Embraer EMB-135ER

Service difficulty reports · 465

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Query with SQL
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 = 'EMB135ER'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR C2XA01TY177Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED NEW ANGLE, SHIM, FILLER AND PLATE. INSTALLED REPAIRED PARTS AND FLOORBEAM IAW EMB-135/145-SRM-53-21-10 & 53-40-02Nov 11, 2001 · N15509 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY176Antenna · corrodedTYS During a scheduled inspection the lower TCAS antenna was found corroded. Maintenance removed and replaced the TCAS antenna I.A.W.-EMB-135-AMM-34-43-03, operational checks were satisfactory. Aircraft released for service.Nov 11, 2001 · N15509 · Emb EMB135ER · Air Collision Avoidance SystemSDR C2XA01TY175Rod End · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE LEFT FUSELAGE TO SPAR 3 ROD END ASSEMBLY HAD CORRODED ON THE LOWER ROD END. MAINTENANCE REMOVED AND REPLACED THE LEFT ROD ASSEMBLY IAW GST-3655A-01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPONov 11, 2001 · N15509 · Emb EMB135ER · Wing Miscellaneous StructureSDR C2XA01TY174Rod End · corrodedTYS DURING A 1-C INSPECTION THE RIGHT FUSELAGE TO SPAR 3 ROD ASSEMBLY HAD CORROSION ON THE LOWER ROD ENDS. MAINTENANCE REMOVED AND REPLACED RIGHT ROD ASSEMBLIES IAW EMB GST-3655A/01 WHICH WAS ACCOMPLISHED. THE AIRCRAFT WILL BE RELEASED TO SERVICE UPON COMPLENov 11, 2001 · N15509 · Emb EMB135ER · Wing Miscellaneous StructureSDR C2XA01TY173Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE AFT GUSSET AT FRAME 18. MAINTENANCE REMOVED AND REPLACED AFT GUSSET AT FRAME 18 IAW EMB-135 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Nov 9, 2001 · N15509 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XAS01TY172Angle · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE CENTER OMEGA BEAM RAMP ANGLE AT FRAME 17. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM 51-20-03, 51-40-02 AND 51-20-01. THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WINov 8, 2001 · N15509 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01CL221Receptacle · burnedCLE FLIGHT NR 3898 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEE WARMERS WHEN EVER THEY WERE ON.MAINTENANCE INSPECTED AND REPLACED THE RECEPTACLE PLUG FOR THE WARMER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 30, 2001 · N14505 · Emb EMB135ER · Buffet/GalleysSDR C2XA01TY171Skin · chafedTYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED MOct 29, 2001 · N16510 · Emb EMB135ER · Cargo/Baggage DoorsSDR C2XA01TYSkin · chafedTYS DURING A SCHEDULED 1C INSPECTION,THE CARGO DOOR SKIN WAS FOUND CHAFED AROUND THE HANDLE CUTOUT. MAINTENANCE BLENDED OUT THE AREA IAW EC5230-01068--5120-04--5120-05 AND 5120-06. ALL WORK WAS ACCOMPLISH AND WILL BE RELEASED UPON COMPLETION OF THE SCHEDULED MOct 29, 2001 · N16510 · Emb EMB135ER · Cargo/Baggage DoorsSDR C2XA01TY170Firewall · damagedTYS DURING A SCHEDULE 1-C INSPECTION,MAINTENANCE FOUND A HOLE RUBBED INTO THE FIREWALL BLANKET. MAINTENANCE USED EC5330-01166 FOR THE REPAIR. ALL WORK WAS DONE IAW THE EC AND AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULE MAINTENANCE.Oct 29, 2001 · N16510 · Emb EMB135ER · Fuselage Main, BulkheadSDR C2XA01TY169Floor Support · brokenTYS DURING A SCHEDULED INSPECTION A FAIRLEAD FLOOR SUPPORT AT THE CENTER OMEGA BEAM WAS FOUND BROKEN AT FR21. MAINTENANCE R/R THE FAIRLEAD FLOOR SUPPORT AND THE WORK WAS FOUND SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF ALL SCHEDULED MAINOct 29, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY168Switch · inoperativeTYS During a scheduled inspection, When doing inspection task card # 35-20-00-720-001-A00, the cabin oxygen masks did not deploy in auto mode. Maintenance removed and replaced the altitude sensing switch. I.A.W.