N14991

Part: WEB — CRACKED (ZONE 100)

FORWARD FUSELAGE I FRAME WEB 04 CRACKED CAUSED BY HINGE OVER EXTENDED. REPAIRED IAW EMBRAER ETD2023-145-024609 REV .:/

Part: SKIN — CORRODED (ZONE 100)

AFT RADIO ALTIMETER BASE AND FUSELAGE SKIN CORRODED. COMPLETED REPAIR IAW EMBRAER ETD2023-145-023314 REV.:/ INTERNAL AND EXTERNAL DET INSPECTION REQUIRED AT THRESHOLD OF 7,173 FC WITH INTERVAL OF 7,173 FC.

Part: SKIN — CORRODED (ZONE 100)

REAR FUSELAGE I LOWER SKIN AT RADIO ALTIMETER CORRODED BETWEEN FRAMES 65-66 REPAIRED IAW EMBRAER ETD2023-145-023822 REV.:/

Part: CROSSBEAM — CRACKED (NLG WW) · airframe 45,189 hrs · 34,731 cycles

NLG UPLOCK BOX AFT CROSS MEMBER CRACKED AT L/H CENTER. REMOVED AND REPLACED CROSS MEMBER. AIRCRAFT STILL IN MAINTENANCE.

Part: SUPPORT FITTING — CRACKED (NLG WW) · airframe 45,189 hrs · 34,731 cycles

NLG UPLOCK BOX SUPPORT FITTING IS CRACKED AT BOTH FORWARD LOWER CORNERS. REMOVED AND REPLACED SUPPORT FITTING. AIRCRAFT STILL IN MAINTENANCE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 45,178 hrs · 34,722 cycles

PILOT REPORTED CONTACTORS TICKING BY THE FO'S SIDEWALL. SLIGHT SMELL ASSOCIATED. MX PERFORMED INSPECTION ON RIGHT SIDE RELAY SUPPORT NO SIGN OF BURN OR BURN SMELL. ALL RELAYS LOOK NORMAL AND CLEAN. A/C APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT HORIZ STAB) · airframe 44,156 hrs · 33,886 cycles

DISCREPANCY: RT HORIZONTAL STABILIZER I/B FITTING HOUSING SLEEVE BUSHING MIGRATED. CORRECTIVE ACTION: REMOVED BUSHING REAMED TO FIRST REWORK AND INSTALLED IN ACCORDANCE WITH SRM 55-10-02.

Part: BUSHING — CORRODED (RT HORIZ STAB) · airframe 44,156 hrs · 33,886 cycles

DISCREPANCY: RT HORIZONTAL STABILIZER O/B FITTING HOUSING SKIN CORROSION. CORRECTIVE ACTION: REMOVED BUSHING REAMED TO FIRST REWORK AND INSTALLED IN ACCORDANCE WITH SRM 55-10-02.

Part: BUSHING — MIGRATED (RT HORIZ STAB) · airframe 44,156 hrs · 33,886 cycles

DISCREPANCY: RT HORIZONTAL STABILIZER O/B FITTING HOUSING SLEEVE BUSHING MIGRATED. CORRECTIVE ACTION: REMOVED BUSHING REAMED TO FIRST REWORK AND INSTALLED IN ACCORDANCE WITH SRM 55-10-02.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 44,156 hrs · 33,886 cycles

LEFT INBOARD FLAP TOP SURFACE HAS AREA OF DELAMINATION AT INBOARD END OF FLAP AT TRAILING EDGE. - CORRECTIVE ACTION - REPAIRED FLAP SURFACE IAW SRM 51-72-03 AND SRM 57-52-00, STEP 5.A.3.

