND REPLACED OVERHEAD CEILING BALLAST NR 4 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR — STUCK (MAIN PAX) · airframe 25,889 hrs · 19,371 cycles

FLIGHT 2504 - JAX - FLIGHT CREW REPORTED PAX DOOR WILL NOT OPEN FROM INSIDE. MX VERIFIED DOOR OPERATION AND COULD NOT DUPLICATE THE PROBLEM ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ROLLER — FAULTY (PAX DOOR) · airframe 25,796 hrs · 19,293 cycles

PAX DOOR HARD TO CLOSE. REMOVED AND REPLACED AFT PAX DOOR ROLLER IAW EMB 145 AMM 53-21-02 AND RIGGED DOOR IAW AMM 52-18-00. OPS CHECK GOOD.

Part: SEAL — DIRTY (CABIN DOOR) · airframe 25,121 hrs · 18,775 cycles

FLIGHT 2893 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN AND CLOSE. EWR MX CLEANED CABIN DOOR SEAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL PANEL — CORRODED (CABIN) · airframe 24,823 hrs · 18,546 cycles

FLIGHT 2548 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHTS INTERMITTENT. EWR MX CLEANED OFF CORROSION FROM F/A CONTROL PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — DEFECTIVE (LT WING) · airframe 24,810 hrs · 18,536 cycles

FLIGHT 2812 - AMA - FLIGHT CREW REPORTED THAT TOWER NOTIFIED THAT ACFT WAS LEAKING FUEL FROM LEFT WING. CREW PROCEEDED WITH AIR RETURN AND LANDED ACFT UNEVENTFULLY. MX REMOVED AND REPLACED FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN SERVICE.

Part: FLAPPER VALVE — LEAKING (LT WING) · airframe 24,810 hrs · 18,537 cycles

AMA - FLIGHT 2812, DURING TAKEOFF THE CREW REPORTED A SUSPECTED FUEL LEAK FROM THE LT WING. THE AIRCRAFT RETURNED TO AMA WHERE IT LANDED WITHOUT INCIDENT. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LEFT FLAPPER VALVE, OPERATIONAL AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (RT AILERON) · airframe 24,710 hrs · 18,463 cycles

RT AILERON OUTBOARD PCA ROD BRACKET OUTBOARD BUSHING HOLE IS OUT OF LIMITS. REMOVED AND REPLACED PCA FITTING IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.

Part: BALLAST — BURNED (GALLEY) · airframe 23,182 hrs · 17,349 cycles

IAH - FLIGHT 2247 - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL FROM THE GALLEY AREA. MAINTENANCE REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: UNKNOWN — ODOR (CABIN) · airframe 22,675 hrs · 17,006 cycles

FLIGHT 2623 - YOW - FLIGHT CREW REPORTED STRANGE FUEL SMELL IN CABIN ROWS 8/9. CONTRACTED MAINTENANCE PERFORMED EVALUATION AND COULD NOT DUPLICATE ANY ODOR. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,302 hrs · 16,774 cycles

RIGHT EMERGENCY EXIT DOOR LIGHT STRIP INOP. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-13, OPS CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 21,740 hrs · 16,407 cycles

TYS - CREW REPORTED SMOKE AND A BURNING SMELL IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE LT SIDEWALL BALLAST IAW EMB 145 AMM 33-21-03, OPS CHECKS GOOD AND WAS RELEASED TO SERVICE.

Part: CONTROL UNIT — SHORTED (CABIN) · airframe 21,738 hrs · 16,406 cycles

IAH - FLIGHT 2380, DURING PREFLIGHT INSPECTION THE CREW REPORTED SMOKE AND A BURNING SMELL FROM THE PASSENGER SERVICE UNIT ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE CONTROL MODULE, INOPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,725 hrs · 16,399 cycles

RIGHT EMERGENCY ESCAPE HATCH LOWER EXIT SIGN IS INOP. REPLACED RIGHT EMERGENCY ESCAPE HATCH LOWER EXIT SIGN IAW EMB 145 AMM 33-50-11- OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — BURNED (CABIN) · airframe 21,008 hrs · 15,861 cycles

