N19966

Part: DUCT — DAMAGED (AC PACK) · airframe 29,599 hrs · 21,492 cycles

SHV - FLIGHT DIVERTED, PACK 1 - 2 OVERLOAD DURING FLIGHT. REMOVED AND REPLACED DAMAGED TUBE ON RT PACK TMDV IAW EMB 145 AMM 21-60-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,504 hrs · 21,870 cycles

RIC - 4A CHECK A/C N19966 LT FWD EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED BAD POWER SUPPLY AND DEAD BATTERY AND INSTALLED REPAIRED POWER SUPPLY AND BATTERY IAW EMB-145 AMM II 33-50-04, OPERATIONAL CHECK GOOD. IPC 33-50-04 FIG 1 IT. 30 AND IT 60. POWER SUPPLY P/N ON: BA5-0933-901 S/N ON: C00438; BATTERY P/N ON: 2013-1A S/N: 96796. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FAULTY (NR 2) · airframe 29,139 hrs · 21,577 cycles

CLE FLT 6025 THE CREW REPORTED SMOKE IN CABIN WHILE AT FL240 DURING CRUISE FLIGHT. SMOKE SMELL IN COCKPIT AS WELL. THE AIRCRAFT DIVERTED INTO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.

Part: CLAMP — LOOSE (AC PACK) · airframe 28,757 hrs · 21,299 cycles

SUPPLEMENT - SAV - IAD - AFTER TAKEOFF THE CREW RECEIVED A BLEED 1 LEAK INDICATION AND REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT WHERE IT WAS INSPECTED BY MAINTENANCE. SEVERAL PACK DUCT CLAMPS WERE RETIGHTENED AND THE CABIN SMOKE WAS DETERMINED TO BE CONDENSATION. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY WAS CLEARED.

Part: ACM — MALFUNCTIONED (NR 1) · airframe 28,490 hrs · 21,081 cycles

FAR - FLIGHT 6084, DURING NR 2 ENGINE START WITH THE NUMBER ONE PACK ON, THE CREW REPORTED SMOKE IN THE COCKPIT. CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FINE DEBRIS TO BE COMING FROM THE PACK, AND NOT SMOKE. MAINTENANCE PLACED THE NUMBER ONE PACK ON MEL 21-51-00-1, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT DEN WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 28,464 hrs · 21,055 cycles

FAR FLT 6084 THE CREW REPORTED SMOKE IN THE COCKPIT AFTER NR 2 ENGINE START WITH NR 1 PACK ON. MAINTENANCE INSPECTED AND PLACED THE NR 1 PACK SYSTEM ON MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE. SUPPLEMENT TO FOLLOW.

Part: ACM — FAULTY (AC BAY) · airframe 28,464 hrs · 21,055 cycles

FAR FLT 6084 THE CREW REPORTED SMOKE IN THE COCKPIT AFTER NR 2 ENGINE START WITH NR 1 PACK ON. MAINTENANCE INSPECTED AND PLACED THE NR 1 PACK ON MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE. MAINTENANCE REPLACED THE NR 1 PACK AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.

Part: SWITCH — MALFUNCTIONED (COCKPIT) · airframe 25,803 hrs · 19,067 cycles

IAH - FLIGHT 2354, THE CREW REPORTED THAT THE CLIMB THRUST PUSHBUTTON WAS STUCK PUSHED IN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PUSHBUTTON SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — DEFECTIVE (NR 1 ENGINE) · airframe 25,529 hrs · 18,864 cycles

SHV - E1 BLEED VALVE FAIL IN FLIGHT. REMOVED AND REPLACED E1 BLEED VALVE IAW EMB 145 AMM 36-11-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TUBE — CRACKED (OIL SYSTEM) · airframe 25,440 hrs · 18,796 cycles

FLIGHT 2949 - EWR - FLIGHT CREW REPORTED ENGINE NR 2 HAD LOW OIL PRESSURE AND LOW OIL QTY ON EICAS DURING DESCENT. CREW DECLARED EMERGENCY AND PROCEEDED WITH EMERGENCY DESCENT AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED CRACKED OIL TUBE AND PERFORMED LEAK AND OPERATIONAL TESTS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 37-38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, LT FUSELAGE SKIN IS CRACKED AROUND RIVETS AT FR 79. REPAIRED SKIN IAW EC 5330-02023. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 24-25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 37-38. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM CORRODED AT FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK - CENTER OMEGA BEAM CORRODED AT FR 43-44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

