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 SIMA200207804Sill · corrodedTHIS IS LEVEL 2 ITEM. CORROSION ON SERVICE DOOR CENTER SILL. BLENDED AND RETREATED SERVICE DOOR CENTER SILL IAW EMB GST-0798/02 AND EMB 135 CPM 51-14-02 AND 51-21-06. (M)Mar 8, 2002 · N722AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200207210Gusset · corrodedABI - FOUND CORROSION ON RIGHT GALLEY FORWARD DIAMOND GUSSETT. REPLACED GUSSETT IAW EMB 135 SRM 51-40-02, 51-40-06. (M)Mar 8, 2002 · N722AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA02CL068Light · inoperativeCLE FLIGHT 3237 THE CREW REPORTED 1 SECTION OF EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY AISLE PATH LIGHTING SECTION. OPERATIONAL CHECKS WERE GOOD.Mar 8, 2002 · N29515 · Emb EMB135LR · Emergency LightingSDR C2XA02CL067Control Unit · intermittentCLE FLIGHT# 3242 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE UPON GEAR RETRACTION.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SEMar 7, 2002 · N12519 · Emb EMB135LR · Landing Gear SelectorSDR SIMA200207908Inverter · inoperativeFLT 4501 - BOS - CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 2, 2002 · N704PG · Emb EMB135LR · Emergency LightingSDR SIMA200206201Proximity Switch · failedRDU - FLT 4879 - RIGHT MAIN GEAR UNSAFE INDICATION ON APPROACH INTO RDU. CREW PERFORMED CHECKLIST. GEAR STILL SHOWING UNSAFE. LANDED WITHOUT INCIDENT HAD GEARS PINNED BEFORE EXITING RUNWAY. RAI CHANNEL A PROX SWITCHES ON RIGHT AND LEFT MLG IAW AMM 32-61-02Mar 2, 2002 · N700LE · Emb EMB135LR · Landing Gear Position and WarningSDR C2XA02CL060Outflow Valve · failedCLE FLIGHT#3146 THE CREW REPORTED A TOTAL LOSS OF PRESSURIZATION IN FLIGHT.THE AIRCRAFT DESENDED TO 10000 FT.AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND REPLACED THE ELECTOPNEUMATIC OUTFLOW VALVE.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS Feb 27, 2002 · N17513 · Emb EMB135LR · Pressure Regulator/Outflow ValveSDR C2XA02TY046Floorbeam · corrodedTYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND UNDER FLOOR SUPPORT CROSS MEMBER AT FR 20 ON THE LEFT OMEGA BEAM. MAINTENANCE CUT OUT DAMAGE AREA, FAB DOUBLER, SHIM AND EXTERNAL ANGLE. INSTALL THE REPAIR PIECES AND PROFILE ANGLE IAW 135/145 SRM 53Feb 27, 2002 · N14516 · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200208304Beam · corrodedABI - THIS IS LEVEL 2 FINDING. CORROSION FOUND ON GALLEY RIGHT BEAM. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0636/02. (M)Feb 25, 2002 · N720AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200208301Floorbeam · corrodedTHIS IS A LEVEL 2 FINDING. CORROSION GALLEY FORWARD DIGITAL. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0634/02. (M)Feb 25, 2002 · N720AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200208302Gusset · corrodedABI - THIS IS A LEVEL 2 FINDING. CORROSION GALLEY CENTER BEAM GUSSET. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0636/02. (M)Feb 25, 2002 · N720AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200205401Apu · failedEWR - FLT 4587 - DURING TAXI OUT, CREW NOTED SMOKE IN CABIN AFTER APU FAIL AND SHUT DOWN. CREW RETURNED TO GATE AND PASENGERS WERE DEPLANED NORMALLY. NO FURTHER INCIDENTS WERE REPORTED. MAINTENANCE WAS SENT FROM LGA. AIRCRAFT WAS INSPECTED AND APU WAS DEFEFeb 23, 2002 · N731BE · Emb EMB135LR · Airborne Auxiliary Power Unit (APU) SystemSDR C2XA02TY045Wire · brokenTYS, DURING A SCHEDULED 1C INSPECTION A BROKEN WIRE WAS FOUND ON EMERGENCY LIGHT STRIP ON PANEL 251DE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW-EMB-135-AMM-33-50-12, OPERATIONAL CHECKED GOOD, AIRCRAFT RELEASED TO SERVICE.Feb 22, 2002 · N29515 · Emb EMB135LR · Light System WiringSDR C2XA02TY044Skin · dentedTYS, DURING A SCHEDULED 1C INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF FR24, BELOW STR 10R. MAINTENANCE RE CONTOURED DENT, PERFORMED DYE-PENATRENT INSPECTION (NO CRACKS NOTED) IAW-EMB-GST-0504/2. REPAIR PROCEDURE WAS SATISFACTORY AND AIRCRAFT WIFeb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Plate/SkinSDR C2XA02TY043Plate · corrodedTYS, During a scheduled 1C inspection, corrosion was found on the forward digital plate aft of cockpit door. Maintenance removed the corrosion by cutting out the center section and installed a new section, fabricated and installed doubler and shims. I/A/W-EMB-Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA02TY042Beam · corrodedTYS, During a scheduled 1C inspection, corrosion was found on the left omega beam ar FR20 under the carbon fiber beam. Maintenance cut out the damage, fabricated an external angle, plate and filler I/A/W-EMB-135/145-SRM-53-21-10 and reinstalled the left ramp aFeb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY041Support · corrodedTYS, During a scheduled 1C inspection, corrosion was found on the center omega beam ramp support between FR19-20. Maintenance removed and replaced the ramp support. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircraft will be releasedFeb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA02TY040Angle · corrodedTYS, During a scheduled 1C inspection, corrosion was found on the support angle at main door entrance below the threshold strip. Maintenance removed and replaced the support angle. I/A/W-EMB-135/145-SRM-51-40-02. Repair procedure was satisfactory and aircraft Feb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA02TY039Floorbeam · corrodedTYS, DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON THE FORWARD DIGITAL PLATE AFT OF COCKPIT DOOR. MAINTENANCE REMOVED CORROSION BY CUTTING OUT THE CENTER SECTION AND INSTALLING A NEW SECTION, FABRICATED AND INSTALLED DOUBLERS AND SHIMS, ALODINED ANFeb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY038Beam · corrodedTYS, During a scheduled 1C inspection, corrosion was found on the forward center omega beam galley area. Maintenance removed corrosion and replaced affected rivits, alodined and primed. I/A/W-EMB-135/145-CPM-51-21-05 & 06. Repair procedure was satisfactory andFeb 21, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02CL056Wire · brokenCLE FLIGHT#3133 THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 9 WAS INOPERATIVE.MAINTENANCE INSPECTED AND REPAIRED A WIRE ON THE EMERGENCY AISLE PATH LIGHTING STRIP.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 20, 2002 · N14514 · Emb EMB135LR · Emergency LightingSDR C2XA02TY037Floorbeam · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE FORWARD DIGITAL PLATE AFT OF THE COCKPIT DOOR WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION BY CUTTING OUT THE CENTER SECTION OF THE DIGITAL PLATE AND FAB. A NEW PART WITH A DOUBLER AND SHIM, ALODINE, PRIME Feb 20, 2002 · N29515 · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02TY035Angle · corrodedTYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND ON THE SUPPORT ANGLE AT THE MAIN DOOR ENTRANCE BELOW THE THRESHOLD. MAINTENANCE REMOVED AND REPLACED THE SUPPORT ANGLES, ALODINE AND PAINTED IAW EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED ANFeb 20, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR C2XA02TY034Lever · gougedTYS DURING A SCHEDULED 1-C INSPECTION THE RT SERVO TAB DOG BONE WAS FOUND WEARING INTO THE ELEVATOR SUPPORT BRACKET WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.Feb 19, 2002 · N29515 · Emb EMB135LR · Elevator, Tab StructureSDR C2XA02TY033Lever · gougedTYS DURING A SCHEDULED 1-C INSPECTION THE LT SERVO TAB DOG BONE WAS FOUND WEARING AGAINST THE ELEVATOR SUPPORT BRACKET, WHICH REQUIRED A GST. ALL