Part: SUPPORT — CRACKED (COCKPIT) · airframe 44,156 hrs · 33,886 cycles

TYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE COCKPIT LT UPPER LATERAL SUPPORT CRACKED. MAINTENANCE REMOVED THE DAMAGED SEGMENT AND SPLICED IN A NEW SEGMENT OF THE BRACKET IAW ETD2019-145-083562. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-30) · airframe 44,156 hrs · 33,886 cycles

DURING C-CHECK INSPECTION, FOUND THE R/H FLOOR SILL HAS FOUND CORROSION SPOTS BETWEEN FRAMES23 THRU 30. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL AT FRAMES 23 THRU 30 IAW EMB 145 SRM.51-40-02.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 44,156 hrs · 33,886 cycles

DURING C-CHECK INSPECTION, FOUND A CORRODED DOUBLER AT THE POTABLE WATER NIPPLE ON EXTERNAL FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 44,156 hrs · 33,886 cycles

DISCREPANCY: FRAME 25, STRINGER 15R-16R CRACKED. CORRECTIVE ACTION: COMPLETED REPAIR TO FRAME 25, STRINGER 15R-16R IN ACCORDANCE WITH SRM 53-00-04.

Part: SKIN — CRACKED (FRAME 75) · airframe 44,156 hrs · 33,886 cycles

L/H UPPER FUSELAGE SKIN CRACKED AT FRAME 75 STRINGER 2L - 3L. CUTOUT DAMAGED SKIN, FABRICATED FILLER, DOUBLER AND DRAG ANGLE AND INSTALLED.

Part: SKIN — CRACKED (FRAME 75) · airframe 44,156 hrs · 33,886 cycles

R/H UPPER FUSELAGE SKIN CRACKED AT FRAME 75. REPAIRED AREA BY CUTTING OUT DAMAGE, FABRICATED AND INSTALLED FILLER, DOUBLER, SHIM AND REPAIR ANGLE, SEALED, ALODINED, PRIMED AND PAINTED. AIRCRAFT STILL IN C CHECK.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING SCHEDULED MX INSPECTION, THE EMERGENCY EXIT SIGN AT SEAT 18D WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN INVERTER, OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (CABIN)

RIC FLIGHT 4330 DURING SCHEDULED MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN AT SEAT 15D WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT SIGN INVERTER WITH OPERATIONAL CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (FLOOD LIGHT) · airframe 41,739 hrs · 31,918 cycles

THE CREW REPORTED SMOKE FROM ABOVE EICAS APPEARED TO COME FROM FLOOD LIGHT OVER EICAS. SMOKE STOPPED WHEN THE FLOOD LIGHT WAS TURNED OFF. MAINTENANCE INSPECTED AND REPLACED THE FLOOD LIGHT ABOVE EICAS AND REPLACED POWER INVERTER. OPERATIONAL CHECKS WERE GOOD. FLOOD LIGHT P/N 10-123C

Part: SEAL — DEPARTED (WINDSHIELD) · airframe 41,692 hrs · 31,875 cycles

WINDSHIELD RUBBER TRIM TORE OFF DURING DESCENT AND WAS POSSIBLY INGESTED INTO NR 1 ENGINE. STRONG BURNING RUBBER ODOR FOR 10 MINUTES FOLLOWED. MX PERFORMED INSPECTION OF THE LT ENGINE FOR POSSIBLE FOD. NO DEFECTS NOTED. RAN ENGINE AT HIGH POWER FOR SEVERAL MINUTES NOT SMOKE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 40,297 hrs · 30,733 cycles

CARGO DOOR CUTOUT LOWER BEAM CORRODED. THE BEAM WAS REPLACED IAW SRM 51-40-02.

Part: CAP — CORRODED (LT MLG) · airframe 40,297 hrs · 30,733 cycles

LEFT MAIN LANDING GEAR AFT LOWER TRUNNION CAP CORRODED. TRUNNION CAP REPLACED IAW 32-10-01.

Part: SHEAR TIE — CRACKED (FRAME 74) · airframe 40,297 hrs · 30,733 cycles

SHEAR TIE CRACKED ON FRAME 74. THE SHEAR TIE WAS REPAIRED IAW EO 145-53-20-00002. PERFORMED HFEC INSPECTION WITH NO FAULTS FOUND.

Part: TRUNNION — CRACKED (RT MLG) · airframe 40,297 hrs · 30,733 cycles

RIGHT MAIN LANDING GEAR AFT UPPER TRUNNION FOUND CRACKED. THE TRUNNION WAS REPLACED IAW ETD2017-145-048465.