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

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, CARGO DOOR LOWER CUTOUT HAS CORROSION. REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 43-44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

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

Part: MOUNT — CRACKED (RT ENGINE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, RT ENG FWD LOWER MOUNT CRACKED. REMOVED AND REPLACED RT ENG FWD LOWER MOUNT IAW EC 5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED BETWEEN FR 18 AND 20. REPAIRED OMEGA BEAM IAW EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,317 hrs · 18,702 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 18-23. REMOVED AND REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 24,410 hrs · 17,997 cycles

CLE - FLT 2743 - THE CREW REPORTED AN ELECTRICAL ODOR IN THE GALLEY, MOST NOTICEABLE NEAR THE COFFEEMAKER. MAINTENANCE INSPECTED AND DEFERRED SYSTEM ON NEF. SUPPLEMENT TO FOLLOW.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,743 hrs · 17,508 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHT ABOVE THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,739 hrs · 17,505 cycles

DSM - FLIGHT 2671 - THE CREW REPORTED THAT ROW 14 AISLE PATH LIGHTING WAS INOPERATIVE. THE CREW PLACED IT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH, MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — FRAYED (ANTI ICE T SWITC) · airframe 23,042 hrs · 17,049 cycles

CLE FLIGHT NR 2118 THE CREW REPORTED A STAB A/I FAIL MSG IN CLIMBOUT FROM CLE. THE CREW COMPLETED THE QRH INSTRUCTIONS AND MSG WAS STILL THERE. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE STAB ANTI/ICE VALVE AND REPAIRED THE WIRE TO THE ANTI-ICE LEAK THERMAL SWITCH. OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,094 hrs · 16,322 cycles

IAH - FLIGHT 2510 - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD AISLE PATH LIGHTING STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)

Part: HYDRAULIC LINE — CHAFED (HYDRAULIC SYS) · airframe 21,729 hrs · 16,075 cycles

SHV - AIRCRAFT 966, FLIGHT NUMBER 2504, EN ROUTE FROM IAH TO BIRMINGHAM HAD A NR 1 HYD SYSTEM FAILURE AT CRUISE ALTITUDE AND MADE AN EMERGENCY LANDING AT SHV. MAINTENANCE FOUND A CHAFED HYDRAULIC LINE AT FRAME 49-50 LT AND REPAIRED THE DISCREPANCY IAW EMB 145 AMM 20-10-03. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,569 hrs · 15,959 cycles

DURING ROUTINE MAINT, MX FOUND EMERGENCY LIGHT FLOOR STRIP AT ROWS 1 AND 2 INOPERATIVE. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: OIL COOLER — DIRTY (NR 2 ENGINE) · airframe 20,672 hrs · 15,372 cycles

IAH - FLIGHT 2206, THE CREW REPORTED THAT ENGINE TWO HAD HIGH OIL PRESSURE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE FUEL OIL COOLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SENSOR — FAULTY (NR 2 ENGINE) · airframe 20,670 hrs · 15,371 cycles

IAH - FLIGHT 2298, THE CREW REPORTED E2 HI OIL PRESSURE WHEN THROTTLES ADVANCED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE OIL PRESSURE SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRANSDUCER — FAULTY (NR 2) · airframe 20,584 hrs · 15,307 cycles

FLT 2609 - EWR - CREW REPORTED ENGINE NR 2 OIL PRESS SPIKE TO THE RED RANGE (ABOUT 165) AND PRESSURE STAYED IN THE AMBER FOR MORE THAN 5 MIN. CREW PERFORMED AIR RETURN AND ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED ENGINE NR 2 OIL PRESS/TEMP TRANSDUCER IAW EMB145 AMM 79-31-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 20,416 hrs · 15,152 cycles

SHV - DURING C-CHECK PANEL 191 RIGHT FWD UPPER SIDE HAS AN AREA OF DELAMINATION ON INTERNAL AND EXTERNAL SIDE AND LEFT FWD EDGE FOUND TO HAVE COMPOSITE DAMAGE. MAINTENANCE REPAIRED RIGHT FWD UPPER SIDE AND LEFT FWD EDGE IAW EC5350-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ATTACH FITTING — DAMAGED (LT AILERON) · airframe 20,416 hrs · 15,152 cycles

