N48901

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,124 hrs · 32,600 cycles

DURING MX THE EMERGENCY LIGHT FLOOR PROXIMITY STRIP ROW 22A TO 24A WAS DISCOVERED INOP. MX PLACED ON MEL. ON 7/24/19 MX REMOVED AND REPLACED THE LIGHT STRIP WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 2) · airframe 42,013 hrs · 32,512 cycles

THE CREW REPORTED FUMES AND VAPOR/MINOR SMOKE IN CABIN IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE #2 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 37,377 hrs · 29,578 cycles

CRACKED FRAME RT SIDE ABOVE RT WINDSHIELD LATERAL POST. REMOVED CRACKED SECTION OF LATERAL BRACKET, INSTALLED NEW SECTION OF LATERAL BRACKET AND DOUBLER. AIRCRAFT STILL IN C CHECK.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,688 hrs · 32,241 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND FUSELAGE CORRODED UNDER THE RA ANTENNA BETWEEN FRAMES 69 AND 70 AND STR 21L AND 21R. MAINTENANCE PERFORMED A DOUBLER ON THE FUSELAGE BELOW THE RA ANTENNA AT FRAMES 69 AND 70 IAW SRM 53-00-23. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 40,111 hrs · 30,992 cycles

DURING MX INSPECTION THE RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT WAS DISCOVERED INOPERATIVE. MX RE-SEATED CANON PLUG AND PERFORMED OPERATIONAL CHECK WITH GOOD RESULT. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,326 hrs · 29,556 cycles

DURING MX INSPECTION, THE MAIN CABIN DOOR, EXIT, OVERHEAD ROW 3, AND FWD LEFT WING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,326 hrs · 29,556 cycles

DURING MX INSPECTION, THE EMERGENCY LIGHTS FROM ROWS 3 TO 7 WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE INVERTER NR 3. OPERATIONAL CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 37,199 hrs · 28,663 cycles

DURING C-CK FR 75 FUSELAGE SKIN IS CRACKED BTW STR 1R-2R. REPAIRED FR 75 SKIN AT STR 1-2R BY CUTTING DAMAGE AND INSTALLING A FILLER AND DOUBLER IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 37,199 hrs · 28,663 cycles

DURING C-CK STRINGER 2L IS CRACKED AT FR 75. REPAIRED STRINGER 2L IAW SRM 53-00-03 TABLE 202. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,826 hrs · 27,521 cycles

DURING ROUTINE MAINTENANCE THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY ASSY IAW AMM 33-50-04. THE LIGHTS OPERATIONALLY CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,803 hrs · 27,501 cycles

DURING ROUTINE MAINTENANCE THE LT WING EXTERNAL FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE GOOD.

Part: SOLENOID VALVE — FAULTY (NLG) · airframe 33,416 hrs · 25,619 cycles

ON APPROACH AT 5000 FT PILOTED REPORTED THE NOSE GEAR DOORS OPENED AND REMAINED OPEN WITH THE GEAR LEVER IN THE UP POSITION. MAINTENANCE R & R THE NOSE GEAR DOOR SOLENOID VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,887 hrs · 25,179 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHT STRIPS WERE NOT ILLUMINATING DURING A TEST. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT DC/AC INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — FAULTY (APU) · airframe 32,373 hrs · 24,765 cycles

THE CREW REPORTED AFTER STARTING APU, RECEIVED A STRONG FUEL ODOR IN COCKPIT, WHICH DISSIPATED. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,547 hrs · 24,129 cycles

DURING MX INSPECTION THE NR 3 EMERGENCY LIGHT BATTERY WOULD NOT ILLUMINATE THE EMERGENCY LIGHTS. MX R & R THE NR 3 EMERGENCY LIGHT SYS BATTERY PACK, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — BROKEN (FUEL SYSTEM) · airframe 31,316 hrs · 23,949 cycles

PILOT REPORTED A SUSPECTED FUEL LEAK, ENGINE NR 2, FUEL PPH AT CRUISE SET SIMILAR, YET TANK NR 2 INDICATOR SHOWED TANK NR 2 FUEL USAGE WAS MUCH GREATER. AFTER INSPECTION MX FOUND A BROKEN FLAP VALVE IN NR 2 FUEL TANK AND R & R WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (ZONE 600) · airframe 29,414 hrs · 22,517 cycles

CREW REPORTED FUEL LEAKING FROM THE RT WING AFTER TAKEOFF ALONG WITH FUEL IMBALANCE. CREW PERFORMED UNEVENFUL AIR RETURN. MX R & R THE RT WING FLAPPER VALVE WITH LEAK CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 28,968 hrs · 22,167 cycles

