Embraer ERJ 190-200 LR
Service difficulty reports · 49
Newest first. General aviation reporting is voluntary.
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 = 'ERJ190200LR' 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.
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 = 'ERJ190200LR' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR R61A2026062900182Power Supply · inoperativeCREW REPORTS 2 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED ELPU #2.SDR R61A2026062700179Engine · faultedENG 2 FAIL AROUND 10,000 FT. N1 WENT TO 15.2. HIGH ENG VIB, ENG #2 ITT GAUGE TURNED RED. UPON LANDING ENG #2 EXCEEDANCE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED ENG #2.SDR R61A2026062400171Engine · vibrationLOW PRESSURE VIBRATION NR 2 ENGINE AT ALTITUDE. RAN QRH, DESCENDED AND REDUCED SPEED, VIBRATIONS IN GREEN AT 3.0. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. INSPECTED ENG NR 2 FAN BLADES AND FOUND NO DEFECTS. PLACED ENGINE NR 2 ON NON-MEL DMI FOR FAN MX WISDR EE4Y2025110523420Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING IINBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED ANDREPAIRED IAW ETD2025-190-925075 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-22SDR EE4Y2025110523419Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING INBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED AND REPAIRED IAWETD2025-190-925074 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-227SDR EE4Y2025100623293Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-511A, S/N 1395001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANELS. THE DENTS WERE EVALUATED AS PER SRM 71-61-01/AD53. MOST OF THE DENTS ARE BEYOND THE LIMITS FSDR EE4Y2025100623292Inlet · dentedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND P/N 341-1010-509F, S/N 1192001, AIR INLET MODULE WITH SEVERAL DENTS ON THE INNER BARREL UPPER AND LOWER ACOUSTIC PANEL. THE DENTS WERE EVALUATED AS PER REF. SRM 71-61-01/AD53. MOST OF THEM ARE BEYOND THE LIMITS FOSDR EE4Y2025100623291Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WE FOUND THE CENTER FUSELAGE I – AT FR31+380MM, S-26R+30MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-92SDR EE4Y2025100623290Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WAS FOUND THE CENTER FUSELAGE I – AT FR27+370MM, S-26R+60MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). DURING THE DOCUMENT CLOSING PROCESS, THE DAMAGE WAS LOCATESDR EE4Y2025100623289Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND ON FORWARD FUSELAGE, AT FR18+18MM AND STGR-26R+85MM, EXTERNAL SKIN WITH A LIGHTNING STRIKE DAMAGE. EVALUATED THOUGH DAMAGE AND FOUND OUT OF LIMITS IAW ERJ190, PART II SRM 53-10-01, AD53, PARAGRAPH 4.B.