N14993

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,982 hrs · 35,769 cycles

IAH - FLIGHT 3985, DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8-9 WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT STRIP ON MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 04/15/20 IAH MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 45,220 hrs · 35,106 cycles

DURING LEFT DV WINDOW BEAM REPLACEMENT (DUE TO CRACK) THE FORWARD FUSELAGE II SKIN PARTIALLY COVERED RIVET THAT REQUIRED REMOVAL. MAINTENANCE TRIMED FORWARD FUSELAGE II SKIN WHERE FASTENER WAS PARTIALLY COVERED AND REMOVED RIVET. WORK ACCOMPLISHED IAW ETD2019-145-124119.

Part: BEAM — CRACKED (LT WINDOW) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND CRACK ON LEFT DV WINDOW LOWER BEAM. MAINTENANCE REPLACED LEFT DV WINDOW LOWER BEAM I/A/W ETD 2019-145-124119 AND SB145-53-0023

Part: SKIN — CRACKED (FUSELAGE) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND 2 CRACKS AT RIVETS AT FRAME 75 JUST ABOVE AND BELOW STRINGER 2R. MAINTENANCE REPAIRED IAW SRM 53-31-01.

Part: BEARING CAP — CORRODED (LT MLG) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND CORROSION PITTING ON THE LEFT MAIN LANDING GEAR AFT LOWER BEARING CAP. MAINTENANCE REPLACED THE AFT LOWER BEARING CAP ON LEFT MAIN LANDING GEAR.

Part: BEAM — CORRODED (FUSELAGE) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND CARGO DOOR THRESHOLD BEAM CORRODED. MAINTENANCE REPAIRED BEAM IAW SRM 53-31-15.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND RIGHT INBOARD FLAP UPPER OUTBOARD END DELAMINATED AT THE CORNER. MAINTENANCE REPAIRED IAW SRM57-52-00 STEP 4.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND RIGHT INBOARD FLAP UPPER INBOARD END DELAMINATED. MAINTENANCE REPAIRED IAW SRM 51-70-06 STEP 6.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND RIGHT INBOARD FLAP LOWER SIDE DELAMINATED. MAINTENANCE REPAIRED FLAP IAW SRM 57-52-00 STEP 6.

Part: FLAP — WORN (RT WING) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND RIGHT INBOARD FLAP TRAILING EDGE WORN THROUGH. MAINTENANCE REPAIRED RIGHT INBOARD FLAP TRAILING EDGE IAW SRM 57-52-00 STEP 6 (E).

Part: FRAME — BENT (FRM 72) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FRAME 72 WAS FOUND BENT BETWEEN STRINGERS 16R AND 17R. MAINTENANCE REPAIRED FRAME 72 WITH SPLICE REPAIR I/A/W SRM 51-30-01, 51-40-02, 53-00-04

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND RIGHT SIDE FRAME SEGMENT 10 CRACKED BELOW DV WINDOW. MAINTENANCE REPLACED RIGHT SIDE FRAME 10 SEGMENT.

Part: FRAME — CRACKED (FUSELAGE) · airframe 45,220 hrs · 35,106 cycles

DURING C CHECK INSPECTION FOUND LEFT FRAME 10 CRACKED BELOW DV WINDOW. MAINTENANCE REPLACED LEFT SIDE FRAME 10 SEGMENT.

Part: CLAMP — LOOSE (A/C PACK) · airframe 42,448 hrs · 32,850 cycles

PILOT REPORTED AN ELECTRICAL ODOR THROUGHOUT THE CABIN & COCKPIT. MX SECURED A LOOSE CLAMP ON THE NR 2 A/C PACK WITH NO FURTHER ODOR NOTED.

