N15983

Part: SOCKET — INOPERATIVE (CABIN) · airframe 44,269 hrs · 34,152 cycles

MAIN CABIN DOOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT SOCKET IAW AMM 33-50-06.

Part: DISPLAY — SHORTED (NR 2) · airframe 41,080 hrs · 31,586 cycles

MFD NR 2 WENT BLANK AT THE SAME TIME AS AN ELECTRICAL BURNING ODOR. MX REMOVED AND REPLACED NR 2 MFD WITH OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,773 hrs · 31,349 cycles

THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHT INOPERATIVE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,773 hrs · 31,349 cycles

THE CREW REPORTED FORWARD FLOOR EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — DENTED (FRAME 19-20) · airframe 39,026 hrs · 29,936 cycles

DENT LOCATED BETWEEN FRAME 19 AND FRAME 20 AT STR 15L AND 16L. CUTOUT DAMAGED SECTION FABRICATED FILLER AND DOUBLER, INSTALLED AND REFINISHED. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — DENTED (FRAMES 62-63) · airframe 37,929 hrs · 29,065 cycles

GROUND PERSONAL REPORTED DENT DAMAGE AROUND RT REAR AREA OF ACFT FUSELAGE BETWEEN STRINGERS 18R & 19R AND FRAMES 62 & 63A. MAINTENANCE INSPECTED AND PERFORMED REPAIR, FILLER AND DOUBLER OF DENT DAMAGE IAW ETD 2015-145-101284 AND SRM 51-40-02. DAMAGE MEASUREMENTS WERE L=5.5" BY 3.75". AND .150" DEEP. ACFT WAS RELEASED FOR SERVICE.

Part: PROFILE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 35,507 hrs · 27,129 cycles

DURING C-CHECK, CARGO DOOR INNER L PROFILE IS CORRODED AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW SRM 51-40-02 A.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 35,507 hrs · 27,129 cycles

DURING C-CHECK, LT OMEGA BEAM FLANGE CORRODED AT FRAME 23. REPAIRED IAW EC5320-01984. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 35,355 hrs · 27,008 cycles

PILOT REPORTED A LAV SMOKE MASTER WARNING ON THE EICAS DURING FLIGHT. OCCURED TWICE FOR APPOXIMATELY 10 SECONDS EACH TIME. MX R & R THE LAVATORY SMOKE SENSOR, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,604 hrs · 26,424 cycles

CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK AND TOWARDS REAR OF ACFT DURING ARRIVAL. ALSO NOTED THE ACFT WAS VERY WARM WITH THE PACKS TO FULL COLD. MX PERFORMED MULTIPLE OPS CHECKS OF PACKS SUCCESSFULLY. MX ALSO PERFORMED GVI OF CABIN WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE ASSY — WORN (NR 1) · airframe 34,421 hrs · 26,278 cycles

THE CREW REPORTED BRAKES COULD NOT BE APPLIED FULL, GRAB HARD AND RELEASE AND PULL LEFT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BRAKE ASSEMBLY. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,301 hrs · 26,182 cycles

DURING ROUTINE MAINTENANCE THE AFT AISLE PATH EMERGENCY LIGHT STRIP WOULD NOT TEST. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,970 hrs · 23,541 cycles

MAIN PAX DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,463 hrs · 22,279 cycles

DURING ROUTINE MX, THE LT SIDEWALL EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX REPLACED THE LT SIDEWALL EMERGENCY EXIT SIGN. OPS CHECKED GOOD.

Part: CHECK VALVE — TORN (FUEL SYSTEM) · airframe 28,918 hrs · 21,849 cycles

FLT 4566. DURING TAKEOFF, A SMALL FUEL LEAK WAS REPORTED FROM THE LT WING. CREW PERFORMED AIR RETURN BACK AS PRECAUTION WITHOUT INCIDENT. MX FOUND DEBRIS AND THE LT WING OTBD CHECK VALVE TORN. MX R & R THE CHECK VALVE IAW AMM 28-11-04. FILLED LT WING WITH FUEL WITH NO LEAKS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 27,315 hrs · 26,016 cycles

MCI - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,306 hrs · 19,738 cycles

RIC - DURING ROUTINE MAINTENANCE, INSPECTION FOUND EMERGENCY LIGHT FLOOR STRIP AT EMERGENCY EXIT (ROW 12) INOPERATIVE. RIC MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — LEAKING (LEFT) · airframe 25,922 hrs · 19,454 cycles