-EMB-135-AMM-51-40-02. operational checked good.Oct 28, 2001 · N16510 · Emb EMB135ER · Oxygen SystemSDR C2XA01TY167Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION, SEVERAL AREAS OF CORROSION WAS FOUND ON THE CENTER FLOORBEAM GUSSET BETWEEN FRAMES 18-22. MAINTENANCE REMOVED AND REPLACED GUSSET TOP CAP. IAW-EMB-135/145-SRM-51-40-02. REPAIR PROCEDURES WERE SATISFACTORY, AIRCRAFT WILL BEOct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY166Gusset · corrodedTYS During a scheduled inspection, corrosion was found on the floor gussets at the entrance to the cockpit, between frames 15 and 18. Maintenance removed and replaced gusset and center section of forward digital plate (fabricated doubler, shims and cockpit stOct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY165Seal · corrodedTYS During a scheduled inspection, corrosion was found on the right floor seal at frame 18. Maintenance removed surface corrosion, alodined, primed and painted. I.A.W.-EMB135/145-CMP-51-21-04,05 and 06. Repair procedure was satisfactory and the aircraft will Oct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Floor PanelSDR C2XA01TY164Antenna · corrodedTYS During a scheduled inspection the lower TCAS antenna was found with corrosion on the base. Maintenance removed and replaced the antenna, operational checked good. I.A.W.-EMB-AMM-34-43-03. Repair procedure was satisfactory and the aircraft will be releasedOct 28, 2001 · N16510 · Emb EMB135ER · Air Collision Avoidance SystemSDR C2XA01TY163Floor Support · corrodedTYS Several areas of corrosion were found on the aft side of service door aft of frame 22.Maintenance removed floor support and replaced it with a new part IAW emb135/145 SRM 51-40-02 and 51-10-02-Work was satisfactory and aircraft will be released upon compleOct 28, 2001 · N16510 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY162Bushing · backed outTYS DURING A SCHEDULED INSPECTION THE PAX-DOOR HOLD OPEN PIN LOWER BUSHING WAS FOUND TO BE MIGRATING OUT. MAINTENANCE INSTALLED BUSHING FROM THE BOTTOM IN REFERENCE TO GST-1662/01. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED ON COMPLETION OF AIRCRAFT MAINOct 28, 2001 · N16510 · Emb EMB135ER · Passenger/Crew DoorsSDR C2XA01TY160Bulb · burned outTYS During a scheduled inspection the overhead emergency light on right side was found out. Maintenance removed and replaced the bulb, operational checks good I.A.W.-EMB-135-AMM-33-50-07, Aircraft released for service.Oct 17, 2001 · N14508 · Emb EMB135ER · Emergency LightingSDR C2XA01CL215Smoke Detector · defectiveCLE FLIGHT#3300 THE CREW REPORTED THE LAV SMOKE DETECTOR WARNING ILLUMINATED.MAINTENANCE INSPECTED AND FOUND NO SMOKE.THEY REPLACED THE LAV SMOKE DETECTOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 15, 2001 · N17507 · Emb EMB135ER · Smoke DetectionSDR C2XA01CL214Odor · detectedCLE FLIGHT 3350 THE CREW REPORTED A BURNING SMELL FROM THE APU WHENEVER THE BLEED AIR WAS USED. MAINTENANCE INSPECTED AND FOUND NO DEFECTS OR SMELLS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 10, 2001 · N14505 · Emb EMB135ER · Air Distribution SystemSDR C2XA01CL213Light · inoperativeCLE FLIGHT NR 3683 THE CREW REPORTED THAT THE 2ND AND 3RD EMERGENCY LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 3RD LIGHT STRIP AND REPAIRED THE WIRING ON THE 2ND LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASEDOct 9, 2001 · N27506 · Emb EMB135ER · Emergency LightingSDR C2XA01CL211Transponder · failedCLE FLIGHT NR 3899 CREW REPORTED THAT THE NUMBER 1 TRANSPONDER NO MODE "C". NUMBER 2 TRANSPONDER ALREADY ON MEL. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND REMOVED AND REPLACED THE NUMBER 1 TRANSPONDER. SYSTEM OPERATIONAL CHECKSOct 3, 2001 · N15509 · Emb EMB135ER · ATC Transponder SystemSDR C2XA01CL204Oil Cap · out of positionCLE FLIGHT 3864 THE CREW REPORTED A LAV SMOKE WARNING INDICATION ON TAXI OUT WITH A SMELL OF SMOKE IN LAV. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE APU OIL SERVICE CAP WAS OFF AND OIL LEAKING OUT OF RESESep 17, 2001 · N16511 · Emb EMB135ER · APU Oil SystemSDR C2XA01IA343Smoke · detectedCLL - FLIGHT 4134 THE CREW REPORTED A LAV SMOKE WARNING AND AND VISIBLE SMOKE PRESENT ON APPROACH TO IAH. THE AIRCRAFT WAS DIVERTED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, GROUND RAN BOTH PACKS FROM ENGINE BLEED AND APU BAug 25, 2001 · N14514 · Emb EMB135ER · Air Distribution SystemSDR C2XA01CL197Connector · burnedCLE FLIGHT 3692 THE CREW REPORTED A BURNING SMELL IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE GALLEY HOT JUG RECEPTACLE TO BE BURNT. THE RECEPTACLE CONNECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Aug 23, 2001 · N14508 · Emb EMB135ER · Buffet/GalleysSDR CWQ2001F00000Clamp · looseDURING ADDITIONAL ACCEPTANCE INSPECTION, IT WAS AGAIN NOTED THE AIRFRAME BLEED AIR CHECK VALVE V-BAND CLAMPS WERE NOT INSTALLED CORRECTLY IAW COMMON INDUSTRY PRACTICE OR AS RECOMMENDED BY THE CLAMP MANUFACTURE.Aug 6, 2001 · N926FM · Emb EMB135ER · Pneumatic Distribution SystemSDR 145450AClamp · looseDURING ACCEPTANCE INSPECTION IT WAS NOTED THAT THE V-BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICAL CHECK OF THE CLAMP.Jul 27, 2001 · N829RN · Emb EMB135ER · Pneumatic Distribution SystemSDR 145450Clamp · looseDURING ACCEPTANCE INSPECTION IT WAS NOTED THAT THE V-BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICAL CHECK OF THE CLAMP.Jul 27, 2001 · N948AL · Emb EMB135ER · Pneumatic Distribution SystemSDR 145450BClamp · looseDURING ACCEPTANCE INSPECTION, IT WAS NOTED THAT THE V BAND CLAMPS ON THE BLEED AIR CHECK VALVE WERE LOOSE DURING PHYSICAL CHECK OF THE CLAMP.Jul 27, 2001 · N486TM · Emb EMB135ER · Pneumatic Distribution SystemSDR C2XA01CL175Engine · failedCLE FLIGHT 3722 THE CREW REPORTED THE NR 1 ENGINE FAILED AT 2800 FT WITH NO ABNORMAL INDICATIONS PRIOR TO FAILURE. THE AIRCRAFT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD. THE AJul 25, 2001 · N14508 · Emb EMB135ER · Engine (Turbine/Turboprop)SDR C2XA01TY099Stringer · chafedTYS DURING A SCHEDULED INSPECTION, STRINGER 19L BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE CHAFED. MAINTENANCE ACCOMPLISHED THE BLEND OUT REPAIR IAW EMB GST 2412/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE.Jul 19, 2001 · N14508 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA01TY098Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE, LOCATED JUST AFT OF COCKPIT ENTRANCE WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE ACCOMPLISHED THE DOUBLER REPAIR IAW EMB GST 2405-01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FJul 19, 2001 · N14508 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY097Nose Cowl · dentedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND ENGINE INLET WAS FOUND DENTED ON THE LOWER EXTERNAL SURFACE. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST 2230/01, THE REPAIR WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICED.Jul 7, 2001 · N14505 · Emb EMB135ER · Engine Air Intake SystemSDR C2XA01CL136Relay · failedCLE FLT 3369 THE CREW REPORTED WARNING ANNUNCIATOR DOES NOT ILLUMINATE FOR BAGGAGE SMOKE DURING FIRE TEST. MAINTENANCE REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR TEST RELAY. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED TO SERVICE.Jun 6, 2001 · N12519 · Emb EMB135ER · Smoke DetectionSDR C2XA01CL126Valve · failedCLE FLT 3962 THE CREW REPORTED NR 1 ENGINE OIL PRESSURE WARNING CONTINUOUSLY IN FLIGHT, PRESSURE NORMAL. AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE OIL TANK PRESSURE VALVE. OPERATIONAL CHECKS WEJun 3, 2001 · N14505 · Emb EMB135ER · Engine Oil PressureSDR C2XA01CL111Unknown · odorCLE FLIGHT 3966 THE CREW REPORTED STRONG SMOKE ODOR INFLIGHT. ODOR WENT AWAY AFTER CREW TURNED OFF PACK NR 1. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER PROBLEM. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF NR1 BLEED SYSTEM NO DEFECTS WERE NOTED AND AMay 16, 2001 · N14505 · Emb EMB135ER · Air Distribution SystemSDR SIMA20011305Rudder Pedal · stiffBOS - FLT 4942 - DURING TAKEOFF ROLL, THE CREW NOTED THE RUDDER PEDALS WERE STIFF TO OPERATE. TAKEOFF WAS ABORTED AND AIRCRAFT WAS RETURNED TO THE GATE. NO FAILURES FOR THE RUDDER SYSTEM WERE REPORTED. JUST BEFORE AIRCRAFT RETURNED TO GATE THE YAW DAMPNER FMay 10, 2001 · N713AE · Emb EMB135ER · Rudder Control SystemSDR C2XA01TY092Stringer · gougedTYS DURING A SCHEDULED INSPECTION EXTERNAL STRINGER 19L WAS FOUND GOUGED AT STATION 15721.0. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB-GST-1459/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.May 5, 2001 · N19503 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA01CL090Light · inoperativeCLE FLIGHT 3863 THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS FROM SEAT 2A TO 6A WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 27, 2001 · N14505 · Emb EMB135ER · Emergency LightingSDR C2XA01TY090Bracket · chafedTYS DURING A SCHEDULED INSPECTION THE MAIN CABIN DOOR, HANDLE BRACKET WAS FOUND TO BE CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB-GST-1405/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 25, 2001 · N16502 · Emb EMB135ER · Passenger/Crew DoorsSDR C2XA01TY089Plate · corrodedTYS DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL PLATE JUST AFT OF FLIGHT DECK WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SLICE REPAIR IAW EMB-GST-1266/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIApr 25, 2001 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY088Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND OMEGA BEAM AFT OF FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EMB-135 SRM-53-21-10, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 24, 2001 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01CL089Receptacle · burnedYYZ FLIGHT 3898 THE CREW REPORTED A BURNING SMELL FROM THE LEFT COFFEE JUG. MAINTENANCE REPLACED THE LEFT COFFEE JUG RECEPTACLE CONNECTOR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Apr 24, 2001 · N14508 · Emb EMB135ER · Buffet/GalleysSDR C2XA01TY087Angle · corrodedTYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AFT RAMP ANGLE FORWARD OF FRAME 20 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-30-01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF Apr 23, 2001 · N16502 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA01TY086Mount · chafedTYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE PYLON FORWARD YOKE MOUNT WAS FOUND CHAFED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1365/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 23, 2001 · N16502 · Emb EMB135ER · Nacelle/Pylon, Attach FittingsSDR C2XA01TY085Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND OMEGA BEAM WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-GST-3120/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPApr 22, 2001 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR C2XA01TY084Fitting · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HORIZONTAL ACTUATOR SUPPORT FITTING WAS FOUND GOUGED. MAINTENANCE ACCOMPLISHED A BLEND REPAIR IAW EMB GST-1340/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 22, 2001 · N16502 · Emb EMB135ER · Stabilizer ActuatorSDR C2XA01TY083Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA RAMP ANGLE WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-135 SRM-51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.Apr 22, 2001 · N16502 · Emb EMB135ER · Fuselage Main, Floor BeamSDR SIMA20011171Floorbeam · corrodedABI - MAINTENANCE REPORTED THE LEFT OMEGA BEAM TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 23 AND 25. MAINTENANCE REPAIRED DAMAGE IAW EMB SRM AND REPAIR STATEMENT GST 1298/01. AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 21, 2001 · N700LE · Emb EMB135ER · Fuselage Main, Floor Beam
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