SHV - DURING C-CHECK LEFT AILERON PCA BRACKET HAT BUSHING HOLES ELONGATED. MAINTENANCE REMOVED AND REPLACED LEFT AILERON PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: ATTACH FITTING — DAMAGED (RT AILERON) · airframe 20,416 hrs · 15,152 cycles

SHV - DURING C-CHECK RIGHT AILERON PCA BRACKET HAT BUSHING HOLES ELONGATED. MX REMOVED AND REPLACED RIGHT AILERON PCA BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 18,327 hrs · 13,637 cycles

RIGHT OUTBOARD FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BLOWN FUSE ON NR 2 EMERGENCY LIGHT BATTERY PACK IAW RADIANT POWER CORP CMM 25-60-03, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FUSE — BLOWN (BATTERY PACK) · airframe 18,327 hrs · 13,637 cycles

RIGHT OUTBOARD FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BLOWN FUSE ON NR 2 EMERGENCY LIGHT BATTERY PACK IAW RADIANT POWER CORP CMM 25-60-03, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,115 hrs · 10,299 cycles

BNA - DURING MAINTENANCE INSPECTION, THE NEXT TO LAST EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED THE AFFECTED EMERGENCY LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 13,675 hrs · 9,963 cycles

IAH - FLIGHT 3347- THE CREW REPORTED A LOUD RUMBLE NOISE PASSING THROUGH 19K COMING FROM THE NOSE, AND DIFFICULTY MAINTAINING 1000 FPM CLIMB AT 23K TO 24K. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE THIRD UPLOCK PROXIMITY SWITCH. OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND WAS THEN APPROVED FOR RETURN TO SERVICE.

Part: HEAT EXCHANGER — ODOR (NR 1 A/C PACK) · airframe 13,533 hrs · 9,854 cycles

CREW REPORTED, BURNING SMELL IN COCKPIT. MAINTENANCE RAN NR 1 AIR CONDITIONING PACK FOR 20 MINUTES WITH NO SMELL NOTED IAW EMB145 MM 21-51-00, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 12,897 hrs · 9,348 cycles

EWR- CO2899, DURING SERVICE CHECK MAINTENANCE FOUND THE AFT EMERGENCY LIGHT FAILING TO LIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK NR 4 IAW EMB 145 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SIGN — LOOSE (EMERGENCY LIGHT) · airframe 12,836 hrs · 9,235 cycles

IAH - FLIGHT 2458, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE GALLEY OVERHEAD EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE LIGHT ASSEMBLY, OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

IAH - DURING ROUTINE INSPECTION, MAINTENANCE FOUND AFT EMERGENCY LIGHT STRIP NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP. OPERATIONAL TESTS WERE SATISFACTORY. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — FAULTY (EMERGENCY LIGHT)

DURING SERVICE CHECK MAINTENANCE FOUND THE AFT CABIN CEILING EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED NR 6 EMERGENCY EXIT SIGN LIGHT INVERTER IAW EMB145 AMM 33-50-01. OPS CHECKED SYSTEM GOOD.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

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

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV-DURING C-CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED AROUND THE NUT PLATES. 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: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV - DURING C-CHECK THE RT FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE RIGHT RAMP SUPPORT ANGLE 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 (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE CENTER FLOORBEAM 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: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

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

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE LEFT HAND MIDDLE FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED IN THE CARGO AREA FROM FRAME 65 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM BUTTSTRAP BETWEEN FRAMES 59-61 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: FIREWALL — CRACKED (APU BAY) · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE LEFT HAND AND RIGHT HAND SUPPORT ROD BRACKETS. MAINTENANCE PERORMED A DOUBLER REPAIR TO THE AFFECTED AREAS IAW EMB 145 SRM 53-32-13. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE CARGO DOOR SILL 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: CROSSBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

DURING C-CHECK THE CROSSBEAM BETWEEN FRAMES 23 AND 24 AT STRINGER 15R WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE MAIN DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PART IAW EMB 145 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,368 hrs · 8,144 cycles

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

Part: STRINGER — GOUGED (FUSELAE) · airframe 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED AT FRAMES 52-53. 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 11,368 hrs · 8,144 cycles

SHV- DURING C-CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. 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: LIGHT — INOPERATIVE (CABIN)

BTV---CO3389, DURING ROUTINE INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT ASSEMBLY IAW EMB145 MM 33-50-09. OPS CHECKED GOOD.