Part: CHANNEL — CORRODED (SERVICE DOOR) · airframe 40,297 hrs · 30,733 cycles

SURFACE CORROSION ON SERVICE DOOR CHANNEL. THE CHANNEL WAS REPAIRED IAW SRM 53-21-02, ITEM 2, FIG 201.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 40,297 hrs · 30,733 cycles

FLOOR SUPPORT ANGLE CRACKED. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: GUSSET — CORRODED (CARGO FLOOR) · airframe 40,297 hrs · 30,773 cycles

CARGO FLOOR LEFT MID GUSSET CORRODED. THE GUSSET WAS REPLACED IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FLOOR SUPPORT) · airframe 40,297 hrs · 30,733 cycles

FLOOR SUPPORT ANGLE CRACKED. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FLOOR) · airframe 40,297 hrs · 30,733 cycles

CARGO FLOOR CENTER GUSSET CORRODED. THE GUSSET WAS REPLACED IAW SRM 51-40-09.

Part: FRAME — CORRODED (FRM 65) · airframe 40,297 hrs · 30,733 cycles

CARGO DOOR SURROUND FORWARD, FRAME 65 CORRODED. THE FRAME WAS REPAIRED IAW SRM 53-31-04, PARAGRAPH 4, FIG 212.

Part: FLOOR SUPPORT — CORRODED (CENTER CABIN) · airframe 40,297 hrs · 30,733 cycles

CENTER FUSELAGE, LEFT FORWARD FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02

Part: BULKHEAD — CRACKED (NLG WW) · airframe 40,297 hrs · 30,733 cycles

NOSE WHEEL WELL CENTER VERTICAL WEB ON PRESSURE BULKHEAD CRACKED. NOSE CENTER VERTICAL WEB REPLACED AS PER SRM 51-40-02.

Part: GUSSET — CORRODED (FLOOR STRUCTURE) · airframe 40,297 hrs · 30,733 cycles

CENTER FUSELAGE 1 LEFT FORWARD GUSSET CORRODED. THE GUSSET REPLACED.

Part: DECK PLATE — CORRODED (CARGO BAY) · airframe 40,297 hrs · 30,733 cycles

CARGO FORWARD DECK PLATE CORRODED. THE DECK PLATE REPLACED IAW SRM 51-40-02.

Part: RIB — CRACKED (LT WING) · airframe 39,758 hrs · 30,323 cycles

LT MLG BAY RIB 5 CRACKED. AIRCRAFT IS PARKED ON THE RAMP GROUNDED AT THIS TIME WAITING FOR PARTS AND TOOLING.

Part: RIB — CRACKED (LT WING) · airframe 39,758 hrs · 30,323 cycles

LT WING RIB 21 CRACKED AT TOP ACCESS 551CB. AIRCRAFT IS PARKED ON THE RAMP AND GROUNDED AT THIS TIME WAITING FOR PARTS AND TOOLING FOR THE RIB 5 REPAIR. (SEE ASOA201610247001)

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 39,188 hrs · 29,870 cycles

PILOT REPORTED AN OCCASSIONAL ELECTRICAL SMELL FROM THE FRONT ENTRANCE IN COCKPIT AREA. MX REMOVED AND REPLACED SEAT 1A CEILING BALLAST WITH OPERATIONAL CHECK. A/C APPROVED FOR RETURN TO SERVICE.

Part: WIRE — UNSECURE (LIGHT) · airframe 38,732 hrs · 29,495 cycles

CREW SMOKE REPORTED COMING FROM SIDEWALL LIGHT LAST ROW. MAINTENANCE SECURED THE WIRE AND OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN LIGHTS) · airframe 35,729 hrs · 27,087 cycles

THE CREW REPORTED SMOKE AND FIRE ABOVE 5A SEEN AND SMELLED BY LIGHT FIXTURE. THE ACFT WAS FERRIED, WHERE IT LANDED WITHOUT INCIDENT, MAINTENANCE INSPECTED ATHE ACFT AND R & R THE AFFECTED CEILING LIGHT WIRING HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — BURNED (CABIN LIGHT) · airframe 35,729 hrs · 27,087 cycles

