N13935

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,751 hrs · 30,178 cycles

DURING ROUTINE CHECK, EXIT MARKER ON THE RT OVER WING EXIT SHROUD WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (ZONE 100) · airframe 29,127 hrs · 27,578 cycles

SUPPLEMENTAL, MX R & R THE NR 2 PACK ACM, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,075 hrs · 27,533 cycles

THE CREW REPORTED THE SERVICE DOOR EMERGENCY LIGHT FAILS TO ILLUMINATE. MX R & R THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — CORRODED (RT AILERON) · corrosion level 2 · airframe 28,836 hrs · 27,305 cycles

DURING C-CHECK, RT AILERON PCA ATTACH POINT 2 OTBD HAT BUSHINGS HAVE PITTING CORROSION. MX R & R RT AILERON PCA ATTACH POINT IAW EC5750-01177 REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 28,836 hrs · 27,305 cycles

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

Part: DISPLAY — OVERHEATED (COCKPIT) · airframe 28,437 hrs · 26,908 cycles

LBB - FLIGHT 4418 THE CREW REPORTED A BURNING SMELL COMING FROM THE BOARDING AREA. THE AIRCRAFT WAS RELEASED ON MEL # 23-81-02, AND SUBSEQUENTLY LANDED IN IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BACK UP COMM DISPLAY, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,002 hrs · 26,450 cycles

IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN ABOVE THE FORWARD FLIGHT ATTENDANT SEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (NR 2 AHRS) · airframe 27,905 hrs · 26,348 cycles

IAH - FLIGHT 3033, THE CREW REPORTED THAT THE NUMBER TWO AHRS OVERHEATED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO AHRS COOLING FAN, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — INOPERATIVE (AHRS) · airframe 27,843 hrs · 26,288 cycles

IAH - FLIGHT 2760 THE CREW REPORTED THE CAPTAINS SIDE ATT AND HDG FLAG WITH THE F/O SIDE ATT FLAG, ATT INDICATOR TUMBLED, HEADING INDICATOR TUMBLED AND ROLLED, AND THE SPEED TAPE AND ALT TAPE WENT BLANK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO AHRS COMPUTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 27,893 hrs · 26,284 cycles

IAH - FLIGHT 2304, THE CREW REPORTED A SYSTEM ONE BLEED LEAK CURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SYSTEM ONE BLEED O-RINGS, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 27,570 hrs · 26,009 cycles

IAH - FLIGHT 2357, DURING TAXI THE CREW REPORTED THE BAGGAGE SMOKE DETECTOR LIGHT ON THE OVERHEAD ILLUMINATED WITH NO ASSOCIATED EICAS WARNINGS. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, OPERATIONALLY TESTED WITH NO DEFECTS, VERIFIED NORMAL OPERATIONS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 26,899 hrs · 25,311 cycles

IAH - FLIGHT 2817 WAS DELAYED DUE TO THE CREW REPORTIA BURNING SMELL IN THE COCKPIT AND CABIN WITH THE PACKS RUNNING. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE PACKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — STUCK (ZONE 100) · airframe 26,808 hrs · 25,219 cycles

MCI - FLIGHT 2647 THE CREW REPORTED THAT THE PRESSURIZATION WENT INTO THE AMBER RANGE DURING CLIMBOUT, AND WERE UNABLE TO REGAIN CABIN ALT OR DELTA P IN MANUAL MODE. THE AIRCRAFT RETURNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CLOSED THE GROUND AIR CONDITIONING FLAPPER VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOLDER — SMOKE (COCKPIT) · airframe 26,488 hrs · 24,885 cycles

IAH - FLIGHT 2937 THE CREW REPORTED THAT A LIGHT ON THE F/O'S YOKE CHART HOLDER STARTED SMOKING FOLLOWED BY BREAKER H11 POPPING. MAINTENANCE REMOVED AND REPLACED THE F/O'S YOKE CHART HOLDER, RESET CIRCUIT BREAKER H11, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 24,071 hrs · 22,313 cycles

TYS - FOUND LIGHTNING STRIKE DAMAGE AT FRAME 38 AND STR 15L. MAINTENANCE REMOVED AND REPLACED BURNED RIVET IAW SRM 51-40-02 AND PAINTED IAW CPM 51-21-06. PRESSURIZATION CHECKS GOOD AND WAS RELEASED.

