N17984

Part: ENGINE — ODOR (NR 1) · airframe 44,020 hrs · 33,606 cycles

THE CREW REPORTED A STRONG OIL ODOR FROM THE PACKS AFTER TAKEOFF. MAINTNENACE INSPECTED AND REPLACED THE NR 1 ENGINE IAW TASK CARD 6271001. OPS CHECKED GOOD.

Part: CHANNEL — CORRODED (DOOR STRUCTURE) · airframe 41,213 hrs · 31,350 cycles

SERVICE DOOR LOWER CHANNEL CORRODED AROUND ANCHOR NUTS. SERVICE DOOR LOWER CHANNEL REPLACED IAW SRM 51-40-02.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 41,213 hrs · 31,350 cycles

CARGO DOOR SURROUND STRUCTURE, LOWER BEAM FOUND CORRODED. OUT OF TOLERANCE. THE LOWER BEAM WAS REPLACED IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 41,213 hrs · 31,350 cycles

CORROSION ON PAX DOOR LOWER FRAME AROUND NUT PLATE HOLES. REPAIRED IAW ETD 2017-145-035391.

Part: SUPPORT — CORRODED (WASTE DRAIN) · airframe 41,213 hrs · 31,350 cycles

SURFACE CORROSION FOUND ON WASTE DRAIN VALVE SUPPORT. WASTE DRAIN VALVE SUPPORT REPLACED IAW SRM 51-40-02.

Part: CHANNEL — CRACKED (FWD BULKHEAD) · airframe 41,213 hrs · 31,350 cycles

RIGHT CHANNEL CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEEL WELL. THE CHANNEL WAS REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (NOT REPORTED) · airframe 41,213 hrs · 31,350 cycles

FLOORBEAM CORRODED UNDER GUSSET AROUND ANCHOR NUT. THE FLOORBEAM WAS REPAIRED IAW SRM 53-24-10, PAR 3, FIG 202, SHEET 3.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 41,213 hrs · 31,350 cycles

CARGO DOOR SURROUND STRUCTURE SHEAR TIE CORRODED AT FRAME 65. THE SHEAR TIE WAS REPAIRED IAW SRM 53-31-04, STEP 4F.

Part: ANGLE — CRACKED (FRAME 10) · airframe 41,213 hrs · 31,350 cycles

COCKPIT LEFT FRAME 10, UPPER ANGLE CRACKED. ANGLE REPLACED IAW SRM 51-40-02.

Part: CROSSBEAM — CRACKED (NLG BAY) · airframe 41,213 hrs · 31,350 cycles

NLG UPLOCK FORWARD CROSSBEAM CRACKED. FORWARD CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.

Part: CROSSBEAM — CRACKED (NLG BAY) · airframe 41,213 hrs · 31,350 cycles

NLG UPLOCK AFT CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.

Part: FIREWALL — CRACKED (APU BAY) · airframe 37,953 hrs · 28,779 cycles

DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE APU FIREWALL AT APPROXIMATELY THE 2 O'CLOCK POSITION NEAR AN EXISTING DOUBLER. MAINTENANCE REMOVED THE EXISTING DOUBLER AND PERFORMED A COMBINATION REPAIR IAW SRM 53-32-13 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,702 hrs · 27,793 cycles

THE CREW REPORTED EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS 2-8 AND EXIT SIGN BY MAIN DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: COMPUTER — SHORTED (COCKPIT) · airframe 32,757 hrs · 24,742 cycles

ELECTRICAL ODOR REPORTED IN COCKPIT WITH TERRAIN MESSAGE ON EICAS. MX R & R THE EGPWS COMPUTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — UNSECURE (PAX DOOR) · airframe 32,515 hrs · 24,541 cycles

MX REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN. MX SECURED THE MAIN DOOR HANDLE BRACKET. OPS CHECK OF THE MAIN DOOR SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GROUND STUD — DAMAGED (EMERGENCY LIGHTS) · airframe 32,513 hrs · 24,539 cycles

MX REPORTED THE EMERGENCY LIGHTS CAME ON WITH THE CEILING AND SIDEWALL LIGHTS ACTIVATION AND LIGHTS IN ARM POSITION. MX FOUND GROUND STUD GS8008DC TO HAVE BAD GROUND CONNECTION. CLEANED THE SURFACE AND OPS CHECK OF THE EMERGENCY LIGHTS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,488 hrs · 24,518 cycles

