N16541

Part: BATTERY PACK — INOPERATIVE · airframe 43,922 hrs · 34,727 cycles

LH FWD WING/FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH FWD EMERGENCY LIGHT LAMP. OPS CHECK FAIL. SUSPECTED EMERGENCY BATTERY #1 NEEDS TO BE REPLACED. REMOVED AND REPLACED BPS #1. OPS CHECK SAT

Part: BATTERY PACK — INOPERATIVE · airframe 43,918 hrs · 34,723 cycles

MULTIPLE EMERGENCY LIGHTS AFT OF EXIT ROW ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK SAT.

Part: BRAKE ASSY — LEAKING · airframe 43,781 hrs · 34,605 cycles

HYD 1 LOW QUANTITY ADVISORY CAME ON IN CRUISE. TRANSFERRED HYDRAULIC FLUID FROM #2 SYSTEM TO #1 SYSTEM. DUE TO HYD 1 LOW ADVISORY MESSAGE, R&R OUTBOARD BRAKES. OPS CHECK SAT. LEAK CHECK GOOD.

Part: SEALANT — MISSING (RT MLG) · airframe 43,345 hrs · 34,186 cycles

SEALANT MISSING FROM RIGHT LANDING GEAR NUT WHERE MAIN BRACE STRUT AND LOWER SIDE ARM CONNECT. APPLIED SEALANT TO RLG NUT.

Part: ARMREST — CRACKED (SEAT 10A) · airframe 43,249 hrs · 34,098 cycles

ARMREST STRUCTURE CRACKED ON PAX SEAT 10A. REMOVED AND REPLACED SEAT 10A INBOARD ARMREST STRUCTURE (SPREADER).

Part: NONE — NONE · airframe 43,247 hrs · 34,097 cycles

FUSELAGE SKIN DAMAGED AT FR29 TO FR31 BETWEEN S12R TO S13R. REMOVED DAMAGED FUSELAGE SKIN STR 13R FR 29R TO 31R. LOCATED AND DRILLED REPAIR DOUBLER AND FILLER. TRIMMED AND DEBURRED REPAIR FILLER AND REPAIR DOUBLER AND COUNTERSUNK REPAIR DOUBLER. TREATED AND PRIMED REPAIR DOUBLER, REPAIR FILLER, AND BARE METAL AT REPAIR AREA ON FUSELAGE. INSTALLED DOUBLER AND FILLER. TOP COATED FASTENERS AND APPLIED CIC.

Part: SHEAR TIE — DAMAGED (ZONE 200) · airframe 43,247 hrs · 34,097 cycles

SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12R AND 13R. REPAIRED SHEAR CLIP AT FRAME 30 BETWEEN STRINGER 12 AND 13R BY STEPPING FASTENER SIZE HOLD UP 1/32 ORG HOLE SIZE IS 5/32 AND IS NOW 3/16. TREATED AND PRIMED FASTENER HOLE. INSTALLED FASTENER.

Part: SKIN — DAMAGED (ZONE 200) · airframe 43,247 hrs · 34,097 cycles

FUSELAGE SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R. REPAIRED CENTER FUSELAGE II SKIN DAMAGE AT FR29 TO FR31 BETWEEN S12R TO S13R.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,709 hrs · 32,772 cycles

THE CREW REPORTED AISLE PATH EMERGENCY LIGHT AFT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT AILSE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD

Part: ENGINE — LEAKING (NR 1) · airframe 40,641 hrs · 31,903 cycles

THE CREW REPORTED ON CLIMBOUT AT 6000 FEET LAV SMOKE WARNING ON EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE #1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL PANEL — FAULTY (SMOKE DETECT) · airframe 40,638 hrs · 33,697 cycles

THE CREW REPORTED @1000' LAV SMOKE MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR PANEL AMD OPERATIONAL CHECKS WERE GOOD.