Part: LIGHT — BROKEN (CABIN) · airframe 41,887 hrs · 32,406 cycles

DURING SCHEDULED MX THE NR7 FLOOR EMERGENCY LIGHT PROX STRIP WAS FOUND BROKEN. MX REMOVED AND REPLACED THE NR7 LIGHT STRIP WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT BRACKET — CRACKED (COCKPIT) · airframe 40,395 hrs · 31,228 cycles

DURING "A-CHECK" INSPECTION THE COCKPIT LATERAL UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH TECHNICAL DISPOSITION ETD2017-145-011028, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 40,395 hrs · 31,228 cycles

DURING "A-CHECK" INSPECTION THE SKIN ON THE LEFT HAND LATERAL T-POST BETWEEN THE UPPER CORNER OF THE CAPTAINS WINDSHIELD WAS FOUND TO BE CRACKED ACROSS TO THE CAPTAINS DV WINDOW. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND REPAIRED THE AFFECTED ARE IN ACCORDANCE WITH SERVICE BULLETIN SB145-53-0079, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 39,940 hrs · 30,786 cycles

PILOT REPORTED ODOR OF COMBUSTION ON TAKEOFF FROM PACK/OIL BURNING SMELL. ITEM INITIALLY PLACED MEL 21-51-00-1. ON 11/25/16 MX RAN PACK NR 1 MULTIPLE TIMES AND COULD NOT DUPLICATE MEL CLEARED. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAULTY (NR 1) · airframe 39,937 hrs · 30,874 cycles

ENGINE 1 HI VIBRATION AND OIL SMELL IN THE COCKPIT. REMOVED AND REPLACED NR 1 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE DETECTION) · airframe 39,903 hrs · 30,840 cycles

THE CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LAVATORY SMOKE DETECTION PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: O-RING — FAILED (GENERATOR) · airframe 39,877 hrs · 30,815 cycles

CREW REPORTED WHILE IN CLIMB, THRUST PACK 1 DISTRIBUTES A STRONG ODOR THAT BURNS EYES. REMOVED AND REPLACED O-RING ON THE CARBON SEAL OF THE NR 3 GENERATOR. OPS CHECK GOOD. A/C APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (BRAKE) · airframe 36,462 hrs · 28,067 cycles

THE CREW REPORTED ACFT WAS NOT GETTING FULL BRAKING WHEN FULL BRAKING WAS APPLIED. OTBD BRAKES WERE COLD AND INBD BRAKES HOT AFTER LANDING. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT. OPS CHECKS WERE GOOD.

Part: PARTITION — GOUGED (COCKPIT) · airframe 36,157 hrs · 27,829 cycles

DURING C-CHECK LT COCKPIT PARTITION UPPER AND LOWER GIUDE PIN HOLES ELONGATED. MAINTENANCE PERFORMED REPAIR TO LT COCKPIT UPPER AND LOWER GUIDE PIN HOLES IAW EC5320-02021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — GOUGED (FRM 70) · airframe 36,157 hrs · 27,829 cycles

DURING C-CHECK, FRAME 70 GOUGED STRINGER 12R-13R. MAINTENANCE REPAIRED FRAME 70 STRINGER 12R-13R IAW EC5320-02022. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 36,157 hrs · 27,829 cycles

DURING C-CHECK, FRAME 65 BETWEEN STRINGERS 16L-17L HAS CORROSION, LOCAL LEVEL 2. MAINTENANCE R & R FRAME 65 BETWEEN STRINGER 16L-17L IAW EC5330-02995 OIG. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 36,157 hrs · 27,829 cycles

DURING C-CHECK, CARGO DOOR LOWER BEAM NEEDS REMOVED. MAINTENANCE R & R CARGO DOOR CUTOUT LOWER BEAM FRAME 65-68 IAW SRM 51-40-02 AND IS DETERMINED TO BE MAJOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 36,157 hrs · 27,829 cycles

DURING C-CHECK ENGINE NR 1 FORWARD MOUNT POSSIBLE CRACK AT LOWER FWD HINGE. MAINTENANCE R & R ENGINE NR 1 FORWARD MOUNT LOWER FORWARD HINGE IAW EC5450-01139. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — FAILED (COCKPIT) · airframe 33,582 hrs · 25,830 cycles

CREW REPORTED F/O MFD WENT BLANK FOLLOWED BY ELECTRICAL BURNING ODOR. MAINTENANCE INSPECTED COCKPIT ELECTRICAL WIRING AND NO DEFECTS WERE FOUND. OPEN