THE CREW REPORTED SMOKE AND FIRE ABOVE 5A SEEN AND SMELLED BY LIGHT FIXTURE. THE ACFT WAS FERRIED, WHERE IT LANDED WITHOUT INCIDENT, MAINTENANCE INSPECTED ATHE ACFT AND R & R THE AFFECTED SIDEWALL LIGHT HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 35,347 hrs · 26,783 cycles

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

Part: SUPPORT — CRACKED (FRAME 10) · airframe 35,347 hrs · 26,783 cycles

DURING C-CHECK. LEFT DV WINDOW SUPPORT CRACKED AT FR. 10. R & R THE SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CRACKED (FRAME 10) · airframe 35,347 hrs · 26,783 cycles

DURING C-CHECK, RT DV WINDOW SUPPORT CRACKED AT FRAME 10. R & R THE SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (NR 4 BRAKE) · airframe 34,542 hrs · 26,149 cycles

THE CREW REPORTED PRONOUNCED RIGHT PULL WHEN BRAKE IS APPLIED AT TAXI SPEEDS, F/O LEFT BRAKE FEELS SPONGY, BRAKES LOUD WHEN APPLIED. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT AND NR 4 BRAKE ASSY. OPS CHECKS WERE GOOD.

Part: DISPLAY — OVERHEATED (COCKPIT) · airframe 33,596 hrs · 25,419 cycles

THE CREW REPORTED AN UNBEARABLE ODOR IN THE COCKPIT AND WERE UNABLE TO AIR IT OUT. MAINTENANCE INSPECTED THE ACFT AND R & R THE NR 2 MFD, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK SHEAR CLIP AT FRM 65 CORRODED (LOCAL LEVEL 2) AT CARGO LOWER CUT OUT. MX R & R SHEAR CLIP AT FRM 65 CARGO LOWER CUTOUT IAW EMB-145, SRM 51-40-02 AND EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK BAGGAGE DOOR MAIN BEAM CORRODED (LOCAL LEVEL 2) FRMS65-68. MX R & R BAGGAGE DOOR MAIN BEAM AT FRMS 65-68 IAW CPM 51-26-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK SHEAR CLIP AT FRM 68 CORRODED AT CARGO DOOR CUTOUT. MX R & R SHEAR CLIP AT FRM 68 AT CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02 AND EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK, NUTPLATE BRACKET CORRODED (LOCAL LEVEL 2) AT UPPER FWD CORNER BAGGAGE DOOR CUTOUT FRM 65. MX PERFORMED REPAIR AND REMOVED CORROSION ON BRACKET AROUND NUTPLATE HOLE AT FRM 65 UPPER FWD CORNER BAGGAGE DOOR CUTOUT AT FRM 65 IAW CPM 51-21-06 AND EC5320-01479, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK, SERVICE DOOR CENTER SILL CORRODED. MX R & R SERVICE DOOR SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK RT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION ON RT HORIZ STABILIZER L/E IAW EC5530-01116, REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK CORRODED CARGO DOOR INNER SKIN AROUND NUT PLATE HOLES. MX PERFORMED REPAIR AT CARGO DOOR INNER SKIN AROUND NUTPLATE HOLES IAW EC5320-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — NICKED (CARGO DOOR) · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK FWD LOWER INNER CARGO DOOR SKIN HAS NICK. MX PERFORMED REPAIR AT FWD LOWER INNER CARGO DOOR SKIN IAW EC5320-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIVET — LOOSE (ZONE 200) · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK WORKING RIVET AT FR 79, STR 9R. MX PERFORMED REPAIR TO WORKING RIVET FR 79, STR 9R IAW EC5330-02699. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 30,595 hrs · 23,093 cycles

DURING C-CHECK LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN CORROSION (LOCAL LEVEL 2) AROUND RIVETS. MX PERFORMED REPAIR AND REMOVED CORROSION (LOCAL LEVEL 2) FROM LT HORIZONTAL STABILIZER L/E UPPER AND LOWER SKIN AROUND RIVETS IAW EC5530-01116 REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — BURNED (CABIN LIGHT) · airframe 29,451 hrs · 22,172 cycles

