N17115

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,655 hrs · 24,811 cycles

TYS A/C WAS IN FOR A SERVICE CHECK WHEN THEY FOUND EMERGENCY MAIN DOOR LIGHT AND MAIN DOOR EXTERIOR LIGHT INOP. MAINTENANCE RE-LAMPED THE MAIN DOOR EXTERIOR LIGHT, CLEANED THE CONNECTORS AND R&R THE NR 1 EMERGENCY LIGHT BATTERY. ALL WORK ACCOMPLISHED AND WAS RELEASED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,315 hrs · 23,872 cycles

DURING INSPECTION, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. REMOVED AND REPLACED THE BATTERY CHARGER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — STUCK (COCKPIT) · airframe 38,123 hrs · 22,369 cycles

CREW REPORTED NOSE UP PITCH TRIM(UNCOMMANDED) RIGHT AFTER TAKEOFF. POSSIBLE PITCH TRIM RUNAWAY. AURAL WARNING"TRIM, TRIM" BUT NO EICASE MESSAGE. SMOOTH LANDING REPORTED ON AIR RETURN BACK TO EWR. MX REMOVED AND REPLACED THE F/O'S YOKE PITCH TRIM SWITCH WITH OPERATIONAL AND CHECK FLIGHT GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 37,673 hrs · 22,056 cycles

IAH - FLIGHT 4438, THE CREW REPORTED A LAV SMOKE INDICATION ON SHORT FINAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,217 hrs · 21,706 cycles

DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING AND EMERGENCY EXIT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFDECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 37,217 hrs · 21,706 cycles

DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING AND EMERGENCY EXIT AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFDECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,792 hrs · 20,009 cycles

DURING 3A INSPECTION THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR LOWER WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK, CARGO DOOR AFT FRAME CORRODED, LOCAL LEVEL 2 AT NUTPLATE. MAINTENANCE PERFORMED REPAIR OF CARGO DOOR AFT FRAME AT NUTPLATE IAW EC5230-01349 UP TO AND INCLUDING FINAL STEP 2.1,2.7. INSTALLED REPAIR IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (CARGO BAY) · corrosion level 2 · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK CARGO DOOR FWD FRAME CORRODED. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR FWD FRAME IAW SRM 51-40-02 AND EC5230-01349. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — DAMAGED (FRAME 19) · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK SHEAR TIE AT FRAME 19, STRINGER 14L IS MISSING RIVETS. MAINTENANCE INSTALLED 2 RIVETS IN SHEAR CLIP AT FRAME 19, STRINGER 14L IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (GALLEY) · corrosion level 2 · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK, GALLEY FWD DIGITAL BUTTSTRAP IS CORRODED, AT VARIOUS FASTENER HOLES. MAINTENANCE PERFORMED REPAIR OF GALLEY FWD DIGITAL LT IAW EC5320-01987. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK, RT OMEGA BEAM IS CORRODED, LOCAL LEVEL 2 AT FASTENER HOLE AT FRAME 23. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM AT FRAME 23 IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FRM 10) · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK, CRACK AT RIVET FRAME 10 UNDER RT DV WINDOW CUTOUT. MAINTENANCE R & R FRAME 10 UNDER RT DV WINDOW CUTOUT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK CARGO DOOR UPPER INTERNAL SKIN CORRODED AT NUTPLATE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR UPPER INTERNAL SKIN IAW EC5230-01349. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK CARGO DOOR LOWER INTERNAL SKIN GOUGED. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR LOWER INTERNAL SKIN IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — DAMAGED (CARGO DOOR) · airframe 33,629 hrs · 19,232 cycles

DURING C-CHECK CARGO DOOR LOWER FRAME BRACKET DAMAGED. MAINTENANCE R & R CARGO DOOR LOWER FRAME "L" BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERNAL) · airframe 32,133 hrs · 18,266 cycles

DURING ROUTINE MAINTENANCE, THE LT AFT EXTERNAL EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSY, OPS CHECKED GOOD.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 31,072 hrs · 17,589 cycles

DURING SCHEDULED MAINTENANCE THE PASSENGER DOOR LOWER EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE RESECURED THE BULB IN THE LIGHT FIXTURE, OPERATIONALLY TESTED THE LIGHT ASSY AND CLEARED THE DISCREPANCY.

