# Service difficulty reports: Embraer ERJ 190-100 IGW

A list on [Embraer ERJ 190-100 IGW](https://openairdocs.org/model/embraer-erj-190-100-igw.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 145 · 7,215 reports

- [SDR EE4Y2026102825150](https://openairdocs.org/sdr/EE4Y2026102825150.md): Skin · dented · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > A DENT WAS FOUND IN THE LH WING SLAT NR 1 NOSE SKIN L/E. THIS CONDITION WAS REPAIRED IAW EMB ETD2011-190-106587 DTD OCT 21 2011 AND DOCUMENTED UNDER COOPESA EO #COO-EO-2026-25012-R00 DTD SEP 21 2026. JOB A1R169 ITEM 21-44
- [SDR EE4Y2026102825149](https://openairdocs.org/sdr/EE4Y2026102825149.md): Heat Shield · damaged · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > AN EXISTING WITH LACKS MATERIAL TRACEABILITY SKIN REPAIR THAT WAS NOTED AT THE RH PYLON AFT FAIRINGS HEAT SHIELD BAY 8, LOCATED AROUND THE GRILL SKIN CUTOUT. DUE TO IT, DETAILS WERE SENT TO EMB FOR EVALUATION AND WAS REPAIRED IAW EMB ETD2026-190-015345 DTD SEP
- [SDR EE4Y2026102825148](https://openairdocs.org/sdr/EE4Y2026102825148.md): Skin · cracked · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > RH WING MAIN BOX LOWER SKIN T/E SKIN WITH CRACK AT RIB 11. THIS CONDITION WAS REPAIRED IAW EMB SRM 57-10-01 REPAIR 54P. JOB A1R169 ITEM 21-28
- [SDR EE4Y2026102825147](https://openairdocs.org/sdr/EE4Y2026102825147.md): Skin · damaged · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING THE REPLACEMENT OF THE RIGHT WING LEADING EDGE SKIN WEAR RIVETS, THE HOLES WERE FOUND ELONGATED. THIS CONDITION WAS REPAIRED IAW EMB ETD2016-190-068049 DTD JUL 23 2016 AND DOCUMENTED UNDER COOPESA EO #COO-EO-2026-24897 DTD AUG 25 2026. JOB A1R169 ITEM 2
- [SDR EE4Y2026102825146](https://openairdocs.org/sdr/EE4Y2026102825146.md): Skin · damaged · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > A LIGHTNING STRIKE WAS DETECTED ON THE FORWARD FUSELAGE SKIN AT FRAME 04 +180MM, 15MM ABOVE STRINGER 22R. PER SRM 53-10-01/AD53 PARAGRAPH 4B(3) STATES THAT THE MINIMUM DISTANCE BETWEEN THE DAMAGE AND THE SKIN EDGE MUST BE 25.4 MM (1.0 IN). IN THIS CASE, THE CU
- [SDR EE4Y2026102825145](https://openairdocs.org/sdr/EE4Y2026102825145.md): Skin · damaged · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Trailing Edge Flaps
  > DURING A STRUCTURAL INSPECTION, DAMAGE WAS FOUND ON THE RH WING INBOARD MAIN FLAP LOWER SURFACE, AFT INBOARD CORNER. THE AFFECTED AREA PRESENTS A MISSING-HEAD FASTENER AND A SLIGHT SKIN BULGE ADJACENT TO THE FASTENER HOLE. DUE TO IT, DETAILS WERE SENT TO EMB
- [SDR EE4Y2026102825144](https://openairdocs.org/sdr/EE4Y2026102825144.md): Seal · cracked · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Nacelle/Pylon, Plate/Skin
  > A CRACK WAS FOUND IN THE LH AND RH PYLONS - INBOARD AND OUTBOARD SUPPORT SEALS. THIS CONDITION WAS REPAIRED IAW EMB ETD2025-190-001674 REV. A DTD MAY 29 2025 AND DOCUMENTED UNDER COOPESA EO #COO-EO-2026-25010-R00 DTD SEP 21 2026. JOB A1R169 ITEM 4-109
