N14950

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 35,239 hrs · 26,594 cycles

F/A REPORTED THE LT COFFEEMAKER PRODUCED A BURN SMELL. MX REMOVED PLASTIC DEBRIS FROM COFFEEMAKER HOT PLATE AS NECESSARY. PERFORMED OPS CHECK SUCCESSFUL. NO FURTHER EVIDENCE OF BURN SMELL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CRADLE — INOPERATIVE (FLASHLIGHT) · airframe 34,952 hrs · 26,365 cycles

CREW REPORTED FA'S AFT FLASHLIGHT INOPERATIVE. INTIALLY PLACED ON MEL. MX R & R THE FA'S AFT FLASHLIGHT CRADLE WITH OPS CHECK SUCCESSFUL. ACFT WAS APRROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 100) · airframe 34,645 hrs · 26,107 cycles

DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE CRACKED BETWEEN FRAMES 7-8 AND STRINGERS 19R-20R. MX PERFORMED A DOUBLER REPAIR TO THE CRACKED AREA IAW EC5330-02685. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 34,645 hrs · 26,107 cycles

DURING C-CHECK THE AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 79, STRINGERS 6L TO 7L. MX REAMED OUT THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02686. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,645 hrs · 26,107 cycles

DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 11-13. MX R& R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 900) · corrosion level 2 · airframe 34,645 hrs · 26,107 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX REMOVED THE CORROSION AND PERFORMED A REPAIR IAW EC5320-01443. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,645 hrs · 26,107 cycles

DURING C-CHECK THE BELLY SKIN SPLICE AT FRAME 13 WAS FOUND TO BE CORRODED. BETWEEN STRINGERS 20R-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-00-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,028 hrs · 24,787 cycles

DURING MX INSPECTION, THE NR 2 AND 3 AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX R & R THE NR 3 EMERGENCY LIGHT DC/AC INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 30,815 hrs · 23,084 cycles

DTW FLT 5865 THE CREW REPORTED A BATTERY 2 OVERTEMP MESSAGE ON APPROACH. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH NR 1 AND NR 2 BATTERIES. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,979 hrs · 22,457 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROWS 8 & 9 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GASKET — BROKEN (BLEED AIR SYS) · airframe 29,981 hrs · 22,458 cycles

IAH - FLIGHT 2281, THE CREW REPORTED A SMELL OF SMOKE IN THE CABIN WHEN FLYING THROUGH RAIN. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT. REMOVED AND REPLACED THE 9TH STAGE BLEED DUCT GASKETS AT THE CHECK VALVE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,644 hrs · 22,203 cycles

SHV - DURING C-CHECK FUSELAGE FITTING-TO-VERTICAL STAB SPAR ATTACHMENT AT FRAME 75 HAS FRETTING CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON FITTING-TO-VERTICAL STAB SPAR ATTACHMENT AT FRAME 75 IAW EC5310-01317. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,644 hrs · 22,203 cycles

SHV - DURING C-CHECK BAGGAGE DOOR LOWER CUTOUT HAS CORROSION BETWEEN FRAME 67 & 68. MAINTENANCE REMOVED AND REPLACED BAGGAGE DOOR LOWER CUTOUT FRAME 67-68 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 29,295 hrs · 21,941 cycles

IAH - FLIGHT 2627, THE CREW REPORTED A STRONG FUEL/HYDRAULIC ODOR IN THE COCKPIT AND SEEMED STRONGER WHEN OPERATING OFF OF THE NUMBER ONE ENGINE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT, AND MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ZERO CABON SEAL, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROBE — FAILED (NR 1 TAT) · airframe 27,457 hrs · 20,586 cycles

FLIGHT 2408 - EWR - FLIGHT CREW REPORTED TAT NR 1 HEAT FAIL ON EICAS DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED TAT PROBE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 27,379 hrs · 20,526 cycles

FLIGHT 3073 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. EWR MX CLEANED AND LUBED MAIN DOOR MECHANISM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,071 hrs · 20,309 cycles

