# Service difficulty reports: N184JB

A list on [N184JB](https://openairdocs.org/aircraft/N184JB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR YENA2023110801362](https://openairdocs.org/sdr/YENA2023110801362.md): Unknown · unknown · Nov 4, 2023 · N184JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: RH BEAM CORRODED BETWEEN FR 86 AND FR 89 Y+10.5; BLENDED RH BEAM BETWEEN FR 86-89 IAW EMB 190 SRM 51-10-03. FOUND TO BE OUT OF LIMITS REF EMB 190 SRM 53-23-10/AD52. REMOVED AND REPLACED RH BEAM PN 170-65669-004 BETWEEN FR86 AND FR89 Y
- [SDR YENA2023110801361](https://openairdocs.org/sdr/YENA2023110801361.md): Unknown · unknown · Nov 4, 2023 · N184JB · Emb ERJ190100IGW · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE: LH BEAM CORRODED FR 86 AND FR 87 Y-10.R MARKED IN RED; BLENDED LH BEAM AT FR 86-87 IAW EMB 190 SRM 51-10-03 PART HAS 100% MATERIAL LOSS PART REMOVED AND REPLACED LH BEAM PN 170-65669-003 AT FR 89Y-10.5 PER EMB -190 SRM 51-40-08 ALL WO
- [SDR YENA2023110801360](https://openairdocs.org/sdr/YENA2023110801360.md): Unknown · unknown · Nov 4, 2023 · N184JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: FWD WET AREA FLOOR STRUCTURE TRACK RIGHT SUPPORT AT FRAME 1714 AND 13 Y+10.5 HAS CORROSION MARKED IN RED; BLENDED CORROSION ON RH SEAT TRACK AT FR-14 PER EMB 190 SRM 51-10-03 BLENDED AREA AT FR -13 MEASURES MATERIAL LOSS.019 ALLOWED
- [SDR YENA2023110801359](https://openairdocs.org/sdr/YENA2023110801359.md): Unknown · unknown · Nov 4, 2023 · N184JB · Emb ERJ190100IGW · Fuselage, Seat/Cargo Attach Fittings
  > DURING HEAVY MAINTENANCE: FWD WET AREA FLOOR STRUCTURE TRACK LEFT SUPPORT @FRAME 19Y-10.5 HAS CORROSION MANRED IN RED; BLENDED CORROSION ON RH SEAT TRACK AT FR -14PER EMB 190 SRM 51-10-03 DAMAGE MEASEURES L=.800 W=.600 H=.52 ORIGINAL THICKNESS IS.07 AND REMAI
- [SDR YENA2022021800075](https://openairdocs.org/sdr/YENA2022021800075.md): None · none · Feb 14, 2022 · N184JB · Emb ERJ190100IGW · Weather Radar System
  > FLT # 2028, MCO-EWR. ON DEPARTURE AT 1000 FT AGL BOTH RADIO ALTIMETERS TURNED AMBER. FO'S HUD PROVIDED ERRONEOUS DATA; COMPLIED WITH INFO NOTICE 2022-T001, NO DEFECTS NOTED, OK FOR SERVICE SUSPECT 5G INTERFERENCE. MCC DAVID NOTIFIED PER AMM 34-31-00-710-801-A
- [SDR YENA2021121300833](https://openairdocs.org/sdr/YENA2021121300833.md): Slide · deployed · Dec 11, 2021 · N184JB · Emb ERJ190100IGW · Escape Slide
  > FLT 1274, CHS-JFK. WHILE T/C C2514012-01 "DOOR SLIDE FIRING CABLE TENSION", THERE WAS A INADVERTENTLY SLIDE DEPLOYMENT ON L2 DOOR; R/R L2 DOOR SLIDE IAW AMM 25-65-01.
- [SDR YENA2021021900127](https://openairdocs.org/sdr/YENA2021021900127.md): Battery · no test · Feb 9, 2021 · N184JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT # 1141, BDL-PBI. R1 EPSU FAILED OPS TEST; R & R R1 SVC DOOR POSITION EPSU W/SERVICEABLE ASSY PER AMM 33-50-01. OPS TEST OK (CORRECT REGISTRATION NUMBER AND DATE)
- [SDR YENA202003020206](https://openairdocs.org/sdr/YENA202003020206.md): Rib · cracked · Feb 28, 2020 · N184JB · Emb ERJ190100IGW · Wing, Rib/Bulkhead
  > DURING HEAVY MAINTENANCE, RH WING LEADING EDGE RIB 17 HAS CRACK; REF AEROMAN 2020-56275: R & R RIB 17 ON LEADING EDGE RH WING IAW E190 SRM 51-40-08 & DRAWING 190-31005-405.
