Embraer EMB-145

Service difficulty reports · 3,003

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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 = 'EMB145'
  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 CHQ000131Duct · leakingBLEED LEAK IN CARGO BIN, FIRE BOTTLES DISCHARGED, AND OVERWEIGHT LANDING.Mar 7, 2002 · N274 · Emb EMB145 · Pneumatic Distribution SystemSDR SIMA200207201Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED. BLENDED CHAFE, FABRICATED TWO DOUBLERS ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH THICK, AND FOUR SHIMS 4.5 INCH BY .75 INCH .080 INCH THICK IAW EMB 145 SRM 145/1142 REV 17 53-25-02, GST-063Mar 6, 2002 · N608AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR SIMA200207202Stringer · chafedDURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19L CHAFED. BLENDED CHAFE. FABRICATED TWO DOUBLER ANGLE 14.5 INCH BY 1.5 INCH, .050 INCH AND FOUR SHIMS 4.5 INCH BY .75 INCH, .080 INCH THICK IAW EMB 145 (SRM 145/1142 REV 17) 53-24-02, GST-0633/02, ETN Mar 6, 2002 · N608AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR CHQ000130Compass · out of toleranceDURING CLIMBOUT RECEIVED AN AMBER HEADING MESSAGE ON BOTH PFD'S. PERFORMED COMPASS SWING AND FLUX DETECTOR TEST, OPS CHECK GOOD.Mar 6, 2002 · N271 · Emb EMB145 · Magnetic CompassSDR C2XA02IA047Beam · corrodedIAH, During C-check inspection the floor beam top plate at frame 14 was found to be corroded beyond limits. Maintenance repaired the affected portion of floor beam utilizing a splice repair in accordance with EMB 145 SRM 53-21-10Mar 5, 2002 · N19966 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA02CL064Turbine Blades · damagedCLE FLIGHT 3303 THE CREW REPORTED ON APPROACH THE NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER INPUT. AFTER ADVANCING LEVER RAPIDLY THE ITT SPIKED TO APPROX 800 DEGREES. THE CAPTAIN SHUT DOWN THE NR 2 ENGINE AS A PRECAUTION. THE AIRCRAFT LANDED WITHOUT FURMar 4, 2002 · N12957 · Emb EMB145 · Turbine SectionSDR CHQ000128Anti-Ice System · malfunctionedICE CONDITION A/I INOP, W/A STAB A/I INOP EICAS MESSAGE AFTER T/O. RESET AIRCRAFT POWER, A/I TEST OPS CHECK GOOD.Mar 3, 2002 · N262 · Emb EMB145 · Airfoil Anti/De-ice SystemSDR SIMA200207009Floor Support · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON THE GALLEY CENTER HAT BEAM. REMOVED CORRODED GALLEY CENTER HAT BEAM. INSTALLED NEW HAT BEAM IAW EMB 145 SRM/1142, REV 17, 51-20-03, 51-40-02, GST-0623/02, ITEM 7 SEP 0114/02 AND STANDARD SRM PRAMar 2, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA02IA050Floorbeam · corrodedIAH - MAINTENANCE FOUND CORROSION OUT OF LIMITS ON THE FLOORBEAM AT FRAME 20. A SPLICE REPAIR WAS ACCOMPLISHED ON THE AFFECTED AREA OF FLOORBEAM IN ACCORDANCE WITH THE EMB SRM 53-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Mar 2, 2002 · N19966 · Emb EMB145 · Fuselage Main, Floor BeamSDR CHQ000127Smoke Warning · false activationBAGGAGE SMOKE WARNING AFTER T/O. CREW BLEW FIRE EXTINGUISHERS, NO EVIDENCE OF FIRE. COULD NOT DUPLICATE SMOKE WARNING AND DETECTION SYSTEM, OPS CHECK GOOD. FERRIED A/C TO CMH FOR FIRE BOTTLES.Mar 2, 2002 · N271 · Emb EMB145 · Smoke DetectionSDR CHQ000125Control Unit · malfunctionedSPOILER FAIL MESSAGE ON EICAS. REMOVED AND REPLACED SPOILER CONTROL UNIT, SPOILER SYSTEM TESTS GOOD AT THIS TIME.Feb 28, 2002 · N294 · Emb EMB145 · Drag Control SystemSDR C2XA02IA042Uplock · failedIAH- ON CLIMBOUT THE CREW NOTED THAT THE LANDING GEAR LEVER DISAGREE/UP