N16944

Part: LIGHT — SHORTED (COCKPIT) · airframe 31,036 hrs · 30,387 cycles

CREW REPORTED COCKPIT READING LIGHT CIRCUIT BREAKER TRIPPED WITH A BURNING ODOR. MX INSPECTED AND R & R F/O'S READING LIGHT ASSY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — OVERHEATED (CABIN) · airframe 30,315 hrs · 29,677 cycles

THE CREW REPORTED A PLASTIC ODOR FROM THE CABIN DOOR ENTRYWAY. MX VERIFIED THE ODOR TO BE COMING FROM THE F/A CABIN LIGHT CONTROL MODULE, DEACTIVATED THE MODULE AND PLACED ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. MX R & R THE AFFECTED CABIN LIGHT CONTROL MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,114 hrs · 29,482 cycles

DURING C-CHECK, THE CENTER FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 14-15 AND STRINGERS 19R-20L. MX R & R THE SKIN IAW EC5330-02761. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 30,114 hrs · 29,482 cycles

DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED DIRECTLY BELOW THE PILOTS DV WINDOW AT STRINGER 9L. MX R & R THE CRACKED FRAME SECTION IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAL — LOOSE (CARGO DOOR) · airframe 28,892 hrs · 28,244 cycles

THE CREW REPORTED A RAPID DEPRESSURIZATION (>3000FPM) WHILE CLIMBING THROUGH 21,000' AND THAT THEY COULD NOT RECOVER PRESSURIZATION. THE CREW PERFORMED AN EMERGENCY DECENT AND LEVELED OFF AT 10,000'. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, FOUND SEAL ON CARGO DOOR LOWER SIDE HAD COME OFF. MX REINSTALLED THE DOOR SEAL, OPERATIONALLY CHECKED PRESSURIZATION AND LEAK CHECKED CARGO DOOR ALL WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 26,822 hrs · 26,183 cycles

FLIGHT 4641, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING FROM ROW 8-12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE EMERGENCY LIGHT BATTERY AT ROW 12A, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,475 hrs · 25,831 cycles

IAH - THE CREW REPORTED A BURNING SMELL IN THE LAV THAT SEEMED TO BE AROUND THE LIGHT. MAINTENANCE INSPECTED THE LAV ARE, AND COULD NOT DUPLICATE THE SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 24-29. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 30-35. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (LT WING) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK LT WING SKIN HAS CRACK JUST FWD OF GROUND SPOILER CTR HINGE POINT. REPAIRED SKIN IAW EC5740-01276. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - LT OMEGA BEAM HAS CORROSION AT FR 50. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK - CENTER OMEGA BEAM HAS CORROSION AT FR 58. REPAIRED OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK LT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 3L TO 6L. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK RT SKIN CRACKED AT FR 75 STR 2R. REPAIRED SKIN IAW EC5330-02340. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK RT FUSELAGE SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 AND 79 STR 4R TO 7R. REPAIRED SKIN CRACKS IAW EC5330-02337. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,265 hrs · 24,602 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 54. REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: JACK — INOPERATIVE (COCKPIT) · airframe 20,393 hrs · 15,574 cycles

IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS BOOM MIC JACK, HAND MIC JACK, RECONNECTED THE F/O'S HAND MIC JACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: JACK — DISCONNECTED (COCKPIT) · airframe 20,393 hrs · 15,574 cycles

IAH - FLIGHT 2586, DURING CLIMB THE CREW REPORTED THE NUMBER ONE COMM HOT MIC WAS TRANSMITTING CONTINUOUSLY. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS BOOM MIC JACK, HAND MIC JACK, RECONNECTED THE F/O'S HAND MIC JACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 25,246 hrs · 24,581 cycles

IAH - FLIGHT 2304 A BURNING SMELL WAS NOTICED IN THE CABIN AT ROW 5. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY AT ROW 5A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,719 hrs · 24,030 cycles