IAH - FLIGHT 2481, ON POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LIGHT ASSEMBLY ABOVE SEAT 6A, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,279 hrs · 15,338 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 24-25. MX REPAIRED LT OMEGA BEAM BETWEEN FR 24-25 IAW EMB 145 SRM 53-00-01 FIG 202. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,279 hrs · 15,338 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 20,279 hrs · 15,338 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,566 hrs · 13,965 cycles

IAH - FLIGHT 2127, THE CREW REPORTED A FAINT BURNING SMELL IN COCKPIT ON TAKEOFFS AND ARRIVALS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, WINDSHIELD ELECTRICAL CONNECTORS, PITOT HEAT RELAYS, ETC WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,566 hrs · 13,965 cycles

IAH - FLIGHT 2080, THE CREW REPORTED THAT WHILE CLIMBING THROUGH 7,000 FEET NOTICED AN ACRID ODOR IN THE COCKPIT FOR 2-3 MINUTES, AND WHILE LEVEL AT 22,000 FEET THE ODOR RETURNED IN THE COCKPIT AND CABIN FOR 5-10 MINUTES, AND AGAIN WHILE DESCENDING THROUGH 10,000 FEET THE ODOR WAS NOTICED AGAIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE PACKS OFF BOTH THE ENGINES AND APOU WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDSHIELD — ARCED (COCKPIOT) · airframe 17,014 hrs · 12,757 cycles

CLE FLIGHT NR 3263, THE CREW REPORTED AFTER TAKEOFF A ELECTRICAL BURNING SMELL WAS NOTED AROUND THE CAPTAINS GLARESHIELD. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,101 hrs · 12,044 cycles

STL - FLIGHT 2764, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE NR 6, 7 & 8 AISLE PATH LIGHTING STRIP WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 6 INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FR 18) · airframe 15,837 hrs · 11,841 cycles

TYS - DURING A SCHEDULED INSPECTION, A CRACK INDICATION WAS FOUND ON THE OUTBOARD UPPER DOOR STOP HOLE AT FRAME 18, STRINGER 14L, CRACK IS AT 9 O'CLOCK HOLE POSITION AND GREATER THAN 50 PERCENT OF STANDARD DEFLECTION. MAINTENANCE REAMED THE DOOR STOP HOLE IAW EA5310-01054 AND EC5310-01351 AND CRACK INDICATION WAS REMOVED.

Part: BLEED VALVE — BYPASSING (APU) · airframe 14,677 hrs · 10,920 cycles

CLE - THE CREW REPORTED A STRONG FUEL SMELL AFTER THE APU WAS STARTED. MAINTENANCE REMOVED AND REPLACED THE APU BLEED VALVE AND THE OPERATIONAL CHECKS WERE GOOD, AND NO FUEL SMELL WAS DETECTED.

Part: WIRE — BROKEN (MLG) · airframe 14,282 hrs · 10,612 cycles

CLE FLIGHT NR 3329 - THE CREW REPORTED THE LANDING GEAR WARNING CAME ON EVERY TIME THE THRUST LEVERS WERE REDUCED ABOVE 15,000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE. MAINTENANCE REPAIRED WIRE NR W001-0643-24 AND OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — SHORTED (COCKPIT)

DTW FLIGHT 2136, THE CREW REPORTED SMOKE IN THE COCKPIT WHEN WINDSHIELD HEAT TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.

Part: FILTER — DIRTY (NR 2 ENGINE)

CLE FLIGHT 3231 THE CREW REPORTED A ENGINE NR 2 FUEL IMPENDING BYPASS WARNING. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE AND REPLACED THE FUEL FILTER AND IMPENDING BYPASS INDICATOR. OPERATIONAL CHECKS WERE GOOD.