IAH - FLIGHT 2496, THE CREW REPORTED AN ACRID BURNING SMELL LIKE TIRES OR GUNPOWDER DESCENDING THROUGH FL270 THAT ONLY LASTED A FEW SECONDS, WITH NOTHING NOTICED BY THE F/A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 25,920 hrs · 19,453 cycles

MCI - FLIGHT 3088, DURING TAXI THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION, THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED E1 & E2 RUNS AND BLEED & PACK SYSTEM CHECKS ALL WITH NO DEFECTS OR SMOKE NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 25,920 hrs · 19,453 cycles

MCI FLT 3088 THE CREW REPORTED SMOKE IN THE CABIN DURING PACK 2 OPERATION.MAINTENANCE PERFORMED ENGINE 1 AND 2 RUNS WITH BLEED 1 AND 2 OPEN AND BOTH PACKS OPERATING. NO DEFECTS WERE FOUND AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK LT OMEGA BEAM IS CORRODED (PNL 231FF) AND RAMP ANGLE AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AND REMOVED AND REPLACED LT OMEGA BEAM RAMP ANGLE AT FRAME 20 IAW EMB-145 SRM 51-40-02 AND 51-30-01 AND ALODINED, PREPPED, PRIMED AND PAINTED AREA IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (FUSELAGE) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK LT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 76-80 (23 RIVETS). MAINTENANCE PERFORMED REPAIR ON LT FUSELAGE SKIN FRAMES 76-80 IAW EC5330-02300. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — WORN (SPOILER) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK RT GROUND SPOILER O/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,862 hrs · 19,406 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 3 · airframe 25,862 hrs · 19,406 cycles

DURING C-CK. CTR OMEGA BEAM HAS CORROSION AT FR 20. R & R OMEGA BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,862 hrs · 19,406 cycles

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

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,862 hrs · 19,406 cycles

DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,862 hrs · 19,406 cycles

DURING C-CK, CTR OMEGA BEAM HAS CORROSION AT FR 34. REPAIRED OMEGA BEAM IAW SRM 53-22-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 REV C AND IAW EMB-145 SRM 53-21-10. RESTORED REWORKED REPAIRED AREA IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION REPAIRED SERVICE DOOR CENTER SILL IAW EMB 145 SRM 53-21-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,862 hrs · 19,406 cycles

DURING C-CK. LT OMEGA BEAM HAS CORROSION AT FR 24. REPAIRED OMEGA BEAM IAW SRM 53-00-10. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK FUSELAGE FITTING-TO-VERTICAL STABILIZER SPAR ATTACHMENT BETWEEN FRAME 75 HAS INDICATION OF CORROSION AT TOP SKIN INTERFACE. MAINTENANCE REMOVED AND RE-INSTALLED FUSELAGE FITTING TO VERTICAL STABILIZER SPAR ATTACHMENT IAW EMB-145 EC5310-01317. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — WORN (SPOILER) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK RT GROUND SPOILER I/B ATTACHMENT FITTING HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED ATTACHMENT FITTING IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (FUSELAGE) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK RT FUSELAGE HAS WORKING RIVETS BETWEEN FRAMES 75-80 (38 RIVETS). MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN RT SIDE FRAMES 75-80 IAW EMB-145 EC5330-02300. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION BETWEEN FR 36-41. REPAIRED IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,862 hrs · 19,406 cycles

SHV - DURING C-CHECK RT OMEGA BEAM IS CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR OF RT OMEGA BEAM AT FRAME 23 IAW EMB-145 EC5320-01443 REV C. SRM 53-21-10 RESTORED TO ORIGINAL FINISH TO REWORKED AREA IAW EMB-145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (FIRE WARNING) · airframe 25,245 hrs · 18,901 cycles

CLE FLT 2537 THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE ON TAKEOFF ROLL. MAINTENANCE INSPECTED THE APU FIRE DETECTOR WIRE HARNESS AND SECURED A LOOSE CONNECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE — CHAFED (AUTOPILOT SYS) · airframe 25,159 hrs · 18,835 cycles

SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA,& F/O MFD'S AND EICAS ALL WENT TO RED X'S FOLLOWED BY THE AUTO PILOT CIRCUIT BREAKER POPPING. THE AIRCRAFT LANDED AT SAV WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE IC-600, OPERATIONALLY TESTED WITH NO DEFECTS, AND PLACED THE AUTO PILOT ON MEL. ON 07/25/10 THE AIRCRAFT FLEW TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A CHAFED WIRE AT THE RUDDER SERVO, OPERATIONALLY TESTED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ICU — INOPERATIVE (ZONE 100) · airframe 25,157 hrs · 18,834 cycles