THE CREW REPORTED SMOKE IN THE CABIN, APPROX 2 MINUTES AFTER SELECTING ENGINE BLEEDS, WITH A SMELL BEING IMMEDIATELY NOTICEABLE. THE ACFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, PERFORMED GROUND RUNS OF THE ENGINES, ALL WITH NO DEFECTS NOTED, AND UNABLE TO DUPLICATE THE DISCREPANCY, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,340 hrs · 21,678 cycles

DURING MX INSPECTION THE CEILING GALLEY EMERGENCY LIGHT WAS FOUND TO BE DIM DURING OPERATION. MX R & R THE CEILING GALLEY EMERGENCY LIGHT BULB, OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 27,538 hrs · 21,046 cycles

DURING C-CHECK CARGO DOOR SILL CORRODED. MX R & R CARGO DOOR SILL IAW CPM 51-21-06 AND SRM 53-31-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,538 hrs · 21,046 cycles

DURING C-CHECK CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS CORRODED (LOCAL LEVEL 2). MX R & R CARGO DOOR CUTOUT FWD AND AFT LOWER CORNERS IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,538 hrs · 21,046 cycles

DURING C-CHECK, SERVICE DOOR CENTER SILL CORRODED, LOCAL LEVEL 2. MX R & R SERVICE DOOR CENTER SILL IAW SRM 51-40-02 AND CPM 51-21-00. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 27,538 hrs · 21,046 cycles

DURING C-CHECK RT OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2, AT NUTPLATE FRAME 19A. MX PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18-19A IAW EC5320-01718 (ORIG). THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANTI-ICE VALVE — DEFECTIVE (NR 2 ENGINE) · airframe 24,084 hrs · 18,306 cycles

FLIGHT 2829 - EWR - FLIGHT CREW REPORTED ENG NR 2 ANTI ICE FAIL IN FLIGHT. EWR MX REMOVED AND REPLACED NR 2 ENG ANTI-ICE VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — DIRTY (LANDING GEAR) · airframe 23,982 hrs · 18,222 cycles

ORD FLT 6131 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND CLEANED AND RE-SECURED LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 22,818 hrs · 17,246 cycles

FLIGHT 2228 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: MANIFOLD — FAULTY (AILERON) · airframe 22,087 hrs · 16,691 cycles

THE CREW REPORTED AN AILERON SYSTEM 2 INOPERATIVE MESSAGE ON THE ECIAS DURING CRUISE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AILERON HYDRAULIC MANIFOLD. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 17,931 hrs · 13,554 cycles

DURING ROUTINE MX, MX FOUND LOWER EMERGENCY LIGHT IDENTIFIER SIGN AT SEAT 12A INOPERATIVE. MX R&R SIGN AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 17,927 hrs · 13,550 cycles

THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE LAV SMOKE DETECTOR ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT LANDED WHERE MX REMOVED AND REPLACED THE NR 2 ENGINE, OPS TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED · airframe 17,927 hrs · 13,550 cycles

SAT - FLIGHT 2630, THE CREW REPORTED A LAV FIRE DETECTION INDICATION IN FLIGHT. THE ACFT RETURNED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE LAV SMOKE DETECTOR ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT LANDED IN IAH WHERE MX R&R THE ENGINE, OPS TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 17,842 hrs · 13,492 cycles

IAH - FLIGHT 2406, THE CREW REPORTED A LAV SMOKE INDICATION ON T/O FROM DAL. THE SYSTEM WAS RESET SUCCESSFULLY PER THE QRH, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 17,813 hrs · 13,475 cycles

FLIGHT 2220 SHV-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTED AT THAT POINT AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUNS AND COULD NOT DUPLICATE THE CONDITION.

Part: INLET — CORRODED (ZONE 400) · airframe 17,811 hrs · 13,474 cycles

VARIOUS BOLTHOLES ON THE LT ENG AIR INLET CORRODED. REPAIRED BOLT HOLE ON LT ENG AIR INLET IAW EC 5420-01179. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 17,811 hrs · 13,474 cycles

CENTER OMEGA BEAM HAS CORROSION IN RADIUS AT FR 20. CENTER OMEGA BEAM WAS REPAIRED IAW SRM 53-21-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (ZONE 600) · airframe 17,811 hrs · 13,474 cycles

SHV DURING C-CHECK RT AILERON UPPER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT UPPER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHROUD — CORRODED (ZONE 500) · airframe 17,811 hrs · 13,474 cycles