Part: SKIN — DAMAGED (ZONE 200) · airframe 24,071 hrs · 22,313 cycles

TYS - AIRCRAFT HAD A LIGHTNING STRIKE DAMAGE AT FR 40 STR 14L. MAINTENANCE REMOVED AND REPLACED THE BURNT RIVET IAW SRM 51-40-02. PAINTED IAW CPM 51-21-06. PRESSURE CHECKS GOOD AND WAS RELEASED TO SERVICE.

Part: MOUNT — CORRODED (ENGINE) · airframe 24,071 hrs · 22,313 cycles

NR 1 AND NR 2 ENG INLET BOLT HOLES SCARED AND/OR HAVE CORROSION. REMOVED DAMAGE AND CORROSION FROM BOLT HOLES ON INLET MOUNT FLANGE IAW EC5420-01158B.

Part: YOKE — CRACKED (NR 1 NACELLE) · airframe 24,071 hrs · 22,313 cycles

NR 1 ENGINE LOWER FWD YOKE WEBBING CRACKED. THE LOWER FWD YOKE WAS REMOVED AND REPLACED.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 24,071 hrs · 22,313 cycles

TYS DURING A CURRENT 6C INSPECTION THE LEFT LOWER WING SKIN WAS FOUND CRACKED AT THE LOWER INBOARD FLAP SHROUD O/B HOLE. MAINTENANCE REPAIRED THE LEFT LOWER WING SKIN AROUND THE LOWER INBOARD FLAP SHROUD OUTBOARD HOLE IAW EC 5710-01160. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FITTING — WORN (VERTICAL STAB) · airframe 24,071 hrs · 22,313 cycles

DURING C-CHECK FRAME 75 TO VERTICAL STAB SPAR FITTING WAS FOUND FRETTING. MX REMOVED AND REPLACED THE VERTICAL STAB SPAR FITTING IAW EC 5310-01317. ACFT STILL IN C-CHECK.

Part: ATTACH BRACKET — WORN (SPOILER) · airframe 24,071 hrs · 22,313 cycles

LT AND RT GROUND SPOILER MIDDLE ATTACH BRACKET HAS MIGRATING HAT BUSHINGS. REMOVED AND REPLACED BOTH LT AND RT BRACKETS IAW EMB 145 SRM 51-20-03.

Part: SKIN — DENTED (RUDDER) · airframe 24,071 hrs · 22,313 cycles

DURING C-CHECK INSPECTION RUDDER 1 WAS DAMAGED DURING REMOVAL CAUSING TWO PROTRUDING DENTS ON THE LEADING EDGE SKIN. ONE OF THE TWO DENTS IS CRACKED. CUT OUT THE DENTED SKIN, FABRICATED A FILLER AND EXTERNAL DOUBLER, ALODINED AND PRIMED. INSTALLED FILLER AND DOUBLER, PRIMED AND PAINTED. REPAIR PERFORMED IAW EC5540-01114.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 23,760 hrs · 21,986 cycles

LCH - DURING MAINTENANCE INSPECTION THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UPLOCK — DEFECTIVE (RT MLG) · airframe 21,649 hrs · 19,848 cycles

IAH - FLIGHT 2742, THE CREW REPORTED A LOUD BANGING SOUND AFTER GEAR RETRACTION COMING FROM THE NOSE GEAR AREA, AND AFTER DEPARTURE THE RIGHT MAIN GEAR INDICATION SWITCHED FROM UP TO AMBER, BACK TO UP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR UPLOCK BOX AND PROXIMITY SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 21,649 hrs · 19,848 cycles