Part: WARNING MESSAGE — ILLUMINATED (BRAKE SYS) · airframe 29,958 hrs · 16,890 cycles

PILOT REPORTED A BRAKE DEGRADED EICAS MESSAGE AFTER SELECTING GEAR DOWN AND THE RT BRAKE WAS LESS EFFECTIVE ON LANDING ROLL. CREW RESET SYS WITH MX CONTROL. MESSAGE NO LONGER EXIST. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,398 hrs · 15,874 cycles

DURING MX INSPECTION, THE AFT AISLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 26,546 hrs · 14,620 cycles

DURING ROUTINE MX, EMERGENCY EXIT SIGN AT RT OVERWING EXIT DOOR WAS FOUND INOPERATIVE. MX RESECURED LOOSE CONNECTION AT THE EXIT MARKER. OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE INDICATION (TE FLAPS) · airframe 25,540 hrs · 13,400 cycles

REJECTED TAKEOFF. THE TAKEOFF CONFIGURATION FLAPS AURAL WARNING MESSAGE CAME ON. CREW RESET AND PERFORMED OPS CHECK OF FLAPS AND TRIM SYSTEMS WERE ALL GOOD. ACFT LEFT WITHOUT INCIDENT.

Part: PROBE — MALFUNCTIONED (FUEL QTY) · airframe 25,287 hrs · 13,791 cycles

FLIGHT 4455 THE CREW REPORTED A FUEL TANK NR 2 FUEL LEVEL ERROR IN FLIGHT, FUEL FLUCTUATING BETWEEN 4100LBS CAUSING IMBALANCE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. R & R THE NR 2 TANK UNIT IN THE RT WING, OPS AND LECK CHECKED WITH NO DEFECTS

Part: LIGHT — OVERHEATED (CABIN) · airframe 23,793 hrs · 12,803 cycles

FLIGHT 2532, THE CREW REPORTED A BURNING ODOR AT ROW 4A. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CABIN LIGHT ASSY AT SEAT 4A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTON — FAULTY (COCKPIT) · airframe 23,527 hrs · 12,663 cycles

EWR - FLT 2370 THE CREW REPORTED THE NR 2 BLEED VALVE CLOSED AFTER TAKEOFF AND WAS UNABLE TO CLEAR THE MESSAGE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 BLEED VALVE PUSHBUTTON. OPERATIONAL CHECKS WERE GOOD.

Part: BLEED VALVE — LOCKED (NR 2) · airframe 22,926 hrs · 12,335 cycles

IAH - FLIGHT 3004, THE CREW REPORTED A BLEED VALVE TWO FAIL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 2 BLEED VALVE TO BE LOCKED IN THE CLOSED POSITION. MAINTENANCE UNLOCKED THE VALVE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,722 hrs · 11,665 cycles

CLE FLT 2777 THE CREW REPORTED A ENGINE 2 ANTI-ICE FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 30-21-01-1. SUPPLEMENT TO FOLLOW.

Part: ACCUMULATOR — DISCHARGED (HYDRAULIC SYS) · airframe 20,333 hrs · 10,898 cycles

IAH - FLIGHT 2412, THE CREW REPORTED THAT THE LANDING GEAR TOOK LONGER THAN NORMAL TO RETRACT, AND RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE LANDING GEAR HYDRAULIC ACCUMULATOR, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — DEFECTIVE (COCKPIT) · airframe 19,774 hrs · 10,596 cycles

IAH - FLIGHT 2198, THE CREW REPORTED THAT THE MLG DID NOT INITIALLY RETRACT, AFTER QRH RECYCLED GEAR AND RETRACTED NORMALLY. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. FLIGHT 2522, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 19,675 hrs · 10,550 cycles

IAH - FLIGHT 2272, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE AND THE GEAR FAILED TO RETRACT ON TAKEOFF, AND FINALLY RETRACTED AFTER SEVERAL ATTEMPTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 19,666 hrs · 10,546 cycles

IAH - FLIGHT 2135, DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON TAKE OFF. THE CREW PERFORMED THE QRH, CYCLED THE GEAR WHICH THEN RETRACTED, AND THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 19,666 hrs · 10,546 cycles