(3): THE DISSDR EE4Y2025100623288Skin · damagedDURING THE MAINTENANCE ACTIVITIES AN EXISTING BLEND OUT WAS FOUND, IT IS LOCATED ON REAR FUSELAGE AT FR94+240MM, BTWN STRG 23R-25R. EVALUATED BLEND OUT WITH CLAD LAYER PENETRATED AND FOUND OUT LIMITS PER ERJ190 PART II SRM 53-30-01, AD 51, FIGURE 104, SHEET 4 SDR EE4Y2025100623287Skin · scratchedDURING THE STRUCTURAL INSPECTION IT WAS FOUND ON FORWARD FUSELAGE, RH-LATERAL SEAT TRACK FROM FR19 TO FR20 OTBD CROWN AREA WITH SCRATCH. EVALUATED BLEND OUT AREAS AND FOUND OUT OF LIMITS PER ERJ190, PART II SRM 53-10-10, AD51, PARAGRAPH 4.B. (NO DAMAGES AREA ASDR EE4Y2025091723170Skin · damagedDURING STRUCTURE INSPECTION, FOUND FWD FUSELAGE, FR 18+50MM, & S27L + 155MM (JUST 8.0MM FROM STR 28L FASTENER ROW), EXTERNAL SKIN WITH LIGHTNING STRIKE WITH EXISTING BLEND OUT. BLEND OUT WAS EVALUATED & CLASSIFIED AS NON-SIGNIFICANT IAW SRM 51-75-16. LIGHTNSDR EE4Y2025091723168Skin · damagedCENTER FUSELAGE I SKIN HAS A LIGHTNING STRIKE DAMAGE AT FRAME 30+290MM AND STRINGER 27R. SEE FIGURE 1. THE DAMAGE WAS REMOVED BY BLENDING AND WAS FOUND BEYOND LIMITS PER SRM 53-21-01/AD 51. SINCE THE DAMAGE IS LOCATED IN THE NOT ALLOWED REPAIR AREA (GREY AREA)SDR EE4Y2025091723167Heat Shield · misrepairedDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED WITHOUT RECORDS AT RH ENGINE PYLON HEAT SHIELD BAY #8. DUE TO THIS FACT, THE REPAIR WAS REMOVED. THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-926307 DTD AUG 08 2025 AND DOCUMENSDR EE4Y2025091723166Seat · corruptedPER CUSTOMER REQUEST, PASSENGER CABIN SEATS DIAPHRAGMS 41191032-35, 41191032-36, 41191032-37, 41191032-38 WERE FOUND WITH CRACKS AND MUST BE REPAIRED.THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-924987 REV. B, AND COOPESA COO-EO-2025-23053,SDR EE4Y2022052315569Skin Panel · nickedLOWER CENTER FUSELAGE I, EXTERNAL SKIN WITH NICKS LOCATED FROM FR29 AND FR30 BETWEEN STRINGER 26LH AND STRINGER 27LH. NOTA: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER INSTRUCTIONS. ( FOR ADDITONAL DETAILS SEE COOPESA JOB: A1M007 SPECIAL ITEM: 21-48 ).SDR EE4Y2022052315568Fitting · crackedRH WING SPAR II, SPOILER #5 INBOARD SIDE FITTING CRACKED. NOTE: THE SPOILER FITTING WAS REPLACED AS PER EMBRAER INSTRUCTIONS. ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1M007 SPECIAL ITEM: 6-26 ).SDR EE4Y2022052315565Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT LOCATED AT FR20+10MM BETWEEN STRINGER 12LH AND STRINGER 13LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-012471 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15334 INSTRUCTSDR EE4Y2022052315567Skin Panel · dentedLOWER REAR FUSELAGE , EXTERNAL SKIN WITH DENT AND OIL CAN LOCATED AT FR95+310MM BETWEEN STRINGER 23LH AND STRINGER 25LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014171 REV:B GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2SDR EE4Y2022051115564Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT AND CREASE LOCATED BETWEEN FR04 AND FR05, BETWEEN STRINGER 10LH AND STRINGER 12LH. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2022-190-014169 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-ESDR EE4Y202051115562Skin Panel · dentedUPPER FORWARD FUSELAGE EXTERNAL SKIN WITH DENT, LOCATED AT FR04+265MM, STRINGER 10RH+20MM. NOTE: THE FUSELAGE SKIN PANEL WAS REPAIRED AS PER EMBRAER ETD2022-190-013658 REV:A GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2022-15381 INSTRUCTIONS (SDR 3CEY20210817001Retaining Ring · deformedQUICK TURN HPC TOP CASE REPAIR IAW 72-00-00 SP001 AND 72-00-00 SP110 CONDUCTED. DURING THE AFFECTED HPC STG2 & 3 BLADES REMOVAL WE NOTED THE STG2 FWD BLADE RETAINER LUG WEAR AND TIGHT CONDITION. FURTER EXAMINATION REVEALED THAT BLADE RETAINER PN 2031M31G01 HASSDR R61A201909130959Rib · crackedMAJOR: FOUND LT HORIZONTAL RIB 12A CRACK. REMOVED AND REPLACED LT HORIZONTAL STAB RIB 12A PER SRM 51-40-08. APPLIED SURFACE PROTECTION PER SRM 51-23-05, 51-03-06. SEE WIPS FOR WORK PERFORMED. SEE W/O H6951 SN 691 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHSDR R61A201909130954Door Sill · corrodedWHILE PERFORMING L2 DOOR LOWER BEAM REWORK, CORROSION FOUND ON TOP OF SILL AT AFT GIRT BAR FITTING. REMOVED AND INSTALLED NEW L2 DOOR LOWER BEAM REF: SRM 51-40-08. SEE W/O H6951 SN 606 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.SDR R61A201901200090Beam · corrodedWHILE PERFORMING 2236:170EO-53-14-0002-170EO-53-14-0002 L1 DOOR LOWER BEAM REWORK FOUND CORROSION AROUND NUTCLIP FASTENER HOLE. REMOVED AND REPLACED L1 LOWER BEAM REF. SRM 51-40-08. RESTORED SURFACE PROTECTION REF. SRM 51-23-04, 51-23-05, AND 51-23-06. SEE W/SDR MASA2018101311443Battery · dischargedAFT FA FLASHLIGHT INOP. REPLACED BATTERY.SDR MASA2018052713259Flashlight · inoperativeFWD FA FLASHLIGHT INOP. PLACED ON MEL.SDR MASA2018052613257Battery Pack · dischargedFWD FA FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED BATTERY PACK.SDR R61A201804110489Doubler · corrodedLT FLOOR DOUBLER CORRODED AS MARKED FR 80. REMOVED AND REPLACED FR 80 STGR 26R - 28R REF SRM 51-40-08, SRM 51-40-02.SDR R61A201802190286Splice · corrodedWHILE AIRCRAFT WAS OUT OF SERVICE FOR HEAVY CHECK, MAINTENANCE FOUND LEVEL 2 CORROSION AT AFT WET AREA LT OUTBD SPLICE PLATE AFT OF L2. THEY REMOVED AND REPLACED SPLICE IAW SRM 51-42-02. AIRCRAFT REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR R61A201711080820Rib · crackedMAJOR REPAIR FCBS 55-10-00-005, CRACKED RIBS ON RT HORIZONTAL STABILIZER BETWEEN FRONT SPAR AND MID SPAR. REMOVED AND REPLACED RIB 11 AND 12 ON RT HORIZONTAL STAB BETWEEN FRONT AND MID SPAR.SDR R61A201702200145Floor Support · corrodedFLOOR SUPPORT AT FRAME 18 LBL 30 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.SDR SIMA20160524002Seal · defectiveMAIN DOOR HOLD OPEN LATCH INOPERATIVE. TRIMMED EXCESS MATERIAL FROM DUST SEAL AS REQUIRED. OPERATIONS CHECKED GOOD.SDR C77A20151120002Doubler · corrodedCORROSION ON SEVERAL AREAS OF FWD CABIN AFT LT FLOOR DOUBLER, PN 170-07311-001 AT FRAME 19, BETWEEN Y= -304 THRU - 850, X=5645. R & R LT AFT DOUBLER IAW SRM 51-41-01 & 51-43-01 ON WO 19451651E1 IAW EO E175-5300-128 REV IR WO 1980904.SDR C77A2015031200001Floor Support · corrodedAFT CABIN RT FLOOR SUPPORT HAS CORROSION AT FRAMES 86 - 89, Y 260.4. R & R THE FLOOR SUPPORT IAW SRM 51-41-02 & 51-43-01.SDR C77A201503050021Skin · corrodedCORROSION ON FUSELAGE SKIN INNER SURFACE AT AFT CARGO COMPARTMENT BETWEEN FRAME 80 & 81, STATION 21446 & OTBD SIDE OF STRINGER 28R. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213041M3 IAW 15-170-017453 & EA E175-53-485 REV IR WO 1834666SDR C77A20150305016Upper Sheet · corrodedAFT CABIN RT UPPER SHEET, PN 170-86101-001 HAS CORROSION BETWEEN FRAME 85 & 86, X= 23041 - 23453, Y=260.4. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 6213171J4 IAW ETD 015-170-016788 & EO E175-5300-100 REV IR WO 1834035.SDR C77A20150305005Door Sill · corrodedFORWARD CABIN RT FWD FLOOR SILL, PN 170-05663-003, HAS CORROSION BETWEEN FRAME 13 & 14, X=4011 - 4270, Y=939.8 TO Y=1244.6. BLENDED CORRODED AREA IAW SRM 51-10-03 & 51-12-01 ON WO 14680921H1 IAW ETD 2015-170-016753A & EO E175-5300-101 REV IR WO 1834324.SDR C77A20140121013Panel Support · corrodedAFT CABIN FLOOR LT PANEL SUPPORT, PN 170-86139-005, IS CORRODED X 24868.0, Y -838. R & R LT PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WORK ORDER 737209-245 IAW EO E175-5300-097 REV IR WORK ORDER 906482.SDR C77A20140121003Panel Support · corrodedAFT CABIN FLOOR RT PANEL SUPPORT, PN 170-66797-001 FWD PANEL SUPPORT HAS CORROSION AT X 4000 Y 718. R & R RT PANEL SUPPORT IAW SRM 51-41-01 & 51-43-01 ON WORK ORDER 737209-216 IAW EO E175-5300-097 REV IR WORK ORDER 906482.SDR R61A201307240659Rib · crackedDURING HEAVY CHECK, REPORTED SECOND INBD BRACKET ON LT HORIZONTAL STAB L/E CRACKED. MX REPAIRED RIB 5 ON LT HORZONTAL STAB L/E, PN 170-62334-001, RIB 5. ACFT REMAINS FOR COMPLETION OF HEAVY CHECK.SDR R61A201304060403Skin · buckledWHILE PERFORMING MAINTENANCE IN HEAVY CHECK MAINTENANCE DAMAGED SKIN AFT LOWER FUSELAGE JACK PAD AREA. MAINTENANCE REPAIRED SKIN IAW EMB ETD 2013-170-006071 AND TI170-13-033. THIS WAS A MAJOR REPAIR. ITEMS REMOVED AND REPLACED WITH THE SKIN REPAIR ARE NON-FSDR R61A201212090737Support · gougedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE NOSE LANDING GEAR ACTUATOR SUPPORT GOUGED FORWARD EDGE INBOARD SIDE. MAINTENANCE BLENDED OUT DAMAGE IAW EMB ETD 2012-170-018181 NOSE LANDING GEAR ACTUATOR SUPPORT FORWARD EDGE INBOARD SIDE. "MAJOR REPAISDR R61A20120001Service Panel · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LAVATORY DUMP SERVICE BOX CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY SERVICE BOX IAW EMB 175 SRM 51-40-02 AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A20110353Door · lack of lubeCREW REPORTED L-2 DOOR DIFFICULT TO ARM/DISARM. MAINTENANCE LUBED AND PERFORMED OPS CHECK OF L-2 DOOR PER EMB AMM, OPS CHECK GOOD.SDR R61A20110354Door · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND LAVATORY WASTE SERVICE DOOR CORRODED. MAINTENANCE REMOVED AND REPLACED LAVATORY WASTE SERVICE DOOR IAW EMB 170SRM 51-00-00. AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR CA090306002Floorbeam · corroded(CAN) AFT GALLEY FLOOR AREA WAS FOUND WITHOUT SEALANT BETWEEN THE FLOORBOARDS. WITH FLOORBOARDS REMOVED, CORROSION WAS DISCOVERED ON SEVERAL FLOORBEAMS, SEAT TRACKS AND SHEAR PLATES.SDR R61A20090002Sensor · failedON CLIMBOUT CREW REPORTED, THEY RECEIVED SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURES AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO A/C TROUBLESHOT SYSTEM FOUND SLAT 2/3 SKEW SENSOR TO BE BAD. REPLA
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