# Service difficulty reports: N294JB, cancelled Dec 9, 2025

A list on [N294JB, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N294JB-2025-12-09.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 · 54 reports

- [SDR YENA2021021900121](https://openairdocs.org/sdr/YENA2021021900121.md): Floor Support · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E2190/B6 CHECK N/R 00391- CORROSION ON FLOOR SILL BTW FR88/FR90 AND LBL 35" AT INTERNAL FLOOR STRUCTURE; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R FLOOR SILL BTW FR88/FR90 AND LBL 35" WAS REPLACED PER EMB-190-SRM-51-42-0
- [SDR YENA2021021900120](https://openairdocs.org/sdr/YENA2021021900120.md): Shear Tie · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00482-CPCP FINDING: CORROSION ON SHEAR CLIP OF FR67 BETWEEN STGR 29R AND 28R.; PER TOMX N/R N294JB/1495/B6 CHECK N/R 00482 - SHEAR CLIP WAS REPLACED PER EMB-190-SRM 51-41-02
- [SDR YENA2021021900119](https://openairdocs.org/sdr/YENA2021021900119.md): Shear Tie · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00506 - CORROSION ON SHEAR CLIP OF FR89 BETWEEN STGR23L AND STGR25L; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00506 - SHEAR CLIP REPLACED PER EMB-190-DWG 170-66658-001, SRM 51-41-02 AND SRM 51-43-03
- [SDR YENA2021021900118](https://openairdocs.org/sdr/YENA2021021900118.md): Seal Rest · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HMV, REF. TOMX N/R N249JB/1495/E190/B6 CHECK N/R 00412 - CPCP FINDING CORROSION ON SEAL REST 3 EA ON AFT DOOR CUTOUT STRUCTURE; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00412-CORROSION WAS REMOVED SEAL REST AFT, CENTER AND FWD, BLEND OUT OF AFT IS W
- [SDR YENA2021021900117](https://openairdocs.org/sdr/YENA2021021900117.md): Doubler · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00429 - CORROSION ON DOUBLER ON FLOOR STRUCTURE BTW FR87 AND FR88 LBL 42.; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R N294JB/1495/E190/B6 CHECK N/R 00429-DOUBLER REPLACED PER EMB-190 SRM 53-23-10 FIG. 55
- [SDR YENA2021021900116](https://openairdocs.org/sdr/YENA2021021900116.md): Doubler · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Floor Panel
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00430-CORROSION ON DOUBLER ON FLOOR STRUCTURE BTW FR87 AND FR88 RBL42; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00430 - DOUBLER REPLACED PER EMB-190-SRM 51-42-02 PAR 4, FIG 1 AND PAR5 FIG 2.
- [SDR YENA2021021900115](https://openairdocs.org/sdr/YENA2021021900115.md): Web · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00458-CORROSION ON WEB BTW FR84 AND FR85 Y=+340 TO Y=+1200.; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00458 - NEW WEB REPLACED PER EMB-190-SRM 51-41-02 PAR 6, FIG 2 AND SRM 51-41-01 PAR 6 FIG.2.
- [SDR YENA2021021900114](https://openairdocs.org/sdr/YENA2021021900114.md): Skin · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · APU Cowling/Containment
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00624 - AFTER REMOVAL OF FIRE SEALANT AT APU COMPARTMENT, FWD EDGE CORROSION ON STRUCTURE.; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00624 - PANEL SKIN BOTTOM REPLACED PER EMB-190-SRM 51-41-01 PAR 6, S
- [SDR YENA2021021900113](https://openairdocs.org/sdr/YENA2021021900113.md): Plate · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00460-CORROSION ON PLATE BETWEEN FR84 AND FR85 Y=-670; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00460-CORROSION ON PLATE WAS REMOVED THEREFORE IS OUT OF LIMITS, PLATE WAS REPLACED PER EMB-190-SRM 51-43
- [SDR YENA2021021900112](https://openairdocs.org/sdr/YENA2021021900112.md): Structure · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00561 - AFTER CLEAN AREA FUSELAGE 3 FINDINGS CORROSION BTW FR86 AND FR87 STGR27 AND STGR28 BELOW WATER TANK.; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00561 - ANGLES AND INTERCOSTAL REPLACED PER EMB-19