EWR - DURING SCHEDULED MAINTENANCE, MX FOUND FLOOR EMERGENCY LIGHT STRIP ADJACENT TO SEATS 9A AND 8A INOPERATIVE. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (AHRS) · airframe 26,631 hrs · 19,967 cycles

IAH - FLIGHT 2278, THE CREW REPORTED THAT THE AHRS 1 OVERHEATED ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AHRS 1 FAN AND INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — MALFUNCTIONED (AHRS) · airframe 26,631 hrs · 19,967 cycles

IAH - FLIGHT 2278, THE CREW REPORTED THAT THE AHRS 1 OVERHEATED ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AHRS 1 FAN AND INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 26,630 hrs · 19,953 cycles

TYS - A/C IN FOR A-CHECK WHEN INSPECTION FOUND THE EXIT SIGN FOR THE SERVICE DOOR TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN IAW AMM 33-50-14. OPS CHECK WAS GOOD AND WAS RELEASED.

Part: CONTROL UNIT — DEFECTIVE (SPOILER) · airframe 26,391 hrs · 19,769 cycles

FLIGHT 2730 - EWR - FLIGHT CREW REPORTED SPOILER FAIL MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SPOILER CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE HARNESS — INOPERATIVE (LT MLG) · airframe 26,021 hrs · 19,484 cycles

IAH - FLIGHT 2424 - THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT MLG NR 1 WOW SWITCH CONNECTOR, AND THE LEFT MLG NR 2 WOW SWITCH HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DAMAGED (RT MLG WOW) · airframe 26,021 hrs · 19,484 cycles

IAH - FLIGHT 2424 - THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT MLG NR 1 WOW SWITCH CONNECTOR, AND THE LEFT MLG NR 2 WOW SWITCH HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (LT MLG) · airframe 26,021 hrs · 19,484 cycles

CVG - FLT 2424 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT DURING CLIMB FROM CVG. THE AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT GEAR NR 2 WOW SWITCH HARNESS AND THE RIGHT GEAR NR 2 WOW SWITCH CONNECTOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 25,794 hrs · 19,302 cycles

FLIGHT 2560, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS INSPECTED AND SUBSEQUENTLY FERRIED TO WHERE IT LANDED WITHOUT INCIDENT, AND MX REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH CONNECTOR, RT MLG SHOCK PROX SWITCH CONNECTOR, AND REMOVED, REPLACED, AND ADJUSTED THE RT MLG PROXIMITY SWITCH, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — INOPERATIVE (RT MLG) · airframe 25,794 hrs · 19,302 cycles

FLIGHT 2560, THE CREW REPORTED A LANDING GEAR, AIR GROUND FAILURE MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS INSPECTED AND SUBSEQUENTLY FERRIED TO WHERE IT LANDED WITHOUT INCIDENT, AND MX REMOVED AND REPLACED THE NLG WOW PROXIMITY SWITCH CONNECTOR, RT MLG SHOCK PROX SWITCH CONNECTOR, AND REMOVED, REPLACED, AND ADJUSTED THE RT MLG PROXIMITY SWITCH, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 25,758 hrs · 19,275 cycles

IAH - FLIGHT 2648, DURING CLIMB THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 25,640 hrs · 19,186 cycles

FLIGHT 2331 - EWR - FLIGHT CREW REPORTED LANDING GEAR FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY AND PROCEED WITH AIR RETURN. CREW LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WINDOW POST — CORRODED (ZONE 200) · airframe 25,082 hrs · 18,777 cycles

SHV-DURING C-CHECK COPILOT WINDSHIELD CUTOUT STRUCTURE LOWER O/B SCREW HOLES CORRODED. MX CLEANED LOWER CO-PILOT WINDSHIELD CUTOUT NUTPLATE HOLES AND FOUND DIRT AND DEBRIS ONLY, NO CORROSION FOUND ON LOWER O/B HOLES IAW 145 CPM 51-00-01. MX ALODINED, PRIMED AND PAINTED CO-PILOT WINDSHIELD LOWER O/B SCREW HOLES IAW EMB-145 CPM 51-21-07. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WINDOW POST — CORRODED (ZONE 200) · airframe 25,082 hrs · 18,777 cycles