Part: ACM — FROZEN (NR 1) · airframe 40,596 hrs · 31,863 cycles

IAH - THE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPEVCTED THE AIRCRAFT, REMOVED AND REPLACED THE #1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCTRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,137 hrs · 31,505 cycles

DURING MX INSPECTION THE ROW 18 CEILING AFT EXIT SIGN WAS FOUND INOP. MX INSTALLED CONNECTORS ON ROW 18 AFT EXIT SIGN WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FRAME 60) · corrosion level 2 · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE LT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 37,735 hrs · 29,579 cycles

DURING C-CHECK INSPECTION, THE UPPER FRAME 10 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED AT A RIVET LOCATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME SECTION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FRAME 60) · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE LEFT INBD FLOOR SUPPORT GUSSET WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND RPELACED THE AFFECTED GUSSET AND TYHE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT GUSSET AT FRAMES 60 - 61 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAME 24) · airframe 37,735 hrs · 29,579 cycles

DURING C-CHECK INSPECTION, THE CENTER FUSELAGE RT SKIN WAS FOUND WAS FOUND TO BE DENTED 3.5 INCH FWD OF FRAME 24 AND 1 INCH BELOW STRINGER 15R. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND INSTALLED A REPAIR DOUBLER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE CENTER AISLE CROSSBEAM SUPPORT AT FRAME 20 WAS FOUND TO HAVE BARE METAL AND CORROSION BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CRACKED (NLG) · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE NLG UPLOCK BOX CROSSBEAM WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (FRAME 72) · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, FRAME 72 WAS FOUND TO BE DAMAGED BETWEEN STRINGERS 15 & 16R. MAINTENANCE REMOVED THE DAMAGED.

Part: SKIN — DAMAGED (FRAME 68) · airframe 37,735 hrs · 29,579 cycles

DURING A C-CHECK INSPECTION, THE AFT FUSELAGE SKIN WAS FOUND TO HAVE A SMALL NICK AT FRAME 68 BETWEEN STRINGERS 10 & 11L. MAINTENANCE BLENDED THE AFFECTED AREA IAW ETD2017-145-045392, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 37,514 hrs · 29,404 cycles

A/C WAS IN FOR A ROUTINE CHECK WHEN INSPECTION FOUND THE AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE FOUND A BROKEN WIRE AND SPLICE THE WIRE BACK IAW SWPM 20-21-OO. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: LAMP — ARCED (LAVATORY LIGHTS) · airframe 35,036 hrs · 27,478 cycles

A BURNING PLASTIC ODOR REPORTED FROM THE GALLEY NEAR THE OVERHEAD LIGHT. MX R & R THE LIGHT BLUBS AT SEAT 1 A WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHTS) · airframe 33,899 hrs · 26,564 cycles

PILOT REPORTED THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE R & R THE F/A CONTROL PANEL ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — SHORTED (FLASHLIGHT) · airframe 33,833 hrs · 26,517 cycles

AN ELECTRICAL BURNING ODOR WAS REPORTED IN THE COCKPIT. MAINTENANCE PERFORMED INSPECTION OF COCKPIT AREA AND FOUND CAPTAIN`S FLASHLIGHT TO BE CAUSE AND PLACED ON MEL. MAINTENANCE R & R CAPTAIN`S FLASHLIGHT BATTERY WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: VALVE — ODOR (NR 1 ENGINE) · airframe 33,678 hrs · 26,401 cycles

PILOT REPORTED BLEED 1 & 2 OVERTEMP IN ICING THEN ODOR OF SOMETHING BURNING. MAINTENANCE R & R NR 1 ENGINE FAN AIR VALVE, FAN AIR THERMOSTATS 1 & 2, A HIGH STAGE PRESSURE SWITCH WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — NO TEST (EMERGENCY LIGHT) · airframe 32,296 hrs · 25,308 cycles

DURING ROUTINE MAINTENANCE, THE CEILING EMERGENCY EXIT LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE EXIT LOCATOR SIGN . OPS CHECKED GOOD.