- [SDR YENA2021021900111](https://openairdocs.org/sdr/YENA2021021900111.md): Plate · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HMV, REF. TOMX N/R N294JB/1495/E90/B6 CHECK N/R 00490 - CORROSION ON PLATE CLOSING OF FWD CARGO DOOR SURROUNDING STRUCTURE CENTER FUSELAGE I; PER TOMX N/R N294JB/1495/E190/B6 CHECK N/R 00490 - PLATE CLOSING WAS REPLACED PER EMB-190 SRM 51-40-08 PARAGRA
- [SDR YENA2021021900110](https://openairdocs.org/sdr/YENA2021021900110.md): Doubler · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Plate/Skin
  > DURING HMV, EC E21-098-01 FUSELAGE/CENTER FUSELAGE III - DOUBLER BETWEEN FRAMES 74- 75 AND STRINGERS 29L- 29R /CORROSION /PERMANENT REPAIR
- [SDR YENA2021021900109](https://openairdocs.org/sdr/YENA2021021900109.md): Stringer · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HMV, EC E21-072-01 FUSELAGE / CENTER FUSELAGE III / STRINGER 23L BTWN FR 89-90 / CORROSION - PERMANENT REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900108](https://openairdocs.org/sdr/YENA2021021900108.md): Rib · cracked · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Aerodynamic Fairings
  > DURING HMV, EC E21-021-01 FUSELAGE / CENTER FUSELAGE II / WING TO FUSELAGE FAIRING CENTER PANEL REAR RIB @ FR45 RH / CRACK - PERMANENT REPAIR. MAJOR REPAIR.
- [SDR YENA2021021900107](https://openairdocs.org/sdr/YENA2021021900107.md): Floorbeam · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Floor Beam
  > DURING HMV, EC E21-042-01 FUSELAGE / CENTER FUSELAGE III / FLOOR STRUCTURE BEAMS AT FR85 AND Y-273 & Y+273 / CORROSION - PERMANENT REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900106](https://openairdocs.org/sdr/YENA2021021900106.md): Structure · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > DURING HMV, EC E21-046-01 PYLONS / LH PYLON / UPPER SPARS AND REINFORCEMENTS / FWD & AFT LUGS / CORROSION DAMAGE – TIME LIMITED REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900105](https://openairdocs.org/sdr/YENA2021021900105.md): Frame · cracked · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Frame
  > DURING HMV, EC E21-030-01 FUSELAGE/ CFII RH WFF FR52/ CRACK- PERMANENT REPAIR. MAJOR REPAIR.
- [SDR YENA2021021900104](https://openairdocs.org/sdr/YENA2021021900104.md): Stringer · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > DURING HMV, EC E21-063-01 FUSELAGE/CENTER FUSELAGE III/ CORROSION ON STRINGER 14L BETWEEN FRAMES 89-90/ PERMANENT REPAIR /// THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2021021900103](https://openairdocs.org/sdr/YENA2021021900103.md): Structure · corroded · Feb 15, 2021 · N294JB · Emb ERJ190100IGW · Nacelle/Pylon, Main Frame
  > DURING HMV, PYLONS / RH PYLON / UPPER SPARS AND REINFORCEMENTS / FWD & AFT LUGS / CORROSION DAMAGE - PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR.
- [SDR YENA2020051830344](https://openairdocs.org/sdr/YENA2020051830344.md): Skin Panel · cracked · May 13, 2020 · N294JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 4; (REF AEROMAN NR 164208) ACCOMPLISHED REPAIR IAW AEROMAN EA57-0355-20 REV. O (COVER & PARTS 1-3), EMBRAER ETD 2020-190-0151501, AND JETBLUE EC NO. E20-443-01.
- [SDR YENA2020051830343](https://openairdocs.org/sdr/YENA2020051830343.md): Skin Panel · cracked · May 13, 2020 · N294JB · Emb ERJ190100IGW · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CRACK LOWER SKIN PANEL RH WING RIB 10; (REF AEROMAN NR 2020-164211) PERFORMED PERMANENT REPAIR IAW SRM 57-10-01 REPAIR 54P ITEM #9 FIG. 201 SHEET 6 TABLE 202. THIS REPAIR IS CAT ""A"" & NO FURTHER ACTION REQUIRED.