SHV DURING C-CHECK LT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PANEL — CORRODED (ZONE 100) · airframe 17,811 hrs · 13,474 cycles

SHV DURING C-CHECK PANEL 191EL WAS FOUND TO HAVE CORRODED BONDING PLATES. MX R&R BONDING PLATES ON PANEL 191EL IAW EC 5750-01315 REV "E". THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 17,811 hrs · 13,474 cycles

SHV DURING C-CHECK SERVICE DOOR LOWER NUTPLATE HOLES HAD CORROSION. MX REPAIRED SERVICE DOOR LOWER NUTPLATE HOLES BY REMOVING CORROSION AND FINDING SERVICE DOOR LOWER NUT PLATE HOLES TO BE WITHIN LIMITS IAW EMB SRM 51-10-03 AND EC 5210-01154. MX THEN TREATED, PRIMED AND PAINTED SERVICE DOOR LOWER NUTPLATE HOLES IAW EMB 145 CPM 51-21-06 AND EC 5210-01154. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SHROUD — CORRODED (ZONE 600) · airframe 17,811 hrs · 13,474 cycles

SHV DURING C-CHECK RT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT AILERON LWR SHROUD IAW EC 5750-01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (BRAKE)

CLE FLIGHT NR 2626 THE CREW REPORTED A NR 1 T/R DISAGREE AND A SPOILER FAIL MSG IN FLIGHT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE BRAKE CONTROL UNIT AND RELAYS KO479 AND K1202. OPS CHECKS WERE GOOD.

Part: BRACKET — BROKEN (BATTERY HOLDER)

ACFT WAS IN FOR A SERVICE CHECK AND THE RT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE NR 2 EMERGENCY BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04. OPS CHECK GOOD AND WAS RELEASED. (S)

Part: PROXIMITY SWITCH — DEFECTIVE (NLG) · airframe 15,836 hrs · 12,106 cycles

FLIGHT 3156 - EWR - CREW REPORTED BANGING NOISE COMING FROM NOSE LANDING GEAR AREA DURING TAXIING. CREW RETURNED TO GATE. EWR MX REMOVED AND REPLACED UPLOCK BOX PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,295 hrs · 11,743 cycles

DURING ROUTINE MAINTENANCE, THE OVERWING EXIT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,648 hrs · 11,273 cycles

LCH - FLIGHT 3015, THE CREW REPORTED THE LEFT HAND WALL EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY EXIT LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 14,458 hrs · 11,126 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT ON SEAT 12A INOP. MX REMOVED THE EMERGENCY LIGHT ASSEMBLY AND FOUND CONNECTOR LOOSE. MX RESECURED CONNECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — SHORTED (TE FLAPS) · airframe 13,978 hrs · 10,781 cycles

IAH - FLIGHT 2852, THE CREW REPORTED A W/S 1 FAIL MESSAGE ON EICAS FOLLOWED BY LOUD CLICKING OF RELAYS AND A STRONG BURNED ELECTRICAL ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE WINDSHIELD HEAT ON MEL 30-42-02 CAT C CTL#124320, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO 06/28/07, WHERE MAINTENANCE SWAPPED THE SENSORS WIRES TO S3 AND S4. OPERATIONALLY CHECKED THE WINDSHIELD HEAT SYSTEM WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 13,147 hrs · 10,172 cycles

EWR MX LOG SQUAWK FLT NR 3005 FOUND EMERGENCY LIGHTS (RT WING FUSELAGE FRONT FAIRING AND ISLE LIGHT NR 2) INOP. REMOVED AND REPLACED CHARGER ASSEMBLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. CLOSED

Part: INVERTER — INOPERATIVE (CABIN) · airframe 10,713 hrs · 8,272 cycles

STL - DURING MAINTENANCE INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,637 hrs · 6,626 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS BETWEEN FRM 29-36. MAINTENANCE REPAIRED LT OMEGA BEAM AT FRM 29 IAW EC5320-01237 AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,637 hrs · 6,626 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION ALONG THE SIDE FR 36 TO 52. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FR 44 IAW EC 5320-01238. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 1,226 hrs · 5,531 cycles

CLE - FLIGHT 3351, THE CREW REPORTED THE EXIT ROW AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FAN — BURNED OUT (FWD AVIONICS) · airframe 7,157 hrs · 5,482 cycles