IAH - FLIGHT 2953, ON CLIMBOUT THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE CREW FOLLOWED THE QRH, CYCLED THE GEAR AND THE GEAR RETRACTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — FAULTY (NLG) · airframe 19,614 hrs · 10,518 cycles

CLE FLT 2781 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE WHILE GEAR WAS IN TRANSIT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL LEVER — INOPERATIVE (COCKPIT) · airframe 19,572 hrs · 10,495 cycles

FLIGHT 2508 - EWR - FLIGHT CREW REPORTED L/G AND AIR/GRND DISAGREE MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LGEU AND L/G CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. SDR - C2XA09RI195 HAS LGEU INFO SRD C2XA09RI196 HAS CONTROL LEVER INFO. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 19,572 hrs · 10,495 cycles

FLIGHT 2508 - EWR - FLIGHT CREW REPORTED L/G AND AIR/GRND DISAGREE MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LGEU AND L/G CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. SDR - C2XA09RI195 HAS LGEU INFO SRD C2XA09RI196 HAS CONTROL LEVER INFO. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,314 hrs · 10,360 cycles

IAH - FLIGHT 2771, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. PERFORMED LANDING GEAR EXTENSION AND RETRACTION TESTS WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 19,110 hrs · 10,244 cycles

ATL - FLIGHT 3128 - THE CREW REPORTED AN ELECTRIC BURNING SMELL IN THE COCKPIT AND FORWARD CABIN DURING CRUISE, WITH A BLEED TWO OVERHEAT WARNING ON EICAS. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE FORWARD FAN AIR VALVE CONTROL THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS) · airframe 19,110 hrs · 10,244 cycles

ATL - FLIGHT 3128 - THE CREW REPORTED AN ELECTRIC BURNING SMELL IN THE COCKPIT AND FORWARD CABIN DURING CRUISE, WITH A BLEED TWO OVERHEAT WARNING ON EICAS. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE AFT FAN AIR VALVE CONTROL THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 19,000 hrs · 10,185 cycles

IAH - FLIGHT 2140, DURING POST FLIGHT INSPECTION THE CREW REPORTED A PIECE OF THE LT WING LEADING EDGE TWO TO BE CORRODED AND MISSING. IAH MAINTENANCE INSPECTED THE LEADING EDGE AND FOUND WHAT APPEARED TO BE DISSIMILAR METAL CORROSION ADJACENT TO A FASTENER FOR A DOUBLER REPAIR AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE LEADING EDGE, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 18,476 hrs · 9,899 cycles

DURING C-CHECK, A MIGRATED HAT BUSHING WAS FOUND ON THE LT AILERON OTBD PCA FITTING INBD LUG. THE AILERON PCA BRACKET WAS REMOVED AND REPLACED IAW EC 5750-01177C. ACFT STILL IN C-CHECK.

Part: FUEL TANK — CHAFED (FUEL SYSTEM) · airframe 18,476 hrs · 9,899 cycles

TYS - DURING C-CHECK THE VENTRAL TANK WAS FOUND CHAFED FROM CONTACT WITH PANEL 197BB. THE VENTRAL TANK WAS REPAIRED IAW EC 2810-01053. A/C STILL IN C-CHECK.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,476 hrs · 9,899 cycles

THE RT REAR FUSELAGE I SKIN HAS A DENT WITH A GOUGE BETWEEN FRM 65 & 66, STR 14 & 15R. MAX DEPTH OF DENT AND GOUGE IS .034 INCH. CUT OUT GOUGED AREA OF SKIN, FABRICATED A FILLER AND DOUBLER. INSTALLED REPAIR PARTS WET WITH SEALANT, ALODINED, PRIMED AND PAINTED IAW EC5330-01933. AIRCRAFT STILL IN C-CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,476 hrs · 9,899 cycles

THE LT CENTER FUSELAGE I SKIN HAS TWO DENTS, ONE BETWEEN FRM 20 & 21 AND A PREVIOUSLY BLENDED AREA BETWEEN FRM 18 & 19 WITH A REMAINING THICKNESS OF .014 INCH. THE DENTS ARE AFT OF THE PAX DOOR CUTOUT. MAINTENANCE CUT OUT PREVIOUS BLENDED AREA OF SKIN, FABRICATED A FILLER AND DOUBLER, ALODINED AND PRIMED THE REPAIR PARTS AND INSTALLED WET WITH SEALANT. APPLIED SEALANT TO THE DOUBLER PERIMETER AND THE GAP BETWEEN THE FILLER AND THE INTERNAL SKIN. PRIMED AND PAINTED THE REPAIRED AREA. RE-CONTOURED THE TWO DENTS, PERFORMED DYE PEN INSPECTION, NO CRACKS NOTED. FILLED ANY REMAINING DENTS WITH HYSOL AND SANDED SMOOTH, PRIMED AND PAINTED AREA. REPAIRED IAW EC5330-01932.