IAH - FLIGHT 2742, THE CREW REPORTED A LOUD BANGING SOUND AFTER GEAR RETRACTION COMING FROM THE NOSE GEAR AREA, AND AFTER DEPARTURE THE RIGHT MAIN GEAR INDICATION SWITCHED FROM UP TO AMBER, BACK TO UP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR UPLOCK BOX AND PROXIMITY SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHOCK ABSORBER — LEAKING (LT MLG) · airframe 21,637 hrs · 19,835 cycles

LFT - FLIGHT 2907 THE CREW REPORTED A THUMPING SOUND ON T/O DURING GEAR RETRACTION WITH AN AMBER HASH MARK INDICATOR FOR THE LEFT MAIN GEAR. THE CREW CYCLED THE GEAR AND THE SOUND REMAINED BUT THE INDICATION CLEARED. THE AIRCRAFT LANDED IN LFT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR SHOCK ABSORBER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 21,462 hrs · 19,655 cycles

IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (MLG BRAKES) · airframe 20,853 hrs · 19,056 cycles

IAH - FLIGHT 2185, THE CREW REPORTED THAT BOTH RIGHT MAIN LANDING GEAR BRAKES WERE INOP. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL UNIT (BCU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (CABIN) · airframe 20,290 hrs · 18,484 cycles

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE AT ROW 3 THRU 7. ALSO THE EXIT LIGHT AT ROW 2 AND THE EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND FOUND THE FUSE BLOWN ON THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — INOPERATIVE (LT MLG) · airframe 19,625 hrs · 17,768 cycles

IAH - FLT 2103, DURING CLIMB THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CRACKED (NLG WW) · airframe 19,514 hrs · 17,644 cycles

SHV-DURING C-CHECK MAINTENANCE FOUND CROSS BEAM AT FRM 5 (NLG WHEEL WELL) CRACKED AT SUPPORT HOUSING. MAINTENANCE INSTALLED REPAIR DOUBLER IAW EC 5320-01352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — BLOWN (NR 2 ENGINE) · airframe 19,243 hrs · 17,327 cycles

DFW - FLIGHT 2536, THE CREW REPORTED AN ENGINE TWO FIRE INDICATION ON TAKEOFF. THE CREW SHUTDOWN THE NUMBER TWO ENGINE AS A PRECAUTION, AND RETURNED TO DFW WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND A BLOWN -Y- DUCT ON THE NUMBER TWO ENGINE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DUCT, OPERATIONAL AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 18,375 hrs · 16,246 cycles

IAH - FLIGHT 2159, DURING PREFLIGHT THE CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,223 hrs · 16,058 cycles

LCH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING AT ROWS 6, 7 & 8 WERE FOUND TO BE 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: INVERTER — INOPERATIVE (CABIN) · airframe 18,057 hrs · 15,850 cycles

LCH - DURING MAINTENANCE INSPECTION, THE GALLEY EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 17,666 hrs · 15,409 cycles

CLE FLT 2503 THE CREW REPORTED THE NR 2 ENGINE HAD HIGH VIBRATION (LP) WHEN THE THRUST LEVER WAS ADVANCED FROM FLIGHT IDLE. ALSO REPORTED A BURNING SMELL IN THE COCKPIT. EMERGENCY WAS DECLARED ON DESCENT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SEVERE FAN BLADE RUBBING. THE NR 2 ENGINE WAS REPLACED. CAUSE OF ENGINE FAILURE WAS A LPT 3 BLADE.