- [SDR EE4Y2026102852514](https://openairdocs.org/sdr/EE4Y2026102852514.md): Inlet · dented · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Engine Air Intake System
  > DENT FOUND ON THE ENGINE #1 INLET INNER BARREL SKIN. DUE TO IT, DETAILS WAS SENT TO EMB AND WAS REPAIRED IAW EMB ETD2026-190-015468 REV. A DTD SEP 28 2026 AND DOCUMENTED UNDER COOPESA EO #COO-EO-2026-24968-R01 DTD SEP 28 2026. JOB A1R169 ITEM 4-9
- [SDR EE4Y2026102825142](https://openairdocs.org/sdr/EE4Y2026102825142.md): Skin · damaged · Oct 28, 2026 · N328JB · Emb ERJ190100IGW · Fuselage Floor Panel
  > LIGHTNING STRIKE DAMAGE FOUND ON CENTER FUSELAGE I SKIN AT FR27+360 MM AND STRINGER 20RH+115 MM. THE DAMAGED AREA WAS DRILLED OUT IN ACCORDANCE WITH SRM 53-21-01 AD53 PARAGRAPH 6C AND SUBSEQUENTLY INSPECTED. DUE TO IT, DETAILS WERE SENT TO EMB WAS REPAIRED IAW
- [SDR EE4Y2026102725140](https://openairdocs.org/sdr/EE4Y2026102725140.md): Skin · dented · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AFFECTED WITH DENTS WAS FOUND IN THE CENTER FUSELAGE I, BTWN FR23/24 BTWN S-13L/15L, WAS REPAIRED AW SRM 53-21-01/REPAIR 64P. JOB A1Q358 ITEM 21-3
- [SDR EE4Y2026102725139](https://openairdocs.org/sdr/EE4Y2026102725139.md): Link · corroded · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > DURING THE ACCOMPLISHMENT OF INSPECTION TASK 54-50-004-0006, THE PYLON LOWER LINK FITTING INBOARD AND OUTBOARD LUGS FIXED BUSHINGS WERE FOUND WITH WEAR. AFTER REMOVAL OF THE BUSHINGS FOR REPLACEMENT, LOCALIZED CORROSION WAS DETECTED BETWEEN THE LUG SURFACE AND
- [SDR EE4Y2026102725138](https://openairdocs.org/sdr/EE4Y2026102725138.md): Seat Track · corroded · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > A CORROSION AFFECTING THE FORWARD FUSELAGE - LH FORWARD FLOOR TRACK UPPER CAP BTW FR13 AND 14, WAS REPAIRED IAW EMB ETD2016-190-055023 REV. A DTD JUN 16 2016 AND DOCUMENTED UNDER COOPESA EO #COO-EO-2026-24818-R00 DTD AUG 03 2026. JOB A1Q358 ITEM 21-2
- [SDR EE4Y2026102725137](https://openairdocs.org/sdr/EE4Y2026102725137.md): Fairing · cracked · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Aerodynamic Fairings
  > A CRACK AFFECTING THE CENTER FUSELAGE II L/H WING-TO-FUSELAGE FAIRING RIB 52, WAS REPAIRED IAW EMB ETD2016-190-054721 DTD JUN 10 2016 AND DOCUMENTED UNDER THE COOPESA EO #COO-EO-2026-24815-R00 DTD AUG 03 2026. JOB A1Q358 ITEM 21-5
- [SDR EE4Y2026102725136](https://openairdocs.org/sdr/EE4Y2026102725136.md): Seat Track · contaminated · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Fuselage Internal Stairs
  > DURING THE STRUCTURE INSPECTION A CORROSION WAS FOUND AFFECTING THE RH SEAT TRACK AT FR84. THE DAMAGE WAS FOUND OUT LIMITS PER SRM PART II 53-23-10 AD 54 DUE TO THE REMAINING THICKNESS BEING LOWER THAN THE PERMISSIBLE PER SRM. DUE TO IT, PERFORMING THE REPAIR
- [SDR EE4Y2026102725134](https://openairdocs.org/sdr/EE4Y2026102725134.md): Tail Cone · dented · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Aerodynamic Fairings
  > DURING AN INSPECTION TO THE TAIL CONE WERE FOUND 2 DENTS AFFECTING THE SKIN, LOCATED LEFT FWD AT 9 O’CLOCK OF THE TAIL CONE ASSY. THE DENTS WERE EVALUATED PER ERJ-190 SRM PART II 53-31-01/AD52 AND ARE DECLARED OUT OF LIMITS DUE TO THE DISTANCES TO FASTENERS. D