ACFT RETURN TO THE GATE WHEN A BURNING ODOR IN THE CABIN WAS DETECTED. MX FOUND THE 2A LIGHT BURNED OUT. ACFT WAS THEN RELEASED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,624 hrs · 21,497 cycles

FLIGHT 6140, DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT ABOVE THE GALLEY SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (SMOKE DETECTOR) · airframe 28,542 hrs · 21,443 cycles

FLIGHT 4427, CREW REPORTED A BAGGAGE SMOKE INDICATION ON TAKE OFF ROLL. MAINTENANCE REMOVED AND REPLACED THE BAGGAGE SMOKE DETECTOR TEST SWITCH, OPS TESTED WITH NO DEFECTS, AND AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 27,184 hrs · 20,394 cycles

GRB FLT 4363 THE CREW REPORTED PRESSURIZATION MALFUNCTION IN FLIGHT. AIRCRAFT CABIN CLIMBED WITH AIRCRAFT ALTITUDE UNTIL 6000 FT. AIRCRAFT LEVELED OUT. THE CABIN RATE SHOWING +3000FT/MIN THEN -2000 FT/MIN THEN AMBER DASHES. THE CREW REPORTED THE SYSTEM FIXED ITSELF AND WORKED NORMALLY REMAINDER OF FLIGHT. MAINTENANCE REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 27,125 hrs · 20,345 cycles

EWR - CREW REPORTED AUTO PRESSURIZATION FAIL IN FLIGHT AND PERFORMED AIR RETURN UNEVENTFULLY. EWR MX REMOVED AND REPLACED THE DIGTITAL PRESSURE CONTROLLER IAW EMB145 AMM 21-31-00 AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,589 hrs · 19,926 cycles

IAH- FLIGHT 2844 THE CREW REPORTED A LOUD SQUEAL IN THE MAIN CABIN DOOR FOLLOWED BY A PARTIAL LOSS OF PRESSURIZATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM IN AUTO AND MANUAL MODES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SEAL — DIRTY (SERVICE DOOR) · airframe 25,659 hrs · 19,194 cycles

IAH - FLIGHT 2572, THE CREW REPORTED A LOUD PRESSURIZATION SQUEAL AT FL350 AND 7.6DELTA P, AND CABIN PRESSURE WENT TO 9000 AT FL350. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED AND LUBRICATED THE SERVICE DOOR SEAL, PRESSURIZED THE AIRCRAFT WITH NO LEAKS OR NOISE NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 25,285 hrs · 18,929 cycles

FLIGHT 2234 - EWR - FLIGHT CREW REPORTED BOTH PACK VALVES CLOSED, AND WOULD NOT OPEN. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 SLEEVE BETWEEN HEAT EXCHANGER AND DUAL TEMPERATURE CONTROL VALVE (SDR # C2XA10RI160) AND REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH (SDR # C2XA10RI161). MX PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SLEEVE — DAMAGED (AC BAY) · airframe 25,285 hrs · 18,929 cycles

FLIGHT 2234 - EWR - FLIGHT CRERW REPORTED BOTH PACK VALVES CLOSED, AND WOULD NOT OPEN. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 SLEEVE BETWEEN HEAT EXCHANGER AND DUAL TEMPERATURE CONTROL VALVE (SDR # C2XA10RI160) AND REMOVED AND REPLACED NR 2 BLEED PUSH BUTTON SWITCH (SDR # C2XA10RI161). MX PERFORMED OPERATIONAL CHECK SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DUCT — OUT OF POSITION (AC BAY) · airframe 24,815 hrs · 18,552 cycles

PACK 2 VALVE FAILED IN FLIGHT. FOUND DUEL TEMP CONTROL VALVE OUTLET DUCT OFF. RE-INSTALLED DUCT IAW EMB 145AMM 21-51-02. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 22,175 hrs · 16,587 cycles