SAV - FLIGHT 2312, THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT AND CABIN, AND ON SHORT FINAL AUTO PILOT FAILED, SECONDARY PITCH TRIM FAIL, THEN CA, & F/O MFD'S AND EICAS ALL WENT TO RED X'S FOLLOWED BY THE AUTO PILOT CIRCUIT BREAKER POPPING. THE AIRCRAFT LANDED AT SAV WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE IC-600, OPERATIONALLY TESTED WITH NO DEFECTS, AND PLACED THE AUTO PILOT ON MEL.

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 24,255 hrs · 18,155 cycles

FLIGHT 2612 - EWR - FLIGHT CREW REPORTED APU FIRE DETECTION SYSTEM FAIL MESSAGE ON EICAS. EWR MX RE-SECURED LOOSE CONNECTOR ON APU FIRE LOOP AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,781 hrs · 17,814 cycles

EWR - DURING ROUTINE MAINTENANCE, EWR MX FOUND EMERGENCY LIGHT OVER RIGHT WING EXIT DOOR INOPERATIVE. MX REMOVED AND REPLACED INVERTER AND PERFORMED OPERATIONAL SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 23,258 hrs · 17,401 cycles

FLIGHT 2138 - RIC - FLIGHT CREW DIVERTED FLIGHT TO RIC DUE TO HYDRAULIC 1 QUANTITY LOW MESSAGE AND FLUID LEVEL DECREASING. CREW LANDED ACFT UNEVENTFULLY. RIC MX SERVICED HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK. NO LEAK WAS FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,100 hrs · 17,278 cycles

CLE FLT 2995 - THE CREW REPORTED THE CAPTAINS WINDSHIELD WAS CRACKED IN THE LOWER LEFT CORNER ABOUT 3-4 INCHES LONG. MAINTENANCE INSPECTED AND REPLACED THE WINDSHIELD.

Part: ECU — FAULTY (TE FLAP) · airframe 21,368 hrs · 16,014 cycles

CLE FLIGHT NR 2841 THE CREW REPORTED A FLAP FAIL MSG ON THE EICAS ATTEMPTING TO RAISE THE FLAPS TO O AFTER TAKEOFF. INDICATION WAS 9 DEGRESS AND THE FLAP HANDLE IN O DEGREE POSITION. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT AND OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,335 hrs · 15,986 cycles

EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 1 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,335 hrs · 15,986 cycles

EWR MX - DURING ROUTINE MX, EWR MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX R&R NR 2 EMERGENCY LIGHT BATTERY CHARGER AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,335 hrs · 15,986 cycles

DURING ROUTINE MX, MX FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MX REMOVED AND REPLACED NR2 EMERGENCY LIGHT BATTERY AND PERFORMED OPS TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,258 hrs · 13,846 cycles

IAH - FLIGHT 2455, THE CREW REPORTED THAT THE FORWARD CEILING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLEX DUCT — DAMAGED (A/C BAY) · airframe 16,830 hrs · 12,770 cycles

FLT 2987 - EWR - FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN COMING FROM FLOOR VENT BETWEEN ROWS 9-11. EWR MX FOUND NR 1 PACK DUCT TO BE OFF RECIRCULATE FAN AND TO BE DAMAGED. MX REMOVED AND REPLACED DUCT IAW EMB 145 MM 21-20-04. MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,375 hrs · 12,422 cycles

DURING C-CHECK CENTER OMEGA BEAM WAS FOUND WITH CORROSION AT FR 18 TO FR 20. MAINTENANCE REPLACED THE CENTER OMEGA BEAM AT FR 17 TO 24 IAW SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,375 hrs · 12,422 cycles

DURING C-CHECK CENTER OMEGA BEAM LOWER FLANGE WAS FOUND WITH CORROSION BETWEEN FRMS 23 AND 29. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRM 24 IAW SRM 53-00-10; RESTORED ORIGINAL FINISH TO BLEND AREAS AT FRMS 23 TO 29 IAW EMB 145 CPM 51-21-07. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PITOT TUBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 16,183 hrs · 12,272 cycles

FLIGHT 2385 - OKC TO IAH - CREW REPORTED EICAS MESSAGE -PITOT 3 INOP- APPEARED WITH ASSOCIATED BURNING SMELL ON SHORT FINAL. THE NR 3 PITOT PROBE WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: PITOT TUBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 16,183 hrs · 12,272 cycles

IAH - FLIGHT 2385, DURING TAXI IN THE CREW REPORTED A PITOT 3 INOP MESSAGE WITH A BURNING SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE PITOT TUBE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (MLG) · airframe 15,321 hrs · 11,600 cycles

CREW REPORTED, LANDING GEAR HANDLE WILL NOT GO UP. AIRCRAFT AIR RETURNED TO TYS AND LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED CHANNEL -A- PROXIMITY SWITCH IAW EMB145 AMM 32-61-01, OPS CHECKED GOOD.