- [SDR EE4Y2026102725133](https://openairdocs.org/sdr/EE4Y2026102725133.md): Cowl Door · damaged · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Engine Thrust Reverser
  > DURING INSPECTION OF THE ENGINE NO. 1 INBOARD TRANSLATING COWL TWO EXISTING FILLED AREAS WITHOUT SUPPORTING REPAIR RECORDS WERE FOUND. THEREFORE, THE EXISTING FILLER MATERIAL WAS REMOVED TO ALLOW PROPER ASSESSMENT OF THE DAMAGE. CUSTOMER HAS PROPOSED TO REPAI
- [SDR EE4Y2026102725131](https://openairdocs.org/sdr/EE4Y2026102725131.md): Heat Shield · cracked · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Nacelle/Pylon, Bulkhead/Firewall
  > DURING INSPECTION, IT WAS NOTED THAT ENGINE NR 1 PYLON AFT FAIRING HEAT SHIELD SKIN NR 8 HAD AN EXISTING REPAIR AT THE AFT LOWER CORNER OF THE EXHAUST GRILL CUTOUT. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR LACKS MATERIAL TRACEABILITY. CONSEQUENTLY,
- [SDR EE4Y2026102725130](https://openairdocs.org/sdr/EE4Y2026102725130.md): Skin · cracked · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND AT THE RH WING LOWER SKIN BETWEEN RIBS 9 AND 11, COMMON TO SPAR II. ACCORDING TO PREVIOUS OPERATOR RECORDS, THE REPAIR WAS INSTALLED IN ACCORDANCE WITH ETD2018-190-071059 REV. C GUIDELINES. HOWEVER
- [SDR EE4Y2026102725129](https://openairdocs.org/sdr/EE4Y2026102725129.md): Skin · cracked · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Leading Edge Devices
  > DURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE LT WING LEADING EDGE SKIN CUTOUT BETWEEN RIBS 19 AND 20. THE AFFECTED AREA WAS TRIMMED IAW SRM 57-49-01 /REPAIR 51P. THE FINAL DIMENSIONS AFTER REWORK EXCEED THE MINIMUM ALLOWABLE LIMITS. DUE TO IT, DET
- [SDR EE4Y2026102725128](https://openairdocs.org/sdr/EE4Y2026102725128.md): Pylon · cracked · Oct 27, 2026 · N306JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > PERFORMED REPAIR TO A CRACK LOCATED LT AND RT PYLONS SUPPORT SEALS 190-03266-00X INBOARD AND OUTBOARD IAW EMB ETD2025-190-001674 REV. A DTD MAY 26 2025 AND DOCUMENTED PER COOPESA EO #COO-EO-2026-25076-R00 DTD OCT 11 2026. JOB A1Q358, ITEM 21-49
- [SDR EE4Y2026102625126](https://openairdocs.org/sdr/EE4Y2026102625126.md): Frame · damaged · Oct 26, 2026 · N397NC · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING THE MAINTENANCE PROCESS THE FRAME 10 INBOARD FLANGE WAS DAMAGED BETWEEN STRINGER 12LH AND STRINGER 13LH. DUE TO IT, A PROPOSED REPAIR LAYOUT HAS BEEN DEVELOPED TO RESTORE THE DAMAGED AREA AND WAS SENT TO EMB FOR APPROVAL. EMB APPROVED THE PROPOSAL REPAI
- [SDR EE4Y2026102325124](https://openairdocs.org/sdr/EE4Y2026102325124.md): Doubler · dented · Oct 23, 2026 · N328 · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE STRUCTURE INSPECTION WAS FOUND DOUBLER DENTED LOCATED IN THE UPPER CENTER FUSELAGE I BTWN FR23+350MM / FR24+165MM BTWN S-13L/16L. DUE TO IT, THIS CONDITION WAS REPAIRED IAW SRM PART II 53-21-01 REPAIR 62 PARAG. 4 FIG. 4, 201 AND PER 51-75-12 PARAG.