Part: PITOT SYSTEM — CONTAMINATED · airframe 30,585 hrs · 23,977 cycles

CREW REPORTED AT FL 370 A NOTICEABLE ICE BUILD UP ON THE UNPROTECTED SURFACES AS WELL AS THE TAT. SHORTLY AFTER IAS AND ALT INSTRUMENTS BEGAN TO FAIL FOLLOWED BY A NR 2 PACK OVERHEAT MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND BEGAN AN IMMEDIATE DESCENT. DURING DESCENT, ENCOUNTERED NUMEROUS MASTER CAUTION MESSAGES INCLUDING RUDDER OVERBOOST, YAW DAMP FAIL, IC WOW1 INOPERATIVE. INSTRUMENTATION FUNCTIONALITY RETURNED BETWEEN FL200 AND 10,000 FT AND THE CREW ELECTED TO DIVERT, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECKS OF THE ANTI-ICE SYSTEM, RADIO COMM1 AND COMM 2, STALL PROTECTION SYSTEM, RUDDER OVERBOOST SYSTEM AND IC 600 COMPUTER. WATER WAS DRAINED FROM THE PITOT/STATIC LINES AND ADC SYSTEMS NR 1 AND NR 2 WERE RESET. AFTER ALL DISCREPANCIES WERE ADDRESSED THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,690 hrs · 23,323 cycles

DURING SCHEDULED MAINTENANCE INSPECTION, THE CENTER AISLE EMERGENCY LIGHTS FROM SEAT 1A-3A WERE FOUND INOPERATIVE. MAINTENCE R & R THE CENTER AISLE LIGHT STRIP WITH OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: NONE — NONE (EMEGENCY LIGHTS) · airframe 28,010 hrs · 22,007 cycles

THE CREW REPORTED EMERGENCY LIGHT NOT ARMED MESSAGE APPEARED WITH NO REASON. REPORTED 2 EMERGENCY LIGHTS WOULD NOT TURN ON. MX INSPECTED AND RESET ACFT SYS AND OPS CHECKS WERE GOOD. NO DEFECT FOUND.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,820 hrs · 21,853 cycles

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

Part: ATTACH FITTING — DAMAGED (VERTICAL STAB) · airframe 27,431 hrs · 21,568 cycles

VERTICAL STAB RT AND LT MOUNT LUGS WORN BEYOND LIMITS. OVERSIZED RT AND LT VERTICAL STAB BEARING HOUSINGS TO 1ST REWORK DIMENSIONS AND INSTALLED BUSHINGS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,793 hrs · 18,655 cycles

DURING ROUTINE MAINTENANCE THE 4TH AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (LT MLG) · airframe 22,886 hrs · 17,914 cycles

EWR FLT 2038 THE CREW REPORTED DURING GEAR RETRACTION RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MESSAGE DID NOT CLEAR. ALSO STATED ON INITAL ATTEMPT TO RETRACT THE GEAR THE HANDLE WOULD NOT MOVE TO THE UP POSITION BUT AFTER A SECOND OR TWO NORMAL RETRACTION WAS PERMITTED. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH LEFT GEAR WOW PROXIMITY SWITCHES, PERFORMED WOW HARNESS CHECKS AND SERVICED THE MAIN GEAR SHOCK ABSORBERS. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — CORRODED (RT SPOILER) · airframe 22,879 hrs · 17,909 cycles

DAY FLT 5857 THE CREW REPORTED THE SPOILERS DEPLOYED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT SPEED BRAKE PROXIMITY SWITCH AND CONNECTOR P1166. OPERATIONAL CHECKS WERE GOOD.

Part: DAU — MALFUNCTIONED (NR 1) · airframe 22,846 hrs · 17,875 cycles

L/G AIR/GROUND FAIL MESSAGE ON EICAS. RECEIVED MESH PROX TRAILING ARM IAW EMB 145AMM 32-63-05 AND REMOVED AND REPLACED DAU NR 1 IAW EMB 145AMM 31-41-01 OPS CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (COCKPIT) · airframe 22,817 hrs · 17,845 cycles

ORD FLT 6112 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER GEAR EXTENSION. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR DOWNLOCK A PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. THE WARNING INDICATION REOCCURRED ON FLT 5837. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 22,357 hrs · 17,472 cycles

DURING ROUTINE MAINTENANCE THE FORWARD CARGO SMOKE DETECTOR FAILED THE TASK CARD CHECK. LED STAYS ON ALL THE TIME. MAINTENANCE REPLACED THE SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 20,987 hrs · 16,246 cycles

CLE FLT 5658 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT GEAR WOW PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 20,543 hrs · 15,823 cycles

IAD FLT 5687 THE CREW REPORTED A ENGINE 2 LOW FUEL PRESSURE WARNING ON TAKEOFF ROLL WHILE ON PUMP A. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL PROCEDURES. SUPPLEMENT TO FOLLOW.