HSV - FLIGHT 2184, THE CREW REPORTED A PLASTIC SMELL COMING FROM THE PACK VENTS. MAINTENANCE PLACED THE LEFT FORWARD ELECTRONIC COMPARTMENT FAN ON MEL 21-26-00 CTL 046030, AND THE AIRCRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT STL FROM FLIGHT 2035 ON 09-21-04 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED ELECTRONIC COMPARTMENT FAN, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR REMAINS OPEN PENDING ADDITIONAL INFORMATION.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 5,707 hrs · 4,374 cycles

SHV- DURING A ROUTINE CHECK THE COCKPIT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE DURING THE EMERGENCY LIGHT FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE BULB IAW EMB 145 AMM 33-50-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING SERVICE/ROUTINE CHECK, MAINTENANCE FOUND FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERATIVE ON THE RT SIDE. REMOVED AND REPLACED RT FORWARD OVERWING EMERGENCY LIGHT IAW EMB145 AMM NR 33-50-07, OPS. CHECKED GOOD.

Part: ODOR — DETECTED (APU)

CLE FLIGHT 2327 THE CREW REPORTED A MOMENTARILY SMOKE ODOR IN THE CABIN ON LANDING WHEN SELECTING THE APU BLEED. MAINTENANCE INSPECTED AND PLACED THE APU BLEED SYSTEM ON MEL.

Part: INVERTER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE AFT 3 EMERGENCY AISLE PATH LIGNT STRIPS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED REAR INVERTER OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 4,276 hrs · 3,253 cycles

SHV-DURING C CHECK THE NUMBER 3 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 4,276 hrs · 3,253 cycles

SHV-DURING C CHECK THE NUMBER 6 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK, THE NUMBER 4 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A EXPOSED WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK, THE NUMBER 5 PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,276 hrs · 3,253 cycles

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

Part: STIFFENER — GOUGED (NACELLE) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK, THE LEFT HAND LOWER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NACELLE) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK, THE RIGHT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NACELLE) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK, THE LEFT HAND UPPER COWLING INTERNAL AFT STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 4,276 hrs · 3,253 cycles

SHV-DURING C CHECK STRINGER 19 LEFT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PEROFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 4,276 hrs · 3,253 cycles

DURING C-CHECK STRINGER 19 RIGHT WAS FOUND TO BE GOUGED BETWEEN FRAMES 52 AND 53. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR — FAULTY (COCKPIT) · airframe 4,191 hrs · 3,184 cycles

CREW REPORTED, LANDING GEAR AURAL WARNING REPEATEDLY WHEN LANDING GEAR RETRACTED. MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW EMB 145 MM 27-53-03 AND OPS CHECKED GOOD. GEAR SWING PERFORMED AND OPS CHECKED GOOD REFERENCE EMB145 MM 32-32-00. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

CREW NOTED THAT THE FLAPS FAILED IN FLIGHT, DECLARED EMERGENCY, DID AN EMERGENCY DESCENT AND LANDED WITHOUT INCIDENT. THE CREW CONTACTED MAINTENANCE CONTROL, PERFORMED FLAP RESET, OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS)

INBOUND, PILOT REPORTED A FLAP FAIL MESSAGE. THE AIRCRAFT LANDED WITH THE FLAPS AT ZERO WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP SYSTEM, PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PUMP — READS HIGH (NR 1 ENG FUEL)

FLIGHT NR 2678, THE CREW REPORTED AT 28000 FT, THE AIRCRAFT BEGAN TO SHAKE AND THE NR 1 ENGINE N1 EXCEEDED 103 PERCENT. THE NR 1 ITT WAS AT LEAST 940 DEGRESS. THE CAPTAIN REDUCED THRUST TO IDLE WITH NO RESPONSE FROM THE ENGINE. THE CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 FUEL PUMP METERING UNIT AND BOTH 1A AND 1B FADEC'S. OPERATIONAL CHECKS WERE GOOD ON THE GROUND.THE AIRCRAFT WAS TEST FLOWN WITH NO DISCREPANCIES. 1A FADEC P/N 23074001 S/N BX160136 1B FADEC P/N 23074001 S/N BX160138

Part: FLAP — MALFUNCTIONED (WING) · airframe 1,857 hrs · 1,319 cycles

BHM/EWR---CO3374, CREW REPORTED, FLAP FAIL INFLIGHT, NO RESET. DECLARED EMERGENCY AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE PERFORMED FLAP RESET. VISUALLY INSPECTED FLAPS, NO DEFECTS NOTED. OPERATED AND INSPECTED FLAPS IAW EMB145 MM 27-50-00. OPS CHECKED GOOD.