FLIGHT 2075 - EWR - FLIGHT CREW REPORTED ABNORMAL BURNT ODOR IN CENTER OF CABIN. EWR MX RUN BOTH PACKS, INSPECTED ALL CEILING AND SIDEWALL LIGHTS AND COULD NOT DUPLICATE ANY ODOR. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 21,883 hrs · 16,325 cycles

FLIGHT 2693 - EWR - FLIGHT CREW REPORTED ELECTRIC BURNING SMELL IN 1A SEAT AREA. EWR MX REMOVED AND REPLACED BALLAST AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROL MODULE — FAULTY (CABIN LIGHT) · airframe 21,823 hrs · 16,317 cycles

CREW REPORTED A ELECTRICAL ODOR FROM OVERHEAD SEAT 1A. MX INSPECTED AND REPLACED THE CABIN LIGHT CONTROL MODULE. OPS CHECKS WERE GOOD.

Part: CONTROL MODULE — FAULTY (CABIN LIGHTS) · airframe 21,824 hrs · 16,318 cycles

CREW REPORTED A ELECTRICAL ODOR IN THE CABIN. MX INSPECTED AND REPLACED THE CABIN LIGHTS CONTROL MODULE. OPS CHECKS WERE GOOD.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 21,312 hrs · 15,913 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND WHILE PERFORMING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 21,102 hrs · 15,756 cycles

IAH - FLIGHT 2523 - THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEE POT WHEN TURNED ON. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO COFFEEMAKER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,093 hrs · 15,752 cycles

IAH - FLIGHT 2400 - THE CREW REPORTED A STRONG ELECTRICAL SMELL WHEN BREWING COFFEE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT OPERATIONALLY TESTED THE NUMBER ONE COFFEEMAKER, ALL WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 21,002 hrs · 15,685 cycles

AIRCRAFT IN FOR A 5C INSPECTION WHEN CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT FRAME NEAR THE AFT LOWER ROLLER. MAINTENANCE REPAIRED FRAME 22 IAW EC5310--01464. COMPLIED WITH COLD WORKING AND FINAL REAM OF LOWER TWO AFT SERVICE DOOR STOPS IAW EA 5310-01054. REFERENCES USED WERE EC5310-01464; EMB135/145 SRM 51-10-03 AND IC 2009-455/01616. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,011 hrs · 15,692 cycles

FUSELAGE SKIN DENTED AFT OF FRM 7 BETWEEN STR 12L AND 13L. CUT AND REMOVED THE DAMAGED SECTION OF SKIN SPLICE STRAP. RE-CONTOURED THE DENTED AREA OF SKIN AND THE PRESSURE BULKHEAD ATTACH FLANGE AND PERFORMED DYE PEN TO SKIN AND FLANGE, NO CRACKS NOTED. INSTALLED NEW SECTION OF SKIN SPLICE STRAP AND FILLED REMAINING DENTS WITH HYSOL. PRIMED AND PAINTED. ALL WORK C/W IAW EC5330-01891. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BUSHING — MIGRATED (WING) · airframe 21,002 hrs · 15,685 cycles

AIRCRAFT IS IN FOR A 5C CHECK WHEN THE LEFT AND RIGHT INBOARD AND OUTBOARD GROUND SPOILER HINGE TO WING BUSHINGS WERE FOUND MIGRATED. MAINTENANCE RESEATED THE BUSHINGS IAW EMB 145 AMM 20-10-08. ALL PROCEDURES COMPLY WITH EC 5740-01152. AIRCRAFT WILL BE RELEASED TO SERVICE AT THE END OF THE CHECK.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,707 hrs · 14,107 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT MARKER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 17,774 hrs · 13,494 cycles

SMOKE SMELL IN COCKPIT. REMOVED AND REPLACED APU IAW EMB 145 MM 49-14-01. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: RESOLVER — INOPERATIVE (THRUST LEVER) · airframe 16,803 hrs · 12,805 cycles

FLT 2723 EWR - CREW REPORTED THAT AFTER LANDING T/R DISAGREE & FAILURE MESSAGES ON EICAS. AFTER T/R STOWED ENGINE 1 WENT TO UNCOMMANDED T/O THRUST. CREW SHUT DOWN THE ENGINE USING FIRE HANDLE. NO ENGINE PARAMETERS WERE EXCEEDED. EWR MX REMOVED AND REPLACED NR 1 THRUST LEVER RESOLVER IAW EMB145 AMM 76-12-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 16,610 hrs · 12,676 cycles