- [SDR YENA201906270373](https://openairdocs.org/sdr/YENA201906270373.md): Unknown · odor · Jun 27, 2019 · N184JB · Emb ERJ190100IGW · Air Distribution System
  > SUPPLEMENTAL INFORMATION: FLT 1037, SJU-SDQ. RETURNED TO FIELD. OVERWHELMING DIRTY SOCK ODOR AFTER TAKEOFF. WE BOTH FELT NAUSEOUS AND HAD HEADACHES. INFLIGHT DID NOT SMELL IT IMMEDIATELY, BUT DID AFTER ABOUT 5 MINS; PERFORMED OPERATIONAL CHECK REF 71-00-01 ALS
- [SDR YENA201901010003](https://openairdocs.org/sdr/YENA201901010003.md): Uplock · faulty · Jan 1, 2019 · N184JB · Emb ERJ190100IGW · Landing Gear Retraction/Extension System
  > FT 1210, JAX-MCO. NOSE GEAR INDICATES UP, THEN EVERY 5 SECONDS AMBER, THEN UP. WE CAN FEEL IT MOVING. R&R NLG UPLOCK PER AMM 32-32-03. OPS CK GOOD.
- [SDR YENA2018111950780](https://openairdocs.org/sdr/YENA2018111950780.md): Power Supply · failed · Nov 15, 2018 · N184JB · Emb ERJ190100IGW · Emergency Lighting
  > FT # 1354, DCA-BOS. LH LOWER EXTERNAL EMERGENCY EXIT LIGHT INOP; R & R POWER SUPPLY #6, OPS NORMAL REF AMM 33-50-01.
- [SDR YENA201710230858](https://openairdocs.org/sdr/YENA201710230858.md): Seal · contaminated · Oct 23, 2017 · N184JB · Emb ERJ190100IGW · Emergency Exits
  > LOUD SQUEAL NOISE FROM OVERWING EXIT AT 12D. OCCURRED ENTIRE FLIGHT ABOVE 10,000 FT. REMOVED & REINSTALLED THE RT OVERWING ESCAPE HATCH IAW AMM 52-21-00/400. INSPECTED DOOR LOCK MECHANISM SEAL IAW AMM 52-21-20/600 & FOUND BUILD UP OF DEBRIS ON THE SEAL. REMOV
- [SDR YENA201710110837](https://openairdocs.org/sdr/YENA201710110837.md): Processor · failed · Oct 11, 2017 · N184JB · Emb ERJ190100IGW · Detection System
  > EMERGENCY DECLARED ON APPROACH. CARGO SMOKE AFT EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT. AFT CARGO SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6, MAU 3, NIC 2.
- [SDR YENA201710110836](https://openairdocs.org/sdr/YENA201710110836.md): Processor · failed · Oct 11, 2017 · N184JB · Emb ERJ190100IGW · Detection System
  > EMERGENCY DECLARED ON APPROACH HAD A CARGO SMOKE AFT ON THE EICAS. RAN QRH. BOTTLE WAS DISCHARGED. AVNX MAU 3B FAULT, CARGO AFT SMOKE MESSAGE DETERMINED TO BE CAUSED BY FAULTY GIO 3B & NIC PROC 6 MAU 3 NIC 2.
- [SDR YENA201709150767](https://openairdocs.org/sdr/YENA201709150767.md): Floor Support · corroded · Sep 15, 2017 · N184JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION DISCOVERED ON THE FLOOR SUPPORT FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.
- [SDR YENA201709150766](https://openairdocs.org/sdr/YENA201709150766.md): Floor Support · corroded · Sep 15, 2017 · N184JB · Emb ERJ190100IGW · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT, FRAMES 86 TO 89. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-43-03, AND DRAWING 170-65660-433.
- [SDR YENA201612021037](https://openairdocs.org/sdr/YENA201612021037.md): Shear Tie · corroded · Dec 2, 2016 · N184JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 16, BETWEEN STRINGERS 27 AND 28R. R & R THE SHEAR TIE IAW SRM 51-42-02 AND 51-43-03.