SHV-DURING C-CHECK PILOT WINDSHIELD CUTOUT STRUCTURE LOWER O/B SCREW HOLES CORRODED. MX CLEANED PILOT WINDSHIELD CUTOUT STRUCTURE LOWER O/B SCREW HOLES AND FOUND NO CORROSION ONLY DIRT AND DEBRIS IAW CPM 51-00-01. MX THEN ALODINED, PRIMED AND PAINTED PILOT WINDSHIELD LWR O/B SCREW HOLES IAW EMB-145 CPM 51-21-07. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 33 AND 34. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK STR 19L HAS CORROSION BETWEEN FR 65-68. R&R STRINGER IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 250,821 hrs · 18,777 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 33-34. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, SKIN PANEL BETWEEN FR 61-69 STR 21L-15L HAS CORROSION. REPAIRED SKIN PANEL AND REPLACED RIVETS IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED LT OMEGA BEAM AT FR 29 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, RT GROUND SPOILER ATTACHMENT BRACKET HAS MIG HAT BUSHING. R&R RT GROUND SPOILER ATTACHMENT BRACKET IAW EMB 145 AMM 57-51-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 59. REPAIRED CENTER OMEGA BEAM IAW IC2009-145/00195. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, STRINGER 18L HAS CORROSION BETWEEN FR 65-68. REMOVED AND REPLACED STRINGER IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 49-50. REPAIRED CENTER OMEGA BEAM IAW IC 2009-145/00195. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK LT OMEGA BEAM AT FR 59 HAS CORROSION. REPAIRED LT OMEGA BEAM IAW IC2009-145/00197. THIS ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK RT OMEGA BEAM @ FR 59 HAS CORROSION. REPAIRED RT OMEGA BEAM IAW IC2009-145/00197. THIS ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, STR 20L HAS CORROSION BETWEEN FR 60-61. REPAIRED STRINGER IAW EMB 145 SRM 51-40-02 AND 53-00-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 45-50. REPAIRED LT OMEGA BEAM IAW IC2009/145-00195. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, STR 19L CORRODED AT FR 61. R&R STRINGER 19L IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

CORROSION STR. 17L FR.63-64. R&R STRINGER 17L IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, CARGO DOOR LOWER CUTOUT CORRODED. R&R CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

CORROSION STR. 21L FR.65-68. R&R STRINGER 21L IAW EMB 145 SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME SPLICE — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK. CIRCUMFERENTIAL SPLICE AFT OF FR 66 HAS AREAS OF CORROSION STR. 19L - 21R. R&R CIRCUMFERENTIAL SPLICE AT STR 19L-21R IAW EMB 145 SRM 53-00-02. THIS ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, LT AILERON BRACKET HAS MIGRATED HAT BUSHINGS. R&R AILERON BRACKET IAW EC5750-01177. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPLICE — CORRODED (ZONE 100) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK. LONGITUDINAL SPLICE HAS AREAS OF CORROSION FR. 65-68 STR 19L-20L. R&R SPLICE IAW EMB 145 SRM 53-00-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 29-30. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

SHV DURING C-CHECK CENTER OMEGA BEAM CORRODED FR 38. MX REPAIRED CENTER OMEGA BEAM FR 38 IAW EMB-145 SRM 53-00-10 AND CPM 51-21-06. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

SHV DURING C-CHECK CENTER OMEGA BEAM CORRODED AT CARBON CROSSBEAM FR 33-34. MX REPAIRED CENTER OMEGA BEAM BTWN FR 33-34 IAW EMB-145 SRM 53-00-10 FIG 203. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