VERT STAB SPAR 1 INTERNAL SUPPORT BRACKET ON FRM 75 FRETTING. REMOVED FITTING AND BLENDED FITTING AND SKIN. FOUND TO BE WITHIN LIMITS. PERFORMED DYE PEN INSPECTION AND FOUND NO CRACKS. ALODINED, PRIMED, SEALED, INSTALLED FITTING AND APPLIED FILLET SEALANT IAW EC5310-01317. AIRCRAFT STILL IN C-CHECK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 16,545 hrs · 12,630 cycles

IAH - FLIGHT 2628, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT SEAT 12A WAS INOP. MAINTENANCE INSPECTED THE SIGN, SECURED A LOOSE CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,519 hrs · 11,826 cycles

SDF - DISCREPANCY - EMERGENCY EXIT LIGHT INOP AT 12A. OPS CHECKED EMERGENCY LIGHTS FOUND EMERGENCY EXIT LIGHT AT 12A TO BE WORKING CORRECTLY IAW 33-50-00.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 15,359 hrs · 11,713 cycles

MOB - FLT 2415, ON DESCENT THE CREW REPORTED THAT THE FIRST OFFICERS WINDSHIELD SHATTERED ON DESCENT. THE AIRCRAFT LANDED AT MOB WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE F/O'S WINDSHIELD, OPERATIONALLY & LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE — LOCKED (MLG) · airframe 14,139 hrs · 10,767 cycles

ON TAXI CREW REPORTED BRAKES ON LT SIDE WERE SQUEALING AND VIBRATING WHILE TAXIING. MX INSPECTED ACFT, PERFORMED OPS CHECKS BRAKE SYS IAW EMB-145 AMM 32-41-00 NO DEFECTS NOTED, AND ACFT RETURNED TO SERVICE. ACFT CONTINUED TO MAF WHERE ON LANDING NR 1 BRAKE LOCKED BLOWING TIRE, AND CAUSING ACFT TO SWERVE. MX R & R NR 1 & NR 2 MAIN WHEEL ASSY'S, NR 1 & NR 2 BRAKE ASSY'S, BRAKE CONTROL UNIT, AND OUTBOARD BRAKE CONTROL VALVE. OPS CHECKS, NO DEFECT, ACFT RETURNED TO SERVICE. [07-13-07] ON 07/03/06 THE MAINTENANCE FOUND THE NR 1 & 2 WHEEL SPEED TRANSDUCER CONNECTORS TO BE CROSSED. MX CORRECTED THE ROUTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 13,503 hrs · 10,246 cycles

CLE FLIGHT NR 2035, CREW REPORTED ROARING NOISE FROM UNDER COCKPIT. AIR RETURN. MAINTENANCE INSPECTED AND FOUND NOSE GEAR PROXIMITY SWITCH INOPERATIVE. REMOVED AND REPLACED NOSE GEAR PROXIMITY SWITCH. OPERATIONAL CHECKS REPORTED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,145 hrs · 9,144 cycles

DURING ROUTINE MAINTENANCE, THE LEFT EMERGENCY DOOR EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 3 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: BULB — BLOWN (EMERGENCY LIGHT) · airframe 10,505 hrs · 7,860 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,901 hrs · 7,396 cycles

CLE- FLIGHT 2267, CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN AT ROW 12. ALL OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN)

CREW REPORTED, ROW 12A EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS IAW EMB145 AMM 33-50-00. OPS CHECKED GOOD.

Part: ENGINE — FAILED (LEFT)

THE CREW REPORTED NR 1 ENGINE VIBRATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO DAYTON AND LANDED. AFTER LANDING THE NR 1 ENGINE HAD A SMALL FIRE OUT THE BACK OF THE ENGINE. THE FIRE WAS EXTINGUISHED AND NO OTHER INCIDENT OCCURRED. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. THE AIRCRAFT WAS INSPECTED AND THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS FOUND DISCHARGED. THE AFFECTED PACK WAS REMOVED AND REPLACED, THE LIGHTING SYSTEM OPERATIONALLY TESTED, AND THE DISCREPANCY CLEARED.