- [SDR EE4Y2026100525064](https://openairdocs.org/sdr/EE4Y2026100525064.md): Heat Shield · cracked · Oct 5, 2026 · N306JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > DURING INSPECTION, IT WAS NOTED THAT ENGINE #1 PYLON AFT FAIRING HEAT SHIELD SKIN #8 HAD AN EXISTING REPAIR AT THE AFT LOWER CORNER OF THE EXHAUST GRILL CUTOUT. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR LACKS MATERIAL TRACEABILITY. CONSEQUENTLY, IT W
- [SDR EE4Y2026100525063](https://openairdocs.org/sdr/EE4Y2026100525063.md): Link · corroded · Oct 5, 2026 · N306JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > DURING THE ACCOMPLISHMENT OF REF. A, THE PYLON LOWER LINK FITTING OUTBOARD LUG FIXED BUSHINGS WERE FOUND WITH WEAR. AFTER REMOVAL OF THE BUSHINGS FOR REPLACEMENT, LOCALIZED CORROSION WAS DETECTED BETWEEN THE LUG SURFACE AND THE PRODUCTION REINFORCEMENT ANGLE.
- [SDR EE4Y2026090824949](https://openairdocs.org/sdr/EE4Y2026090824949.md): Thrust Reverser · scratched · Sep 8, 2026 · N306JB · Emb ERJ190100IGW · Powerplant System
  > DURING THE CURRENT MAINTENANCE A DEFECT WAS REPORTED IN COMPONENT T/R OUTBD P/N: 601E0100-542, S/N: MR-ER-0575. VERIFIED THE WEAR AT 37.83MM FROM THE REAR EDGE AND FOUND OUT LIMITS BECAUSE IT EXCEEDS 50% OF THICKNESS. DUE TO THIS, WAS QREPAIRED IAW ETD2026-190
- [SDR 2026FA0000686](https://openairdocs.org/sdr/2026FA0000686.md): Thrust Reverser · scratched · Sep 8, 2026 · N306JB · Emb ERJ190100IGW · Engine Thrust Reverser
  > DURING THE CURRENT MAINTENANCE A DEFECT WAS REPORTED IN COMPONENT 601E0001-525 SN MR-ER-0574. VERIFIED THE WEAR AT 37MM FROM THE REAR EDGE AND FOUND OUT LIMITS BECAUSE IT EXCEEDS 50% OF THICKNESS. DUE TO THIS, WAS QREPAIRED IAW ETD2026-190-014032 DTD AUG 17 2
- [SDR EE4Y2026090824946](https://openairdocs.org/sdr/EE4Y2026090824946.md): Rib · cracked · Sep 8, 2026 · N306JB · Emb ERJ190100IGW · Aerodynamic Fairings
  > DURING THE INSPECTION, WAS FOUND IN THE LT WING TO FUSELAGE FAIRING AT FR52 THE RIB CRACKED, DUE TO THIS, WAS PERFORMED A PERMANENT REPAIR IAW ETD2016-190-054721 DTD JUN 10 2016 AND DOCUMENTED UNDER COOPESA EO # COO-EO-2026-24815-R00 DTD AUG 03 2026. JOB A1Q35
- [SDR BAGA2027072700001](https://openairdocs.org/sdr/BAGA2027072700001.md): Power Supply · failed · Jul 24, 2026 · N128BZ · Emb ERJ190100IGW · Emergency Lighting
  > FLIGHT DECK EMERGENCY LIGHT DOES NOT COME ON WHEN THE EMERGENCY LIGHTS ARE SELECTED ON. REMOVED AND REPLACED THE FWD RH ELPU.