IAH - FLIGHT 2935, DURING POST-FLIGHT INSPECTION THE CREW REPORTED SOME EXIT ROW FLOOR LIGHTING TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 14,604 hrs · 23,914 cycles

CRP - FLIGHT 2096, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE NR 2 PFD WENT BLANK AND SMOKED. THE PFD WAS PLACED ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 PFD, OPERATIONALLY TESTED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,818 hrs · 23,094 cycles

CRP - DURING PRE FLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE COCKPIT CROWN PANEL SKIN BY THE CAPTAINS DV WINDOW. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE CROWN PANEL SKIN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — DEFECTIVE (AC BAY) · airframe 23,498 hrs · 22,761 cycles

IAH - FLIGHT 2569, THE CREW REPORTED THAT THE PACK TWO VALVE CLOSED ON CLIMBOUT WITH NO PRESSURIZATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE PACK 2 EXHAUST DUCT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (AC SYSTEM) · airframe 23,490 hrs · 22,752 cycles

IAH - FLIGHT 2165, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED TWICE DURING CLIMB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, RE-SECURED SEVERAL CLAMPS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 23,490 hrs · 22,752 cycles

IAH - FLIGHT 2165, THE CREW REPORTED THAT THE BLEED 1 VALVE CLOSED FROM T/O TO 10'000 FEET. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED SEVERAL CLAMPS, OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — LEAKING (BLEED AIR SYS) · airframe 23,459 hrs · 22,716 cycles

IAH - FLIGHT 2617, THE CREW REPORTED A BLEED ONE LEAK MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PRECOOLER, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LANDING GEAR — LOW (NLG) · airframe 23,443 hrs · 22,698 cycles

IAH - FLIGHT 2413, THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE AFTER TAKEOFF WITH A THRUST REVERSER DISAGREE EICAS MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND SERVICED THE NOSE LANDING GEAR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: METERING UNIT — MALFUNCTIONED (NR 2 ENGINE) · airframe 22,624 hrs · 21,800 cycles

MFE - FLIGHT 2627, THE CREW REPORTED THAT E2 WOULD NOT ADVANCE 85 PERCENT N2 OR 90 PERCENT N1 AND ITT WAS SPIKING ERRONEOUSLY BETWEEN 300-500 DEGREES, WITH AN EICAS CHECK MESSAGE ON MFD WITH BOTH IGNITERS ON FOR E2. THE ISSUE RESOLVED ITSELF AFTER TWO MINUTES, AND THE AIRCRAFT LANDED AT MFE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO FPMU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 21,309 hrs · 20,400 cycles

IAH DURING A CHECK INSPECTION THE AFT 3 AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY LIGHTING OVERHEAD AND FLOOR BY EMERGENCY EXITS ARE DIM. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD. (S)

Part: SKIN — CRUSHED (FUSELAGE) · airframe 18,825 hrs · 17,860 cycles

TYS - AIRCRAFT SUFFERED GROUND DAMAGE FROM A BAGGAGE CART TO THE FUSELAGE UNDER WINDOWS 4 AND 5. MAINTENANCE REMOVED AND REPLACED STRINGERS 11L, 12L AND FRAME 27 AND 2 SHEAR CLIPS ON FRAME 29 AND 30. REPLACED SKIN PANEL FROM FRAME 23 TO FRAME 36. ALSO, REPLACED LT WING LEADING EDGE. ALL WORK WAS ACCOMPLISHED IAW EA5330-01104. STRINGER P/N-145-20559-005-S/N-145-21675-001.

