# Service difficulty reports: Embraer ERJ 190-200 LR

A list on [Embraer ERJ 190-200 LR](https://openairdocs.org/model/embraer-erj-190-200-lr.md).

Newest first. General aviation reporting is voluntary.

- [SDR R61A2026062900182](https://openairdocs.org/sdr/R61A2026062900182.md): Power Supply · inoperative · Jun 29, 2026 · N748YX · Emb ERJ190200LR · Emergency Lighting
  > CREW REPORTS 2 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED ELPU #2.
- [SDR R61A2026062700179](https://openairdocs.org/sdr/R61A2026062700179.md): Engine · faulted · Jun 27, 2026 · N411YX · Emb ERJ190200LR · Engine (Turbine/Turboprop)
  > ENG 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 R61A2026062400171](https://openairdocs.org/sdr/R61A2026062400171.md): Engine · vibration · Jun 24, 2026 · N111HQ · Emb ERJ190200LR · Engine (Turbine/Turboprop)
  > LOW 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 WI
- [SDR EE4Y2025110523420](https://openairdocs.org/sdr/EE4Y2025110523420.md): Rib · corroded · Nov 5, 2025 · N688DR · Emb ERJ190200LR · Wing, Rib/Bulkhead
  > DURING 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-2025-22
- [SDR EE4Y2025110523419](https://openairdocs.org/sdr/EE4Y2025110523419.md): Rib · corroded · Nov 5, 2025 · N688DR · Emb ERJ190200LR · Wing, Rib/Bulkhead
  > DURING 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-2025-227
- [SDR EE4Y2025100623293](https://openairdocs.org/sdr/EE4Y2025100623293.md): Inlet · dented · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Engine Air Intake System
  > DURING 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 F
- [SDR EE4Y2025100623292](https://openairdocs.org/sdr/EE4Y2025100623292.md): Inlet · dented · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Engine Air Intake System
  > DURING 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 FO
- [SDR EE4Y2025100623291](https://openairdocs.org/sdr/EE4Y2025100623291.md): Skin · damaged · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > AZORRA 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 ETD2025-190-92
- [SDR EE4Y2025100623290](https://openairdocs.org/sdr/EE4Y2025100623290.md): Skin · damaged · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > AZORRA 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 LOCATE
- [SDR EE4Y2025100623289](https://openairdocs.org/sdr/EE4Y2025100623289.md): Skin · damaged · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > DURING 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 DIS
- [SDR EE4Y2025100623288](https://openairdocs.org/sdr/EE4Y2025100623288.md): Skin · damaged · Oct 6, 2025 · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > DURING 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 EE4Y2025100623287](https://openairdocs.org/sdr/EE4Y2025100623287.md): Skin · scratched · Oct 6, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > DURING 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 A
- [SDR EE4Y2025091723170](https://openairdocs.org/sdr/EE4Y2025091723170.md): Skin · damaged · Sep 17, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > DURING 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. LIGHTN
- [SDR EE4Y2025091723168](https://openairdocs.org/sdr/EE4Y2025091723168.md): Skin · damaged · Sep 17, 2025 · N688DR · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > CENTER 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 EE4Y2025091723167](https://openairdocs.org/sdr/EE4Y2025091723167.md): Heat Shield · misrepaired · Sep 17, 2025 · N688DR · Emb ERJ190200LR · Nacelle/Pylon, Main Frame
  > DURING 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 DOCUMEN
- [SDR EE4Y2025091723166](https://openairdocs.org/sdr/EE4Y2025091723166.md): Seat · corrupted · Sep 17, 2025 · N688DR · Emb ERJ190200LR · Passenger Compartment Equipment
  > PER 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 EE4Y2022052315569](https://openairdocs.org/sdr/EE4Y2022052315569.md): Skin Panel · nicked · May 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, Structure
  > LOWER 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 EE4Y2022052315568](https://openairdocs.org/sdr/EE4Y2022052315568.md): Fitting · cracked · May 23, 2022 · N140BZ · Emb ERJ190200LR · Spoilers
  > RH 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 EE4Y2022052315565](https://openairdocs.org/sdr/EE4Y2022052315565.md): Skin Panel · dented · May 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, Structure
  > UPPER 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 INSTRUCT
- [SDR EE4Y2022052315567](https://openairdocs.org/sdr/EE4Y2022052315567.md): Skin Panel · dented · May 23, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, Structure
  > LOWER 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-2
- [SDR EE4Y2022051115564](https://openairdocs.org/sdr/EE4Y2022051115564.md): Skin Panel · dented · May 11, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, Structure
  > UPPER 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-E
- [SDR EE4Y202051115562](https://openairdocs.org/sdr/EE4Y202051115562.md): Skin Panel · dented · May 11, 2022 · N140BZ · Emb ERJ190200LR · Fuselage Main, Structure
  > UPPER 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 3CEY20210817001](https://openairdocs.org/sdr/3CEY20210817001.md): Retaining Ring · deformed · Aug 13, 2021 · Emb ERJ190200LR · Turbine Engine Compressor Section
  > QUICK 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 HAS
- [SDR R61A201909130959](https://openairdocs.org/sdr/R61A201909130959.md): Rib · cracked · Sep 6, 2019 · N118HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR: 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 CH