Part: FITTING — DAMAGED (VERTICAL STAB) · airframe 11,519 hrs · 8,464 cycles

TYS AFTER REAMING THE RT VERTICAL STAB SPHERICAL BEARING CASTING, THE HORIZ STAB FAIL THE DIHEDRAL CHECK. REMOVED AND REPLACED THE RT VERTICAL HINGE FITTING IAW EC 5510-01067 C/W BACKLASH CHECK IAW EMB 145 AMM27-40-00; C/W INCIDENCE AND DIHEDRAL CHECKS IAW EMB 145-AMM 51-50-01; ALSO C/W A TEST FLIGHT TO ASSURE ALL FLIGHT CONTROLS WERE IN A SAFE MANNER. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: GUSSET — CORRODED (FLOORBEAM) · airframe 11,519 hrs · 8,464 cycles

DURING A SCHEDULED 3C INSPECTION THE GUSSET ON THE RT FLOORBEAM FOR PANEL 247AF WAS CORRODED. MAINT REMOVED OLD GUSSET AND FAB A NEW GUSSETT. ALODINED, PRIMED AND INSTALL NEW FAB GUSSET IAW EMB 135/145 SRM 51-40-04 AND 51-40-06, CPM 51-21-04-05-06 AND SRM 51-40-02. ALL WORK WAS ACCOMPLISH AND WILL BE REL UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED (FUSELAGE) · airframe 11,518 hrs · 8,464 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CARGO DOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB SRM 51-20-03 AND 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 11,518 hrs · 8,464 cycles

TYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND GALLEY FLOORBEAM DOUBLER AT FRAME 20 AND 22. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW EMB SRM 51-30-01, 51-40-02 AND CPM 51-21-04, 05, 06. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,518 hrs · 8,468 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE LT OMEGA BEAM WAS FOUND CORRODED. MAINT REMOVED CORRODED AREA, FABRICATED A NEW DOUBLER AND INSTALLED FILLER, SHIMS, PLATE AND DOUBLER. ALODINED, PRIMED AND REPAINTED WORK AREA. REINSTALLED RAMP ANGLE. ALL WORK WAS ACCOMPLISHED IAW EMB 135/145 SRM 51-21-04; 51-40-02 AND EMB 135/145 CPM51-21-04/05/06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,518 hrs · 8,468 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE CENTER OMEGA BEAM AT FR 20 WAS CORRODED. MAINT INSTALLED A NEW OMEGA BEAM IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,518 hrs · 8,464 cycles

TYS DURING A SCHEDULED 3C INSPECTION THE RT SIDE OF THE RAMP ANGLE WAS FOUND CORRODED. MAINT REMOVED AND REPLACED THE RAMP ANGLE IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: UPLOCK — INOPERATIVE (LT MLG)

IAH- MAINTENANCE NOTED THAT THE LANDING GEAR INDICATION DISAGREES WITH THE LEVER. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK BOX,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

CLT DURING PREFLIGHT INSPECTION THE CREW FOUND CABIN EMERGENCY LIGHTS TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER AND OPERATIONALLY CHECKED THE LIGHTING SYSTEM. THE SYSTEM TESTED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — LIGHTNING STRIKE (ELEVATOR) · airframe 10,877 hrs · 7,937 cycles

A/C 962 WAS FERRIED TO TYS AFTER A PRELIMIARY INSPECTION FOUND A/C SATISFACTORY FOR A FERRY FLIGHT. MAINTENANCE REMOVED AND REPLACED THE RT ELEVATOR TRAILING EDGE FITTING; CUT OUT THE DAMAGED AREA AND FAB A DOUBLER, FILLER AND INSTALLED; ALODINED PRIMED AND PAINTED REPAIR DOUBLER AND FILLER IAW IC2003-145/2448 AND 51-40-02, AS WELL AS 135/145 CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE REL UPON COMPLETION OF ALL WORK. PERFORMED A LIGHTNING STRIKE INSPECTION, ALL SERVICEABLE.