- [SDR YENA201901230041](https://openairdocs.org/sdr/YENA201901230041.md): Unknown · odor · Jan 23, 2019 · N294JB · Emb ERJ190100IGW · Air Distribution System
  > FLT 1887, ORH-MCO. LEVEL 1 TRANSIENT ODOR FLIGHT DECK ONLY, DURING LEVEL OFF AT 6,000FT N1 APPROX 33% LASTED APPROX 30 SEC. BURNING SMELL AND FO HAD MINOR EYE IRRITATION; C/W FIM TASK 21-20-00-810-801-A. NO ABNORMAL SMOKE/SMELL IN COCKPIT OR CABIN. RAN BOTH PA
- [SDR YENA201805270921](https://openairdocs.org/sdr/YENA201805270921.md): Door Sill · damaged · May 27, 2018 · N294JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, AN ELONGATED HOLE WAS DISCOVERED. REFER TO EC E18-425-01. FUSELAGE / CENTER FUSELAGE II / FLOOR STRUCTURE SILL FR42-43 & STR 17R / ELONGATED HOLE - PERMANENT REPAIR; THIS PERMANENT REPAIR IS APPROVED PER REF /2/ ETD AS CATEGORY A AND
- [SDR YENA201705230386](https://openairdocs.org/sdr/YENA201705230386.md): Wire Harness · defective · May 23, 2017 · N294JB · Emb ERJ190100IGW · Door System Wiring
  > THE FLIGHT CREW REPORTED VIA ARINC THAT THEY WERE GETTING AN INTERMITTENT AURAL WARNING IN FLIGHT. THE R1 DOOR INDICATION WAS ON MEL AND THE WARNINGS THAT THE DOOR IS OPEN IS INTERMITTENTLY ACTIVATING. THE CREW REPORTED THAT THE AURAL WARNINGS WERE A DISTRACTI
- [SDR YENA201701090024](https://openairdocs.org/sdr/YENA201701090024.md): Girt Bar · dirty · Jan 9, 2017 · N294JB · Emb ERJ190100IGW · Emergency Equipment
  > L1 DOOR IS UNABLE TO BE DISARMED AFTER LANDING. HANDLES ARE FROZEN IN DOWN POSITION. REMOVED AND INSTALLED THE DOOR EVACUATION SLIDE IAW AMM 52-11-40. FOUND DEBRIS ON DOOR FLOOR FITTING. CLEANED DEBRIS IAW AMM 52-11-00. PERFORMED OPS CHECK. OPS CHECK PASSED
- [SDR YENA20151115565](https://openairdocs.org/sdr/YENA20151115565.md): Stringer · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > CORROSION, STR 21L HAS CORROSION FRAME 89-90. COMPLIED WITH E15-1067-01 BY CUTTING OUT DAMAGED STR SECTION, FABRICATING NEW STR SECTION, HFEC, INSTALLED NEW STRINGER SECTION, AND RESTORING TOPCOAT.
- [SDR YENA20151115564](https://openairdocs.org/sdr/YENA20151115564.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STRINGER 19L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP IAW JB EA E15-1076-01, INSTALLED NEW FABRICATED SHEAR CLIP.
- [SDR YENA20151115563](https://openairdocs.org/sdr/YENA20151115563.md): Stringer · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 23L AT FRAME 91. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, R & R STRINGER.
- [SDR YENA20151115562](https://openairdocs.org/sdr/YENA20151115562.md): Stringer · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > STR 23L CORRODED AROUND FASTENERS AT FRAME 90-91 AS MARKED. BLENDED CORROSION, HFEC, NO DEFECTS NOTED, FABRICATED L-ANGLE DOUBLER, INSTALLED DOUBLER, ALODINED, PRIMED AND TOP-COATED.
- [SDR YENA20151115561](https://openairdocs.org/sdr/YENA20151115561.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > LT SHEAR CLIP CORRODED AT FRAME 89 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP. LOCATED, DRILLED, AND TREATED NEW SHEAR CLIP. INSTALLED AND TOP-COATED NEW SHEAR CLIP.
- [SDR YENA20151115560](https://openairdocs.org/sdr/YENA20151115560.md): Stringer · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > STR 17L CORRODED, 14" AFT OF FRAME 88. CUT OUT DAMAGE. FABRICATED AND INSTALLED REPAIRED DOUBLER. COMPLIED WITH E15-1067-01.
- [SDR YENA20151115559](https://openairdocs.org/sdr/YENA20151115559.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > SHEAR CLIP CORRODED AT FRAME 85 BETWEEN STR 27L AND STR 28L. REMOVED CORRODED SHEAR CLIP, FABRICATED NEW SHEAR CLIP, HFEC FABBED SHEAR CLIP, ALODINED, PRIMED, TOPCOATED AND INSTALLED NEW SHEAR CLIP.
