# Service difficulty reports: N304JB, cancelled Jun 8, 2026 A list on [N304JB, cancelled Jun 8, 2026](https://openairdocs.org/deregistered/N304JB-2026-06-08.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 77 reports - [SDR EE4Y2026030924077](https://openairdocs.org/sdr/EE4Y2026030924077.md): Rib · corroded · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead > DURING A STRUCTURAL INSPECTION, CORROSION WAS FOUND AT A FASTENER HOLE LOCATED ON THE LH WINGLET LOWER SURFACE, AT THE SUPPORT STRUCTURE OF ACCESS PANEL 551AB, SEE FIGURE 1 FOR DAMAGE OVERVIEW. THE AFFECTED FASTENER HOLE INVOLVES BOTH THE WING SPAR II AND WING - [SDR EE4Y2026030924076](https://openairdocs.org/sdr/EE4Y2026030924076.md): Skin · damaged · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > CUSTOMER REPORTS TWO LIGHTNING STRIKE DAMAGES AFFECTING THE CENTER FUSELAGE I SKIN, LOCATED AT FR33 + 242 MM (DAMAGE #1) AND FR33 + 394 MM (DAMAGE #2) ON STR 26L. DAMAGE #1 WAS COMPLETELY REMOVED BY BLEND-OUT. DAMAGE #2, DEPTH EXCEEDED 50% OF THE SKIN THICKNES - [SDR EE4Y2026030924075](https://openairdocs.org/sdr/EE4Y2026030924075.md): Skin · damaged · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > DURING THE STRUCTURAL INSPECTION, DAMAGE CAUSED BY A LIGHTNING STRIKE WAS FOUND ON THE EXTERNAL SKIN OF THE CENTER FUSELAGE I, AT FR24 + 327MM, STR-27LH + 8MM. AFTER PERFORMING A LIGHT BLEND-OUT, IT WAS DETERMINED THAT IN A POINT, THE DAMAGE EXCEEDED 50% OF TH - [SDR EE4Y2026030924074](https://openairdocs.org/sdr/EE4Y2026030924074.md): Skin · cracked · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Wing, Plate/Skin > CRACKS (2EA) AND ONE ELONGATED HOE WERE FOUND AFFECTING THE LH WING LOWER SKIN AFT SPAR 2 BTWN RIB 10/11. SRM PART II 57-10-01 REP. 54 WAS EVALUATED. THE CRACK #1 IS NOT REPAIRABLE DUE TO THE LOCATION OF THE CRACK AND CRACK #2 IS REPAIRABLE PER SRM AND THE ELO - [SDR EE4Y2026030924073](https://openairdocs.org/sdr/EE4Y2026030924073.md): Doubler · misinstalled · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > DURING STRUCTURAL INSPECTION, THE CUSTOMER FOUND AN EXTERNAL REPAIR DOUBLER AT FR74 + 105 MM AND STR 24L + 85 MM, REPORTEDLY INSTALLED IN ACCORDANCE WITH EMB IC2009-190/05358C DATED 09-JUL-2009. ONCE THE AVAILABLE DOCUMENTATION LACKED ESSENTIAL INFORMATION, TH - [SDR EE4Y2026030924072](https://openairdocs.org/sdr/EE4Y2026030924072.md): Skin · damaged · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > WAS REPORTED THAT DURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS IDENTIFIED AT FR32 AND JUST ABOVE STR-26LH. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DET - [SDR EE4Y2026030924071](https://openairdocs.org/sdr/EE4Y2026030924071.md): Skin · damaged · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > DURING THE STRUCTURAL INSPECTION, AN EXISTING BLEND-OUT WAS FOUND IN THE CENTER FUSELAGE III LOWER SKIN BETWEEN FRAMES 86-87 AND STRINGERS 27R-28R. SINCE NO PREVIOUS RECORD OF THIS BLEND-OUT EXISTS, IT WAS INSPECTED AND EVALUATED. THE CONDITION WAS FOUND TO BE - [SDR EE4Y2026030924069](https://openairdocs.org/sdr/EE4Y2026030924069.md): Skin · damaged · Mar 9, 2026 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > CUSTOMER REPORTS LIGHTNING STRIKE DAMAGE