PILOT REPORTED EMERGENCY LIGHTS INOPERATIVE. MX R & R THE NR 3 AND NR 4 EMERGENCY LIGHT SYS BATTERY PACKS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — FAULTY (NR 1 ENGINE OIL) · airframe 31,036 hrs · 23,412 cycles

FLIGHT DIVERTED, CREW REPORTED NR 1 ENGINE OIL PRESSURE IN FLIGHT FLUCTUATED BETWEEN 98-151 PSI. CREW SHUTDOWN ENGINE IN FLIGHT. MX R & R NR1 ENGINE OIL PRESSURE/TEMP SENSOR WITH OPS AND LEAK CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,489 hrs · 22,959 cycles

EMERGENCY LIGHT FLOOR STRIPS NR 2 & 3 INOPERATIVE. R & R NR 3 INVERTER. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,324 hrs · 22,823 cycles

DURING ROUTINE INSPECTION, MX THE FORWARD 3 EMERGENCY AILSE PATH LIGHT STRIPS WERE INOPERATIVE. MX REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: FAN — ODOR (E/E BAY) · airframe 29,288 hrs · 21,957 cycles

CREW REPORTED AN ELECTRICAL ODOR. INSPECTED AVIONICS BAY AND FOUND RECIRCULATION FANS INOPERATIVE. THE SYS WAS RESET AND OPS CHECKED GOOD. NO ELECTRICAL ODOR WAS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,212 hrs · 20,371 cycles

IAH - DURING MAINTENANCE INSPECTION THE AFT AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATOINALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 26,958 hrs · 20,166 cycles

DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY EXIT SIGN AT THE OVERWING ESCAPE HATCH WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: HINGE — GOUGED (RUDDER) · airframe 26,351 hrs · 19,716 cycles

SHV - DURING C-CHECK RUDDER II LOWER CENTER HINGE HAS A GOUGE. MAINTENANCE REMOVED AND REPLACED RUDDER II LOWER CENTER HINGE IAW EC5540-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 26,351 hrs · 19,716 cycles

SHV - DURING C-CHECK CARGO DOOR INNER STRUCTURE BELOW FWD PULLEY HAS MISS DRILL DAMAGE. MAINTENANCE PERFORMED REPAIR ON CARGO DOOR INNER STRUCTURE AND RESTORED TO ORIGINAL FINISH IAW EMB-145 EC5230-01208 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — LOOSE (FUSELAGE) · airframe 26,351 hrs · 19,716 cycles

SHV - DURING C-CHECK VERTICAL STAB SPAR 1 ATTACHMENT AT FRAME 75 SHOWS SIGNS OF MOVEMENT AT O/B AREAS (INSIDE AFT AVIONICS BAY). MAINTENANCE PERFORMED REPAIR OF FRAME 75 FITTING IAW EMB-145 EC5310-01317 REV B. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 26,351 hrs · 19,716 cycles

SHV - DURING C-CHECK SERVICE DOOR AFT CUTOUT HAS CORROSION AT LOWER NUT PLATE HOLE. REPAIRED FRAME IAW EC5310-01548. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 26,351 hrs · 19,716 cycles

SHV - DURING C-CHECK FRAME 65 HAS AREAS OF CORROSION. REPAIRED FRAME IAW EC5310-01505. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 25,623 hrs · 19,140 cycles

EWR FLT 2940 THE CREW REPORTED GLIDESLOPE ISSUES GOING INTO DTW. REPORTED A 1/2 DOT DIFFERENCE BETWEEN GLIDESLOPE INDICATIONS DURING CAT II GS COMPARATIVE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 NAV UNIT AND OPERATIONAL CHECKS WERE GOOD.