Part: ACM — SMOKE (NR 1) · airframe 16,902 hrs · 14,551 cycles

FLT NR 2786, PILOT REPORT SMOKE IN COCKPIT AFTER SELECTING PACKS AT 500' AGL. ACFT RETURNED TO FIELD. MTX PLACED NR 1 PACK ON MEL AS PER MEL 21-51-00 CAT C, CONTROL NR 059007 AND WAS RELEASED. NR 1 ACM WAS REMOVED AND REPLACED UPON ACFT'S ARRIVAL INTO CLE, MEL WAS CLEARED AND ACFT WAS RELEASED TO SERVICE.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 16,399 hrs · 14,001 cycles

CREW REPORTED, CABIN AFT EMERGENCY LIGHTS NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY IAW EMB145ER AMM 33-50-04, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,085 hrs · 13,670 cycles

DURING ROUTINE MAINTENANCE IN CLEVELAND THE EMERGENCY LIGHT ON THE SERVICE DOOR DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL TESTS WERE GOOD.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 16,085 hrs · 13,670 cycles

DURING ROUTINE MAINTENANCE IN CLEVELAND THE EXIT SIGN ON THE RIGHT FORWARD BULKHEAD (FORWARD OF SEAT 3B) DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE CYCLED THE EMERGENCY LIGHT CIRCUIT BREAKER AND THE OPERATIONAL TEST WAS GOOD.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 15,564 hrs · 13,115 cycles

YUL- CO3442, CREW REPORTED, BULKHEAD EXIT SIGN WILL NOT ILLUMINATE. MAINTENANCE RECONNECTED LOOSE CONNECTOR AT EMERGENCY EXIT SIGN, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INTERMITTENT (EMERGENCY LIGHT) · airframe 15,232 hrs · 12,762 cycles

CLE - FLIGHT NR 2212, THE CREW REPORTED THE EMERGENCY CEILING LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESET THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS CORRODED. REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (CARGO BAY) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK BAGGAGE DOOR LOWER BEAM FOUND CORRODED. REPLACED THE LOWER BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 54. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC5320-01168. AIRCRAFT APPROVED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED DOUBLER REPAIR IAW 53-22-01. AIRCRAFT APPROVED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 24. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT APPROVED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 38 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-23-10 AND EC5320-01168. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK, THE LT OMEGA BEAM WAS FOUND CORRODED AROUND NUT PLATES AT FRAMES 29 AND 33. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT OMEGA BEAM AT FRAME 22 WAS FOUND CORRODED. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND CORRODED AT FRAME 50. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5320-01168. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW 53-21-10 AND EC 5320-01168. AIRCRAFT RETURNED TO SERVICE.

Part: BEARING CAP — CORRODED (NLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK RIGHT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02.

Part: BEARING CAP — CORRODED (NLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE LEFT NOSE GEAR BEARING CAP WAS FOUND PITTED. REPLACED BEARING CAP IAW 32-20-02.

Part: BEARING CAP — CORRODED (LT MLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK FOUND THE LEFT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01.

Part: BEARING CAP — CORRODED (RT MLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK FOUND THE RIGHT MAIN GEAR FORWARD BEARING CAP PITTED. REPLACED BEARING CAP IAW 32-10-01.

Part: BEARING CAP — CORRODED (LT MLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK FOUND THE LEFT MAIN GEAR AFT BEARING CAP PITTED. REPLACED THE BEARING CAP IAW 32-10-01.

Part: BEARING CAP — CORRODED (RT MLG) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK THE RIGHT MAIN GEAR AFT BEARING CAP FOUND PITTED. REPLACED THE BEARING CAP IAW 32-10-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 15,206 hrs · 12,735 cycles

DURING C-CHECK EDDY CURRENT INSPECTION OF MAIN PASSENGER DOORSTOP BOLT HOLE AT FRAME 18 AND STRINGER 14 REVEALED A CRACK. OVERSIZED HOLE REINSPECTED AND NO CRACKS NOTED IAW EC5310-01297.

