N11547

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,039 hrs · 28,535 cycles

FLT 3991 EWR PILOT REPORTED ROW 18 RIGHT SIDE EMERGENCY LIGHT INOP. MX RESECURED RT EMERGENCY LIGHT EXIT IDENTIFIER WITH OPERATIONAL CHECK GOOD.

Part: SKIN — CORRODED (FRAME 74) · airframe 33,807 hrs · 26,713 cycles

EXTERNAL FUSELAGE SKIN HAS A .25 INCH CRACK AT THE 1ST FASTENER BELOW STRINGER 2R, FRAME 74. REPAIRED THE SKIN IAW SRM 53-31-01.

Part: SKIN — CRACKED (FRAME 74) · airframe 33,807 hrs · 26,713 cycles

EXTERNAL FUSELAGE SKIN HAS A .25 INCH CRACK AT THE 1ST FASTENER BELOW STRINGER 2R AT FRAME 74. REPAIRED THE SKIN IAW SRM 53-31-01.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 33,807 hrs · 26,713 cycles

LEFT UPPER SEAT TRACK FRAME 36-46 CORRODED. R & R SEAT TRACK IAW E145 AMM 53-01-06.

Part: SEAT TRACK — DAMAGED (FRAMES 36-45) · airframe 33,807 hrs · 26,713 cycles

RIGHT INBD SEAT TRACK, FRAMES 36 - 45 FOUND GOUGED AND CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 33,807 hrs · 26,713 cycles

LEFT NR 2 FLOOR SUPPORT CORRODED. R & R THE FLOOR SUPPOERT IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRAMES 18-24) · airframe 33,807 hrs · 26,713 cycles

LEFT OTBD SEAT TRACK, FRAMES 18 - 24 IS GOUGED AND CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-06.

Part: FLOORBEAM — CORRODED (FRAME 18) · airframe 33,807 hrs · 26,713 cycles

FLOORBEAM, FRAME 18 AND HAS CORROSION AROUND THREE NUTPLATE HOLES. R & R THE FLOORBEAM IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRAMES 45-52) · airframe 33,807 hrs · 26,713 cycles

RIGHT OTBD SEAT TRACK, FRAMES 45 - 52 IS GOUGED AND CORRODED. R & R THE SEAT TRACK.

Part: CONTROL UNIT — FAILED (BRAKES) · airframe 33,292 hrs · 26,307 cycles

CREW REPORTED INBOARD BRAKES INOPERATIVE AFTER LANDING. REMOVED AND REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL AND TAXI CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 32,850 hrs · 25,979 cycles

DURING ROUTINE MAINTENANCE, THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE IN THE GALLEY AND THE FIRST 3 AISLES. MAINTENANCE INSPECTED AND SECURED THE CONNECTOR ON THE NR 2 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 32,850 hrs · 25,979 cycles

DURING ROUTINE MAINTENANCE, THE RIGHT WING EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FUSE IN THE NR 4 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: LANDING GEAR — MALFUNCTIONED · airframe 32,585 hrs · 25,788 cycles

WHEN PILOT FLYING CALLED FOR GEAR DOWN THE PILOT NOT PLYING TOUCHED GERA LEVER, BEFORE PILOT NOT FLYING LOWERED THE HANDLE THE GEAR WAS HEARD COMING DOWN. PERFORMED LANDING GEAR CONTROL LEVER TEST, LANDING GEAR EXTENSION AND RETRACTION (ELECTRICAL) TEST AND LANDING GEAR EXTENSION AND RETRACTION TEST. ALL OPS CHECKED GOOD, COULD NOT DUPLICATE. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: RELAY — INOPERATIVE (ZONE 100) · airframe 31,670 hrs · 25,034 cycles

THE CREW REPORTED THAT PRESSURIZATION WAS RISING THROUGH 10K FT, NO OTHER INDICATIONS BESIDES CABIN ALTITUDE. THE CREW PERFORMED THE QRH BUT FOUND THE CONTROLLER TO BE ERRATIC. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R RELAYS K0124 & K0264, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE (CABIN PRESSURE) · airframe 31,670 hrs · 25,034 cycles

THE CREW REPORTED THAT PRESSURIZATION WAS RISING THROUGH 10K FEET, NO OTHER INDICATIONS BESIDES CABIN ALTITUDE. THE CREW PERFORMED THE QRH BUT FOUND THE CONTROLLER TO BE ERRATIC. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R RELAYS K0124 & K0264, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,640 hrs · 25,011 cycles

DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS OVERWING WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK AND NR 4 BATTERY POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 31,640 hrs · 25,011 cycles

DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHTS OVERWING WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK AND NR 4 BATTERY POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,089 hrs · 23,786 cycles

DURING ROUTINE MAINTENANCE SEVERAL EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: LIGHT — ARCED (CABIN) · airframe 29,676 hrs · 23,445 cycles

CREW REPORTED SIDEWALL LIGHTING AT SEAT 7A CAUSING BURNING ODOR. CONTRACT MX PLACED ON MEL 33-20-00-1. MAINTENANCE R & R 7/8A PASSENGER LIGHT ASSY WITH OPERATIONAL CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 29,676 hrs · 23,445 cycles

CREW REPORTED SIDEWALL LIGHTING AT SEAT 7A CAUSING BURNING ODOR.

Part: CARBON SEAL — FAILED (NR 2 ENGINE) · airframe 29,163 hrs · 23,056 cycles

ACFT WAS FERRIED DUE TO SMOKE ON SHUTDOWN AND OIL PUDDLE IN THE COWLING. MAINTENANCE R & R ENGINE IAW RR MANUAL 72-00-00. OPS AND LEAK CHECKS WERE PERFORMED AND WILL BE RELEASED AT THE END OF ALL CHECKS.

Part: BEAM — CORRODED (FRAMES 65-66) · airframe 28,894 hrs · 22,839 cycles

DURING C-CK. CARGO DOOR UPPER CUTOUT STRUCTURE CORRODED. REPAIRED CARGO DOOR UPPER CUTOUT STRUCTURE IAW EC5310-01833. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 1 ENGINE) · airframe 28,894 hrs · 22,839 cycles

DURING C-CK. ENGINE NR 1 FWD LOWER YOKE FITTING CRACKED. R & R 31 ENGINE FWD LOWER MOUNT FITTING IAW EC5450-01138. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 28,894 hrs · 22,839 cycles

DURING C-CK. CARGO DOOR LOWER BEAM CORRODED BETWEEN FRAME 65-68. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 10-11) · airframe 28,894 hrs · 22,839 cycles

DURING C-CK, STR 21R CORRODED BETWEEN FR 10-11. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — WORN (NR 1 ENGINE) · airframe 27,398 hrs · 21,659 cycles

PILOT REPORTED STRONG OIL ODOR IN COCKPIT AND CABIN DURING FLIGHT BECAME WORSE DURING APPROACH AND LANDING. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FERRIED ON 8/03/2014. MAINTENANCE R & R LT ENGINE "0" BEARING CARBON SEAL ASSEMBLY. PERFORMED GROUND RUNS AND OPS CHECKS. ACFT APPROVED FOR RETURN TO SERVICE ON 8/06/2014.

Part: FUEL CONTROL — LEAKING (APU) · airframe 24,343 hrs · 19,298 cycles

CREW REPORTED A CONTINUIOUS STRONG ODOR OF FUEL WHEN THE APU IS POWERING THE PACKS. R & R THE APU FUEL CONTROL WITH OPS AND LEAK CHECKS SUCCESSFUL.

Part: CONNECTOR — DIRTY (MLG) · airframe 23,715 hrs · 18,812 cycles

IMMEDIATELY AFTER TAKE OFF RECEIVED A LG AIR/GROUND FAIL MESSAGE ON EICAS. GEAR WOULD NOT COME UP AND THE LEVER WAS LOCKED DOWN. CLEANED CONNECTOR AND INSTALLED CONNECTOR P2834. PERFORMED OCF AND CONFIRMED FIX.

Part: ENGINE — SURGES · airframe 21,864 hrs · 17,298 cycles

THE CREW REPORTED THEY LOST ACCELERATION, THEN ENGINES SURGED ON TAKEOFF. THE TAKEOFF WAS ABORTED. MX INSPECTED AND PERFORMED ENGINE PERFORMANCE RUNS. NO DEFECTS WERE NOTED. DOWNLOAD DFDR AND CMC AND NO DEFECTS WERE REPORTED. THE ACFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,659 hrs · 17,117 cycles

DURING SCHEDULED MX CHECK THE AFT RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R LAMP IAW AMM 33-50-10 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,217 hrs · 16,788 cycles

DURING SCHEDULED MX INSPECTION, THE GALLEY DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX R & R THE GALLEY DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-10 WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE DETECTOR — DEFECTIVE (NR 1 ENGINE) · airframe 19,354 hrs · 15,349 cycles