POSITION/RIGHT MAIN NOT FULLY RETRACTED (AIRBORNE). THE CREW DECLARED EMERGENCY AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE UPLOCK BOX IN THE RIGHT MAIN LAFeb 25, 2002 · N16963 · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR SIMA200207001Doubler · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION, PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20. REMOVED PREVIOUS REPAIR, CORROSION LIMITED TO PREV REPAIR. FABRICATED A DOUBLER ANGLE AND FILLER. A PLATE AND TWO SHIMS. WORK DONE IAW EMB 145Feb 24, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR RAIA00202082Pressure Switch · failed5270-PIT- TAKE OFF CONFIGURATION WARNING: "BRAKE". MAINTENANCE REMOVED AND REPLACED PARKING BRAKE PRESSURE SWITCH.Feb 23, 2002 · N801HK · Emb EMB145 · Landing Gear Brake SystemSDR RAIA00202081Adc · inoperative5292-BGM- ON TAKE OFF ROLL GOT NUMEROUS WARNING MESSAGES: SPS, GPWS, AND #1 AHRS INOP. MAINTENANCE REMOVED AND REPLACED THE #1 AIR DATA COMPUTER, OPS CK OK.Feb 22, 2002 · N806HK · Emb EMB145 · Integrated Flight SystemSDR CHQ000120Warning System · malfunctionedCREW REPORTS SPOILER FAIL MESSAGE ON EICAS, ABORTED TAKEOFF. SPOILER DEPLOYED, MESSAGE WENT OUT. ATTEMPTED ANOTHER TAKEOFF, NO PROBLEMS NOTED.Feb 22, 2002 · N375 · Emb EMB145 · Drag Control SystemSDR C2XA02TY056Bellcrank · crackedTYS DURING A SCHEDULED EA-2730-01044 INSPECTION, THE RIGHT SIDE QUADRANT BELLCRANK WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT BELL QUADRANT IAW EMB-145 MM 27-31-03. OPS CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.Feb 21, 2002 · N15974 · Emb EMB145 · Elevator Control SystemSDR SIMA200208305Skin · corrodedABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ALONG FUSELAGE SKIN EDGE JUST BELOW BATTERY COMPARTMENT ACCESS DOOR. BLENDED, INSPECTED DAMAGE AND IT WAS ACCEPTED AS IS IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR SIMA200207203Sill · corrodedABI - RIGHT SILL BETWEEN FRAME 23 AND 29 HAS CORROSION. BLENDED OUT, PERFORMED NDT AND TREATED IAW EMB GST-0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200207204Frame · corrodedABI - RIGHT HAT BEAM AT FRAME 22 HAS CORROSION. BLENDED AND NDT'D AND TREATED HAT BEAM AT FRAME 22 IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, FrameSDR SIMA200207205Structure · corrodedABI - GALLEY AREA AFT DIGITAL HAS CORROSION. BLENDED OUT, PERFORMED NDT, AND TREATED FOR CORROSION IAW EMB 145 CPM 51-21-03, 51-21-04, 51-21-05, 51-21-06. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200207206Beam · corrodedABI - FOUND LEFT OMEGA BEAM BETWEEN FRAME 24 AND 25 HAS CORROSION. BLENDED AND PERFORMED NDT INSPECTION AND TREATED FOR CORROSION IAW EMB GST 0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200207207Beam · corrodedABI - CENTER OMEGA BEAM BETWEEN FRAME 23 AND 25 HAS CORROSION. BLENDED, PERFORMED NDT AND TREATED FOR CORROSION IAW EMB GST-0623/02. (M)Feb 20, 2002 · N608AE · Emb EMB145 · Fuselage Main, StructureSDR C2XA02IA055Gusset · corrodedIAH- DURING "C" CHECK THE LEFT FLOOR BEAM WAS CORRODED AT FR. 59 TO 61. IAH- MAINTENANCE REMOVED THE CORROSION BETWEEN FRAMES 59 to 61, DRILLED OUT THE CORRODED AREA AND INSTALLED #5 RIVET, TREATED PRIMED AND PAINTED THE AREA, AND. THE AIRCRAFT WAS APPROVED Feb 20, 2002 · N19966 · Emb EMB145 · Fuselage Main, Floor BeamSDR C2XA02IA054Floorbeam · corrodedIAH DURING C-CHECK INSPECTION IT WAS NOTED THAT CORROSION ON RIVET HEADS AND AROUND SCREW HOLES ON TOP OF FLOORBEAMS AT FRAME 20.Feb 19, 2002 · N19966 · Emb EMB145 · Fuselage Main, Floor BeamSDR RAIA00202068Control Valve · failed5324-PIT- CREW REPORTED NR 2 PAC OVERLOAD WARNING MESSAGE DURING TAKEOFF. MAINTENANCE REMOVED AND REPLACED DUAL TEMP CONTROL VALVE, OP CHECK OK.Feb 18, 2002 · N809HK · Emb EMB145 · Cabin Temperature Control SystemSDR SIMA200206506Beam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, CORROSION WAS FOUND ON THE LEFT OMEGA BEAM AT FRAME 20 WHICH EXCEEDED SRM LIMITS. COMPLETELY REMOVED CORROSION BY CUT OUT. FABRICATED .050 INCH, A DOUBLER ANGLE 18 INCH BY 3.75 INCH AND FILLER 12.1125 INCH BY 3.5 Feb 15, 2002 · N609AE · Emb EMB145 · Fuselage Main, StructureSDR SIMA200206502Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF THE AIRCRAFT, THE CENTER FLOORBEAM IN THE GALLEY AREA WAS FOUND TO BE CORRODED BEYOND SRM LIMIT AT FRAMES 20, 22 AND 23. REMOVED ENTIRE CENTER GALLEY FLOORBEAM. INSTALLED NEW FLOORBEAM IAW EMB 145 SRM, 145/1142 (REV 17) 51-Feb 14, 2002 · N609AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200204601Charger · meltedORD - FLT 4178 BURNING OR HOT INSULATOR ODOR IN THE VICINITY OF THE FA SEAT NOTED DURING DESCENT INTO ORD. AIRCRAFT LANDED SAFELY NO FURTHER INCIDENTS NOTED. NO EMERGENCY REPORTED. NOTED F/A FLASHLIGHT HOLDER ASSEMBLY DEFORMED. RAI FLASHLIGHT HOLDER. OPSFeb 14, 2002 · N607AE · Emb EMB145 · Emergency EquipmentSDR SIMA200206503Floorbeam · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON RIGHT GALLEY FLOORBEAM AT FRAME 22. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER IAW EMB GST 0467/02, ITEM 2 AND STANFeb 12, 2002 · N609AE · Emb EMB145 · Fuselage Main, Floor BeamSDR SIMA200206510Structure · corrodedABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON FORWARD DIGITAL BEYOND SRM LIMITS AFT BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR DOUBLER 4.3 INCH BY 2.1 INCH .040 INCH THICK. REPAIR DFeb 12, 2002 · N607AE · Emb EMB145 · Fuselage Main, StructureSDR CHQ000116Warning System · activatedOUTBOARD BRAKE FAIL MESSAGE ON EICAS.Feb 11, 2002 · N271 · Emb EMB145 · Landing Gear Brake SystemSDR CHQ000115Smoke Warning · activatedAFTER TAKEOFF LAV SMOKE WARNING.Feb 10, 2002 · N283SK · Emb EMB145 · Smoke DetectionSDR SIMA200206501Sill · corrodedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CARGO DOOR CUTOUT CENTER SILL BEAM CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED NEW SILL BEAM IAW EMB 145 SRM 145/1142, REV 16, 51-40-02 AND STANDARD SRM PRACTICES. (M)Feb 9, 2002 · N609AE · Emb EMB145 · Fuselage Miscellaneous StructureSDR SIMA200206505Skin · dentedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, REQUIRES PERMANENT REPAIR OF DENT LEFT FUSELAGE BETWEEN FRAMES 19 AND 20, STRINGERS 15L AND 16L. REMOVED DENT BY CUT OUT. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIFeb 7, 2002 · N609AE · Emb EMB145 · Fuselage Main, Plate/SkinSDR CHQ000113Control Unit · failedSPOILER FAIL MESSAGE, E-2 REVERSER DISAGREE MESSAGE. REMOVED AND REPLACED BRAKE CONTROL UNIT AND OPS CHECK GOOD.Feb 7, 2002 · N293 · Emb EMB145 · Drag Control SystemSDR SIMA200206504Frame · gougedABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND GOUGE AT BOTTOM FRAME 81 BEYOND SRM LIMITS. REMOVED DAMAGED FRAME. INSTALLED NEW FRAME IAW EMB 145 (SRM145/1142, REV 16) 51-20-03, 51-40-02 AND STANDARD SRM PRACTICES. (M)Feb 6, 2002 · N609AE · Emb EMB145 · Fuselage Main, FrameSDR C2XA02CL038Control Handle · intermittentCLE FLIGHT 3226 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE UPON GEAR RETRACTION. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Feb 6, 2002 · N14974 · Emb EMB145 · Landing Gear SelectorSDR CHQ000112Windshield · delaminatedF/O'S WINDSHIELD DELAMINATING, AOG FOR WINDSHIELD.Feb 6, 2002 · N270 · Emb EMB145 · Flight Compartment WindowsSDR SIMA200206511Stringer · chafedABI - DURING IN IMBV INSPECTION OF AICRAFT, STRINGER 19R WAS FOUND TO BE CHAFED BY THE AFT BELLY FAIRING AT HYDRAULIC BAY WALL. BLENDED CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE AREA WITH NO DEFECTS NOTED. APPLIED ALODINE AND EPOXY PRIMER TO Feb 5, 2002 · N609AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR RAIA00202049Sensor · malfunctioned5318-PIT- RIGHT INBOARD BRAKE OVER TEMP INDICATION DURING TAXI. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD BRAKE TEMP SENSOR, OPS CK OK.Feb 3, 2002 · N809HK · Emb EMB145 · Landing Gear Brake SystemSDR C2XA02TY020Bulb · blownTYS, During a scheduled routine check the emergency light at seat 12A was found not working, Maintenance removed and replaced the bulb I/A/W-EMB-145-AMM-33-50-00. operational checks good, aircraft released to service.Feb 2, 2002 · N14972 · Emb EMB145 · Emergency LightingSDR CHQ000102Relay · burnedELECTRICAL BURNING SMELL IN COCKPIT AND CABIN DURING FLIGHT, NO SMOKE PRESENT ALL SYSTEMS SEEMS NORMAL NO POPPED CIRCUIT BREAKERS UNABLE TO LOCATE SOURCE. UPON INSPECTION FOUND 3 RELAY SOCKETS WITH SIGNS OF OVERHEATING, R&R ALL 3 RELAYS AND SOCKETS.Jan 31, 2002 · N269 · Emb EMB145 · Landing Gear Retraction/Extension SystemSDR CHQ000110Battery · dischargedALL EMERGENCY LIGHTS OFF OF NR 4 BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERIES.Jan 30, 2002 · N265 · Emb EMB145 · Emergency LightingSDR C2XA02TY016Battery · burned outTYS DURING A ROUTINE CHECK THE EMERGENCY PROXIMITY STRIPS WERE OUT. MAINTENANCE R/R #4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK WAS GOOD. AIRCRAFT WAS REL. TO SERVICE UPON COMPLETION OF WORK.Jan 30, 2002 · N13969 · Emb EMB145 · Emergency LightingSDR SIMA200206705Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R CHAFED BETWEEN FRAME 52 AND 53. FABRICATED AND INSTALLED A TEMPORARY DOUBLER AND TWO SHIMS IAW EMB GST-0154/02 PERMANENT REPAIR BY NEXT C-CHECK IAW GST-0289/02. (M)Jan 29, 2002 · N607AE · Emb EMB145 · Fuselage Main, Longeron/StringerSDR RAIA00201040SillMX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AN THE GALLEY TIE DOWN POINT JUST FORWARD OF SERVICE DOOR. REMOVED AND REPLACED SERVICE DOOR FORWARD MEMBRANE SILL IAW SRM 53-21-10.Jan 28, 2002 · N803HK · Emb EMB145 · Fuselage Internal Mounting StructureSDR RAIA00201043WebMX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT FORWARD DIGITAL WEB PLATE. REMOVED AND REPLACED FORWARD DIGITAL WEB, IAW SRM 53-21-10 FIG 203.Jan 26, 2002 · N803HK · Emb EMB145 · Fuselage Miscellaneous StructureSDR C2XA02IA024Floorbeam · corrodedIAH- DURING C-CHECK INSPECTION IT WAS NOTED THAT HEAVE CORROSION ON THE LEFT HAND INBOARD FLOORBEAM AT FRAME 20 AT THE COMPOSITE FLOOR SUPPORT ATTACHMENT AREA. MAINTENANCE REPAIRED THE AREA, IAW EMB145 SRM 53-21-10, STEP NR 2 AND PAGE 204, FIGURE 201. THE AJan 25, 2002 · N16963 · Emb EMB145 · Fuselage Main, Floor BeamSDR RAIA00201042Support BracketMX-STL- DURING BLOCK CHECK FOUND MODERATE CORROSION AT FORWARD CENTER FLOOR BOARD ANGLE SUPPORT. REMOVED AND REPLACED ANGLE SUPPORT CENTER FLOOR BEAM IAW SRM 51-40-02.Jan 25, 2002 · N803HK · Emb EMB145 · Fuselage Floor Panel
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