Part: CONNECTOR — LOOSE (CABIN) · airframe 18,455 hrs · 14,063 cycles

DURING ROUTINE MAINTENANCE, THE LEFT OVERWING EMERGENCY LIGHT EXIT SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED THE EXIT SIGN CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: ATTACH BRACKET — DAMAGED (ZONE 600) · airframe 18,154 hrs · 13,831 cycles

DURING C-CK. RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED ATTACHMENT BRACKET IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (AUDIO SYSTEM) · airframe 18,075 hrs · 13,769 cycles

FLIGHT 3064 - RIC - FLIGHT CREW REPORTED THAT NAV NR 1 AND NAV NR 2 DASHED OUT - NO NAV INFLIGHT. CREW DIVERTED FLIGHT TO RIC AND LANDED ACFT UNEVENTFUL. RIC MX REMOVED AND REPLACED NR 1 AUDIO CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: THRUST REVERSER — FAULTY (NR 2 ENGINE) · airframe 17,655 hrs · 13,473 cycles

CLE FLIGHT 2767 - THE CREW REPORTED AN ENGINE 2 THRUST REVERSER DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 78-34-00. ON 03/10/09 MAINTENANCE REPLACED THE NR 2 T/R AND OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 17,304 hrs · 13,215 cycles

THE CREW REPORTED, LEVEL AT FL360 RAPID DECOMPRESSION CABIN ALT REACHED 12,000. THE ACFT LANDED WITHOUT INCIDENT WHERE MX REMOVED AND REPLACED THE DIGITAL CONTROLLER, OPERATIONALLY TESTED AITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE LOOP — CHAFED (NR 1 ENGINE) · airframe 17,279 hrs · 13,197 cycles

IAH - FLIGHT 2386, THE CREW REPORTED A NUMBER ONE ENGINE FIRE DETECTOR FAIL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL TESTS WERE SATISFACTORY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL VALVE — DEFECTIVE (BRAKE SYS)

FLIGHT 2295 - EWR - FLIGHT CREW REPORTED "BRK INBD INOP" ON EICAS DURING APPROACH. CREW ABORTED APPROACH, AND PROCEEDED WITH NEW APPROACH AND LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: CONTROL UNIT — DEFECTIVE (BRAKE)

FLIGHT 2295 - EWR - FLIGHT CREW REPORTED "BRK INBD INOP" ON EICAS DURING APPROACH. CREW ABORTED APPROACH, AND PROCEEDED WITH NEW APPROACH AND LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 13,426 hrs · 10,432 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23-25. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, ITEM 4, FIG 203 AND EMB 145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 10,262 hrs · 7,981 cycles

PITCH TRIM RUNAWAY ON VECTORS FOR APPROACH (NOSE UP) WARNING PITCH TRIM FAIL ON EICAS. PERFORMED OPS CHECK OF PITCH TRIM SWITCHES AND AUTO PILOT IAW EMB 145AMM 22-11-00 OPS CK GOOD. TEST FLEW AIRCRAFT VERIFIED PITCH TRIM AND AUTO PILOT SYSTEMS. TEST FLIGHT SATISFACTORY AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,756 hrs · 6,777 cycles

SHV - DURING C-CHECK MAINTENANCE, FOUND LT OMEGA BEAM LOWER FLANGE HAS CORROSION AT FRAMES 19A TO 23. MAINTENANCE REPAIRED LT OMEGA BEAM LOWER FLANGE IAW EC 5320-01257 REV A. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 8,756 hrs · 6,777 cycles

SHV - DURING C-CHECK, APU FIREWALL HAS A CRACK AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED THE FIREWALL AT 3 O`CLOCK POSITION IAW EC5330-01483. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,756 hrs · 6,777 cycles

SHV - DURING C-CHECK, THE LT OMEGA BEAM HAS CORROSION AT NUT PLATE BETWEEN FS 22-23. MAINTENANCE REPAIRED THE LT OMEGA BEAM CORROSION BETWEEN FS 22-23 IAW EC5320-01257. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 7,145 hrs · 5,538 cycles

DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,145 hrs · 5,538 cycles

DURING SCHEDULED MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT FLOOR EMERGENCY LIGHT STRIP, OPERATIONALLY CHECKED THE LIGHT STRIP AND CLEARED THE DISCREPANCY. SEE SDR CONTROL NUMBER C2XA04IA169 FOR DOCUMENTATION OF THE NR 3 EMERGENCY LIGHT BATTERY PACK REPLACEMENT FOR THIS SAME OCCURRENCE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 7,126 hrs · 5,521 cycles

IN SDF, FLIGHT 2068, THE PILOT WROTE UP THAT THE EMERGENCY LIGHTS ARE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 LIGHT STRIP IAW EMB 145 AMM-33-50-12 AND THE NR 3 EMERGENCY BATTERY IAW EMB-145 AMM-43-50-04, OPS CHECKED GOOD.

Part: BALLAST — SHORTED (LAVATORY) · airframe 6,259 hrs · 4,835 cycles

CLE FLIGHT NR 2131 CREW REPORTED AN ELECTRICAL ODOR IN CABIN DURING POST FLIGHT INSPECTION. MAINTENANCE INSPECTED AND FOUND THAT THE LAV LIGHT BALLAST HAD SHORTED OUT. MAINTENANCE REPLACED THE LAV LIGHT BALLAST. ALL OPERATIONAL CHECKS WERE GOOD.

Part: RELAY — FAULTY (EMERGENCY LIGHT)

CREW REPORTED, EMERGENCY LIGHT NOT ARMED, EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED RELAY K0275 AND PERFORMED WIRING CHECKS IAW EMB145 33-50-50 AND RELAY IAW EMB145 WM 20-13-02. OPS CHECKED SYSTEM GOOD.

Part: CONTROL PANEL — FAULTY (EMERGENCY LIGHT)

CREW REPORTED, EMERGENCY LIGHTS WOULD NOT ARM, MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED COCKPIT CONTROL PANEL AND OPS. CHECKED SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PANEL — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT MESSAGE ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE ARMED POSITION. THE POWER WAS RESET AND THE MESSAGE INITIALLY CLEARED BUT ILLUMINATED AGAIN AFTER A SHORT PERIOD OF TIME. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.

Part: LIGHT — MALFUNCTIONED (CABIN)

CLE FLIGHT 2846, THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT ARM. THE CREW RESET THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — FAULTY (EMERGENCY LIGHT)

DURING CRUISE THE EMERGENCY LIGHT NOT ARMED CAUTION ADVISORY ILLUMINATED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LIGHTING CONTROL MODULE. OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV-DURING C-CHECK THE CARGO DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV-DURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — DENTED (LT COWLING) · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE LEFT UPPER COWLING INBOARD EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGE MEMBER IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE MAIN DOOR FORWARD U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — NICKED (FUSELAGE) · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE OUTER SKIN WAS FOUND TO BE NICKED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE MAIN DOOR AFT U-BRACKET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RIGHT UPPER APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE LEFT HAND OMEGA BEAM AT FRAME 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,419 hrs · 3,426 cycles

SHV- DURING C-CHECK THE CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DETECTOR — FAULTY · airframe 2,150 hrs · 1,583 cycles

EWR---CO3264, CREW REPORTED ENGINE NUMBER ONE FIRE DETECTOR FAILED ON EICAS.....MAINTENANCE REMOVED AND REPLACED ENGINE NUMBER ONE FIRE DETECTOR IAW EMB145 AMM #26-11-01. OPS.CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — OUT OF ADJUST

EWR-STL FLIGHT#3543 THE CREW REPORTED A GUST LOCK LIGHT ILLUMINATED IN FLIGHT.THE AIRCRAFT DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.ON TOCHDOWN THE MESSAGE CLEARED.MAINTENANCE INSPECTED AND ADJUSTED THE LEFT SPRING CARTRIDGE POSITION MICROSWITCH FOR THE ELECTROMECHANICAL GUST LOCK SYSTEM.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.