Part: WIRE — DAMAGED (EXIT LIGHT)

CLE FLIGHT 2150 THE CREW REPORTED THE RIGHT FORWARD PARTITION EXIT LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED SPLICE SP9220. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (ROW 3)

CLE FLIGHT 3411 - THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON ROW 3 BULKHEAD WAS INOPERATIVE. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHTS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

CLE FLIGHT 2006, THE CREW REPORTED THE EMERGENCY LIGHT ABOVE 3A DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REPAIRED THE EMERGENCY LIGHT CONNECTOR AT SEAT 3A. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT)

ORD FLIGHT 2210, THE CREW REPORTED THE FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. THE CREW PERFORMED A RESET AND OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — WILL NOT TEST (CABIN)

CLE FLIGHT 2041, THE CREW REPORTED THE EMERGENCY EXIT SIGN WOULD NOT TEST. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE GOOD.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C CHECK INSPECTION, THE RT FLOORBEAM AT FRAME 22 WAS FOUND TO HAVE CORROSION. MAITENANCE REPAIRED AFFECTED AREA OF FLOORBEAM AND REMOVED AND REPLACED A DOUBLER IAW EC 5320-01073. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM AT AFT GALLEY MOUNTS NUT PLATE HOLES HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CRACKED (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C CHECK, SPLICE ANGLE WAS FOUND CRACKED AT LT FLOORBEAM BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED AFFECTED AREA AND PERFORMED A SPLICE REPAIR ON LT FLOORBEAM BETWEEN FRAMES 16 AND 17. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

DURING C CHECK INSPECTION, LT FLOORBEAM WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 19 AND 21. MAINTENANCE REMOVED AFFECTED PARTS AND REPAIRED LT FLOORBEAM IAW EMB SRM 53-21-10. THE AIRCRAFT WAS RETURN TO MAINTENANCE

Part: BUTT STRAP (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV DURING C CHECK LEFT HAND LATERAL FLOOR BEAM STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 15 AND 19. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS EC 5320-01074.THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK DOUBLER AT FRAME 22 WAS FOUND TO HAVE CORROSION IN NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED DOUBLER AT FRAME 22 IAW IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 20 AND 23 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION, CENTER FLOORBEAM STRAP FOUND TO HAVE NUT PLATES CORRODED AND SURFACE CORROSION FROM FRAME 15 TO 17. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS IAW EMB 145 SRM 53-21-10 PG 210 ITEM 4 FIG 203, INSTALLED REPAIR PARTS IAW EMB 145 SRM 53-21-10 AND SRM 51-40-02. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION THE RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR WERE FOUND TO HAVE SURFACE CORROSION. MAINTENANCE REMOVED AND REPLACED RIGHT SILLS FORWARD AND AFT OF SERVICE DOOR IAW EMB 145 SRM 51-20-01, SRM 51-40-02, SRM 51-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION, THE RIGHT SILL AFT OF THE SERVICE DOOR HAD CORRODED NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND SILL AFT OF THE SERVICE DOOR IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

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

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV DURING C-CHECK INSPECTION CENTER FLOORBEAM STRAP AT FRAME 18 WAS FOUND TO HAVE CORROSION IN NUT PLATES HOLES. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON NUT PLATE HOLES ON DOUBLER AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CORRODED DOUBLER AT FRAME 20 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION CORRODED NUT PLATE HOLES WERE FOUND ON CENTER FLOORBEAM BUTT STRAP AT FRAME 18. MAINTENANCE REMOVED AND REPLACED BUTT STRAP BETWEEN FRAMES 17 AND 19 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK, CENTER FLOOR SUPPORT BETWEEN FRAMES 18 AND 20 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP BETWEEN FRAMES 18 AND 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV- DURING C-CHECK INSPECTION, THE LEFT SILL HAD CORROSION AROUND THE NUT PLATE HOLES BETWEEN FRAMES 60 AND 61. MAINTENANCE REMOVED AND REPLACED THE LEFT SILL BETWEEN FRAMES 60 AND 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV-DURING C-CHECK INSPECTION, THE RIGHT HAND LATERAL FLOOR BEAM WAS FOUND TO HAVE CORROSION AROUND THE NUTPLATE HOLES BETWEEN FRAMES 59 AND 61.MIANTENANCE REMOVED AND REPLACED THE RIGHT HAND BUTT STRAP BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTT STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