- [SDR BAGA2026061800004](https://openairdocs.org/sdr/BAGA2026061800004.md): Downlock · sheared · Jun 18, 2026 · N116BZ · Emb ERJ190100IGW · Landing Gear Position and Warning
  > DURING LANDING ROLLOUT LANDING GEAR AURAL WARNING SOUNDED ACCOMPANIED BY UNSAFE INDICATION OF RIGHT MAIN GEAR, LG LEVER DISAG WARNING ANNUNCIATION, AND LG NO DISPATCH CAUTION ANNUNCIATION. PULLED CLEAR OF RUNWAY AND CALLED MECHANIC TO INSPECT GEAR BEFORE TAXII
- [SDR EE4Y2026061224637](https://openairdocs.org/sdr/EE4Y2026061224637.md): Electrical Box · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Electrical Power System
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA THROUGH THE
- [SDR EE4Y2026061224636](https://openairdocs.org/sdr/EE4Y2026061224636.md): Unknown · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Standard Practices/Structures
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA BY THE FORWA
- [SDR EE4Y2026061224635](https://openairdocs.org/sdr/EE4Y2026061224635.md): Unknown · fire · Jun 12, 2026 · N309JB · Emb ERJ190100IGW · Standard Practices/Structures
  > A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO BAY NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA BY THE FWD CARGO BAY USING FIRE EXTINGUISHER. VISU
- [SDR EE4Y2026061124632](https://openairdocs.org/sdr/EE4Y2026061124632.md): Electrical Box · fire · Jun 11, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. FROM THE MOMENT THE SPARK AND FIRE BEGAN TO THE INITIATION OF COOPESA’S EM
- [SDR EE4Y2026061124630](https://openairdocs.org/sdr/EE4Y2026061124630.md): Electrical Box · fire · Jun 11, 2026 · N309JB · Emb ERJ190100IGW · Electrical Power System
  > COOPESA REPORTS THAT A FIRE OUTBREAK OCCURRED INSIDE THE FORWARD FUSELAGE, SPECIFICALLY WITHIN THE FORWARD CARGO COMPARTMENT NEAR THE INTERNAL SIDE OF THE EXTERNAL AC POWER RECEPTACLE. THE COOPESA EMERGENCY RESPONSE TEAM ACCESSED THE AFFECTED AREA THROUGH THE
- [SDR BAGA2026052600006](https://openairdocs.org/sdr/BAGA2026052600006.md): Power Supply · no test · May 24, 2026 · N115BZ · Emb ERJ190100IGW · Emergency Lighting
  > FWD LT EMERGENCY LIGHT BATTERY FAILED TO TEST. EMERGENCY LIGHTS ILLUMINATING WHEN THE AIRCRAFT IS POWERED DOWN AND EMER LT SWITCH IS IN THE OFF POSITION. REPLACED THE LT FWD ELPU PER AMM.
- [SDR BAGA2026052600005](https://openairdocs.org/sdr/BAGA2026052600005.md): Power Supply · no test · May 24, 2026 · N115BZ · Emb ERJ190100IGW · Emergency Lighting
  > LEFT MIDDLE ELPU FAILED TO TEST. EMERGENCY LIGHTS ILLUMINATING WHEN THE AIRCRAFT IS POWERED DOWN AND EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. REPLACED THE LT MIDDLE ELPU IAW AMM.
- [SDR BAGA2026062300005](https://openairdocs.org/sdr/BAGA2026062300005.md): Battery · failed · May 13, 2026 · N110BZ · Emb ERJ190100IGW · Emergency Lighting
  > HEAVY CHECK, LOWER FUSELAGE MID RH EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY BATTERY.
- [SDR EE4Y2026051324480](https://openairdocs.org/sdr/EE4Y2026051324480.md): Skin · corroded · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING THE STRUCTURAL INSPECTION, CORROSION SPOTS WERE FOUND ON THE EXTERNAL SKIN SURFACE BETWEEN FR16-17, AND BETWEEN STRINGERS 26R-27R, AROUND THE ANTENNA CUT-OUT AREA. THE CORROSION WAS REMOVED BY BLEND-OUT IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMEN
- [SDR EE4Y2026051324479](https://openairdocs.org/sdr/EE4Y2026051324479.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR03 AND Y=25MM, SEE FIGURE 1. SINCE THE DAMAGE DEPTH EXCEEDED 50% OF THE SKIN THICKNESS, IT WAS REMOVED BY DRILLING THROUGH THE SKIN ONLY. AFTER REMOVING THE FRAME PRODUCTION FAST
- [SDR EE4Y2026051324478](https://openairdocs.org/sdr/EE4Y2026051324478.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Passenger/Crew Doors
  > DURING THE STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND AT THE FORWARD AREA OF THE LH MLG DOOR SKIN. SINCE THE PREVIOUS OPERATOR DID NOT PROVIDE REPAIR RECORDS, THE REPAIR WAS REMOVED. AFTER REMOVAL, A SKIN CUTOUT WAS IDENTIFIED. THE SRM WAS CONSULTED