Part: LANDING GEAR — UNDERSERVICED (NLG)

DURING CLIMB THE CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE NOSE LANDING GEAR WAS UNDERSERVICED. THE LANDING GEAR WAS SERVICED AND THE AIRCRAFT TEST-FLOWN. THE TEST FLIGHT WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TUBE — MALFUNCTIONED (NLG)

FLIGHT 2766 - CREW REPORTED THAT THE LANDING GEAR FAILED TO RETRACT WITH AN ASSOCIATED LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE FOUND THE NOSE LANDING GEAR SLIDING TUBE TO BE LOCKING UP IN THE NOSE GEAR STRUT HOUSING. THE NOSE LANDING GEAR ASSEMBLY WAS REMOVED AND REPLACED, OPERATIONALLY TESTED, AND THE DISCREPANCY CLEARED.

Part: CONNECTOR — LOOSE (CABIN) · airframe 8,534 hrs · 6,342 cycles

PILOT REPORT, PORT EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE PORT EMERGENCY EXIT LIGHT CONNECTOR. AIRCRAFT WAS RELEASED.

Part: PROXIMITY SWITCH — FAULTY (LT MLG)

CLE FLIGHT 2249 THE CREW REPORTED THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED ON THE EICAS DURING FLIGHT. MAINTENANCE INSPECTED THE LEFT MAIN GEAR AND REPLACED BOTH DOWNLOCK PROXIMITY SWITCHES. OPERATIONAL CHECKS WERE GOOD. P/N 8-527-1, S/N 14544.

Part: LAMP — BLOWN (EMERGENCY LIGHT) · airframe 7,630 hrs · 5,619 cycles

DURING C CHECK THE LT EMERGENCY EXIT WALL LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAMP IAW EMB 145 AMM 33-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (NR 2 NACELLE) · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK MAINTENANCE FOUND THE NR 2 ENGINE UPPER COWLING AFT STIFFENER TO BE CHAFED. 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: STIFFENER — CHAFED (NR 2 NACELLE) · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE NR 2 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED ALONG THE ENTIRE RADIUS. MAINTENANCE REMOVED THE DAMAGED AFT STIFFENER AND REPLACED IT WITH A NEW AFT STIFFENER IAW WITH EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (NR 1 COWL) · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK MAINTENANCE FOUND THE NR 1 LOWER ENGINE COWLING CENTER RIB TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED RIB IAW EMB 145 SRM 51-21-04 AND 51-21-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (NR 1 NACELLE) · airframe 7,614 hrs · 5,608 cycles

SHV-DURING C CHECK A NR 1 ENGINE LOWER COWLING INBOARD RIB 8 INCHES FORWARD OF AFT RIB WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE RIGHT HAND SILL BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE CORRODED. MIANTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE RT SILL BETWEEN FRAMES 19 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

SHV-DURING C CHECK THE LEFT FLOORBEAM BETWEEN FRAMES 20 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE LT FLOORBEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE SERVICE DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SEVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

SHV-DURING C CHECK THE AFT DIGITAL STRAP BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01079. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

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

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C CHECK THE LT SILL BETWEEN FRAMES 18 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

SHV-DURING C-CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRAP — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

SHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 15 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (CABIN) · corrosion level 2 · airframe 7,614 hrs · 5,608 cycles

DURING C-CHECK THE CENTER RAMP ANGLE AT FRAME 20 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: ECU — INOPERATIVE (MLG)

STL-EWR CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AFTER A UNSUCCESSFUL RECYCLE THE A/C DIVERTED INTO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED THE LANDING GEAR ELECTRONIC GEAR UNIT AND LANDING GEAR CONTROL HANDLE IAW EMBRAER MM 32-32-01 AND 32-32-02. OPS CHECK WERE GOOD IAW 32-32-02. A/C WAS RELEASED FOR SERVICE.