- [SDR YENA201612021036](https://openairdocs.org/sdr/YENA201612021036.md): Shear Tie · corroded · Dec 2, 2016 · N184JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > DURING ROUTINE MAINTENANCE, CORROSION WAS FOUND ON SHEAR TIE AT FRAME 17 BETWEEN STRINGERS 27 - 28R. R & R THE SHEAR TIE IAW SRM 51-41-02, AND 51-43-03.
- [SDR YENA20160606544](https://openairdocs.org/sdr/YENA20160606544.md): Engine · vibration · Jun 6, 2016 · N184JB · Emb ERJ190100IGW · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTED HIGH ENGINE VIBRATION ON DEPARTURE. ACFT DIVERTED DUE TO HIGH VIBRATION AND ENGINE EXCEEDANCE ON NR 1 ENGINE. NR 1 ENGINE R & R.
- [SDR YENA20150629238](https://openairdocs.org/sdr/YENA20150629238.md): Connector · malfunctioned · Jun 29, 2015 · N184JB · Emb ERJ190100IGW · Light System Wiring
  > COCKPIT EMERGENCY LIGHT INOPERATIVE. RESET CONNECTOR AT RT EMERGENCY LIGHT BATTERY PACK. EMERGENCY LIGHT SYSTEM OK.
- [SDR YENA20150425093](https://openairdocs.org/sdr/YENA20150425093.md): Display · failed · Apr 25, 2015 · N184JB · Emb ERJ190100IGW · Central Display
  > DURING FLIGHT, ODOR OF HOT PLASTIC "MFD 2 OVHT". PERFORMED AND COMPLIED WITH INSPECTION FOR ABNORMAL ODOR OF SMOKE IAW 21-20-00-810-801-A. R & R NR 2 MFD IAW AMM 31-61-01. OPS CHECK GOOD.
- [SDR YENA20150225030](https://openairdocs.org/sdr/YENA20150225030.md): Shear Tie · corroded · Feb 25, 2015 · N184JB · Emb ERJ190100IGW · Fuselage Internal Mounting Structure
  > ON MAINTENANCE CHECK, FOUND FRAME 81 BETWEEN STR 27 & 28R HAS ONE CORRODED SHEAR CLIP. REF EAMS NR 4490-1611, REMOVED DAMAGE SHEAR CLIP, PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED NEW SHEAR CLIP. ALL WORK ACCOMPLISHED IAW EA E15-146-01.
- [SDR YENA20140707127](https://openairdocs.org/sdr/YENA20140707127.md): Circuit Card · failed · Jul 7, 2014 · N184JB · Emb ERJ190100IGW · Central Computers
  > AIRCRAFT DIVERTED DUE TO AN INTERMITTENT FIRE INDICATION ON NR 1 ENGINE ITT GAUGE, NO ORAL WARNINGS, FIM 26-11-00-810-807A FAULT CODE 26110014UT1 GENERIC I/O MODULE 1, MAU 1 MOD 11/12, FAILED. R & R GEN I/O MOD MAU 1 SLOT 11/12. ACCOMPLISHED SUCCESSFUL TARGE
- [SDR YENA20130824185](https://openairdocs.org/sdr/YENA20130824185.md): Pressure Switch · warning message · Aug 24, 2013 · N184JB · Emb ERJ190100IGW · Landing Gear Brake System
  > PARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. FAULT CODE 32400001UT1. R & R EMERGENCY PARK BRAKE PRESSURE SWITCH SYS 1 IAW AMM 32-44-09. A
- [SDR YENA20130824184](https://openairdocs.org/sdr/YENA20130824184.md): Valve · warning message · Aug 24, 2013 · N184JB · Emb ERJ190100IGW · Landing Gear Brake System
  > PARKING BRAKE NOT RELEASED MESSAGE ILLUMINATED. QRH COMPLETED STAYED ILLUMINATED. DECLARED EMERGENCY AND BRACED FOR LANDING. PERFORMED FIM TASK 32-41-00-810-852-A. R & R DUAL EMERGENCY PARK BRAKE VALVE IAW AMM 32-44-01. ALL OPS AND LEAK CHECKED OK.
- [SDR YENA20130725161](https://openairdocs.org/sdr/YENA20130725161.md): Light · inoperative · Jul 25, 2013 · N184JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MX L1 AND L2 LOW LEVEL EMERGENCY LIGHT IDENTIFIERS HAS SECTIONS INOPERATIVE. R & R BOTH L1 AND L2 EXIT IDENTIFIERS LIGHT ASSY IAW AMM 33-50-15. OPS CHECK OK.