SHV DURING C-CHECK LT OMEGA BEAM CORRODED I/B SIDE LWR FLANGE AT FR 29. MX REPAIRED LT OMEGA BEAM I/B SIDE LWR FLANGE AT FR 29 IAW EMB-145 SRM 53-00-10 FIG. 202. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,082 hrs · 18,777 cycles

SHV DURING C-CHECK LT OMEGA BEAM CORRODED I/B SIDE FR 33-34. MX REPAIRED LT OMEGA BEAM BTWN FR 33-34 IAW EMB-145 SRM 53-00-10 FIG. 202. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE IN THE AFT CABIN. MAINTENANCE INSPECTED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. (A)

Part: UNKNOWN — SMOKE (CABIN) · airframe 20,730 hrs · 15,676 cycles

FLT 2438 - ORF - CREW REPORTED SMOKE IN CABIN. PACK NR 1 SYSTEM WAS MELED. MX IAH PERFORMED OPERATIONAL CHECK OF PACK SYSTEMS 1 AND 2 AND COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL AND FUNCTIONAL CHECKS WERE PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — ODOR · airframe 20,418 hrs · 15,439 cycles

IAH - FLIGHT 2367, THE CREW REPORTED SMOKE IN THE CABIN AND A LAV SMOKE WARNING AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED GROUND RUNS AND FOUND THE ODOR TO BE RESIDUAL OIL. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 20,418 hrs · 15,438 cycles

IAH - FLIGHT 2978, THE CREW REPORTED THAT ON TOUCHDOWN HAD HEAVY SMOKE IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 19,264 hrs · 14,510 cycles

FLIGHT 2321 - THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTING HAD SEGMENTS THAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A CHAFED WIRE ON THE LIGHT STRIP AT SEAT 7A. THE WIRE WAS REPAIRED, LIGHTING OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,253 hrs · 13,725 cycles

MCI - DURING MAINTENANCE INSPECTION THE GALLEY OVERHEAD AND LEFT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND FOUR INVERTERS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 16,439 hrs · 12,294 cycles

FLIGHT 2442 EWR TO GSP: DURING CLIMBING OUT OF EWR, CREW REPORTED PRESSURIZATION PROBLEMS. FLIGHT WAS DIVERTED TO RIC. RIC MAINTENANCE REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER. MAINTENANCE PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS THEN APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,331 hrs · 12,212 cycles

STL - DURING SCHEDULED MAINTENANCE, THE EMERGENCY EXIT SIGN AT ROW 3BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN INVERTER, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,020 hrs · 11,953 cycles

CLE - THE CREW REPORTED THE EMERGENCY EXIT SIGN ON THE FORWARD WIND SCREEN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,479 hrs · 11,516 cycles

SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM I/B SIDE FWD OF FRM 44. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR IAW EMB 145 SRM 53-23-10. NO FURTHER ACTION REQUIRED PER EC 5320-01219. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

CLE FLIGHT 2249, THE CREW REPORTED THE EMERGENCY LIGHT IN THE CABIN AT SEAT 3B WAS NOT WORKING. MAINTENANCE INSPECTED AND CONNECTED EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 3158 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: TUBE — LEAKING (NR 1 ENGINE)

ON APPROACH INTO CUU THE NR 1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. THE AIRCRAFT LANDED AT CUU WITHOUT INCIDENT WHERE THE AIRCRAFT WAS INSPECTED. THE OIL PRESSURE TUBE ASSEMBLY/REGULATING TEE, WAS FOUND TO BE LEAKING AND WAS REPLACED. THE NR 1 ENGINE OIL WAS SERVICED, LEAK CHECKED AND THE DISCREPANCY CLEARED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE FUSELAGE SKIN BETWEEN FRAMES 67 AND 71 STRINGERS 15R AND 20L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW EC 5330-01065. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT 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 FIGURE 204 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RAMP ANGLE ON THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 18 AND 19 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 20 AND 23 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: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CARGO DOOR CUTOUT BEAM 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: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 14 AND 17 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED OMEGA BEAM IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK CENTER BUTTSTRAP WAS FOUND TO HAVE CORROSION AT NUTPLATES BETWEEN FRAMES 14 AND 17. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INTAKE — GOUGED (NR 1 COWLING) · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK THE NUMBER ONE ENGINE INTAKE WAS FOUND TO BE GOUGED AT THE TOP COWLING GUIDE PIN HOLE. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5410-01067. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STIFFENER — GOUGED (RT COWLING) · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT HAND LOWER COWLING AFT INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 58 AND 61 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: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE LEFT HAND SILL AT FRAME 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (RT COWLING) · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 12,033 hrs · 8,843 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 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM BETWEEN FRAMES 58 AND 61 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 12,033 hrs · 8,843 cycles