- [SDR R61A201909130954](https://openairdocs.org/sdr/R61A201909130954.md): Door Sill · corroded · Aug 27, 2019 · N118HQ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > WHILE 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 R61A201901200090](https://openairdocs.org/sdr/R61A201901200090.md): Beam · corroded · Jan 2, 2019 · N216JQ · Emb ERJ190200LR · Fuselage Main, Structure
  > WHILE 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 MASA2018101311443](https://openairdocs.org/sdr/MASA2018101311443.md): Battery · discharged · Oct 13, 2018 · N85351 · Emb ERJ190200LR · Emergency Equipment
  > AFT FA FLASHLIGHT INOP. REPLACED BATTERY.
- [SDR MASA2018052713259](https://openairdocs.org/sdr/MASA2018052713259.md): Flashlight · inoperative · May 27, 2018 · N89357 · Emb ERJ190200LR · Emergency Equipment
  > FWD FA FLASHLIGHT INOP. PLACED ON MEL.
- [SDR MASA2018052613257](https://openairdocs.org/sdr/MASA2018052613257.md): Battery Pack · discharged · May 26, 2018 · N86312 · Emb ERJ190200LR · Emergency Equipment
  > FWD FA FLASHLIGHT RED LIGHT NOT BLINKING. REPLACED BATTERY PACK.
- [SDR R61A201804110489](https://openairdocs.org/sdr/R61A201804110489.md): Doubler · corroded · Mar 20, 2018 · N880RW · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > LT 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 R61A201802190286](https://openairdocs.org/sdr/R61A201802190286.md): Splice · corroded · Feb 19, 2018 · N209JQ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > WHILE 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 R61A201711080820](https://openairdocs.org/sdr/R61A201711080820.md): Rib · cracked · Oct 19, 2017 · N125HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/Rib
  > MAJOR 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 R61A201702200145](https://openairdocs.org/sdr/R61A201702200145.md): Floor Support · corroded · Feb 6, 2017 · N867RW · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FRAME 18 LBL 30 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01.
- [SDR SIMA20160524002](https://openairdocs.org/sdr/SIMA20160524002.md): Seal · defective · May 24, 2016 · N233NN · Emb ERJ190200LR · Passenger/Crew Doors
  > MAIN DOOR HOLD OPEN LATCH INOPERATIVE. TRIMMED EXCESS MATERIAL FROM DUST SEAL AS REQUIRED. OPERATIONS CHECKED GOOD.
- [SDR C77A20151120002](https://openairdocs.org/sdr/C77A20151120002.md): Doubler · corroded · Nov 19, 2015 · N616CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > CORROSION 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 C77A2015031200001](https://openairdocs.org/sdr/C77A2015031200001.md): Floor Support · corroded · Mar 12, 2015 · N603CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > AFT 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 C77A201503050021](https://openairdocs.org/sdr/C77A201503050021.md): Skin · corroded · Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > CORROSION 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 1834666
- [SDR C77A20150305016](https://openairdocs.org/sdr/C77A20150305016.md): Upper Sheet · corroded · Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > AFT 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 C77A20150305005](https://openairdocs.org/sdr/C77A20150305005.md): Door Sill · corroded · Mar 2, 2015 · N602CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > FORWARD 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 C77A20140121013](https://openairdocs.org/sdr/C77A20140121013.md): Panel Support · corroded · Jan 19, 2014 · N622CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > AFT 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 C77A20140121003](https://openairdocs.org/sdr/C77A20140121003.md): Panel Support · corroded · Jan 19, 2014 · N622CZ · Emb ERJ190200LR · Fuselage Miscellaneous Structure
  > AFT 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 R61A201307240659](https://openairdocs.org/sdr/R61A201307240659.md): Rib · cracked · Jul 24, 2013 · N111HQ · Emb ERJ190200LR · Horizontal Stabilizer, Spar/Rib
  > DURING 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 R61A201304060403](https://openairdocs.org/sdr/R61A201304060403.md): Skin · buckled · Apr 6, 2013 · N134HQ · Emb ERJ190200LR · Fuselage Main, Plate/Skin
  > WHILE 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-F
- [SDR R61A201212090737](https://openairdocs.org/sdr/R61A201212090737.md): Support · gouged · Dec 9, 2012 · N102HQ · Emb ERJ190200LR · Landing Gear Actuator
  > WHILE 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 REPAI
- [SDR R61A20120001](https://openairdocs.org/sdr/R61A20120001.md): Service Panel · corroded · Dec 29, 2011 · N116HQ · Emb ERJ190200LR · Waste Disposal System
  > WHILE 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 R61A20110353](https://openairdocs.org/sdr/R61A20110353.md): Door · lack of lube · Nov 7, 2011 · N164HQ · Emb ERJ190200LR · Passenger/Crew Doors
  > CREW 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 R61A20110354](https://openairdocs.org/sdr/R61A20110354.md): Door · corroded · Nov 6, 2011 · N118HQ · Emb ERJ190200LR · Service Doors
  > WHILE 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 CA090306002](https://openairdocs.org/sdr/CA090306002.md): Floorbeam · corroded · Feb 27, 2009 · Emb ERJ190200LR · Fuselage Main, Floor Beam
  > (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 R61A20090002](https://openairdocs.org/sdr/R61A20090002.md): Sensor · failed · Jan 19, 2009 · N125HQ · Emb ERJ190200LR · Leading Edge Slat Actuator
  > ON 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

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/embraer-erj-190-200-lr/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.