- [SDR EE4Y2026051324477](https://openairdocs.org/sdr/EE4Y2026051324477.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > CUSTOMER REPORTS A LIGHTNING STRIKE DAMAGE AFFECTING THE FORWARD FUSELAGE SKIN, LOCATED AT FR19 + 292 MM, STRG22R + 17 MM. A REPAIR CANNOT BE PERFORMED IN ACCORDANCE WITH ERJ190 SRM PART II, 531001, AD53 BECAUSE THE DISTANCE BETWEEN THE DAMAGE AND THE ADJACENT
- [SDR EE4Y2026051324476](https://openairdocs.org/sdr/EE4Y2026051324476.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > THIS JOB WAS PERFORMED BY CUSTOMER REQUEST TO REDO EXISTING REPAIR LOCATED AT WING MAIN BOX - RH WING MAIN BOX LOWER SKIN AT RIB-JACKING FITTING. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS PER E
- [SDR EE4Y2026051324474](https://openairdocs.org/sdr/EE4Y2026051324474.md): Skin · temp repair · May 13, 2026 · N309JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > THIS JOB IS PERFORMED BY CUSTOMER REQUEST, TO REDO AN EXISTING REPAIR LOCATED AT WING MAIN BOX - CRACK FOUND L/H WING LOWER SKIN AFT EDGE BTW RIB 9-10. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS
- [SDR EE4Y2026051324470](https://openairdocs.org/sdr/EE4Y2026051324470.md): Skin · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > AN EXISTING BLEND-OUT WAS IDENTIFIED AT FR78 + 290 MM, BETWEEN STRINGERS 27R-28R. THE BLEND-OUT WAS PERFORMED IN ACCORDANCE WITH SRM PART II 51-10-03, TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE BLEND-OUT EXCEEDS THE LIMITS SPECIFIED IN SRM PART II 53
- [SDR EE4Y2026051324469](https://openairdocs.org/sdr/EE4Y2026051324469.md): Crossbeam · damaged · May 13, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > THIS REPORT IS PERFORMED BY CUSTOMER REQUEST TO PERFORM EXISTING REPAIR LOCATED AT THE CENTER FUSELAGE II - CROSS BEAM AT FR57 WITH TOOL MARK. THIS CONDITION REPORTED WAS REPAIRED IAW ETD2017-190-026630 REV. A DTD APR 06 2017 AND DOCUMENTED UNDER COOPESA EO CO
- [SDR BAGA2026051500003](https://openairdocs.org/sdr/BAGA2026051500003.md): Windshield · failed · May 8, 2026 · N115BZ · Emb ERJ190100IGW · Flight Compartment Windows
  > FO WINDSHIELD SHATTERED DURING CLIMB. REMOVED AND REPLACED WINDSHIELD.
- [SDR BAGA2026051100001](https://openairdocs.org/sdr/BAGA2026051100001.md): Power Supply · failed · May 7, 2026 · N116BZ · Emb ERJ190100IGW · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAULOT, RH CTR ELPU HARD FAULTED CAUSING SOME OF THE EMERGENCY LIGHTS TO TURN ON AND OFF UNCOMMANDED. REPLACED THE RH CTR ELPU.
- [SDR BAGA2026062300006](https://openairdocs.org/sdr/BAGA2026062300006.md): Battery · failed · Apr 30, 2026 · N110BZ · Emb ERJ190100IGW · Emergency Lighting
  > HEAVY CHECK, UPPER FUSELAGE PAX CABIN EXIT MARKER LT & RT EMERGENCY LIGHT INOP. REPLACE ELPU NR 3.
- [SDR EE4Y2026042524380](https://openairdocs.org/sdr/EE4Y2026042524380.md): Structure · fire · Apr 25, 2026 · N309JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING AIRCRAFT PREPARATION FOR MAINTENANCE, THERE WAS A FIRE OUTBREAK IN THE CARGO COMPARTMENT COMMON TO THE INTERNAL AREA OF THE EXTERNAL POWER RECEPTACLE. THIS CONDITION WAS REPORTED TO EMB. FOR ADDITIONAL DETAILS SEE JOB A1Q349 ITEM 997-6.5
- [SDR BAGA2026042700006](https://openairdocs.org/sdr/BAGA2026042700006.md): Battery Pack · failed · Apr 24, 2026 · N126BZ · Emb ERJ190100IGW · Emergency Lighting
  > EMERGENCY LIGHTS FLICKERING ON AND OFF IN ARMED PPOSITION. EMERGENCY LIGHTS ALSO TURNED ON AFRTER AIRCRAFT WAS POWERED DOWN WITH SWITCH IN OFF POSITION. ERMER LT BATT FAULT EICAS INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT NR 4.

Next page: https://openairdocs.org/model/embraer-erj-190-100-igw/reports.md?page=2

## 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 = 'ERJ190100IGW'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-erj-190-100-igw/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.