Embraer EMB-135LR

Service difficulty reports · 2,545

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'EMB135LR'
  ORDER BY difficulty_date DESC"

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SDR SIMA200322503Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND CLEANED THE REPAIR AREA. INSTALLED NEW SILL IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-06 AND 51Aug 8, 2003 · N719AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL143Inverter · inoperativeCLE FLIGHT NR 2138 THE CREW REPORTED THE FRONT EMERGENCY LIGHT DID NOT ILLIMINATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INVERTER. OPERATIONAL CHECKS WERE GOOD.Aug 7, 2003 · N17524 · Emb EMB135LR · Emergency LightingSDR C2XA03IA077Gcu · faultyIAH - FLT NR 3325 - UPON APPROACH TO IAH THE CREW REPORTED THAT GENERATOR NUMBERS 1, 2, 3, AND APU SHOWING VOLTS BUT NO AMPS AND THAT GENERATOR 4 WENT OFF LINE AT 1500FT. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AAug 6, 2003 · N24517 · Emb EMB135LR · AC RegulatorSDR C2XA03TY102Engine · lack of lubeTHE LT ENGINE IMPENDING OIL BYPASS INFLIGHT. AFTER APPROXIMATELY 2 MINUTES OIL PRESSURE DROPPED INTO THE RED, 32 PSI AND DROPPING. THE CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. LANDED AT MEM. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW-TASK CAJul 30, 2003 · N29515 · Emb EMB135LR · Engine (Turbine/Turboprop)SDR SIMA200321805Beam · corrodedABI - DURING AN IMBV INSPECTION, THE GALLE FLOOR CENTER BEAM WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER BEAM AND INSTALLED NEW BEAM. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-20-01,03, 51-40-02,04. RESTORED SURFACE Jul 29, 2003 · N713AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200320812Light · inoperativeCREW REPORTED THE FORWARD MOST FLOOR PROXIMTIY EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Jul 27, 2003 · N727AE · Emb EMB135LR · Emergency LightingSDR SIMA200321005Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED AREA AND PERFORMED AN NDT INSPECTION. FABRICATED A FILLER, EXTERNAL ANGLE AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRJul 27, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200321001Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM 145/1142, REV 22, CHAPTERS 51-40-02, 51-40-06, 51-20-03. (M)Jul 25, 2003 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200321002Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT THE DAMAGED AREA OF LEFT OMEGA BEAM AND PERFORMED NDT INSPECTION. FABRICATED AN EXTERNAL DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAWJul 25, 2003 · N713AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200321003Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL AND INSTALLED NEW SILL IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTERS 51-20-03, 51-40-02, 51-40-06 AND 51-20-01. (M)Jul 25, 2003 · N713AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL127Inverter · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN ON THE RIGHT WINDSCREEN DIDN'T ILLUMINATE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.Jul 25, 2003 · N16525 · Emb EMB135LR · Emergency LightingSDR SIMA20030808Light · inoperativeDURING OVERNIGHT MAINTENANCE, THE FLOOR PROXIMITY EMERGENCY LIGHTING AT SEAT 10A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHTS TRIPS IAW EMB MM. OPS CHECK WAS GOOD AND AIRCARFT WAS RETURNED TO SERVICE. (M)Jul 24, 2003 · N733KR · Emb EMB135LR · Emergency LightingSDR SIMA200321006Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL BETWEEN FRAMES 16 AND 18 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUTOUT A 16 INCH BY 21 INCH SECTION OF DAMAGED FORWARD DIGITAL. PREPARED A SECTION OF DIGITAL MATERIAL. FABRICATED SHIM AND TWO DOUBLERSJul 24, 2003 · N713AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200321004Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION. APPLIED TREATMENT TO THE BARE METAL SURFACE. FABRICATED A REPAIR DOUBLER, REPAIR DONE IAW EMB REPAIR STATJul 23, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200320805Skin · gougedABI - DURING AN IMBV INSPECTOIN, SEVEN GOUGES WERE FOUND JUST AFT OF FRAME 24 AND BELOW STRINGER 18L. COMPLETELY REMOVED DAMATE BY PERFORMING A CUTOUT. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMBL 145 SRM, SRM 145/1142 REV 22, 53-22-01, CPM 51-21-0Jul 22, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200320802Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, CORROSION FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CREATIN A CUTOUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND A PLATE. REPAIR DONE IAW EMB 145 SRM, 145-1142 REV 22, 53-21-10 PARA 2 FIG 201 SHJul 22, 2003 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200320806Bearing Cover · corrodedABI - THIS IS A LEVEL TWO ITEM FOUND DURING AND IMBV INSPECTION, THE LEFT AND RIGHT LOWER NOSE LANDING GEAR TRUNNION BEARING CAPS PITTED. REMOGED AND INSTALLED SERVICEABLE CAPS ON NLG IAW EMB 135 AMM 32-20-01. (M)Jul 21, 2003 · N713AE · Emb EMB135LR · Nose/Tail Landing Gear Attach SectionSDR SIMA200320201Inverter · inoperativeBGR - FOUND EMERGENCY EXIT SIGN FOR LEFT OVERWING EXIT WOULD NOT ILLUMINATE. MAINTENANCE INSTALLED NEW INVERTER, OPS CHECK GOOD AND RETURNED A/C TO SERVICE. (M)Jul 18, 2003 · N707EB · Emb EMB135LR · Emergency LightingSDR SIMA200321806Beam · corrodedABI - THIS LEVEL TWO ITEM FOUND DURING AN IMBV INSPECTION, THE CENTER BEAM WEB EXTENSION CORRODED AT FRAMES 22-23. REMOVED CORRODED CENTER BEAM WEB EXTENSION AND INSTALLED SERVICEABLE BEAM IAW EMB 135 SRM 51-20-03, 51-40-06, 51-40-02. (M)Jul 18, 2003 · N715AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200319707Skin · gougedAIRCRAFT ARRIVED FOR PERMANENT REPAIR OF TDMI NR 71153018B, REPAIR OF BLENDED GOUGE BETWEEN STATION 66-67 AND BETWEEN STRINGERS 15-16R. PERFORMED EDDY CURRENT INSPECTION A POSITIVE CRACK INDICATION AS DETECTED. PERFORMED A CUTOUT OF THE DAMAGED AREA. AN ADDJul 10, 2003 · N711PH · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200319002Elevator · damagedCLT - FLT 4430 - DURNG TAKEOFF ROLL AT ABOUT 60 KNTS CREW NOTED YOKES BEING SLAMMED TOWARDS THEM. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. DURING POST FLIGHT NOTED LEFT ELEVATOR TRIM STUCK DOWN IN THE 90 DEGREE POSITION. MAINTENANCE REMOVED AND REJul 8, 2003 · N726AE · Emb EMB135LR · Empennage StructureSDR C2XA03CL117Charger · faultyDURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTS WERE DIM. MAINTENANCE REPLACED THE NR 2 EMERGENCY BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD.Jul 2, 2003 · N15527 · Emb EMB135LR · Emergency LightingSDR SIMA200318104Sign · inoperativeMAINTENANCE REPORTED THE OVERWING EMERGENCY EXIT SIGN TO BE INOPERATIVE. (M)Jun 29, 2003 · N707EB · Emb EMB135LR · Emergency LightingSDR SIMA200317608Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM LOEW FLANGE AND WEB WERE FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 20 AND 22. BLENDED THE DAMGE AREA TO REMOVE ALL CORROSION. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECJun 23, 2003 · N712AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200317604Floorbeam · corrodedABI - DURING AN IMBV INSPECTION, FOUND CORROSOIN ON THE EXISTING REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED EXISTING REPAIR. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND INSTALLED. REPAIR DONE IAW EMB 145, SRM 145/1142 REV 22, 53-21-10 PARA 2 Jun 21, 2003 · N712AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200317404Relay · inoperativeDURING CLIMB CREW REPORTED AN ELECTRICAL EMERGENCY ABNORMAL EICAS MESSAGE ABOUT 1 SECOND AFTER TURNING APU OFF AS PER CLIMB-OUT PROCEDURE. AIRCRAFT WAS RETURNED TO FIELD. THE CREW RESTARTED THE APU AND REESTABLISHED ELECTRICAL POWER TO THE AIRCRAFT. MAINTENJun 19, 2003 · N731BE · Emb EMB135LR · DC Power Distribution SystemSDR SIMA200317401Sill · corrodedABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING CENTER SILL, INSTALLED NEW CENTER SILL IAW EMB REPAIR STATEMENT IC2003-145/0818 AND STANDARD SRM, SRM 145/1142 REV 22 PRACTICES. (M)Jun 18, 2003 · N712AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL113Inverter · inoperativeCLE FLIGHT NR 2153, THE CREW REPORTED THE EXIT SIGN OVER THE SERVICE DOOR NOT ILLUMINATING. MAINTENANCE INSPECTED AND REPLACED THE NR 2 INVERTER AND EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. EXIT SIGN P/N 7444-1.Jun 18, 2003 · N16525 · Emb EMB135LR · Emergency LightingSDR SIMA200316903Sill · corrodedDURING AN IMBV INSPECTION, THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS BETWEEN FRAMES 65-67. REMOVED EXISTING SILL. CLEANED AND TREATED THE AREA. INSTALLED NEW SILL IAW EMB SRM, SRM EMB 145/1142 REV 22, CHAPTERS 51-40-02 AND 51-20-03. (M)Jun 14, 2003 · N710TB · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03CL111Bulb · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT IN THE CEILING AT ROW 2 WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB AT ROW 2. OPERATIONAL CHECKS WERE GOOD.Jun 14, 2003 · N14522 · Emb EMB135LR · Emergency LightingSDR C2XA03IA063Connector · looseIAH- DURING PREFLIGHT THE CREW NOTED THAT THE EXIT SIGN ABOVE SEAT 1A OVERHEAD DOES NOT ILLUMINATE. IAH- MAINTENANCE RESECURED THE FEMALE CONNECTOR, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVEDJun 12, 2003 · N28529 · Emb EMB135LR · Light System WiringSDR C2XA03CL107Connector · looseCLE FLIGHT 2026 THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR ON THE EMERGENCY LIGHT NR 2 INVERTER. OPERATIONAL CHECKS WERE GOOD.Jun 9, 2003 · N16525 · Emb EMB135LR · Emergency LightingSDR C2XA03IA060Proximity Switch · malfunctionedAFTER TAKEOFF THE CREW NOTED THAT THE LANDING GEAR AURAL WARNING WAS SOUNDING AFTER GEAR RETRACTION. THE CREW RETURNED THE AIRCRAFT TO CLL, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE PROX SWITCHES AND RERACKED THE AWU. THE AIRJun 6, 2003 · N28529 · Emb EMB135LR · Landing Gear Position and WarningSDR SIMA200316001Module · inoperativeDURING FLIGHT CREW RECEIVED AN E2 FIRE WARNING. ENGINE WAS SHUTDOWN AND LIGHT EXTINGUISHED. AIRCRAFT WAS DIVERTED TO ALB. AFTER LANDING CREW RECEIVED ANOTHER FIRE WARNING. FIRE BOTTLE WAS FIRED AND AN EMERGENCY EVACUATIO AS DONE ON THE TAXIWAY. MAINTEANCEJun 5, 2003 · N738NR · Emb EMB135LR · Fire DetectionSDR SIMA200313205Circuit Board · inoperativeDURING CRUISE FLIGHT, THE CREW REPORTED THE OVERHEAD LIGHT AT 12C FLASHING OFF AND ON WITH A BURNING ELECTRICAL ODOR. MAINTENANCE REMOVED AND REPLACED DIODE BOARD FOR THE PASSENGER SERVICE UNIT AT SEAT 12C IAW CMM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNEMay 9, 2003 · N717AE · Emb EMB135LR · Passenger Compartment EquipmentSDR SIMA200313201Uplock Switch · inoperativeBGR - FLT 4626 - CREW REPORTED THE NOSE LANDING GEAR DOOR OPENED UNCOMMANDED DURING DESCENT. AIRCRAFT LANDED WITH NO FURTHER INCIDENT REPORTED. MAINTENANCE FOUND AN INOPERATIVE UPLOCK PROXIMITY SWITCH. THE UPLOCK SWITCH WAS REMOVED AND REPLACED IAW EMB MM. May 7, 2003 · N713AE · Emb EMB135LR · Landing Gear Position and WarningSDR C2XA03SH127Floorbeam · corrodedSHV DURING C CHECK THE LEFT HAND FLOORBEAM WAS FOUND TO HAVE CORROSION UNDER COMPOSITE