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 SIMA200222106Skin · corrodedDURING INSPECTION, FOUND CORROSION ON LT OMEGA BEAM AT FRAME 20. CUT OUT CORRODED AREA AND FABRICATED DOUBLER ANGLE AND FILLER AND PLATE AND TWO SHIMS. REPAIR DONE IAW SRM PRACTICES.Aug 9, 2002 · N734EK · Emb EMB135LR · Fuselage Main, Plate/SkinSDR C2XA02TY121Engine · corrodedTYS, During a schedule inspection corrosion was found on the left engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, EC7220-01009, AE3007A-70-0Aug 7, 2002 · N24517 · Emb EMB135LR · Powerplant SystemSDR C2XA02TY120Engine · corrodedTYS, During a schedule inspection corrosion was found on the right engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, Ec7220-01009, AE3007A-70-Aug 7, 2002 · N24517 · Emb EMB135LR · Powerplant SystemSDR SIMA200222108Floorboard · corrodedTHIS IS A LEVEL TWO FINDING ON CRIC NR 23858. GALLEY AREA FLOORBOARD EXTENSIONS HAVE CORROSION. GALLEY AREA FLOORBOARD EXTENSIONS HAVE CORROSION. REMOVED AND INSTALLED EXTENSION IAW SRM.Aug 5, 2002 · N734EK · Emb EMB135LR · Fuselage Floor PanelSDR SIMA200222107Sill · corrodedTHIS IS LEVEL TWO FINDING ON CRIC NR 23854. LEFT SILL IN GALLEY AREA HAS CORROSION. C/A: INSTALLED SERVICEABLE SILL IAW SRM.Aug 5, 2002 · N734EK · Emb EMB135LR · Standard Practices/StructuresSDR C2XA02CL162Receptacle · burnedSLP - FLIGHT 4153, THE CREW REPORTED A STRONG SMELL OF BURNING RUBBER FROM THE NR 2 COFFEE JUG. THE AIRCRAFT WAS RELEASED IAW 25-60-02/3D. MAINTENANCE REPLACED THE COFFEE POT RECEPTACLE IN THE GALLEY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASEAug 4, 2002 · N15527 · Emb EMB135LR · Buffet/GalleysSDR SIMA200222105Skin · damagedDURING INSPECTION FOUND DAMAGE ON THE LOWER LT ELEVATOR SKIN. PERFORMED TWO CUSTS TO REMOVE DAMAGE. FABRICATED A REPAIR DOUBLER. REPAIR DONE IAW STATEMENT AND SRM PRACTICES.Aug 2, 2002 · N733KR · Emb EMB135LR · Elevator, Plate/SkinSDR C2XA02CL157Control Unit · inoperativeCLE - THE CREW REPORTED A PITCH TRIM 1 INOP MESSAGE DURING CLIMBOUT. BOTH TRIM SWITCHES ON YOKE WERE INOPERATIVE. THE BACKUP TRIM WAS OPERATIONAL. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HSCU. OPERATIONAL CHECAug 2, 2002 · N27523 · Emb EMB135LR · Stabilizer Position IndicatingSDR C2XA02TY119Skin · gougedTYS - DURING A SCHEDULED 1-C INSPECTION, THE CENTER WING BOX OF THE HORIZONTAL STAB HAS SOME SCRATCHES AND GOUGES. MAINTENANCE BLENDED DAMAGE, PERFORMED DYE-PENETRANT INSPECTION. WILL BE RELEASED UPON COMPLETION OF ALL WORK.Aug 2, 2002 · N24517 · Emb EMB135LR · Horizontal Stabilizer, Plate/SkinSDR C2XA02TY118Frame · chafedTYS DURING A SCHEDULED 1-C INSPECTION, A CHAFE MARK WAS FOUND ON FRAME 70 NEXT TO THE BLEED AIR DUCT. BLENDED OUT THE AREA, PERFORM A DYE INSPECTION, ALODINED AND PAINTED. NO DEFECTS WERE FOUND AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Aug 2, 2002 · N24517 · Emb EMB135LR · Fuselage Main, FrameSDR C2XA02TY116Gusset · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE AFT GUSSET IN THE GALLEY WAS FOUND CORRODED. MAINTENANCE R/R THE AFT GUSSET IAW 135/145 SRM 51-40-02.R/R SCREWS IAW EMB 135/14553-01-06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK.Aug 1, 2002 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY115Floorbeam · corrodedTYS, DURING A SCHEDULED INSPECTION THE FORWARD DIGITAL WAS FOUND CORRODED FROM FRAME 13 TO 16. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED DOUBLER, SHIM AND INSTALLED, ALODINED, PRIMED AND PAINTED IAW-EMB-135/145-SRM-53-21-10 AND 51-40-02. THE REPAIR WAS SAAug 1, 2002 · N24517 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY114Skin · dentedTYS, DURING A SCHEDULED INSPECTION THE LEFT, NR 2 LEADING EDGE WAS FOUND DENTED AROUND A SCREW HOLE ON THE LOWER CENTER SIDE. MAINTENANCE REPAIRED THE DENT IAW-EMB-GST2378/02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THAug 1, 2002 · N24517 · Emb EMB135LR · Leading Edge DevicesSDR SIMA200222104Beam · corrodedABI - DURING INSPECTION, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER, TWO SHIMS AND A PLATE. REPAIR DONE IAW EMB 145, SRM 145/1142, CHAPTER 53, REV 18, 53-21-10 PARA 2, FIG 201 SHEETJul 29, 2002 · N733KR · Emb EMB135LR · Fuselage Main, StructureSDR SIMA200219701Sign · inoperativeBOS - FLT 4642 - CREW REPORTED THE EMERGENCY EXIT SIGNS BY THE PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THR NR 2 BATTERY PACK IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT RETURNED TO SERVICE. (M)Jul 16, 2002 · N716AE · Emb EMB135LR · Emergency LightingSDR C2XA02CL146Wire Harness · faultyCLE FLIGHT 3462 THE CREW REPORTED A ELECTRICAL SMELL COMING FROM SIDE WALL PANEL AT ROW 4A. MAINTENANCE INSPECTED AND FOUND A MELTED PLASTIC CONNECTOR FOR THE CABIN LIGHT BULB. THE AIRCRAFT WAS RELEASED FOR SERVICE. REPLACED SIDEWALL LIGHTING HARNESS ASSEMBJul 10, 2002 · N29515 · Emb EMB135LR · Light System WiringSDR C2XA02BT031Harness · faultyDSM/EWR---CO3463, CREW REPORTED "BURNING SMELL COMING FROM SIDEWALL PANEL IN ROW 4 SEAT A....MAINTENANCE IN DSM RELEASED AIRCRAFT IAW MEL #33-20-00 CATEGORY "C" PLACARD #023338 AIRCRAFT RETURNED TO SERVICE. CO 4362, EWR MAINTENANCE CLEARED PLACARD BY REMOVINJul 10, 2002 · N29515 · Emb EMB135LR · Passenger Compartment LightingSDR C2XA02TY107Skin · dentedTYS, DURING A SCHEDULED INSPECTION A DENT WAS FOUND IN THE SKIN BETWEEN FRAMES 25 AND 26, STRINGERS 12R AND 13R. MAINTENANCE REFORMED THE DENT, PERFORMED DYE PENETRANT INSPECTION, ALODINED AND PRIMED IAW-EMB-GST-2071/02. THE REPAIR WAS SATISFACTORY AND THE AJul 2, 2002 · N28518 · Emb EMB135LR · Fuselage Main, Plate/SkinSDR C2XA02CL136Fire Loop · chafedDTW FLIGHT 3318 THE CREW REPORTED A NR 2 FIRE DETECT FAIL MESSAGE ON TAKEOFF. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE LOOP DETECTOR AND CLEANED THE NR 2 ENGINE FIRE BOTTLE CANNON PLUGJun 27, 2002 · N15527 · Emb EMB135LR · Fire DetectionSDR SIMA200217303Light · not seatedFLOOR EMERGENCY LIGHT ROW 5 INOPERATIVE. C/A SEATED FLOOR EMERGENCY STRIP IN ROW 5 OPS CHECKED GOOD.Jun 22, 2002 · N717AE · Emb EMB135LR · Emergency LightingSDR SIMA200217322Frame · bentAPU COWLING INTERIOR FORWARD FRAME IS BENT ABOVE THE TOP LEFT MOUNT HOLE, RECONTOURED FORWARD FRAME, PERFORMED NDT, NO DEFECTS. DONE IAW SRM AND MFG GST.Jun 21, 2002 · N732DH · Emb EMB135LR · APU Cowling/ContainmentSDR SIMA200217316Skin · gougedTHREE GOUGES BETWEEN FRAMES 15-16, BETWEEN STRINGERS 16L AND 17L. (SUP) BLENDED GOUGES, PERFORMED NDT WITH NO DEFECTS. GOUGES ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200217317Skin · gougedGOUGE IN FUSELAGE SKIN BETWEEN FRAMES 71 AND 72 AND STRINGERS 16R AND 17R. BLENDED GOUGE, PERFORMED NDT WITH NO DEFECTS. GOUGE ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200217318Skin · gougedGOUGE ON FORWARD EDGE OF MAIN DOOR SKIN. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. GOUGED ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Passenger/Crew DoorsSDR SIMA200217319Structure · gougedGOUGE BETWEEN JUNCTION 1 AND FRAME 14, ALONG STRINGER 15L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200217320Structure · gougedGOUGE BETWEEN FRAMES 16-17 BETWEEN STRINGERS 16L AND 17L. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200217321Skin · gougedLEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.Jun 19, 2002 · N732DH · Emb EMB135LR · Wing, Plate/SkinSDR C2XA02CL133Autopilot Sys · malfunctionedCLE FLIGHT 4015 THE CREW REPORTED A AUTO PILOT FAIL MESSAGE AFTER FLIGHT INTO MODERATE TURBULENCE ASSOCIATED WITH BURNING SMELL IN THE COCKPIT AND CABIN. MAINTENANCE INSPECTED AND PERFORMED AUTO PILOT CHECKS AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASJun 16, 2002 · N14514 · Emb EMB135LR · Autopilot SystemSDR C2XA02IA129Odor · detectedCLE- FLIGHT 4138, AFTER LANDING THE CREW NOTED THAT THERE WAS A FUEL SMELL IN THE COCKPIT. MAINTENANCE PERFORMED AN AIR BLEED SYSTEM OPERATIONAL CHECK, NO DEFECTS NOTED, COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jun 14, 2002 · N16525 · Emb EMB135LR · Air Distribution SystemSDR SIMA200216406Structure · chafedFORWARD FLOOR EXTENSION IS CHAFED AT FRAME 22. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS. BLENDED OUT CHAFE, WITHIN MFG SRM LIMITS.Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200216404Longeron · dentedRIGHT UPPER COWLING LOWER INBOARD LONGERON DENTED. C/A FABRICATED AND INSTALLED. A DOUBLER, REPAIR DONE IAW SRM.Jun 11, 2002 · N731BE · Emb EMB135LR · Engine Cowling SystemSDR SIMA200216408Longeron · dentedLEFT UPPER COWLING LOWER INBOARD LONGERON DENTED. RECONTOURED LONGERON, PERFORMED EDDY CURRENT, NO DEFECTS. ACCEPTED AS IS IAW. TREATED FOR CORROSION.Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)SDR SIMA200216407Gusset · gougedCENTER GUSSET GOUGED FROM FRAMES 20 T0 22. C/A REMOVED GOUGED BY BLENDING, WITHIN SRM LIMITS. RESTORED SURFACE PROTECTION.Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)SDR SIMA200216405Extinguisher · chafedAFT FLOOR EXTENTION IS CHAFED FROM FRAMES 22-23. C/A PERFORMED EDDY CURRENT INSPECTION. NO DEFECTS. BLENDED CHAFE IAW SRM LIMITS.Jun 11, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)SDR SIMA200216409Bracket · gougedAPU FIREWALL GOUGED BY APU BLEED AIR VALUE BRACKET. PERFORMED EDDY CURRENT, NO DEFECTS. REPAIR DONE ON GOUGE IAW SRM.Jun 10, 2002 · N731BE · Emb EMB135LR · Fuselage Structure (General)SDR C2XA02CL124Valve · leakingCLE FLIGHT#2980 THE CREW REPORTED A SLIGHT VIBRATION AND SAID IT SOUNDED LIKE THE NOSE GEAR DOORS WERE NOT FULLY CLOSING.MAINTENANCE REPLACED THE NOSE GEAR SOLENOID VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Jun 4, 2002 · N12528 · Emb EMB135LR · Landing Gear Door Retract SectionSDR SIMA200215118Frame · misdrilledDURING AN MBV INSPECTION, FOUND DAMAGE TO STRINGER 16L FORWARD OF FRAME 20, AT JOINT DRILL MARKS AND OVERSIZE HOLE. REMOVED DRILL MARKS BY BLENDING. REAMED HOLES, INSTALLED NEW FASTENERS IAW STANDARD SRM PRACTICES.May 29, 2002 · N726AE · Emb EMB135LR · Fuselage Structure (General)SDR SIMA200215101Skin · dentedDURING AN MBV INSPECTION, FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGER 15 AND 17L, RIVETS IMPROPERLY INSTALLED. REMOVED