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,833 hrs · 24,471 cycles

DURING SCHEDULED MX INSPECTION EMERGENCY LIGHTS ABOVE THE FWD F/A SEAT, COCKPIT STEP, AND ABOVE THE GALLEY WERE FOUND INOPERATIVE. MX CLEANED AND RESECURED THE CONNECTOR ASSOCIATED WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER GEN — BURNED (APU) · airframe 29,988 hrs · 22,993 cycles

CREW REPORTED A STRONG ELECTRICAL ODOR COMING FROM PACK NR 2 FOLLOWED BY APU GEN FAILURE. FOUND THE APU STARTER GEN SHOWING SIGNS OF BEING BURNED. MX R & R THE APU STARTER GENERATOR WITH OPS CHECKS SUCCESSFUL.

Part: LIGHT — BURNED (CABIN) · airframe 29,896 hrs · 22,930 cycles

DURING CRUISE THE CREW RPORTED AN ELECTRIC BURNING ODOR IN THE CABIN. THE ACFT LANDED WITHOUT INCIDENT WHERE MX INSPECTED THE ACFT AND R & R THE LIGHT ASSY ABOVE ROW 15-16. OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 29,892 hrs · 22,927 cycles

ELECTRICAL BURNING ODOR IN CABIN REPORTED BY CREW. MX R & R THE LIGHT ASSY ABOVE ROW 15-16.

Part: FIREWALL — CRACKED (APU) · airframe 29,037 hrs · 22,197 cycles

APU FIREWALL CRACKED. MX R & R APU FIREWALL IAW EA5310-01072, REV A. THE ACFT APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — DEFECTIVE (LANDING GEAR) · airframe 26,369 hrs · 20,069 cycles

TYS - A/C WAS EN ROUTE FROM BHM TO ORD WHEN CREW GOT A AIR GROUND FAIL MESSAGE ON THE ICIAS AND GEAR WOULDN'T RETRACT. CREW RETURNED TO BHM WITHOUT INCIDENT. A/C WAS FERRIED TO TYS WHERE MAINTENANCE COMPLIED WITH LANDING GEAR PROX SWITCHES ADJUST/TEST PROCEDURES IAW EMB 145 AMM 32-63-05. NO FAULT FOUND, OPS CHECK GOOD. REMOVED AND REPLACED THE LGEU IAW EMB 145AMM 32-32-01, OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 26,308 hrs · 20,015 cycles

ALB FLT 6139 THE CREW REPORTED THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL PANEL — DEFECTIVE (COCKPIT) · airframe 26,308 hrs · 20,015 cycles

FLIGHT 6139 - EWR - FLIGHT CREW REPORTED LAV SMOKE DETECTOR TEST INOPERATIVE. EWR MX REMOVED AND REPLACED LAV SMOKE FIRE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 24,013 hrs · 18,155 cycles

FLIGHT 2076 - EWR - FLIGHT CREW REPORTED BURN SMELL AT ROW 12A. EWR MX REMOVED AND REPLACED LIGHT ASSY AT ROW 12A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,082 hrs · 17,450 cycles

TYS - AIRCRAFT IN FOR SERVICE ROUTINE WHEN INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEAT 8A-9A INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY STRIP IAW AMM 33-50-12. OPS CHECK GOOD.

Part: TRANSPONDER — MALFUNCTIONED (COMM SYS) · airframe 22,430 hrs · 16,970 cycles

FLIGHT 2061 - EWR - FLIGHT CREW REPORTED COMM NR 1 WAS LOST DURING FLIGHT - COULD NOT TRANSMIT. EWR MX PERFORMED ELECTRICAL RESET FOR COMM NR 1 AND PERFORMED OPERATIONAL CHECK OF THE SYSTEM SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,984 hrs · 16,631 cycles

SHV - DURING C-CK, CRACKS IN FUSELAGE SKIN FR 79 STR 5R AND 6R. SKIN REPAIRED IAW EC5330-01947. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 21,984 hrs · 16,631 cycles

SHV - DURING C-CK, CRACKS IN FUSELAGE SKIN FR 79 STR 5L AND 6L. REPAIRED SKIN IAW EC5330-01947. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — DAMAGED (RUDDER) · airframe 21,984 hrs · 16,631 cycles