Part: SEALANT — ODOR (STATIC PORT) · airframe 23,117 hrs · 17,256 cycles

IAH - FLIGHT 2886, THE CREW REPORTED A BURNING SMELL WHILE TAXIING IN AND WAS STRONGER IN INTENSITY AS THE PARKING BRAKE WAS SET, AND WAS FOUND TO BE STRONGER IN THE MAIN CABIN DOOR / GALLEY AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SMELL TO BE COMING FROM RESIDUAL SEALANT ON THE NUMBER FOUR STATIC PORT WHICH HAD BEEN CHANGED PREVIOUSLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 21,601 hrs · 16,112 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR BEAM AREA CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UPLOCK — FAULTY (RT MLG) · airframe 18,265 hrs · 13,804 cycles

CLE FLIGHT 2251 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING IN FLIGHT. THE AIRCRAFT DIVERTED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,639 hrs · 13,359 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND CEILING EMERGENCY LIGHTS AT ROW 3 AND ROW 14 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB145 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 12,975 hrs · 17,113 cycles

IAH - FLIGHT 2598, THE CREW REPORTED A LOUD NOISE AND VIBRATION IN THE NOSE ARE DURING CRUISE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG UPLOCK BOX PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 17,016 hrs · 12,905 cycles

IAH - FLIGHT 2528, THE CREW REPORTED A -BRK OUTBD- MESSAGE ON EICAS ON FINAL APPROACH, AND THAT THE OUTBOARD BRAKES DID NOT WORK ON ROLLOUT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BRAKES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,996 hrs · 12,886 cycles

SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM FROM FR 20 TO 23. MX REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 18-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 14,849 hrs · 11,206 cycles

CLE FLIGHT 3245 THE CREW REPORTED LOUD NOISE FROM NOSE GEAR AREA DURING CLIMBOUT ABOVE 1700 AND DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT RETRACT. THE NLG DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: WIRE HARNESS — BURNED (CABIN LIGHT) · airframe 12,636 hrs · 9,452 cycles

FLT 2969 - RIC - PRE-FLIGHT - DURING PRE-FLIGHT INSPECTION, SIDE WALL LIGHT AT SEAT 2A WAS SMOKING. RIC MAINTANACE REMOVED AND REPLACED LAMP HARNESS ASSY AND PERFORMED OPERATIONAL TESTS. OPS TEST GOOD. ACFT WAS APPROVED TO RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 12,147 hrs · 9,063 cycles

SHV - DURING C-CHECK THE RT OMEGA BEAM NUT PLATE IS CORRODED JUST AFT OF FRAME 23. MAINTENANCE INSTALLED HAT BEAM REPAIR ON RT OMEGA BEAM AT NUT PLATE HOLE AFT OF FR 23 IAW EMB SRM 53-21-10 FIG 206. INSTALLED NUT PLATE IAW EC 5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 12,147 hrs · 9,063 cycles

DURING C CHECK, PREVIOUS REPAIR TO LT OMEGA BEAM AT FS 20 WAS FOUND TO BE CORRODED. MX REMOVED DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02 AND EMB 145 SRM 51-40-02, EC5320-01140 AND EC 5320-01137. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — BURNED OUT (CABIN) · airframe 11,331 hrs · 8,420 cycles

RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT FLOOR STRIP, BY SEAT 6A, INOP. MAINTENANCE REMOVED AND REPLACED STRIP. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ODOR — DETECTED (CABIN/COCKPIT) · airframe 10,506 hrs · 7,751 cycles

CREW REPORTED, (STRONG FUEL ODOR IN AIRCRAFT WHILE APU IS RUNNING.) MAINTENANCE TROUBLESHOT NO DEFECTS FOUND AND PLACED THE AIRCRAFT ON MEL FOR FURTHER FOLLOWUP. STL MAINTENANCE OPS. CHECKED THE APU WITH BOTH PACKS NR 1 AND NR 2 RUNNING FOR 30 MINUTES, NO DEFECTS, NO FUEL ODOR NOTED AT THIS TIME. OPS CHECKED GOOD, MEL PLACARD ITEM REMOVED AND AIRCRAFT RETURNED TO SERVICE -SDR CLOSED-

Part: FIREWALL — CRACKED (APU BAY) · airframe 7,601 hrs · 5,442 cycles

DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE TOP RIGHT HAND MOUNT. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EC 5330-01250, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