Part: MODULE — FAULTY (COCKPIT) · airframe 10,311 hrs · 7,489 cycles

EWR---CO2306, CREW REPORTED AUTO PRESSURIZATION FAILURE IN FLIGHT. AFTER DUMPING QRH AND TAXIING TO MAINTENANCE COULD NOT GET PRESSURIZATION TO STABILIZE IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED CABIN PRESS ACQUISION MODULE (CPAM) IAW EMB145 MM 21-32-01. OPS CHECKED AND LEAK CHECKED GOOD IAW EMB145 MM 21-31-01 AND 34-13-00. AUTO AND MANUAL MODES OF PRESSURIZATION OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LEVER — FAULTY (MLG) · airframe 10,215 hrs · 7,413 cycles

CREW REPORTED "AFTER TAKEOFF FROM PHL ENROUTE TO CLE, LANDING GEAR WOULD NOT RETRACT. HANDLE WORKED FINE. (DIVERTED TO EWR, LANDED UNEVENTFULLY) POST FLIGHT INSPECTION REVEALED NO GEAR PINS IN LANDING GEAR." AIRCRAFT MAINTENANCE FERRIED TO BTV GEAR DOWN, MAINTENANCE REMOVED AND REPLACED LT NR 2 MAIN LANDING GEAR PROXIMITY SWITCH IAW EMB145 AMM, REMOVED AND REPLACED LGEU IAW EMB145 AMM AND REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM. OPS. CHECKED LANDING GEAR GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

THE CREW REPORTED A LANDING GEAR LEVER DISAGREE DURING GEAR EXTENSION. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — INOPERATIVE (#1 AIE COND. BAY)

IAH- FLIGHT 3906, THE CREW NOTED A STRONG SMOKE SMELL WHEN CLEARED INTO POSITION AND HOLD.SMELLED ELECTRICAL IN NATURE, AND, OCCURED AFTER ALL LIGHTS WERE TURNED ON. IAH- MAINTENANCE FOUND PACK #1 OVERHEAT MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE #1 ACM, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED (CABIN)

EWR FLIGHT 3324 THE CREW REPORTED A BURNING ODOR COMING FROM THE CABIN LIGHTS AT ROW 4 AND 5. MAINTENANCE INSPECTED AND REPLACED THE CABIN SIDEWALL LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LEVER — DEFECTIVE (COCKPIT) · airframe 8,698 hrs · 6,181 cycles

EWR---CO3869, CREW REPORTED, "AFTER T/O. LDG SELECTED UP. NOSE GEAR FAILED TO RETRACT. CYCLED GEAR AND MAIN GEAR FAILED TO RETRACT. CYCLED GEAR A SECOND TIME AND ALL GEAR FAILED TO RETRACT. AIRCRAFT AIR RETURNED TO EWR AND LANDED UNEVENTFULLY.....MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED LANDING GEAR LEVER CONTROL IAW EMB145 AMM REFERENCE #32-32-02. OPS.CHECKED GOOD IAW EMB145 AMM #32-32-00 ALSO, REFERENCE M-602 #513174. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (CABIN)

CLE FLIGHT NR 3275 THE CREW REPORTED THE EMERGENCY LIGHT ARMED INDICATION WAS NOT ON WHILE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING C-CK INSPECTION THE LEFT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED AND CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN ACCORDANCE WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAME 20L)

DURING C-CK INSPECTION THE FLOOR SUPPORT AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IN ACCORDANCE WITH THE EMB 145 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — BROKEN (APU)

GSP - FLIGHT 4205 - APU WILL NOT START, PILOT PLACED ON MEL, AND CONTINUED NORMAL FLIGHTS. DURING TROUBLESHOOTING, MAINTENANCE FOUND THE APU COMBUSTION HOUSING V-BAND CLAMP BROKEN. THE APU WAS REMOVED AND REPLACED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — CORRODED (RT EMER EXIT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE CLEANED CORROSION FROM THE LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FIRE LIGHT — ILLUMINATED (BAGG COMPT)

IAH - FLT 4210 - DURING TAXI TO GATE, THE CREW REPORTED THE BAGGAGE EXTINGUISHER LIGHT ILLUMINATED. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE BAGGAGE FIRE DETECTION SYSTEM VERIFYING NORMAL OPERATION IAW EMB145 MM 26-15-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY HAS NOT REPEATED TO-DATE. (X)