- [SDR YENA20130725159](https://openairdocs.org/sdr/YENA20130725159.md): Power Supply · failed · Jul 25, 2013 · N184JB · Emb ERJ190100IGW · Emergency Lighting
  > DURING MX, RT OVERWING EMERGENCY LIGHT FOUND INOPERATIVE. R & R EMERGENCY POWER SUPPLY UNIT IAW AMM 33-50-01, OPS CHECKED GOOD.
- [SDR YENA20120818582](https://openairdocs.org/sdr/YENA20120818582.md): Hydraulic Line · ruptured · Aug 18, 2012 · N184JB · Emb ERJ190100IGW · Hydraulic System, Main
  > FLT 1678 KIN-FLL, CREW DECLARED EMERGENCY DUE TO HYD 2 ELEC PUMP FAIL FOLLOWED BY HYD 2 LO QTY. QRH CALLED FOR CREW AWARENESS. QTY WAS 0 BUT PRESS WAS 2900. PHONE PATCH TO MX, ASKED CREW TO PUT HYD 2 ELEC SW TO ON. AT THAT POINT HYD 2 SYS FAILED. TROUBLES
- [SDR YENA20120803570](https://openairdocs.org/sdr/YENA20120803570.md): Hydraulic Line · leaking · Aug 3, 2012 · N184JB · Emb ERJ190100IGW · Hydraulic System, Main
  > FLT 1055 JFK-PIT, HYDRAULIC SYSTEM 2 FAIL - FLUID ZERO QUANTITY AFTER NORMAL GEAR EXT / NO HYD OVERHEAT MSG. PERFORMED DETAIL VISUAL INSPECTION AND FOUND RETRACT/EXT HOSE ASSY LEAKING. REMOVED AND REPLACED HOSE ASSY IAW AMM 20-10-03. HYDRAULIC QTY LOW SERVI
- [SDR YENA20120522506](https://openairdocs.org/sdr/YENA20120522506.md): Power Supply · inoperative · May 21, 2012 · N184JB · Emb ERJ190100IGW · Emergency Lighting
  > FLT 746 SJU-MCO FOUND OVERHEAD EMERGENCY LIGHT INOP ABOVE ROW 1. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IAW AMM 33-50-00, OPS CHECK NORMAL.
- [SDR YENA20111126388](https://openairdocs.org/sdr/YENA20111126388.md): Bypass Valve · failed · Nov 26, 2011 · N184JB · Emb ERJ190100IGW · Cabin Cooling System
  > FLT 974 FLL-BOS, AIRCRAFT DIVERTED TO MCO DUE TO CABIN AND FLIGHT DECK TEMPERATURE UNCONTROLLABLE, TEMP WAS MODULATING BETWEEN HOT AND COLD. REMOVED AND REPLACED NR 2 PACK BYPASS VALVE PER AMM 21-51-10-04 OPS CHECK OF TEMP CONTROL OK.
- [SDR YENA20110928351](https://openairdocs.org/sdr/YENA20110928351.md): Converter · faulty · Sep 28, 2011 · N184JB · Emb ERJ190100IGW · Pneumatic Distribution System
  > FLT 1080 CLT-JFK, BURNING OIL SMELL IN COCKPIT ON TAKEOFF. DUE TO HISTORY WITH RECIRCULATION FILTERS ALREADY REPLACED, THE TECHNICIAN REMOVED AND REPLACED LT OZONE CONVERTER PER AMM 36-30-00. LEAKS CHECK OK.
- [SDR YENA20101010138](https://openairdocs.org/sdr/YENA20101010138.md): Detector · shorted · Oct 10, 2010 · N184JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT 522 MCO-EWR, AIR TURNBACK TO MCO DUE TO NR 2 ENG BLEED LEAK EICAS MESSAGE WHILE CLIMBING THROUGH FL300. CREW PERFORMED QRH PROCEDURE AND MESSAGE EXTINGUISHED. FOUND LOOP 5 LEAK DETECTOR SHORTED. REMOVED AND REPLACED AS PER AMM 36-21-02.