SHV-DURING C-CHECK INSPECTION, THE LEFT LATERAL BEAM AND CENTER FLOOR BEAM NUTPLATE HOLES WERE FOUND TO BE CORRODED AT BETWEEN FRAMES 59 AND 61.MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT HAND AND CENTER BUTT STRAP'S BETWEEN FRAMES 59 AND 61 IN ACCORDANCE WITH EMB 145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (PAX DOOR) · corrosion level 2 · airframe 11,197 hrs · 8,664 cycles

DURING C CHECK INSPECTION, THE MAIN DOOR STRUCTURE WAS FOUND TO HAVE A DENT AFT OF ACTUATING LEVER. MAINTENANCE REMOVED AND REPAIRED DAMAGED AREA IAW EMB 145 SRM 52-10-01. PERFORMED LEAK TEST. LEAK TEST GOOD. IAW EMB 145 MM 21-31-00-700-808-A. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT 4007 THE CREW REPORTED THE EMERGENCY LIGHT ON THE WALL FACING SEAT 3A WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN)

IAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY EXIT LIGHT ON THE LEFT HAND PANEL AROUND THE EMERGENCY DOOR OVERWING IS INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT DC/AC INVERTER, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE — DETECTED (CABIN)

CREW REPORTED, DECLARED EMERGENCY FOR SMOKE IN CABIN, SEEMED TO BE COMING FROM NR 2 PACK. MAINTENANCE RAN NR 2 PACK IAW EMB145 MM 21-51-00, NO SMOKE DETECTED. REPEATED PROCESS SEVERAL TIMES, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — LOOSE (COCKPIT)

CREW REPORTED AFTER SHUTTING DONE ENGINES AT THE GATE, SMOKE NOTICED IN COCKPIT, APU SUBSEQUENTLY SHUTDOWN. MAINTENANCE RAN ENGINES AND FOUND NO SMOKE. OPS CHECKED GOOD. INSPECTED COCKPIT, FOUND TWO WIRES INSIDE PEDESTAL NOT SECURED. REPAIRED WIRING IAW EMB145 MM 20-00-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

CLE FLIGHT 4272 THE CREW REPORTED THE REAR PORTION OF EMERGENCY FLOOR LIGHTS WAS INOPERATIVE. MAINTENANCE INSPECTED AND PLACED ON MEL 33-50-00/2. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF EMERGENCY LIGHTS AND NO DEFECTS WERE FOUND . THE MEL WAS CLEARED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

CLE FLIGHT3989 THE CREW REPORTED CABIN EMERGENCY LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SEAT TRACK — WORN (COCKPIT)

DURING C-CHECK INSPECTION THE CAPTAINS AND FIRST OFFICERS SEAT TRACKS WERE FOUND TO BE WORN. MX REMOVED/REPLACED SEAT TRACKS IAW EMB145 AMM 53-01-05. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE AFFECTED OMEGA BEAM. (M)

Part: STRAP — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 13 TO 18. MAINTENANCE REPAIRED THE AFFECTED BUTT STRAP. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BLEED VALVE — FAILED (NR 1 ENGINE)

ATL-CLE - FLT 4016 - THE CREW REPORTED THAT ON TAKEOFF THE NR 1 ITT WENT TO 921C, THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE COMPRESSOR ACCELERATION BLEED CONTROL VALVE IAW EMB145 MM 75-31-02 AND PERFORMED OPERATIONAL CHECKS IAW ALLISON MM 72-00-00, NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ITT INDICATION — OUT OF RANGE (NR 1 ENGINE)