IAH - FLIGHT 2816 THE CREW REPORTED AN ENGINE ONE FIRE DETECTION FAIL ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE ENGINE ONE FIRE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (LAVATORY) · airframe 19,103 hrs · 15,166 cycles

DURING MAINTENANCE THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — INOPERATIVE (LAVATORY) · airframe 19,065 hrs · 15,132 cycles

FLIGHT 6212 - LGA - FLIGHT CREW REPORTED LAV SMOKE DETECTOR WOULD NOT TEST. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 19,055 hrs · 15,124 cycles

BTV - FLT 6009 THE CREW REPORTED A LAV SMOKE WARNING INDICATION IN FLIGHT. NO SMOKE OR SMELL WAS NOTED. MAINTENANCE INSPECTED AND PERFORMED ENGINE RUNS WITH PACKS ON. NO SMELL OR SMOKE WAS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,055 hrs · 15,123 cycles

FLIGHT 6009 - BTV - FLIGHT CREW REPORTED LAV SMOKE EICAS WIRNING INDICATION IN FLIGHT. CREW PERFORMED QRH. NO SMOKE WAS DETECTED EITHER VISUALLY OR BY ODOR. MESSAGE DISAPPERED ABOUT 15 MIN AFTER APEARED. MX PERFORMED INSPECTION AND OPERATIONAL CHECK - NO DEFECTS FOUND. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TEST PANEL — FAULTY (SMOKE WARNING) · airframe 18,986 hrs · 15,067 cycles

ORD - FLT 5845 THE CREW REPORTED THE LAV SMOKE DETECTOR WOULD NOT TEST. MAINTENANCE REPLACED THE LAV SMOKE DETECT PANEL. OPERATIONAL CHECKS WERE GOOD.

Part: O-RING — DETERIORATED (BLEED AIR SYS) · airframe 18,493 hrs · 14,632 cycles

ORD - FLT 5972 - THE CREW REPORTED A BLEED 1/2 LEAK MESSAGE ON THE EICAS ON FINAL APPROACH. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE O-RING AT JOINT 15 OF THE BLEED AIR SYSTEM AND RE-SECURED THE DUCT. OPERATIONAL CHECKS WERE GOOD.

Part: FIRE LOOP — FAULTY (NR 1 ENGINE) · airframe 17,200 hrs · 13,422 cycles

ORD FLT 5766 THE CREW REPORTED A ENGINE NR 1 FIRE DETECT FAIL MESSAGE RIGHT BEFORE PUSHBACK. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECT LOOP. OPERATIONAL CHECKS WERE GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 14,155 hrs · 10,880 cycles

SHV - DURING C-CHECK THE SERVICE DOOR CUTOUT WAS FOUND TO BE CORRODED AROUND A NUT PLATE AT FRAME 22, STRINGER 16R. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED OUT (CABIN) · airframe 13,796 hrs · 10,627 cycles

FLT MX - ONT TO ONT - WHILE PERFORMING OVERNIGHT SERVICE CHECK MX PERSONNEL FOUND EMERGENCY PROXIMITY LIGHT STRIP INOP ON ROWS 8 & 9. MX PERSONNEL REMOVED AND REPLACED EMERGENCY PROXIMITY LIGHT STRIP ON ROW 8 & 9 OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — WORN (FUEL SYSTEM) · airframe 13,392 hrs · 10,352 cycles

FL 0060 - TUS TO OMA - FLIGHT CREW REPORTED FUEL LEAK ON LT WING. FLIGHT CREW RETURNED TO BLOCK AND MX PERSONNEL IAH RECOVERY REMOVED AND REPLACED FLAPPER VALVE, OPERATIONALLY AND LEAK CHECK SATISFACTORY. A/C WAS RELEASE TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,703 hrs · 9,196 cycles

DURING SCHEDULED MAINTENANCE THE LEFT FORWARD FAIRING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE NR 1 EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED, THE SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 10,465 hrs · 8,183 cycles

CO3288, CREW REPORTED, ENGINE NR 2 FIRE DETECTION FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FIRE LOOP IAW EMB145 MM NR 26-11-01, OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 9,186 hrs · 7,177 cycles

SHV - DURING C-CHECK, THE APU FIREWALL WAS FOUND TO CRACKED AT THE UPPER LEFT APU MOUNT. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EMB 145 SRM 53-32-13, FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,500 hrs · 5,092 cycles

MCI - FLIGHT 2034, DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 6,207 hrs · 4,865 cycles

CREW REPORTED STRONG BURNING SMELL OF OIL IN COCKPIT DURING ENTIRE FLIGHT. RAN ENGINES AND APU AND COULD NOT DUPLICATE ITEM.