- [SDR YENA20101009137](https://openairdocs.org/sdr/YENA20101009137.md): Warning System · false activation · Oct 9, 2010 · N184JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT 590 PBI-HPN, FLT CREW DECLARED EMERGENCY AND A/C DIVERTED TO MCO DUE TO BLEED 2 LEAK MSG IN FL 310. QRH PROCEDURE COMPLETED. BLEED 2 SELECTED OFF (XBLEED) CAS MSG EXTINGUISHED. INTERROGATED CMC FOUND BLEED 2 LEAK, ODS PACK LOOP 5 (RT BLD) [C1] /WRG FAUL
- [SDR YENA20100326043](https://openairdocs.org/sdr/YENA20100326043.md): Turbine Blades · damaged · Mar 26, 2010 · N184JB · Emb ERJ190100IGW · Turbine Section
  > FLT JB1224 LGB-PDX FLIGHT FROM LONG BEACH TO PORTLAND OREGON DIVERTED TO OAK DUE TO ENGINE NR 1 FIRE DETECTION FAIL MESSAGE DURING CRUISE. PERFORMED QRH PROCEDURES AND LANDED UNEVENTFUL. INSPECTION OF NR 1 ENGINE FOUND LOW PRESSURE TURBINE BLADE DAMAGE LPT ST
- [SDR YENA20091211170](https://openairdocs.org/sdr/YENA20091211170.md): Connector · loose · Dec 11, 2009 · N184JB · Emb ERJ190200IGW · Landing Gear System Wiring
  > FLT JB1401 FLL-AUS "STEER FAIL" AMBER EICAS MESSAGE DISPLAYED AT GEAR EXTENSION, LOSS OF NOSE WHEEL STEERING ON LANDING AIRCRAFT TOWED TO GATE. MX PERFORMED TROUBLESHOOTING NO FAULT CODE FOUND, RESET AIRCRAFT AND ACCOMPLISHED STEERING ELECTRONIC SYSTEM INSPEC
- [SDR YENA20091113155](https://openairdocs.org/sdr/YENA20091113155.md): Actuator · failed · Nov 13, 2009 · N184JB · Emb ERJ190100IGW · Leading Edge Slat Actuator
  > FLT JB78 - MCO-JFK "SLAT FAIL" AT ZERO DURING DESCENT FOR LANDING, SLATS SELECTED AND FAILED TO MOVE. CREW NOTIFIED ATC, AIRCRAFT LANDED SAFELY. MX TROUBLESHOT PER AMM FIM 27-81-00 FOUND RIGHT WING SLAT ACTUATOR NR 4 AT FAULT, REMOVED AND REPLACED RT WING NR
- [SDR YENA20090913112](https://openairdocs.org/sdr/YENA20090913112.md): Bleed Air Sys · leaking · Sep 13, 2009 · N184JB · Emb ERJ190200IGW · Engine Bleed Air System
  > FLT 1326 BWI-BOS - DEPARTED BWI WITH LEFT ENGINE BLEED DEFERRED. ON CLIMBOUT AT 19000FT THE NR 2 ENGINE BLEED LEAK EICAS MESSAGE APPEARED. LEVELED OUT AT 20000FT TO EVALUATE SITUATION. CONFIRMED BLEED LEAK INDICATION REQUESTED DESCENT TO 10000FT. AT 12000
- [SDR YENA20090906110](https://openairdocs.org/sdr/YENA20090906110.md): Hinge · loose · Sep 6, 2009 · N184JB · Emb ERJ190100IGW · Fixed Inner Doors
  > FLT 1119 - COCKPIT DOOR UNATTACHED FROM DOOR FRAME. FOUND UPPER HINGE LOOSE, SECURED UPPER HINGE AND INSTALLED COCKPIT DOOR AS PER AMM 52-51-01. OPS CHECK GOOD.
- [SDR YENA20090901107](https://openairdocs.org/sdr/YENA20090901107.md): Pin · damaged · Sep 1, 2009 · N184JB · Emb ERJ190100IGW · Fire Protection System
  > FLT 1417, AT FLT 280. BLEED 2 LEAK. REMOVED AND REPLACED LEAK DETECTOR CERAMIC PINS AT (P2146) AND (J2148) LOCATED FWD TOP PYLON IAW AMM 36-20-01. CHANNEL NR2 OPS CHECK GOOD.