Part: BEAM — CORRODED

IAH, During C-check inspection the floor beam top plate at frame 14 was found to be corroded beyond limits. Maintenance repaired the affected portion of floor beam utilizing a splice repair in accordance with EMB 145 SRM 53-21-10

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH - MAINTENANCE FOUND CORROSION OUT OF LIMITS ON THE FLOORBEAM AT FRAME 20. A SPLICE REPAIR WAS ACCOMPLISHED ON THE AFFECTED AREA OF FLOORBEAM IN ACCORDANCE WITH THE EMB SRM 53-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (CABIN)

IAH- DURING "C" CHECK THE LEFT FLOOR BEAM WAS CORRODED AT FR. 59 TO 61. IAH- MAINTENANCE REMOVED THE CORROSION BETWEEN FRAMES 59 to 61, DRILLED OUT THE CORRODED AREA AND INSTALLED #5 RIVET, TREATED PRIMED AND PAINTED THE AREA, AND. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE AFTER RELEASE FROM "C" CHECK.

Part: FLOORBEAM — CORRODED (FUSELAGE)

IAH DURING C-CHECK INSPECTION IT WAS NOTED THAT CORROSION ON RIVET HEADS AND AROUND SCREW HOLES ON TOP OF FLOORBEAMS AT FRAME 20.

Part: CONTROL UNIT — FAILED (COCKPIT)

CLE FLIGHT 4233 THE CREW REPORTED A LOUD NOISE AND VIBRATION UNDER THE FLIGHT DECK ON CLIMB OUT. RECYCLED THE LANDING GEAR AND RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE. THE GEAR WAS RECYCLED AGAIN, RECEIVED 3 GREEN DOWN AND LOCK INDICATIONS. THE AIRCRAFT RETURNED AND LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEARING — FAILED (NLG)

MCI FLIGHT 4107 THE CREW REPORTED DURING TAXI TO THE GATE A LOUD SQUEAL AND VIBRATION WAS FELT FROM THE NOSE GEAR. MAINTENANCE INSPECTED AND FOUND THE RIGHT NOSE WHEEL BEARING HAD FAILED AND CAUSED DAMAGE TO THE STRUT AXLE.BOTH NOSE WHEEL ASSEMBLY''S WERE REPLACED ALONG WITH THE NOSE LANDING GEAR ASSEMBLY. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POTENTIOMETER — FAILED (NLG STEERING) · airframe 5,224 hrs · 3,488 cycles

MEM FLIGHT 3694. THE PILOT REPORTED THAT AFTER LANDING THEY RECEIVED A LANDING GEAR GROUND MESSAGE AND THE AIRCRAFT SLIGHTLY VEERED TO THE RIGHT. MAINTENANCE INSPECTED THE LANDING GEAR SYSTEM AND AFTER EXTENSIVE TROUBLESHOOTING THE AIRCRAFT WAS TEST FLOWN TO TYS. THE TEST FLIGHT WAS UNSATISFACTORY, MAINTENANCE REMOVED AND REPLACED THE RUDDER PEDAL POTENTIOMETER IAW EMB-145-MM 32-50-02, OPERATIONAL CHECKS AND TEST FLIGHT WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — OUT OF ADJ (NLG)

PIT FLIGHT 4141 ON LANDING IN PITT THE AIRCRAFT SKIDDED OFF THE RUNWAY. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE AND NO DAMAGE WAS FOUND. MAINTENANCE ALSO FOUND THE AIRCRAFT WAS PULLING TO THE RIGHT ON TAXI. FOUND THE STEERING CONTROL WHEEL WAS OFF 7 DEGREES. THE NOSEWHEEL STEERING TILLER WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE STEERING CONTROL MODULE AND STEERING MANIFOLD WERE REPLACED FOR PRECAUTIONARY REASONS.

Part: STRAP — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE CENTER BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 15 TO FRAME 18. MAINTENANCE REMOVED THE CORRISION, AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01141, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. A/C TT=3937.4 CYC=2616

Part: STRAP — CORRODED (CABIN)

IAH-DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CHAFED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING MAINTENANCE INSPECTION, THE LEFT WING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-07, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)