DURING A SCHEDULED INSPECTION THE CENTER RAMP ANGLE AT FRAME 20 WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WAS RELEASED FOR SERVICE AT COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE DIGITAL PLATE WAS FOUND CORRODED AT FR20 & 22. MAINTENANCE REMOVED AND REPLACED THE LEFT TOP CAP DIGITAL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FIREWALL — CRACKED (NACELLE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE APU FIREWALL WAS FOUND CRACKED. MAINTENANCE STOP DRILLED THE CRACK, FABRICATED A DOUBLER AND INSTALLED IAW EC5330-01250. THE REPAIR IS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

DURING A SCHEDULED INSPECTION THE LT SILL WAS FOUND CORRODED IN SEVERAL PLACES BETWEEN FR 19 AND 20. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND SILL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE LEFT AFT OUTBOARD FLOORBEAM IN LAV HAS CORRODED INSERTS AND SURFACE OXIDATION. MAINTENANCE REMOVED AND REPLACED THE CARBON FLOORBEAM IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT AFT FLOOR SILL AT FR22-23 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE AFT SERVICE DOOR SILL IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR LOWER BEAM IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE DIGITAL PLATE AT FR20 & 22 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PLATE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR SILL CHANNEL WAS FOUND CORRODED. MAINTENANCE BLENDED THE CORRODED AREA, FILLED WITH EPOXY RESIN, FABRICATED AND INSTALLED A DOUBLER IAW GST1927/02A AND CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE LOWER RAMP ANGLE ON OMEGA BEAM WAS FOUND CORRODED AT FR20. MAINTENANCE REMOVED AND REPLACED THE LOWER RAMP ANGLE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION, CORRODED INSERTS AND SURFACE OXIDATION WAS FOUND ON FLOORBEAM, LEFT OUTBOARD AFT IN LAV. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN LAV IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE OMEGA BEAM BETWEEN FR20 AND 23 WAS FOUND CORRODED IN SEVERAL PLACES. MAINTENANCE CUT OUT THE DAMAGED AREAS, FABRICATED AND INSTALLED ANGLES, SHIMS, FILLER AND PLATE IAW EMB-135/145 SRM 53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEAM, IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,601 hrs · 5,442 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT SIDE OF RAMP AT FR20 AND CROSSBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CENTER RAMP ANGLE IAW EMB-135/145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN)

ONE SECTION OF EMERGENCY LIGHTS NOT WORKING. MAINTENANCE RELEASED IAW MEL. MAINTENANCE REMOVED AND REPLACED THE EMERGENCT LIGHT STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STARTER — FAILED

Crew reported a momentary #2 engine fire indication. The aircraft returned to IAH and landed without incident. Maintenance inspected the right engine and found that the air turbine starter had failed causing heat damage to the engine outer bypass duct and lower cowling. Maintenance removed and replaced the #2 engine, #2 air turbine starter, and performed repairs to the right lower cowl.

Part: COFFEEMAKER — FAILED (GALLEY)

THE CREW REPORTED A BURNING ELECTRICAL SMELL FROM THE COFFEE WARMER. MAINTENANCE REPLACED THE COFFEE WARMER.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — SEIZED (FUSELAGE)

CLE FLIGHT#3222 THE CREW REPORTED SMOKE IN THE CABIN WITH #2 PACK ON OPERATED OFF THE APU BLEED.MAINTENANCE INSPECTED AND REPLACED THE #2 PACK ACM.OPERATIONAL CHECKS WERE GOOD.

Part: COFFEEMAKER — BURNED (GALLEY)

CLE FLIGHT 3062, THE CREW REPORTED A BURNING SMELL COMING FROM GALLEY HOT JUG. MAINTENANCE INSPECTED AND REPLACED THE GALLEY HOT JUG. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - FLIGHT 3823, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS FROM ROW 12 ON ILLUMINATED WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — MALFUNCTIONED (FA PANEL)

IAH - FLIGHT 4027, THE CREW REPORTED THAT THE EMERGENCY LIGHTS FLASHED INTERMITTENTLY DURING FLIGHT. MAINTENANCE RESET THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (AFT)

CLE - FLT 3829 - AFTER TAKEOFF ON INITIAL CLIMB, THE CREW REPORTED A LAVATORY SMOKE ALARM ILLUMINATED ON THE EICAS. THE BLEEDS AND PACKS WERE SELECTED ON. THERE WAS A SLIGHT HAZE IN THE CABIN. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU THAT WAS ON MEL IAW 49-10-01 AND 36-00-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)