Part: LAMP — FAILED (CABIN LIGHTS) · airframe 17,512 hrs · 16,429 cycles

EWR LOG SQUAWK ELECTRICAL SMOKE ODOR IN THE CABIN. FOUND TO BE FORWARD SIDEWALL LIGHT ON SEAT 1A. MEL'D. LATER RE-LAMPED LIGHT AT SEAT 1A 2A IAW EMB145 AMM 33-21-01. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,131 hrs · 14,823 cycles

TYS - DURING A ROUTINE C-CHECK INSPECTION THE RIGHT SIDE OMEGA BEAM IN THE GALLEY WAS CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGE AREA AND FABRICATED A NEW PART AND INSTALL DOUBLER IAW EC5320-01291. ALL WORK WAS ACCOMPLISHED AND A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 16,131 hrs · 14,823 cycles

TYS - DURING A SCHEDULE 2C INSPECTION CORROSION WAS FOUND AT THE CARGO DOOR CUTOUT ON LOWER SILL AT STR 16L AT FR 65. MAINTENANCE BLENDED ALL SIGNS OF CORROSION, CUT OUT DAMAGE SECTION, FABRICATED A SPLICE AND CUT A NEW SECTION OF SHEAR CLIP. INSTALLED SPLICE AND SHEAR CLIP, ALODINED, PRIMED AND PAINTED IAW EC5320-01293. A/C WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: BEARING — WORN (VERTICAL STAB) · airframe 14,119 hrs · 12,650 cycles

TYS DURING A MODIFICATION OF AIRCRAFT, INSPECTION FOUND THE VERTICAL STAB, LEFT HAND SPHERICAL BEARING HAD AXIAL AND LATERAL PLAY. MAINTENANCE REAMED THE THE VERTICAL BEARING HOUSING AND INSTALL NEW BUSHINGS IAW EC5510-01108. ALL WORK WAS ACCOMPLISHED AND OPS CHECKS GOOD. A/C WAS REL AFTER ALL WORK WAS C/W WITH.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 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 11,840 hrs · 10,195 cycles

SHV- DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 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: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV- DURING C-CHECK THE SERVICE 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: STRUCTURE — GOUGED (LT COWLING) · airframe 11,840 hrs · 10,195 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: STRUCTURE — GOUGED (RT COWLING) · airframe 11,840 hrs · 10,195 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE FORWARD DIGITAL PANEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FORWARD DIGITAL PANEL IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A FILLER REINFORCEMENT REPAIR IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

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

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 18 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: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV- DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 65 AND 68 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: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,840 hrs · 10,195 cycles

SHV- DURING C-CHECK THE LEFT HAND SILL BETWEEN FRAMES 61 AND 64 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: ANGLE — WARPED (CABIN) · airframe 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE CARGO DOOR CUTOUT FRAME 66 ANGLE WAS FOUND TO BE WARPED OUT OF CONFIGURATION. 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 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE OMEGA BEAM BUTTSTRAP AT FRAME 58 TO 62 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 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE CARGO DOOR LOWER CUTOUT BEAM WAS FOUND TO 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 11,840 hrs · 10,195 cycles

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

Part: ANGLE — WARPED (FUSELAGE) · airframe 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE CARGO DOOR CUTOUT FRAME 66 ANGLE WAS FOUND TO BE WARPED OUT OF CONFIGURATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — WARPED (FUSELAGE) · airframe 11,840 hrs · 10,195 cycles

SHV-DURING C-CHECK THE ANGLE ON THE CARGO CUT FRAME 67 WAS FOUND TO BE WARPED OUT OF CONFIGURATION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CLE FLIGHT 2135 THE CREW REPORTED THE EMERGENCY SIGN ON THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE CHECK MAINTENANCE FOUND OVERWING EMERGENCY LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY AND BATTERY CHARGER. OPERATIONAL CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

BDL FLIGHT NR 2351 THE CREW REPORTED THE EMERGENCY LIGHTING DID NOT TEST AFT OF THE EMERGENCY EXIT ROW. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHT)

DURING ROUTINE MAINTENANCE BOTH OVERWING EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 POWER SUPPLY AND THE RIGHT OVERWING LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (EMERGENCY)

THE CREW REPORTED THE EXIT LIGHT BY THE MAIN CABIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET POWER. PERFORMED OPERATIONAL CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

THE CREW REPORTED THE AFT SECTION OF THE AISLE PATH EMEREGENCY LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LIGHT STRIP SECTION. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (FUSELAGE)

DURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY LIGHT DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD.