Part: LANDING GEAR — LOW (NLG) · airframe 15,303 hrs · 11,586 cycles

IAH - FLIGHT 3027, THE CREW REPORTED THAT ON DEPARTURE FROM IAH, RECEIVED A LANDING GEAR AIR GROUND FAIL AND THE LANDING GEAR HANDLE WOULD NOT UNLOCK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE NLG, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 15,289 hrs · 11,577 cycles

IAH - FLIGHT 2787, THE CREW REPORTED AN AIR/GROUND FAILURE ON CLIMB AND THAT THE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,522 hrs · 10,205 cycles

SDF - AFT EMERGENCY LIGHT STRIP INOP. REMOVED AND REPLACED AFT EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12, OPS CHECK GOOD.

Part: LIGHT — ARCED (INSTRUMENT PANEL) · airframe 13,335 hrs · 10,064 cycles

EWR---CO2996, CREW REPORTED ON CLIMB-OUT, ARC FLASHING OBSERVED BELOW LEFT CAPTAINS INSTRUMENT PANEL. CAPTAINS INSTRUMENT PANEL LIGHTS OUT AND CIRCUIT BREAKER POPPED. ALSO, INSULATION BURNING ODOR NOTED. EWR, MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL NR 33-10-00 CATEGORY "C" CONTROL NUMBER 062418, AIRCRAFT RETURNED TO SERVICE. EWR, MAINTENANCE RESET CAPTAINS PILOT LIGHTS CIRCUIT BREAKER AND PERFORMED OPERATIONAL CHECK OF PILOTS INSTRUMENT PANEL LIGHTS IAW EMB145 AMM NR 33-12-00. OPS CHECKED GOOD, NO BURNING SMELL NOTED. MEL CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 12,592 hrs · 9,466 cycles

DURING SERVICE ROUTINE CHECK, MAINTENANCE FOUND THE COCKPIT STEP UP AND FORWARD OVERHEAD EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT INVERTER IAW EMB AMM NR 33-50-10, OPS CHECKED GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 11,721 hrs · 8,778 cycles

SHV - DURING C-CHECK LT CENTER FUSELAGE 1 SKIN DENTED FWD OF LT STATIC PORT IN RVSM CRITICAL AREA. MAINTENANCE REPAIR THE DAMEGE AREA AND PERFORMED RVSM INSPECTION IAW EC5330-01450. THE AIRCRAFT WAS APRROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,709 hrs · 8,770 cycles

IND - FLIGHT 2428, THE CREW REPORTED THAT THE EMERGENCY FLOOR LIGHT AFT OF ROW 12 WAS INOPERATIVE. THE EMERGENCY LIGHT WAS PLACED ON MEL 33-50-00/2 CONTROL NUMBER 049776, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED IN IAH ON FLIGHT 2428 WHERE MAINTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS FOUND, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE — ERRATIC (MLG) · airframe 1,049 hrs · 7,756 cycles

REPORT TAKEN FROM LOGPAGE 958380. THE PILOT REPORTED THAT ON LANDING, THAT ON THE ROLL ON A DRY RUNWAY, THE BRAKES FELT AS IF THE ANTI-SKID WAS ACTIVATING OR THE BRAKES WERE GRABBING WITH NORMAL BRAKE PRESSURE. MAINTENANCE BLED THE BRAKES AND PERFORMED OPS CHECKS AMM 32-40-00. OPS CHECKS WERE GOOD AND A/C WAS RELEASED.

Part: ATTACH BRACKET — WORN (HORIZONTAL STAB) · airframe 10,232 hrs · 7,602 cycles

A/C 983 WAS HERE FOR A MOD AND A 5A INSPECTION, UPON INSPECTING THE VERTICAL STAB,THE LT AND RT SPHERICAL BEARINGS WERE FOUND WORN. MAINT. ENLARGED BOTH LT AND RT SPHERICAL BEARING HOUSINGS AND INSTALL THE OVERSIZES BUSHINGS CALL FOR IN EC-55-10-01086. ALL WORK WAS IAW THIS EC(5510-01086). ALL WORK WAS COMPLIED WITH WITH ALL DEFLECTION CHECKS AND WAS RELEASED UPON COMPLETION OF ALL WORK.