WORK WAS ACCOMPLISHED IAW GST-0522/02 AND WILL BE RELEASED UPON COMPLETION OF THE INSPECTION.Feb 19, 2002 · N29515 · Emb EMB135LR · Elevator, Tab StructureSDR C2XA02TY032Wire · brokenTYS DURING A SCHEDULED 1-C INSPECTION A BROKEN WIRE WAS FOUND ON THE PROXIMITY LIGHT STRIP ON PANEL 251DF. MAINTENANCE REMOVED AND REPLACED THE LIGHT STRIP IAW EMB 135/145 AMM 33-50-12. OPS CHECK GOOD AND WILL BE RELEASED UPON COMPLETION OF INSPECTION.Feb 18, 2002 · N29515 · Emb EMB135LR · Light System WiringSDR C2XA02TY031Duct · corrodedTYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND BETWEEN THE OUTER BYPASS AND THE FAN CASE ON NR 2 ENGINE. MAINTENANCE CLEANED THE AFFECTED AREA, APPLIED A CHEMICAL COATING AND APPLIED CORROSION RESISTANT PAINT IAW EC7000-01001. WORK WAS ACCOMPLISHFeb 18, 2002 · N29515 · Emb EMB135LR · Turbine Engine Bypass SectionSDR C2XA02TY030Support · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE RAMP SUPPORT ON THE CENTER OMEGA BEAM BETWEEN FR'S 19 AND 20 HAS A AREA OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RAMP SUPPORT IAW EMB 135/145 SRM 51-40-02. WORK WAS SATISFACTORY AND WILL BE RELEASED UPON COFeb 18, 2002 · N29515 · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200206509Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20 WHICH EXCEEDED SRM LIMITS. FABRICATED DOUBLER ANGLE, A FILLER, AND PLATE. WORK DONE IAW EMB 145 SRM 145/1142 CHAPTER 53 REV 17 53-21-10 PARA 2 AND STANDARD SRM Feb 14, 2002 · N718AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200206508Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON FORWARD DIGITAL STATION 163 AND BL 0.0 THAT WAS BEYOND SRM LIMITS. FABRICATED REPAIR DOUBLER, WORK DONE IAW EMB GST-0508/02, EMB145 SRM 145/1142, REV 17, STANDARD PRACTICES AND CPM 51-21-04, Feb 14, 2002 · N718AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR C2XA02CL047Receptacle · burnedCLE FLIGHT 3041 THE CREW REPORTED A BURNING SMELL COMING FROM THE COFFEE WARMERS. MAINTENANCE INSPECTED AND REPLACED THE NR 2 COFFEE WARMER RECEPTACLE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 12, 2002 · N28518 · Emb EMB135LR · Buffet/GalleysSDR C2XA02IA025Battery · dischargedIAH- DURING PREFLIGHT THE CREW NOTED THAT THE EMERGENCY LIGHTS FAILED TO OPERATE. IAH- MAINTENANCE REMOVED and REPLACEDTHE FORWARD BATTERY PACK, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPEROVEFeb 10, 2002 · N27523 · Emb EMB135LR · Emergency LightingSDR C2XA02CL044Check Valve · dirtyCLE THE CREW REPORTED ON APPROACH THE APU FAILED DURING START UP AND A FUEL SMELL WAS NOTED. ON THE GROUND THE APU DID START AND THE FUEL ODOR WAS PRESENT AGAIN. MAINTENANCE INSPECTED AND CLEANED THE APU COMBUSTER DRAIN CHECK VALVE. OPERATIONAL CHECKS WERE Feb 10, 2002 · N12519 · Emb EMB135LR · APU Engine Fuel and ControlSDR SIMA200208307Cap · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR BEARING CAP TO BE CORRODED. BEARING CAP WAS REMOVED AND REPLACED IAW EMB MM. (M)Feb 7, 2002 · N717AE · Emb EMB135LR · Main Landing GearSDR SIMA200208308Cap · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR BEARING CAP. MAINTENANCE REMOVED AND REPLACED THE BEARING CAP IAW EMB MM. (M)Feb 7, 2002 · N717AE · Emb EMB135LR · Main Landing GearSDR C2XA02CL036Light · inoperativeCLE MAINTENANCE FOUND THE FORWARD AISLE PATH EMERGENCY LIGHT WAS INOPERATIVE. THE FORWARD EMERGENCY LIGHT STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 4, 2002 · N17521 · Emb EMB135LR · Emergency LightingSDR SIMA20204209Floor Support · corrodedMBV - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE LEFT FLOOR SUPPORT IN CARGO BAY AT FRAME 71. MAINTENANCE REMOVED CORROSION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0331/02. (M)Jan 28, 2002 · N719AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200208306Sill · corrodedDURING MBV INSPECTION, MAINTENANCE FOUND LEVEL 2 CORROSION ON THE SERVICE DOOR FORWARD SILL. MAINTENANCE REMOVED AND REPLACED THE FORWARD SILL IAW EMB SRM 51-40-02. (M)Jan 26, 2002 · N719AE · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200204210Beam · corrodedABI - DURING MBV INSPECTION MAINTENANCE, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. MAINTENANCE REMOVED CORROSION AND RETREATED SURFACE IAW EMB REPAIR STATEMENT GST 0332/02. (M)Jan 26, 2002 · N719AE · Emb EMB135LR · Fuselage Main, StructureSDR C2XA02CL024Actuator · leakingCLE FLIGHT#4015 THE CREW REPORTED THE #1 HYDRAULIC SYSTEM INDICATED ZERO QUANTITY IN FLIGHT.THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE INSPECTED AND FOUND THE RIGHT WING SPOILER ACTUATOR LEAKING.THE ACTUATOR WAS REPLACEDJan 25, 2002 · N12519 · Emb EMB135LR · Drag Control ActuatorSDR C2XA02CL018Light · inoperativeCLE MAINTENANCE FOUND THE 2ND ROW OF EMERGENCY FLOOR PATH LIGHTING WAS INOPERATIVE DURING ROUTINE MAINTENANCE. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jan 23, 2002 · N24517 · Emb EMB135LR · Emergency LightingSDR SIMA200206507Floorbeam · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE LEFT OMEGA BEAM AT FRAME 20. FABRICATED A DOUBLER, FILLER, PLATE, AND TWO SHIMS. WORK DONE IAW EMB 145 SRM 145/1172 REV 16, 53-21-10 AND STANDARD SRM PRACTICES. (M)Jan 22, 2002 · N715AE · Emb EMB135LR · Fuselage Main, Floor BeamSDR SIMA200201801Power Supply · dischargedRDU - FLT 4612 - SEVERAL EMERGENCY INTERIOR LIGHTS ARE INOPERATIVE. REPLACED NR 2 BATTERY SUPPLY, OPS CHECK GOOD. (M)Jan 18, 2002 · N704PG · Emb EMB135LR · Emergency LightingSDR C2XA02BT001Smoke Detector · dirtyEWR---CO3443/MX, CREW REPORTED AFTER TAKEOFF FROM DAY, LAV SMOKE MASTER WARNING ON CLIMBOUT. AIRCRAFT RETURNED TO DAY. AIRCRAFT INSPECTED AND RELEASED IAW MEL. AIRCRAFT RETURNED TO SERVICE. UPON ARRIVAL IN NEWARK MAINTENANCE CLEANED SMOKE DETECTOR SENSOR IJan 14, 2002 · N14505 · Emb EMB135LR · Smoke DetectionSDR C2XA02TY012Light · inoperativeTYS DURING A SCHEDULED INSPECTION THE NR 3 AISLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 AISLE EMERGENCY LIGHT ASSEMBLE LIGHT BULB IAW EMB-135 MM 33-50-08, THE OPERATIONAL CHECK WERE SATISFACTORY. THE AIRCRAFT WAS RELEASEJan 11, 2002 · N17513 · Emb EMB135LR · Emergency LightingSDR SIMA200202309Cap · corrodedABI - DURING MBV INSPECTION, MAINTENANCE FOUND CORROSION ON THE NOSE LANDING GEAR BEARING CAPS. MAINTENANCE REPLACED THE NOSE LANDING CAPS IAW EMB135 MM 32-20-01-400-001-A. (M)Jan 4, 2002 · N714BZ · Emb EMB135LR · Nose/Tail Landing GearSDR SIMA200202308Cap · corrodedABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT MLG BEARING CAP TO BE CORRODED. MAINTENANCE REPLACED THE MAIN LANDING GEAR BEARING CAP IAW EMB MM 32-10-10-400-801A. (M)Jan 4, 2002 · N714BZ · Emb EMB135LR · Main Landing GearSDR C2XA02IA001Engine · leakingIAH- FLIGHT NUMBER 3792 THE CREW NOTED SMOKE IN THE CABIN AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, PERFORMED A OPERATIONAL AND LEAK CHECK. NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVJan 4, 2002 · N27523 · Emb EMB135LR · Engine (Turbine/Turboprop)SDR SIMA200202301Gusset · corrodedABI - DURING MBV INSPECTION MAINTENANCE FOUND, THE AFT DIAMOND GUSSET TO BE CORRODED AT FRAME 20. MAINTENANCE REPLACED THE GUSSET IAW EMB 135 SRM 51-40-02. (M)Jan 2, 2002 · N714BZ · Emb EMB135LR · Fuselage Miscellaneous StructureSDR SIMA200202302Gusset · corrodedABI - DURING MBV INSPECTION MAINTENANCE FOUND, THE FORWARD DIAMOND GUSSET TO BE CORRODED AT FRAME 20. MAINTENANCE REPLACED THE GUSSET IAW EMB 135 SRM 51-40-02. (M)Jan 2, 2002 · N714BZ · Emb EMB135LR · Fuselage Miscellaneous Structure
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