CROSSBEAM AT FRAME 20. MAITENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR TO AFFECTED BEAM IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APRROVED TO RETURN TO SERVICE.May 5, 2003 · N16525 · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200312602Carbon Seal · leakingCREW REPORTED FOUL ODOR IN COCKPIT IN CABIN DURING FLIGHT. MAINTENANCE FOUND THE LT ENGINE LEAKING OIL FROM SPINNER. THE ZERO CARBON SEAL WAS REPLACED IAW ENGINE MM. OPERATIONAL AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)May 3, 2003 · N723AE · Emb EMB135LR · Engine (Turbine/Turboprop)SDR C2XA03IA045Line · looseTHE CREW NOTED AN UNCONTROLABLE PRESSURE RISE ON TAKEOFF. THE CREW RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL. MAINTENANCE TIGHTENED A LINE ON THE PNEUMATIC OUTFLOW VALVE, PERFORMED A OPERATIONAL CHECK OF THE PRESMay 2, 2003 · N17521 · Emb EMB135LR · Pressure Regulator/Outflow ValveSDR C2XA03SH126Strap · corrodedSHV DURING C CHECK THE CENTER BUTTSRAP BETWEEN FRAMES 14 AND 19 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03SH125Beam · corrodedSHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED BEAM IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Main, StructureSDR C2XA03SH124Floorbeam · corrodedSHV - DURING C-CHECK RAMP ANGLE ON CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION ON AFT END AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED RAMP ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA03SH123Bracket · corrodedSHV DURING C CHECK CORROSION WAS FOUND UNDER THE MAIN DOOR'S THRESHOLD BETWEEN FRAMES 15 AND 18. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED THRESHOLD SUPPORT ANGLES IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA03SH122Butt Strap · corrodedSHV- DURING C-CHECK LEFT HAND BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 16 AND 17. MAINTENANCE REMOVED DAMAGE AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Main, StructureSDR C2XA03SH121Bracket · gougedSHV - DURING C-CHECK SUPPORT BRACKET AFT OF PAX DOOR SECOND FROM THE TOP WAS FOUND GOUGED BY FRAME 18. MAINTENANCE REMOVED AND REPLACED AFFECTED BRACKET IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.May 2, 2003 · N16525 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200312702Floorbeam · corrodedDURING AN IMBV INSPECTION, THE LEFT SECTION OF THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 6 INCHES BY 3.5 INCHES SECTION OF THE LEFT SECTION OF THE FORWARD FLOORBEAM BY CUTOUT. FABRICATED A REPLACEMENT FORWARD FLOORBEAM Apr 30, 2003 · N709GB · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200312601Lever · inoperativeDURING APPROACH CREW REPORTED THE FLAPS FAILED. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TApr 30, 2003 · N711PH · Emb EMB135LR · Trailing Edge Flap Control SystemSDR SIMA200312701Floorbeam · corrodedABI - DURING AN MBV INSPECTION, THE CENTER SECTION OF THE FORWARD FLOORBEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.375 INCH BY 21.5 INCH SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD FLOORBEAM CENTER SECTIOApr 29, 2003 · N709GB · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200311805Floorbeam · corrodedDURING AN IMBV INSPECTION, THE LT FLOORBEAM AT FRAME 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. CUT OUT THE DAMAGED SECTION ON THE LEFT FLOORBEAM. CLEANED, AND TREATED THE REPAIR AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EApr 23, 2003 · N708AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200312718Sill · corrodedTHIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB SRM 51-40-02. (M)Apr 22, 2003 · N709GB · Emb EMB135LR · Fuselage Miscellaneous Structure
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