CLE - FLT 4045 - THE CREW REPORTED THEY ABORTED TAKEOFF DUE TO THE NR 1 ITT WENT OVER 924 CELSIUS ON TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE DOWNLOADED THE CMC AND FOUND NO EXCEEDANCES RECORDED THEY PERFORMED POWER ASSURANCE RUNS AND FOUND ALL PARAMETERS TO BE NORMAL IAW ALLISON AE3007A MM 72-00-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: SKIN — DENTED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE DENTED ADJACENT TO PANEL 272DR. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01099, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL FIN 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 EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SKIN — CREASED (CARGO DOOR)

IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR SKIN WAS FOUND TO CREASED. MAINTENANCE REPAIRED THE DOOR SKIN AND APPLIED A DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5230-01056, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRAP — CORRODED (FRAME 13-18)

IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 13 TO 18. MAINTENANCE REPAIRED THE AFFECTED BUTT STRAP IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01031, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: FITTING — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE INBOARD FORWARD GALLEY ATTACH FITTINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BEAM — CORRODED (FRAME 20)

IAH - DURING C-CHECK INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REPAIRED THE AFFECTED OMEGA BEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: SUPPORT — CORRODED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (VERTICAL STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL FIN TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

PIT - FLT 4131 - CREW REPORTED THAT THE LEFT ENGINE FLAMED OUT ON LANDING ROLL WITH REVERSER ON, THE ENGINE WOULD NOT RESTART ON EITHER FADEC USING THE APU OR CROSS BLEED. MAINTENANCE INSPECTED THE AIRCRAFT SYSTEMS AND FOUND THAT THE LEFT ENGINE HAD EXCEEDED MANUFACTURES LIMITS FOR ITT. THE LEFT ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: HEATER — INOPERABLE (NR 1 TAT PROBE)

CLW - FLT 4091 - CREW REPORTED THAT DURING TAXI, THE NR 1 TAT HEAT WAS INOPERATIVE. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 TAT PROBE IAW EMB-145 MM 34-15-03. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)

Part: BLADE — DAMAGED (LT ENGINE)

CLE - DURING A SCHEDULED BORESCOPE INSPECTION THE LEFT ENGINE TURBINE BLADES WERE FOUND TO HAVE DAMAGE BEYOND MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: ENGINE — OVERTEMP (NR 1)

EWR - AFTER LANDING, NR 1 ENGINE FLAMED OUT. MAINTENANCE DOWNLOADED CMC. FOUND ITT LIMITS 1,050 DEGREES CELSIUS FOR 3 SECONDS. REMOVED AND REPLACED ENGINE DUE TO OVERTEMP. ACFT TT: 2,104.8 HOURS. ACFT TC: 1,413. (X)

Part: CONTOL UNIT — FAILED (CABIN)

CLE - FLT 4004 - CREW REPORTED THE EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS CONTROL MODULE IAW EMB-145 MM 33-21-01. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 1,894.5 HOURS. TOTAL CYCLES: 1,269. (X)

Part: ENGINE — FAILED (LEFT)

CLE - DURING SCHEDULED INSPECTIONS, THE LEFT HAND ENGINE OIL PRESSURE WAS FOUND TO EXCEED MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. PLEASE REFER TO SDR NR C2XA97CL093 FOR THE RIGHT HAND ENGINE REPLACEMENT. (X)

Part: ENGINE — FAILED (RIGHT)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE OIL PRESSURE WAS FOUND TO EXCEED MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)

Part: ENGINE — FAILED (RT ENG OIL PRESS)

CLE - FLT 4030 - CREW REPORTED ON CLIMB-OUT, THE RIGHT HAND ENGINE OIL RPESSURE WAS HIGH, IT EXCEEDED 91 PSI UNTIL APPROXIMATELY 10,000 FEET. MAINTENANCE INSPECTED THE AIRCRAFT AND THEN REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. ALL OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)