- [SDR YENA20151115558](https://openairdocs.org/sdr/YENA20151115558.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > LT SHEAR CLIP IS CORRODED AT FRAME 89, AT STR 19L. REMOVED CORRODED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IAW TASK CARD NR E15-1076-01. INSTALLED FABRICATED SHEAR CLIP.
- [SDR YENA20151115557](https://openairdocs.org/sdr/YENA20151115557.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > SHEAR CLIP CORRODED AT FRAME 87 BETWEEN STR 26L AND STR 27L. REMOVED SHEAR CLIP. FABRICATED NEW SHEAR CLIP IN COMPLIANCE WITH E15-1085-01. INSTALLED FABRICATED SHEAR CLIP. RESTORED TOPCOAT.
- [SDR YENA20151115556](https://openairdocs.org/sdr/YENA20151115556.md): Stringer · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Main, Longeron/Stringer
  > STR 19L CORRODED AT FRAME 91. R & R CORRODED STRINGER JUNCTION. RESTORED TOPCOAT.
- [SDR YENA20151115555](https://openairdocs.org/sdr/YENA20151115555.md): Shear Tie · corroded · Nov 15, 2015 · N294JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STR 29L AND STR 29R. REMOVED CORRODED SHEAR CLIP, LOCATED, DRILLED, AND TREATED NEW CLIP. INSTALLED AND TOPCOATED NEW CLIP.
- [SDR YENA20150911420](https://openairdocs.org/sdr/YENA20150911420.md): Battery Pack · no test · Sep 11, 2015 · N294JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MAINTENANCE WHILE PERFORMING EMERGENCY, BATTERY PACKS FAILED TEST. R & R IAW AMM 33-50-01.
- [SDR YENA20150911419](https://openairdocs.org/sdr/YENA20150911419.md): Battery Pack · no test · Sep 11, 2015 · N294JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MAINTENANCE WHILE PERFORMING EMERGENCY, LIGHT POWER UNITS FAILED TEST. R & R BATTERY PACK IAW AMM 33-50-01.
- [SDR YENA20150911418](https://openairdocs.org/sdr/YENA20150911418.md): Battery Pack · inoperative · Sep 11, 2015 · N294JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MAINTENANCE, WHILE PERFORMING EMERGENCY. POWER UNITS FUNCTIONAL TEST FAILED. R & R BATTERY PACK & FUNCTION TEST IAW AMM 33-50-01.
- [SDR YENA20150823378](https://openairdocs.org/sdr/YENA20150823378.md): Acm · failed · Aug 23, 2015 · N294JB · Emb ERJ190100IGW · Cabin Cooling System
  > RETURNED TO DEPARTURE SHORTLY AFTER TAKEOFF, LAVATORY SMOKE INDICATION, R & R ACM IAW AMM 21-51-05, OPS AND LEAK CHECKED GOOD.
- [SDR YENA20150708258](https://openairdocs.org/sdr/YENA20150708258.md): Heat Exchanger · contaminated · Jul 8, 2015 · N294JB · Emb ERJ190100IGW · Cabin Cooling System
  > RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF COFFEE GRINDS IN NR 2 PACK ACM ASSY. R & R NR 2 ACM IAW MM 21-51-05 NO LEAKS NOTED. OPS CHECKS GO
- [SDR YENA20150708257](https://openairdocs.org/sdr/YENA20150708257.md): Acm · contaminated · Jul 8, 2015 · N294JB · Emb ERJ190100IGW · Cabin Cooling System
  > RETURNED TO DEPARTURE, LAV SMOKE EICAS WARNING AT 500 AGL CABIN CREW REPORTED SMOKE IN AFT CABIN. ACCOMPLISHED INSPECTION FOR SMOKE IN CABIN. FOUND EVIDENCE OF COFFEE GRINDS IN NR 2 PACK ACM ASSEMBLY. R & R NR 2 ACM IAW MM 21-51-05, NO LEAKS NOTED, OPS CHEC
- [SDR YENA20130803170](https://openairdocs.org/sdr/YENA20130803170.md): Loop · out of position · Aug 3, 2013 · N294JB · Emb ERJ190100IGW · Overheat Detection
  > ACFT DIVERTED DUE TO BLEED 2 LEAK EICAS MESSAGE DURING CLIMB OUT. RUN QRH PROCEDURES AND MESSAGE EXTINGUISHED. PERFORMED FIM TASK 36-21-00-810-803-A, FOLLOW CH 1 SHORT CONDITION AT 1630 FOUND ODS LOOP INSULATION POSITIONED IMPROPERLY. REPOSITIONED INSULATION
- [SDR YENA20130502095](https://openairdocs.org/sdr/YENA20130502095.md): Windshield · cracked · May 2, 2013 · N294JB · Emb ERJ190100IGW · Flight Compartment Windows
  > FLT 1706 SDQ-MCO, AFTER LANDING THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO CAPT WINDSCREEN CRACKED AND CAUGHT ON FIRE. REMOVED AND REPLACED CAPT'S SIDE LEFT WINDSHIELD PER EMB AMM TASK 56-11-00. NO OTHER DAMAGED NOTED AROUND WINDSHIELD AREA OK TO CONTINUE.