SHV-DURING C CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 58 AND 61 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: CAP — GOUGED (MLG) · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK AFT LOWER MAIN LANDING GEAR BEARING CAP WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED AFT LOWER MAIN LANDING GEAR BEARING CAP IN ACCORDANCE WITH EMB 145 AMM 32-10-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: SKIN — GOUGED (LT COWLING) · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK LEFT LOWER ENGINE COWLING WAS FOUND TO BE GOUGED APPROXIMATELY 24 INCHES FROM AFT END. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A PATCH REPAIR IN ACCORDANCE WITH EMB 145 SRM 54-40-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: CAP — CORRODED (RT MLG) · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK RIGHT MAIN LANDING GEAR LOWER BEARING CAP WAS FOUND TO BE PITTED. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR LOWER BEARING CAP IN ACCORDANCE WITH EMB 145 AMM 32-10-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK CENTER OMEGA BEAM WAS IDENTIFIED AS CORRODED AT FR 19-22. MAINTENANCE REMOVED AMD REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 12,033 hrs · 8,843 cycles

SHV DURING C CHECK STR 19L WAS IDENTIFIED AS GOUGED FR 52-53. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB 145 SRM 53-24-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,866 hrs · 5,623 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND DIGITAL AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE AFFECTED DIGITAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — NOISY

CLE FLIGHT#4119 THE CREW REPORTED THEY HEARD A "BANG" NOISE DURING GEAR RETRACTION.THE SOUND WA S COMING FROM THE NOSE AREA.MAINTENANCE INSPECTED AND REPLACED THE LEFT NOSE GEAR DOOR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,500 hrs · 4,688 cycles

TYS DURING A SCHEDULED INSPECTION THE FORWARD RIGHT HAND EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD RIGHT HAND EMERGENCY EXIT LIGHT ASSEMBLY IAW EMB-145 MM 33-50-10. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.

Part: SENSOR — INOPERATIVE (RT MLG)

IAH - FLIGHT 4095, THE CREW REPORTED THAT A LANDING GEAR AIR/GND FAIL MESSAGE APPEARED BEFORE THE GEAR WERE FULLY RETRACTED, AND DISAPPREARED AFTER FULL RETRACTION. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR LOWER PROXIMITY SENSOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CRACKED (VERTICAL TO BODY)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EA5330-01032, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP AT FRAME 21 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL TO BODY)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINGEERING CHANGE AND REPAIR AUTHORIZATION EA5330-01032, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M0

Part: SMOKE — DETECTED (CABIN)

EWR - FLT 4209 - CREW REPORTED SMOKE IN CABIN AND LAV SMOKE MSG ON EICAS. MAINTENANCE TROUBLESHOOTING SYSTEM. (M)

Part: LIGHT — INOPERATIVE (LT & RT OVERWING)

EWR - FLT 4218 - DURING 3A INSPECTION MAINTENANCE, FOUND EMERGENCY LIGHTS OVER LEFT AND RIGHT WING INOPEATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY AND OPS CHECK SYSTEM GOOD. (M)

Part: CARBON SEAL — WORN (RT ENGINE)