AFFECTING THE CENTER FUSELAGE III SKIN, LOCATED AT FR74 AND STR 28L. THE DAMAGE WAS REMOVED BY BLENDING THE AFFECTED AREA IN ACCORDANCE WITH SRM 51-10-03, BLEND-OUT TYPE D. AFTER EVALUATION, IT WAS DETERMINED THAT THE B - [SDR YENA2023041300352](https://openairdocs.org/sdr/YENA2023041300352.md): Unknown · unknown · Apr 11, 2023 · N304JB · Emb ERJ190100IGW · Wing, Control Surfaces > DURING HEAVY MAINTENANCE: LH WING TE AREA, LOWER SKIN HAS 2 EACH CRACK O/B PYLON; REF: TOMX W/O 2191 NR-00014 REPAIRED PER ETI-190-23-535 REV 3 AND ETD-2023-190-008554 REV B. NO SPECIFIC OR ADDITIONAL INSPECTIONS ARE NECESSARY. TOMX MECH 10000726 INSP 325718. - [SDR YENA2023041300351](https://openairdocs.org/sdr/YENA2023041300351.md): Unknown · unknown · Apr 11, 2023 · N304JB · Emb ERJ190100IGW · Wing Main, Frame Structure > DURING HEAVY MAINTENANCE: WINGS/ LH WING MAIN BOX / TRAILING EDGE LOWER SKIN AT AFT SPAR 2 BETWEEN RIB 10 AND RIB 11/ CRACK AND ELONGATED HOLES - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR) - [SDR YENA2022051700493](https://openairdocs.org/sdr/YENA2022051700493.md): Skin · damaged · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, PROTUBERANCE EXTERNAL SKIN FR 30-31 STR 26-27; MAJOR REPAIR REF TOMX NR 1894-00330 - EVALUATED AND REPAIRED PROTUBERANCE IAW EMB 190 SRM 53-21-01/AD52, SRM 53-21-01/R62P, 51-75-13 PAR. 5 AND SRM 51-75-00F. - [SDR YENA2022051700491](https://openairdocs.org/sdr/YENA2022051700491.md): Skin · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin > DURING HEAVY MAINTENANCE, CORROSION ON INTERNAL SKIN BTW FR86/FR87 AND STGR 29L/28L; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. PER EMB 190 SRM 53-23-01/ADS51. PERFORMED REPAIR PER EC E22-324-01, ETI 190-22-561 REV 6 AND EDT2022-190-015055 REVD. WOR - [SDR YENA2022051700489](https://openairdocs.org/sdr/YENA2022051700489.md): Finger Doubler · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR77/78, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. REMOVED AND REPLACED FINGER PLATE PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/ AD53, 51-43-01 AND 51- - [SDR YENA2022051700490](https://openairdocs.org/sdr/YENA2022051700490.md): Finger Doubler · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION ON FINGER PLATE AT AFT CARGO DOOR CUTOUT BTW FR79/80, STGR 27R/28R; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. REMOVED AND REPLACED FINGER PLATE PER EMB 190 SRM 51-12-01, 51-10-01, 53-23-11/AD53, 51-43-01, AND 51- - [SDR YENA2022051700488](https://openairdocs.org/sdr/YENA2022051700488.md): Seal Rest · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION ON LWR CENTRAL SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION, EVALUATED AND FOUND OUT OF LIMITS. REMOVED AND REPLACED CENTRAL SEAL REST PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/AD52 AND 51-41-01. WORK ACCOMPLISHE - [SDR YENA2022051700487](https://openairdocs.org/sdr/YENA2022051700487.md): Seal Rest · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure > DURING HEAVY MAINTENANCE, CORROSION ON LOWER FORWARD SEAL REST AT AFT CARGO DOOR CUTOUT; REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FWD SEAL REST PER EMB 190 SRM 51-12-01, 51-10-03, 53-23-11/AD52 AND 51-40-08. WORK