SHV - DURING C-CK, RUDDER 1 NR 3 HINGE POINT FROM TOP HAS MIGRATED HAT BUSHING. REPAIRED RUDDER FITTING IAW EC5540-01116. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,183 hrs · 16,027 cycles

FLIGHT 3071 - EWR - FLIGHT CREW REPORTED AISLE PATH LIGHT BETWEEN 3A-7A INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER ABOVE GALLEY CEILING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FADEC — FAULTY (NR 1 ENGINE) · airframe 23,417 hrs · 23,417 cycles

CLE FLIGHT 2733 - THE CREW REPORTED, LOST NR 1 ENGINE INDICATION SEVERAL TIMES. THE CREW PERFORMED PROCEDURES FROM THE CFM. MAINTENANCE INSPECTED AND REPLACED THE 1B FADEC. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — BROKEN (DOOR INDICATOR) · airframe 17,289 hrs · 13,274 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT INDICATE LATCH CLOSED. MAINTENANCE INSPECTED AND REPAIRED WIRE W717-0010-24. MAIN CABIN DOOR WARNING OPERATIONAL CHECKS WERE GOOD.

Part: BUSHING — WORN (RUDDER) · airframe 17,000 hrs · 13,050 cycles

TYS DURING A CURRENT 2C INSPECTION THE MIDDLE BUSHION ON THE RUDDER 2 WAS FOUND WORN. MAINTENANCE REMOVED AND REPLACED THE BRACKET WITH A NEW BUSHION IAW EMB 135/145 SRM 51-40-02 AND EC 5540-01028. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: ODOR — DETECTED (COCKPIT & CABIN) · airframe 14,461 hrs · 11,077 cycles

IAH - FLIGHT 2080, THE CREW REPORTED AN ELECTRICAL OR SULFUR SMELL IN THE COCKPIT AND CABIN DURING TAXI AND CLEARED IN 3 TO 5 MINUTES. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU BAY) · airframe 12,259 hrs · 9,323 cycles

DURING C-CHECK THE APU FIREWALL AT FRAME 81 HAS CHAFE MARKS FROM RIVETS. MAINTENANCE REPAIRED THE APU FIREWALL AT FRAME 81 IAW EC5330-01507. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE.

Part: ODOR — DETECTED (CABIN) · airframe 12,062 hrs · 9,165 cycles

CREW REPORTED, VERY STRONG FUEL OR EXHAUST ODOR IN GALLEY AND GALLEY CLOSETS. RAN NR 1 AND NR 2 ENGINES, OPS CHECK OF ENGINE BLEED SYSTEMS CHECKS GOOD, VISUAL INSPECTION OF FORWARD CABIN AREA [GALLEYS, CLOSETS, SPACES] NO DEFECTS, NO ODORS NOTED IAW EMB145 AMM 71-00-01, 36-11-01, AND 05-20-18. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — MALFUNCTIONED (CABIN) · airframe 11,382 hrs · 8,641 cycles

OKC - FLIGHT 2964, DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT AT THE FORWARD FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NOTE: THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 11,331 hrs · 8,606 cycles

DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (MAIN CABIN DOOR) · airframe 11,331 hrs · 8,606 cycles

CLE - CREW REPORTED THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,907 hrs · 5,948 cycles

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

Part: STRUCTURE — DENTED (LT COWLING) · airframe 7,907 hrs · 5,948 cycles

SHV-DURING C-CHECK THE LEFT UPPER COWLING AFT EDGE MEMBER WAS FOUND TO BE DENTED. MAINTENANCE REFORMED THE DENTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — DENTED (FUSELAGE) · airframe 7,907 hrs · 5,948 cycles

SHV-DURING C-CHECK THE CENTER BUTTSTRAP AT FRAME 64 WAS FOUND TO BE DENTED. MAINTENANCE REMOVED AND REPLACED THE CENTER BUTTSTRAP IAW EMB 145 SRM 53-31-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (LT COWLING) · airframe 7,907 hrs · 5,948 cycles