EWR - FLT 4209 - CREW REPORTED THAT AFTER TAKEOFF SMOKE WAS NOTICED IN THE CABIN AND RECEIVED A LAVATORY SMOKE INDICATION ON THE EICAS. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE RIGHT ENGINE FAN SHAFT SEAL (ZERO CARGO SEAL) WAS LEAKING OIL INTO THE COMPRESSOR SECTION. THE AIRCRAFT WAS MAINTENANCE FERRIED TO TYS AND THE RIGHT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY)

CLE - FLT 3961 - AFTER TAKEOFF FROM CLEVELAND, THE CREW REPORTED A LAVATORY SMOKE WARNING INDICATION. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED SMOEK DETECTOR PANEL IAW 145 EMB MM 26-14-02. MAINTENANCE ALSO REPLACED THE LAVATORY SMOKE SENSOR IAW 26-14-01. PERFORMED OPERATIONAL CHECKS IAW 26-14-00. MAINTENANCE DID NTO DETECT ANY EVIDENCE OF SMOKE. THE AIRCRAFT WAS RELEASED FOR SERVICE (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

CLE - FLT 3961 - AFTER TAKEOFF FROM CLEVELAND, THE CREW REPORTED A LAVATORY SMOKE WARNING INDICATION. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR PANEL IAW 145 EMB MM 26-14-02. MAINTENANCE ALSO REPLACED THE LAVATORY SMOKE SENSOR IAW 26-14-01. PERFORMED OPERATIONAL CHECKS IAW 26-14-00. MAINTENANCE DID NOT DETECT ANY EVIDENCE OF SMOKE. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SWITCH — FAILED (RT MLG)

CLE - FLT 3875 - THE CREW REPORTED, RECEIVED LANDING GEAR AIR/GROUND FAIL MESSAGE DURING LANDING APPROACH. THE LANDING WAS ABORTED AND THE CREW PERFORMED THE PROCEDURES IN THE QRH MANUAL. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 WEIGHT ON WHEELS SWITCH ON THE RIGHT MAIN LANDING GEAR. OPERATIONAL CHECKS WERE GOOD IAW EMBRAER 145 MM 32-63-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: BRAKE — FAILED (LT TE FLAP)

CLE - THE CREW REPORTED THAT AFTER TAKEOFF THE FLAP LOW SPEED ADVISORY CAME ON, THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT AND RIGHT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27-51-01, SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB145 MM 27-51-00-700-801-A. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: BRAKE — FAILED (LT TE FLAP)

CLE - THE CREW REPORTED THAT AFTER TAKEOFF THE FLAP LOW SPEED ADVISORY CAME ON, THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT AND RIGHT FLAP TRANSMISSION BRAKES IAW EMB145 MM 27-51-01, SYSTEM OPERATIONAL CHECK WAS GOOD IAW EMB145 MM 27-51-00-700-801-A. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: APU — SEIZED (TAILCONE)

EWR - CREW REPORTED SMOKE IN COCKPIT AND CABIN ON GROUND WITH APU RUNNING, THE APU SHUTDOWN AUTOMATICALLY. MAINTENANCE FOUND APU SEIZED AND WON'T TURN. APU FAILURE. AIRCRAFT RELEASED IAW MEL 49-00-00 PLACARD NR 175634. APU CHANGED RAN AND OPERATIONALLY CHECKED GOOD. (M)

Part: BULB — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING 1A INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LGEU — MALFUNCTIONED (LANDING GEAR)

LG AIR/GND FAIL MESSAGE IN FLIGHT. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT (LGEU) IAW EMB145 MM 32-32-01. OPS CHECK GOOD. THIS WAS AN AIR RETURN. (M)

Part: CHARGER — INOPERATIVE (CABIN)

IAH - DURING 3A CHECK, FOUND LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY PACK CHARGER/INVERTER IAW EMB-145 MM 33-50-11. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - FLT 4191 - THE PILOT REPORTED THE FORWARD AISLE PATH LIGHTING AT THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER/POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)