Part: MECHANISM — LACK OF LUBE (PAX DOOR)

DURING POSTFLIGHT INSPECTION THE MAIN PASSENGER DOOR WAS FOUND DIFFICULT TO OPERATE. MAINTENANCE LUBRICATED THE PASSENGER DOOR LOCKING MECHANISM AND OPERATIONALLY TESTED THE DOOR.

Part: FIREWALL — CRACKED (APU BAY) · airframe 4,614 hrs · 3,617 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RT APU MOUNT. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 19 AND 20 AT STRINGER 7L, JUST AFT OF THE MAIN DOOR. MAINTENANCE REMOVED THE AFFECTED SECTION OF STRINGER 7L, RE-CONTOURED THE DENTED AREA OF SKIN, AND INSTALLED A NEW 7L STRINGER SECTION IAW CONTINENTAL EXPRESS EC 5330-01242. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE FLOORBEAM ANGLE AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: REINFORCEMENT — CHAFED (FUSELAGE) · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19 LEFT WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 4,614 hrs · 3,617 cycles

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

Part: STRUCTURE — GOUGED (NR 2 ENG INTAKE) · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE RIGHT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,614 hrs · 3,617 cycles

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

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 4,614 hrs · 3,617 cycles

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

Part: STRUCTURE — GOUGED (LT ENG INTAKE) · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE LEFT ENGINE INTAKE UPPER COWLING GUIDE PIN HOLE SURROUNDING AREA WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A CHAFE STRIP IAW EXPRESS JET EC 5410-01067. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FLOORBEAM) · corrosion level 2 · airframe 4,614 hrs · 3,617 cycles

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

Part: REINFORCEMENT — CHAFED (FUSELAGE) · airframe 4,614 hrs · 3,617 cycles

SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19R WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING SCHEDULED MAINTENANCE THE LT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP AND OPERATIONALLY TESTED THE LIGHTING SYSTEM.

Part: STARTER — LEAKING (NR 1 ENGINE) · airframe 4,103 hrs · 3,218 cycles

LOST OIL NR 1 ENGINE ON FINAL APPROACH. QUANTITY AT 3 QUARTS. CONTRACT MAINTENANCE FOUND THE AIR TURBINE STARTER LEAKING. IAH MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR TURBINE STARTER IAW EMB 145 AMM 80-10-01. OPS AND LEAK CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE TWO AFT EMERGENCY LIGHTS WERE INOP. MTY- MAINTENANCE INSPECTED THE AIRCRAFT. THE AIRCRAFT WAS RELEASED IAW MEL. MAINTENANCE RECONNECTED THE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. REMOVED FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)

CAPT LOST PRESSURIZATION, MANUAL MODE WAS WORKING. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — FAULTY

EWR---CO3495, "ON THE OUTSIDE OF AIRCRAFT AFT EMERGENCY EXIT LIGHTS #1 AND #2 WERE INOPERATIVE. AIRCRAFT PREVIOUSLY RELEASED IAW MEL #33-50-00 CATEGORY "C" CONTROL NUMBER 032880.....MAINTENANCE REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER IN THE #4 POSITION. AND REPAIRED WIRING. OPS. CHECKED GOOD. IAW EMB145 AMM CHAPTER #20 AND 33-50-04. MEL ITEM CLEARED AND AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED

During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the aircraft and found the #4 battery pack to be inoperative. The affected pack was removed and replaced and the emergency lighting system was operationaly

Part: BATTERY — DISCHARGED

During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the aircraft and found the #2 battery pack to be inoperative. The affected pack was removed and replaced and the emergency lighting system was operationaly tested.

Part: BATTERY — DISCHARGED

During a postflight inspection the emergency lighting system was found to be inoperative. Maintenance inspected the aircraft and found the #3 battery pack to be inoperative. The affected pack was removed and replaced and the emergency lighting system was operationaly

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

ORF FLIGHT 3037 THE CREW REPORTED THE NR 1 ENGINE DID A COMPRESSOR STALL WHEN TAKEOFF POWER WAS APPLIED. THE ITT ALSO INCREASES TO 920 DEGREES. MAINTENANCE REPLACED THE NR 1 ENGINE. THE AIRCRAFT WAS RELEASED FOR SERVICE.