Part: COLLAR — DAMAGED (NLG) · airframe 11,288 hrs · 9,641 cycles

BTV---CO 2943, DURING 2A INSPECTION FOUND DENT/CRACK DAMAGE TO NOSE LANDING GEAR COLLAR . DURING REMOVAL PROCESS FOR REPLACEMENT OF THE DAMAGED COLLAR, INSPECTED AND FOUND SLIDING TUBE ASSEMBLY DAMAGED AND INNER BORE OF NOSE LANDING GEAR DAMAGED (DEEPLY SCORED) CAUSED BY LOCKING BOLT SHEARED ON TOP OF THE STRUT BARREL. REMOVED AND REPLACED NOSE LANDING GEAR ASSEMBLY IAW EMB145 AMM NR 32-20-01 WITH SERVICEABLE UNIT, OPS. CHECKED AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — ERRATIC (MLG)

CLE FLIGHT 2367 THE CREW REPORTED A LANDING GEAR AIR/GROUND CAUTION MESSAGE ON DESCENT. THE SOLENOID SWITCH IN THE GEAR HANDLE CYCLING WITH THE GEAR DOWN.THE MESSAGE CLEARED ON ROLLOUT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROL UNIT — FAULTY (COCKPIT)

ROC FLIGHT 2160 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT ON CLIMBOUT. THE AIRCRAFT RETURNED TO ROC AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — LOOSE (CABIN) · airframe 10,593 hrs · 8,936 cycles

EWR ON PREFLT FOUND MAIN CABIN DOOR EMERGENCY LIGHTS INOP. RERACKED EMERGENCY BATTERY IAW EMB 145MM 33-50-04. OPS CHECK GOOD.

Part: MANIFOLD — CRACKED (#2 ENGINE)

DURING INSPECTION MAINTENANCE FOUND THE #2 ENGINE BLEED DUCT MANIFOLD CRACKED APPROX. 4.5 INCHES.THE DUCT IS LOCATED AT THE 14 STAGE BLEED VALVE AT THE TOP OF THE ENGINE.MAINTENANCE REPLACED THE 14TH STAGE CUSTOMER BLEED DUCT MANIFOLD.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — FAULTY (LEFT GEAR)

CLE FLIGHT#3085 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE RIGHT AND LEFT WOW PROXIMITY SWITCHES ON THE LEFT MAIN GEAR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BLEED VALVE — WORN (APU)

CLE FLIGHT 3040 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WITH APU RUNNING WITH BLEEDS ON. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — STICKING (APU)

CLE FLIGHT# 3157 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN AFTER APU START.MAINTENANCE INSPECTED AND STRAIGHTENED A KINKED DRAIN HOSE AND REPLACED THE COMBUSTOR DRAIN CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

CLE FLIGHT 3151 THE CREW REPORTED A FUEL ODOR IN THE CABIN DURING APU START. MAINTENANCE PERFORMED OPERATIONAL CHECKS GOOD. NO FUEL SMELL WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (COCKPIT)

CLE FLIGHT 3015 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN AND COCKPIT WHEN THE APU WAS STARTED. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — STICKING (APU)

CLE FLIGHT# 4065 THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN WHEN THE APU WAS STARTED.MAINTENANCE REPLACED THE APU START FUEL CHECK VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DRAIN LINE — LOOSE (APU)

CLE FLIGHT#3275 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER APU START ON THE GROUND OR IN FLIGHT.MAINTENANCE INSPECTED AND RESECURED DRAIN LINE ON THE APU FUEL PUMP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — FAULTY (APU BAY)

IAH- DURING FLIGHT NUMBER 3973 FROM PNS TO IAH, IN FLIGHT, THE APU WAS STARTED AND STRONG SMELL OF JET-A FUEL WAS NOTED IN THE COCKPIT AND CABIN. DURING START, APU RPM REACHED 15 PERCENT, THEN 10 PERCENT, BEFORE STARTING UPWARD TO 103 PERCENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE REMOVED AND REPLACED THE APU, PERFORMED A OPERATIONAL CHECK AND A LEAK CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,620 hrs · 6,166 cycles