PREVIOUS REPAIR DOUBLER, INSTALLED IAW STANDARD SRM PRACTICES.May 23, 2002 · N726AE · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200215117Skin · damagedDURING AN MBV INSPECTION FOUND PREVIOUS REPAIR BETWEEN FRAMES 19 AND 20, AND STRINGERS 15 AND 17L, RIVETS IMPROPERLY INSTALLED. REMOVED C PREV. REPAIR FAB A REPAIR DOUBLER, REPAIR DONE IAW STANDARD SRM PRACTICES.May 23, 2002 · N726AE · Emb EMB135LR · Fuselage Main, Plate/SkinSDR SIMA200213811Floorbeam · corrodedDURING AN MBV MAINTENANCE FOUND CORROSION ON LEFT HAND OMEGA BEAM AT FRAME 20 REMOVED CORROSION BY CUT OUT. FABRICATED A DOUBLER ANGLE, FILLERS AND SHIMS. REPAIR DONE, IAW MFG SRM.May 15, 2002 · N727AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02CL117Receptacle · burnedCLE FLIGHT 3178 THE CREW REPORTED BURNING SMELL FROM THE HOT JUG IN THE GALLEY. MAINTENANCE INSPECTED AND REPLACED THE HOT JUG RECEPTACLE. OPERATIONAL CHECKS WERE GOOD.May 15, 2002 · N17524 · Emb EMB135LR · Buffet/GalleysSDR C2XA02CL115Acm · inoperativeIAH FLIGHT # 3958 CREW REPORTED SMOKE IN CABIN WITH #1 PACK RUNNING. MAINTENANCE REPLACED #1 PACK ACM OPERATIONAL CHECK GOOD.May 14, 2002 · N17513 · Emb EMB135LR · Cabin Cooling SystemSDR C2XA02CL114Fan · inoperativeEWR FLIGHT 3406 CREW REPORTED BURNING SMELL COMING FROM PACK #1.NO SMOKE FOUND WHEN PACK #1 WAS DESELECTED SMELL WENT AWAYMAINTENANCE REPLACED #1 PACK RECIRCULATION FAN. OPERATIONAL CHECKS WERE GOOD.AIRCRAFT RETURNED TO SERVICE.May 11, 2002 · N12519 · Emb EMB135LR · Air Distribution FanSDR SIMA200213011Floorbeam · corrodedABI - DURING INSPECTION, FOUND FORWARD DIGITAL CORRODED AT RIVETS AND NUTPLATE BETWEEN FRAME 16 AND 18. REMOVED CORROSION BY CUT OUT. REPAIRED IAW EMB 145, SRM 145/1142, CHAPTER 53 REV 17 53-21-10, AND STANDARD SRM PRACTICES. (M) (M)May 7, 2002 · N728AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200213002Battery Pack · dischargedBOS - FLT 4527 - AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED NR 4 BATTERY PACK IAW WC NR 33-700-15. OPS CHECK GOOD. (M)May 5, 2002 · N714BZ · Emb EMB135LR · Emergency LightingSDR SIMA200214821Floor Support · corrodedABI - THIS IS A LEVEL 2 FINDING. CENTER BEAM GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED NEW CENTER BEAM IAW EMB 135 SRM 51-40-02. (M)May 2, 2002 · N728AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200214820Crossbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. FLOOR EXTENSION CROSSMEMBER CORRODED AT FRAME 22. REMOVED AND REPLACED CROSSMEMBER IAW EMB 135 SRM 51-40-02. (M)May 2, 2002 · N728AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200214819Floorbeam · corrodedABI - THIS IS A LEVEL 2 FINDING. LEFT OMEGA BEAM CORRODED AT FRAME 20. BLENDED AND TREATED CORROSION IAW EMB GST-1472/02. (M)May 2, 2002 · N728AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200214818Support · corrodedABI - THIS IS A LEVEL 2 FINDING. RAMP SUPPORT CORRODED AT FRAME 20. INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02. (M)May 2, 2002 · N728AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200214817Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. FORWARD DIAMOND GUSSET CORRODED AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE GUSSET IAW EMB 135 SRM 51-40-02. (M)May 2, 2002 · N728AE · Emb EMB135LR · Fuselage Miscellaneous Structure
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