Part: AXLE — CORRODED (RT MLG) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK RT MLG SHOCK STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED RT MLG SHOCK STRUT LOWER ATTACH AXLE IAW EMB AMM 32-10-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: AXLE — CORRODED (LT MLG) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK LT MLG STRUT LOWER ATTACH AXLE CORRODED. MAINTENANCE REMOVED AND REPLACED LT MLG STRUT LOWER ATTACH AXLE IAW EMB 145XR AMM 32-10-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK BAGGAGE DOOR CUTOUT LOWER CENTER BEAM HAS CORROSION. MAINTENANCE REMOVED AND REPLACED LOWER BEAM FOR BAGGAGE DOOR CUTOUT IAW EMB 145 SRM 51-40-02. INSTALLED NUT PLATES IAW EC 5320-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PLATE — CORRODED (FAIRING) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK 191 WING TO FUSELAGE FAIRING HAS CORRODED BONDING PLATE ON LOWER TRAILING EDGE. MAINTENANCE REPAIRED 191 PNL LOWER TRAILING EDGE BONDING PLATE IAW EC5750-01315 REV-E. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION BETWEEN FR 19-21. MAINTENANCE REPAIRED LEFT OMEGA BEAM BETWEEN FRS 19-21 IAW EC 5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ATTACH FITTING — DAMAGED (RT AILERON) · airframe 14,038 hrs · 7,753 cycles

SHV - DURING C-CHECK RIGHT AILERON PCA HAS PLAY WHEN HYD ARE PRESSURIZED. MAINTENANCE REMOVED AND REPLACED RIGHT AILERON PCA FITTING AND PAINTED IAW EC5750-01179. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,184 hrs · 4,936 cycles

TYS DURING A CURRENT 2C INSPECTION INTERGRANNULAR CORROSION WAS FOUND THROUGHOUT THE BAGGAGE DOOR LOWER BEAM. MAINTENANCE REMOVED AND REPLACED THE LOWER CARGO DOOR SILL IAW EMB 145XR SRM 51-20-03,51-40-02 AND 51-40-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK INSPECTION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,393 hrs · 4,509 cycles

SDF - NR 2 EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT NR 2 IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,343 hrs · 4,481 cycles

IAH - DURING MAINTENANCE INSPECTION THE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,175 hrs · 4,393 cycles

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EXIT ROW EMERGENCY EXIT SIGN TO BE INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE AFFECTED LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY REPEATED ON FLIGHT 2723 IN IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY EXIT SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 5,196 hrs · 2,779 cycles

DURING PREFLIGHT, THE MAIN CABIN DOOR WAS HARD TO OPEN AND CLOSE. MAINTENACE LUBED THE SEAL AND OPERATIONALLY CHECKED THE DOOR. AIRCRAFT RETURNED TO SERVICE.

Part: DRIVE SHAFT — SEIZED (RIGHT FLAP)

CLE FLIGHT 2221, THE CREW REPORTED A FLAP FAIL IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT FLAP NR 4 FLEX SHAFT. OPERATIONAL CHECKS WERE GOOD.

Part: MANIFOLD — DISLODGED (NR 1 ENGINE)

IAH - AFTER ROTATION THE CREW REPORTED THAT THE NR 1 ENGINE EXCEEDED ALLOWABLE TEMPERATURE LIMITS. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND THAT THE UPPER BYPASS DUCT PANEL AND MANIFOLD ASSEMBLY HAD PULLED LOOSE FROM THE OUTER BYPASS DUCT. THE NR 1 ENGINE WAS REMOVED AND REPLACED, OPERATIONALLY TESTED AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.