IAH - DURING C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH EMB-145 SRM 53-21-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,620 hrs · 6,166 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND DIGITAL RECESS CENTER GUSSET WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GUSSET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,620 hrs · 6,166 cycles

IAH - DURING C-CHECK INSPECTION, THE RIGHT HAND DIGITAL RECESS HAT SECTION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HAT SECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

CLE FLIGHT 3862 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT STAY ON WHEN ACTIVATED. MAINTENANCE REPLACED THE NR 1, 2, 3, 4 EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.NR 2 S/N 63071 TSN4496/CSN3372/, NR 3 S/N 49851 TSN1719/CSN1557, NR 4 S/N 63662 TSN4246/CSN325, TSO 703.

Part: LIGHT — INOPERATIVE (CABIN)

DURING A ROUTINE INSPECTION MAINTENANCE FOUND THE EMERGENCY LIGHT ON THE CEILING AFT OF THE EMERGENCY EXIT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AND PERFORMED THE OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (CABIN)

BTV-DURING 1A INSPECTION MAINTENANCE FOUND EMERGENCY LIGHTS, RT OVERHEAD LIGHT BY ESCAPE HATCH INOPERATIVE. RELAMPED RT, OVERHEAD EMERGENCY LIGHT BY ESCAPE HATCH. OPS. CHECKED GOOD. IAW EMB145 MM 33-50-00.

Part: BATTERY PACK — DISCHARGED (FUSELAGE)

IAH-DURING A CHECK INSPECTION, THE AISLE PATH EMERGENCY LIGHT STRIP FROM SEAT 7 TO SEAT 12 WAS FOUND TO BE INOPERATIVE. MX REMOVED/REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

IAH-CREW REPORTED A FALSE BAGGAGE SMOKE WARNING DUEING TAKEOFF ROLL. TAKEOFF WAS ABORTED WITHOUT INCIDENT, AND A/C RETURNED TO THE GATE WHERE MX REMOVED AND REPLACED THE AFFECTED SMOKE DETECTOR AND THE A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (CARGO)

CLE FLIGHT 3686-THE CREW REPORTED A INTERMITTENT BAGGAGE SMOKE WARNING IN FLIGHT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT.MAINTENANCE REMOVED AND REPLACED BAG SMOKE DETECTOR I/A/W EMB 145 MAINTENANCE MANUAL 26-15-01. PERFORMED DETECTOR OPERATIONAL CHECKS I/A/W EMB145 MAINTENANCE MANUAL 26-15-00. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

EWR - FLT 4025 - CREW REPORTED INTERMITTENT BAGGAGE SMOKE LIGHT ON GROUND. MAINTENANCE REMOVED AND REPLACED AFT BAGGAGE SMOKE DETECTOR. OPS CHECKED SATISFACTORY. (M)

Part: ENGINE — MAKING METAL (LEFT)

TYS - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE WAS FOUND TO BE MAKING METAL BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. (X)

Part: CONNECTOR — DIRTY (LANDING GEAR)

FLT 4084 - CREW REPORTED 'UNABLE TO RAISE GEAR'. MAINTENANCE CLEANED LGEU CANNON PLUGS. PERFORMED SEVERAL GEAR RETRACTIONS AND EXTENSIONS OPERATIONAL, TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 1,862.1 HOURS. ACFT CYCLES: 1,787. (X)

Part: WIRE HARNESS — FAILED (NR 2 ENGINE)

IAH - FLT 4153 - THE PILOT REPORTED THE NR 2 ENGINE HAD A LOW N1 INDICATION. AN AUTO SHUT DOWN OCCURRED AND THE CREW WAS ABLE TO RE-START THE ENGINE AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ITT 'A' SYSTEM MAIN HARNESS. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: CONNECTOR — DIRTY (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE CLEANED THE CANNON PLUG ON THE LIGHT CONTROLLER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)