- [SDR YENA20130110008](https://openairdocs.org/sdr/YENA20130110008.md): Pressure Sensor · failed · Jan 10, 2013 · N294JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT 663 SYR-MCO, AIRCRAFT DIVERTED TO IAD DUE TO NR 1 ENGINE BLEED OVER PRESSURE MESSAGE AT 129 PSI. UNABLE TO RESET PER THE QRH. REFERENCE FIM 36-14-00-810-804-A, REMOVED AND REPLACED LEFT BLEED PRESSURE SENSOR REF AMM 36-14-02. BLEED FAIL CLEARED.
- [SDR YENA20120209438](https://openairdocs.org/sdr/YENA20120209438.md): Electrical Box · defective · Feb 9, 2012 · N294JB · Emb ERJ190100IGW · Audio/Video Monitoring
  > FLT 1258 IAD-BOS, WHILE AIRCRAFT WAS SLOWING AND BEING VECTORED ON APPROACH, THE FLIGHT ATTENDANTS CALLED TO SAY A BURNING SMELL LIKE BURNING RUBBER WAS AROUND ROW 23. THERE WAS NO SMOKE OR FIRE JUST SMELL. IT DISSIPATED AFTER ABOUT 3-4 MINUTES. PERFORMED I
- [SDR YENA20111220398](https://openairdocs.org/sdr/YENA20111220398.md): Power Unit · failed · Dec 20, 2011 · N294JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 1712 SDQ-MCO, ON GROUND MAINTENANCE CHECK FOUND FWD LT DOOR EMERGENCY EXIT IDENTIFIER SIGN INOP. REMOVED AND REPLACED POWER UNIT IAW AMM 33-50-01. OPS CHECK GOOD.
- [SDR YENA20110725308](https://openairdocs.org/sdr/YENA20110725308.md): Shutoff Valve · stuck · Jul 25, 2011 · N294JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT 335 IAD-MCO, UPON DEP AT 1500 AGL - REQ'D BLEED 1 OVERPRESS EICAS WHILE RUNNING QRH. BLEED 2 IS FLUCTUATING FROM 2-98 PSI WITH BLEED 1 ALREADY ON MEL, ELECTED TO RETURN TO AIRPORT. NO OTHER EICAS MESSAGES REC'D. INSPECTED AND FOUND NR 1 NAPRSOV STUCK IN
- [SDR YENA20110721304](https://openairdocs.org/sdr/YENA20110721304.md): Acm · failed · Jul 21, 2011 · N294JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 1791, AIR TURNBACK & EMERGENCY DECLARED - AFTER TAKEOFF CLIMBING THROUGH 500 FT, RECEIVED "LAV SMOKE" MESSAGE & ALARM. AFT F/A REPORTED SMOKE STARTED IN FWD CABIN THEN AFT THEN MID. SMOKE WAS COMING IN THROUGH SIDEWALL VENTS. SMOKE DISSIPATED ON DESCENT,
- [SDR YENA20110424241](https://openairdocs.org/sdr/YENA20110424241.md): Slide · failed · Apr 24, 2011 · N294JB · Emb ERJ190100IGW · Escape Slide
  > PRIOR TO DEPARTURE WITH L1 DOOR CLOSED, THE F/A REPORTED L1 DOOR SLIDE TOUGH TO ARM. TECH HAD TO REMOVE THE SLIDE IN ORDER TO OPEN DOOR. REPLACED L1 DOOR SLIDE ASSY IAW 25-65-01. OPS CHECKED GOOD.

Next page: https://openairdocs.org/deregistered/N294JB-2025-12-09/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 = 'N294JB' AND deregistration_id = 'N294JB-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N294JB-2025-12-09/reports

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