Part: WARNING LIGHT — ILLUMINATED (MLG)

BNA FLIGHT 2831, THE CREW REPORTED THE LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. ALSO RECEIVED A LANDING GEAR/LEVER DISAGREE WARNING ON THE EICAS. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE LANDING GEAR. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE EMERGENCY LIGHT ON PANEL 811XW WAS FOUND TO BE NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE NUMBER 1 BATTERY POWER SUPPLY CHARGER IAW EMB 145 AMM 33-50-04-801-A. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 19 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 7,718 hrs · 5,635 cycles

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: STRINGER — GOUGED (FUSELAGE) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK STRINGER 19R WAS FOUND GOUGED ON THE EXTERIOR BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — DENTED (NR 2 NACELLE) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE NUMBER TWO UPPER COWLING INBOARD EDGE MEMBER WAS FOUND DENTED. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED (PAX DOOR) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK PASSANGER DOOR WAS FOUND TO HAVE TWO DENTS ON OUTER SKIN AFT OF HANDLE. MAINTENANCE REMOVED DAMAGE AND REPAIRED SKIN SECTION AFFECTED IAW EMB 145 SRM 52-10-00. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — GOUGED (NR 1 NACELLE) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK NUMBER ONE ENGINE LOWER COWLING SKIN WAS FOUND GOUGED BY FRAME 7. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (ZONE 400) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE NUMBER ONE LOWER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHANNEL — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK U-CHANNEL WAS FOUND TO HAVE CORROSION UNDER MAIN THRESHOLD. MAINTENANCE REMOVED AND REPLACED AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CHANNEL — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK U-CHANNEL WAS FOUND TO HAVE CORROSION UNDER MAIN DOOR THRESHOLD. MAINTENANCE REMOVED AND REPLACED AFFECTED CHANNEL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — CHAFED (NACELLE) · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE NUMBER ONE UPPER COWLING AFT EDGE MEMBER WAS FOUND CHAFED. MAINTENANCE REMOVED AND REPLACED AFFECTED MEMBER IAW EMB 145 SRM 54-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

DURING C-CHECK THE RIGHT HAND FLOORBEAM DOUBLER WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED DOUBLER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

SHV-DURING C-CHECK THE LEFT HAND FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR ON THE AFFECTED BEAM IAW EMB 145 SRM 53-21-10 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

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

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 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: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,718 hrs · 5,635 cycles

SHV-DURING C-CHECK THE LEFT HAND SILL AT FRAME 65 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: CONTROL VALVE — FAULTY (BRAKE SYS)

IAH - FLT 2711 - CREW REPORTED THAT THE OUTBOARD BRAKES FAIL MESSAGE ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURN TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE OUTBOARD BRAKE CONTROL VALVE TO BE FAULTING. THE VALVE WAS REMOVED AND REPLACED, THE BRAKE SYSTEM OPERATIONALLY TESTED, AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING POST FLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHT STRIP ON FLOOR PANELS 251FF & 261BF FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIPS ON PANELS 251FF & 261BF, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — FAULTY (NR 2 PYLON)

IAH- FLIGHT 4127, THE CREW NOTED THAT NR 2 BLEED OVERTEMP LIGHT ILLUMINATED INFLIGHT. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED TEMP SENSOR IN THE NR 2 PYLON IAW EMB 145 MM 36-11-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — FAULTY (CARGO BAY)

IAH- FLIGHT 4127, THE CREW NOTED THAT NR 2 BLEED OVERTEMP LIGHT ILLUMINATED INFLIGHT. THE CREW RETURNED THE AIRCRAFT TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED TEMP SENSOR, IN THE CARGO COMPARTMENT IAW EMB 145 MM 36-11-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN)

CREW REPORTED ELECTRICAL BURNING SMELL NOTICED ON APPROACH. MAINTENANCE INSPECTED THE ELECTRICAL SYSTEM IAW EMB145 MM CHAPTER 20-00-00. COULD NOT DUPLICATE THE SMELL. INSPECTION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE)

IAH - DURING MAINTENANCE INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE DENTED JUST FORWARD OF THE LEFT STATIC PORTS. MAINTENANCE REPAIRED THE AFFECTED SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01134, THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M)