ACCOMPLISHED ON TO - [SDR YENA2022051700486](https://openairdocs.org/sdr/YENA2022051700486.md): Skin · corroded · May 16, 2022 · N304JB · Emb ERJ190100IGW · Fuselage Internal Stairs > DURING HEAVY MAINTENANCE, FUSELAGE / CENTER FUSELAGE III / LOWER SKIN / BTW FR86 - FR87 AND STGR 29LH - 29RH / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR). - [SDR YENA2022030900132](https://openairdocs.org/sdr/YENA2022030900132.md): Controller · failed · Mar 7, 2022 · N304JB · Emb ERJ190100IGW · Pneumatic System > FLT#384, MCO-MCO.'BLEED 2 LEAK CLIMBING THROUGH FL 290; PER FIM 36-21-00-810-804-A PERFORMED BLEED LEAK CHECK ON ENG #2 NO LEAK NOTED INSPECTION ODS LOOP ELECTRICAL CONNECTOR NO FOUND CONTAMINATION AND FAILURE NEXT STEP REMOVED AND REPLACED AMS CONTROLLER PROC - [SDR YENA2021121300837](https://openairdocs.org/sdr/YENA2021121300837.md): Clamp · migrated · Dec 11, 2021 · N304JB · Emb ERJ190100IGW · Pneumatic Indicating System > FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTACT WITH PYLON STRUCTURE. PERFORMED ESPM REPAIR 20-41-20ON PIGTAIL AND RESECURED CLAMP AS REQUIRED. FO - [SDR YENA2021121300836](https://openairdocs.org/sdr/YENA2021121300836.md): Clamp · migrated · Dec 11, 2021 · N304JB · Emb ERJ190100IGW · Pneumatic Indicating System > FLT 940, SRQ-BOS(DIVERTED TO MCO). BLEED 2 LEAK QRH COMPLETED; T/S PER FIM 36-11-10 FOUND MIGRATED SUPPORT CLAMP ALLOWING PIGTAIL J2148 OF LOOP 5 TO MAKE CONTACT WITH PYLON STRUCTURE. PERFORMED ESPM REPAIR 20-41-20ON PIGTAIL AND RESECURED CLAMP AS REQUIRED. FO - [SDR YENA2021010700010](https://openairdocs.org/sdr/YENA2021010700010.md): Power Supply · no test · Jan 3, 2021 · N304JB · Emb ERJ190100IGW · Emergency Lighting > DURING HEAVY MAINTENANCE, ELPU NR 2 FAILED OPERATIONS CHECK. R & R ELPU NR 2, IAW AMM 33-50-01-000-801-A AND 33-50-01-801-A. REF TO MX NR 00033. - [SDR YENA2019062720344](https://openairdocs.org/sdr/YENA2019062720344.md): Power Supply · failed · Jun 22, 2019 · N304JB · Emb ERJ190100IGW · Emergency Lighting > FT # 2167, RH AFT OVERWING EMERGENCY LIGHT INOP; REMOVED AND REPLACED ELPSU # 4 IAW AMM 33-50-01 OPS CHECK NORMAL. - [SDR YENA201901050012](https://openairdocs.org/sdr/YENA201901050012.md): Repair · corroded · Jan 5, 2019 · N304JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON (141-57) CENTER FUSELAGE III FLOOR STRUCTURE, CORROSION FOUND ON PREVIOUS SEAT TRACK REPAIR BTW FR 84-85 AND LBL 11''; REF NRC 4000173-2000-0173, SEAT TRACK REPAIR BTW FR 84-85 AND LBL11'' IAW SRM II 53-23- - [SDR YENA201803240150](https://openairdocs.org/sdr/YENA201803240150.md): Shear Panel · corroded · Mar 24, 2018 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA MIDDLE SHEAR PANEL AT FRAME 87 - 88. REPLACED THE SHEAR PANEL IAW SRM IAW 51-42-01, AND 51-42-03, REV 37. - [SDR YENA201803240149](https://openairdocs.org/sdr/YENA201803240149.md): Floor Panel · corroded · Mar 24, 2018 · N304JB · Emb ERJ190100IGW · Fuselage Floor Panel > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT WET AREA FLOOR PANEL CORRODED AT FRAME 78. REPLACED THE FLOOR PANEL IAW SRM 51-42-01, AND 51-42-03. - [SDR YENA201702020057](https://openairdocs.org/sdr/YENA201702020057.md): Pump · failed · Feb 2, 2017 · N304JB · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), Main > FLIGHT CREW REPORTED EDP 2 FAIL FOLLOWED BY COMPLETE LOSS OF NR 2 HYDRAULIC SYSTEM. DIVERTED. EMERGENCY DECLARED. REPLACED NR 2 ENGINE EDP HYDRAULIC PUMP IAW AMM 29-11-01. PERFORMED OPS CHECK. OPS CHECK TEST PASSED. - [SDR YENA20160510445](https://openairdocs.org/sdr/YENA20160510445.md): Frame · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Main, Frame > DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 17, RBL 8.5"; CORROSION WAS REMOVED AND 2 L SHAPED REINFORCEMENT ANGLES WERE INSTALLED, REF E16-346-01. - [SDR YENA20160510444](https://openairdocs.org/sdr/YENA20160510444.md): Frame · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Main, Frame > DURING MAINTENANCE AT HEAVY CHECK BS, CORROSION WAS FOUND ON FRAME 14 RBL 23"; CORROSION WAS R & R DOUBLERS WERE INSTALLED. - [SDR YENA20160510443](https://openairdocs.org/sdr/YENA20160510443.md): Frame · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Main, Frame > DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON FRAME 14 RBL 15.5; CORROSION WAS REMOVED AND REPAIRED DOUBLERS WERE INSTALLED. - [SDR YENA20160510442](https://openairdocs.org/sdr/YENA20160510442.md): Seat Track · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings > DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FR84, RBL 10". REFERENCE EAMS NR 00187, CORROSION WAS REMOVED. NEW DOUBLER WAS FABRICATED AND INSTALLED. - [SDR YENA20160510441](https://openairdocs.org/sdr/YENA20160510441.md): Seat Track · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings > DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK BEAM FRAME 84, RBL 12", CORROSION WAS REMOVED. NEW DOUBLER WAS FABRICATED AND INSTALLED. - [SDR YENA20160510440](https://openairdocs.org/sdr/YENA20160510440.md): Seat Track · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings > DURING MAINTENANCE AT HEAVY CHECK STATION, CORROSION WAS FOUND ON RT SEAT TRACK AT THE GALLEY MOUNT BETWEEN FRAMES 13-14 IN THE FWD CABIN. CORROSION WAS R & R WITH A DOUBLER/STRAP AND FILLER INSTALLATION. - [SDR YENA20160510439](https://openairdocs.org/sdr/YENA20160510439.md): Frame · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Main, Frame > DURING MAINTENANCE, CORROSION WAS FOUND ON FRAME 17, 8" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES, REF E16-346-01. - [SDR YENA20160510438](https://openairdocs.org/sdr/YENA20160510438.md): Frame · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Main, Frame > DURING MAINTENANCE, CORROSION WAS FOUND ON FR 17, 7" LBL; REMOVED ALL CORROSION BY BLENDING AND CUTTING ALL AREAS. INSTALLED 2 L SHAPED REINFORCEMENT ANGLES REF E16-346-01. - [SDR YENA20160510437](https://openairdocs.org/sdr/YENA20160510437.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR87, LBL 44". REF EAMS NR 00179; REMOVED CORROSION AND REPLACED LT SUPPORT PANEL, REF SRM 51-10-03 AND SRM 51-75-16. - [SDR YENA20160510436](https://openairdocs.org/sdr/YENA20160510436.md): Floor Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON FLOOR SUPPORT 6" AFT FRAME 15, 45" LBL. REF EAMS NR 00199. REPLACED FLOOR SUPPORT. REF SRM 51-43-03. - [SDR YENA20160510435](https://openairdocs.org/sdr/YENA20160510435.md): Shear Plate · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA CENTER SHEAR PANEL 5" AFT FR87, LBL 4"; REPLACED CENTER SHEAR PANEL. REF SRM 51-42-01, 51-23-06. - [SDR YENA20160510434](https://openairdocs.org/sdr/YENA20160510434.md): Gusset · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT GUSSET PLATE FR 90, RBL 24, REPLACED GUSSET IAW SRM 51-41-02. - [SDR YENA20160510433](https://openairdocs.org/sdr/YENA20160510433.md): Seat Track · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SEAT TRACK FR 87, RBL 12. SEAT TRACK REPLACED IAW SRM 51-41-01, 51-42-01, AND 51-43-03. - [SDR YENA20160510432](https://openairdocs.org/sdr/YENA20160510432.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 89, RBL 43"; REPLACED PANEL SUPPORT. REF SRM 51-41-02, 51-43-01. - [SDR YENA20160510431](https://openairdocs.org/sdr/YENA20160510431.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA LT PANEL SUPPORT FR90, LBL 42". REPLACED PANEL SUPPORT REF SRM 51-41-01, 5141-02, 51-42-02, 51-43-03. - [SDR YENA20160510430](https://openairdocs.org/sdr/YENA20160510430.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FRAME 84, RBL 24", REPLACED PANEL REF SRM 51-41-02, 51-43-04. - [SDR YENA20160510429](https://openairdocs.org/sdr/YENA20160510429.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT PANEL SUPPORT FR 84, RBL 42". REF EAMS NR 00193. REPLACED PANEL REF SRM 51-41-02, 51-43-04. - [SDR YENA20160510428](https://openairdocs.org/sdr/YENA20160510428.md): Support · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT WET AREA RT SUPPORT PANEL FR 84, RBL 24". REF EAMS NR 00192, REPLACED PANEL. REF SRM 51-41-02, 51-42-02, 51-43-04, 51-23-06. - [SDR YENA20160510427](https://openairdocs.org/sdr/YENA20160510427.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 20 49" RBL. UAW EAMS NR 00221. REPLACED SILL REF SRM 51-41-02. - [SDR YENA20160510426](https://openairdocs.org/sdr/YENA20160510426.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 13.5" AFT, FR19, 49" RBL. REF EAMS NR 00220. REPLACED SILL REF SRM 51-41-02. - [SDR YENA20160510425](https://openairdocs.org/sdr/YENA20160510425.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 11" AFT FRAME 18, RBL 49". REF EAMS NR 00219, REPLACED SILL, REF SRM 51-41-02. - [SDR YENA20160510424](https://openairdocs.org/sdr/YENA20160510424.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON FWD RT SILL 8" AFT FR13, 49" RBL. REF EAMS NR 00209. REPLACED SILL. REF SRM 51-41-02. - [SDR YENA20160510423](https://openairdocs.org/sdr/YENA20160510423.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL FRAME 17, 42.5" RBL. REF EAMS NR 00215, REPLACED SILL. REF SRM 51-42-01. - [SDR YENA20160510422](https://openairdocs.org/sdr/YENA20160510422.md): Structure · corroded · May 10, 2016 · N304JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure > DURING MAINTENANCE, CORROSION WAS FOUND ON AFT RT SILL 1.5" AFT FR 17, 48" RBL. REF EAMS NR 00216, REPLACED AFT RT SILL REF SRM 51-41-02. Next page: https://openairdocs.org/deregistered/N304JB-2026-06-08/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 n_number = 'N304JB' AND deregistration_id = 'N304JB-2026-06-08' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N304JB-2026-06-08/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.