SHV-DURING C-CHECK THE LEFT LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFT EDGE MEMBER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK THE FORWARD DIGITAL BUTTSTRAP BETWEEN FRAMES 15 AND 17 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: STRINGER — GOUGED (FUSELAGE) · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK STRINGER 19 LEFT BETWEEN FRAME 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: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

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

Part: STRINGER — GOUGED (FUSELAGE) · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK STRINGER 19 RIGHT BETWEEN FRAME 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: STIFFENER — GOUGED (NR 2 COWLING) · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK THE NR 2 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

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

Part: SKIN — NICKED (FUSELAGE) · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK, THE RIGHT SIDE OF THE FUSELAGE WAS FOUND TO BE NICKED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PATCH REPAIR IAW EMB 145 SRM 53-31-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK, THE CENTER BUTTSTRAP WAS FOUND TO CORRODED AROUND THE NUT PLATES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 53-24-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,948 cycles

SHV- DURING C-CHECK, THE CENTER OMEGA BEAM BUTTSTRAP 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: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,907 hrs · 5,984 cycles

SHV- DURING C-CHECK, THE CENTER OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — STUCK (MLG YOKE)

ON TAKEOFF ROLL THE CREW NOTED A STEERING INOP MESSAGE. ABORTED THE TAKEOFF. MAINTENANCE CYCLED THE DISCONNECT SWITCH, PERFORMED AN OPERATIONAL CHECK OF THE NOSE WHEEL STEERING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (AIR COND. BAY)

IAH- DURING FLIGHT 3588 THE CREW NOTED THAT THE NUMBER 2 PACK ON IN FLIGHT PRODUCES BURNING SMELL AND SMOKE IN MAIN CABIN. IAH- MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 AIR CYCLE MACHINE, PERFORMED A OPERATIONAL CHECK OF THE AIRCONDITIONING SYSTEM, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPLICE — DISCONNECTED (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EXIT SECTION OF THE EMERGENCY LIGHTS IN THE FLOOR INOPEERATIVE. IAH- MAINTENANCE RESECURED THE CONNECTORS ON THE EMERGENCY LIGHT FLOOR STRIP BY SEAT 11 and 12, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED MAINTENANCE THE LEFT EMERGENCY EXIT SIDEWALL LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RECEPTACLE — BURNED (GALLEY)

IAH- THE CREW NOTED A ELECTRIC SMELL FROM THE GALLEY HOT JUG AREA. MAINTENANCE INSPECTED THE AIRCRAFT, AND, THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE C-CHECK, REMOVED AND REPLACED RECEPTACLE CONNECTORS AT AFT GALLEY AREA, PERFORMED A OPERATIONAL CHECK OF THE HOT JUG SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAILED (LEFT) · airframe 2,869 hrs · 1,992 cycles

CLT FLIGHT 4083. CREW REPORTED THAT THE LEFT HAND ENGINE FAILED IN FLIGHT, ATTEMPTED RESTARTS WERE UNSUCCESSFUL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ENGINE TO BE SEIZED-UP AND METAL ON THE CHIP DETECTORS. THE ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

CLT - FLIGHT 4083, THE CREW REPORTED THAT THE NUMBERONE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN OF FLIGHT. THE CREW TRIED TO RESTART THE ENGINE WITH NO SUCCESS, AND DIVERTED TO CLT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FILED OPEN AWAITING FINAL DETERMINATION OF CAUSE...

Part: LIGHT — INOPERATIVE (CABIN)

IAH- FLIGHT 3912, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE AFT SECTION OF THE AISLE PATH EMERGENCY EXIT LIGHTS WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — VIBRATION (LEFT)

IAH - FLT 4203, CREW REPROTED THAT DURING TAXI THE NR 1 ENGINE EMMITTED A HUMMING SOUND AND VIBRATION AT LOW TO MEDIUM POWER SETTINGS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENIGNE IAW ROLLS ROYCE MAINTENANCE MANUAL 71-00-00. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — INOPERATIVE (NR 1 FADEC)

ATL - FLT 4179 - THE CREW REPORTED THAT THE NR 1 ENGINE SHUTDOWN UNCOMMANDED IN FLIGHT. THE AIRCRAFT DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NR 1B FADEC WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FADEC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)