- [SDR YENA20090728081](https://openairdocs.org/sdr/YENA20090728081.md): Computer · failed · Jul 26, 2009 · N184JB · Emb ERJ190100IGW · Central Computers
  > FLT 1068, AUS-JFK, DIVERTED TO BNA, "AVNX MAU 1A FAIL" IN FLIGHT AT 370, AUTO PILOT DISCONNECT AND MULTIPLE ASSOCIATED FAILURES ON EICAS. TROUBLESHOT MAU 1A FAIL FAULT CODE 45452143CMC IAW EMB 190 FIM 45-45-00-810-939-A00. MAU1 NIC PROC 1 CHECKS FAULTY, REMOV
- [SDR YENA20090616062](https://openairdocs.org/sdr/YENA20090616062.md): Sensor · failed · Jun 15, 2009 · N184JB · Emb ERJ190100IGW · Pneumatic Indicating System
  > FLT 462, RSW-BOS - THE BLEED 2 LEAK MSG APPEARED ALONG WITH LEAK ROW ON 2 BUTTON. RAN QRH, ALL INDICATIONS REMAINED THE SAME. DIVERTED TO MCO. PERFORMED FIM TASK 36-21-00-810-804A, FOUND FAILURE OF LEAK DETECTOR LOOP 5 SEGMENT 1RT0186 CHANNEL 1. REMOVED &
- [SDR YENA20090522052](https://openairdocs.org/sdr/YENA20090522052.md): Controller · failed · May 20, 2009 · N184JB · Emb ERJ190100IGW · Cabin Pressure Controller
  > FLT 1402, AUS-SFO, CLIMBING THRU FL 280, BLEED 2 LEAK AMBER EICAS MESSAGE ILLUMINATED (ENGINE BLEED SYS-SINGLE-NO ICING). RETURN TO AUS DUE NR 1 BLEED ON MEL. REF FIM 36-21-00-810-804A. REMOVED AND REPLACED BOTH AMS CONTROLLER PROCESSOR MODULES (CH A&B) AS P
- [SDR YENA20090512046](https://openairdocs.org/sdr/YENA20090512046.md): Module · failed · May 7, 2009 · N184JB · Emb ERJ190100IGW · Landing Gear Steering System
  > FLT 1068, AUS-JFK, STEER FAIL ON APPROACH WHEN DOWN LANDING GEAR. DECLARED EMERGENCY, FOLLOWED QRH. REMOVED AND REPLACED NR 2 STEERING FEEDBACK SENSOR NR 2 FOR TROUBLESHOOTING. REMOVED & REPLACED STEERING MODULE PER AMM 32-53-01. PERFORMED ADJUSTMENT & FEE
- [SDR YENA20090410033](https://openairdocs.org/sdr/YENA20090410033.md): Warning System · malfunctioned · Apr 10, 2009 · N184JB · Emb ERJ190100IGW · Leading Edge Slat Control System
  > FLT 337, IAD-MCO, "SLAT FAIL" EICAS MESSAGE ON SLAT EXTENSION, 220 KIAS AT 6000FT (SPD BRK EXT) LANDED FLAPS "2" SLAT "0" PER QRH. APP SPEED 166 KIAS BRAKE TEMP PEAKED AT 315 DEG. FAULT DETERMINED TO BE TRANSITORY CONDITION PER E190 FIM 27-81-00-810-802-A.
- [SDR YENA20090306023](https://openairdocs.org/sdr/YENA20090306023.md): Indication Sys · malfunctioned · Mar 5, 2009 · N184JB · Emb ERJ190100IGW · Fuel Pressure Indicating
  > FLT 5110, BNA-JFK - AIR RETURN TO BNA, ENG 1 FUEL LO PRESS, AMBER MSG AT 8000FT AFTER DEPARTURE, ACCOMPLISHED OPS TEST OF FUEL PRESS. SYSTEM PER 73-31-00-801-803-A. OPS TEST GOOD. ACCOMPLISHED ENG FEED EJECTOR PUMP OPS CHECK PER AMM 28-21-13, REF FIM 28-21-
- [SDR YENA20090217013](https://openairdocs.org/sdr/YENA20090217013.md): Unknown · smoke · Feb 13, 2009 · N184JB · Emb ERJ190100IGW · Air Distribution System
  > FLT 115 JFK-MSY - SMOKE IN COCKPIT AFTER TAKEOFF. SMELL THROUGHOUT A/C. DOME LIGHT TURNED ON, SMOKE CONFIRMED. ACCOMPLISHED MX PROCEDURES. PERFORMED POWER ASSURANCE TEST ON BOTH ENGS PER AMM 71-00-00 AND BLEED TEST PER AMM 36-11-00, NO ODOR OR SMOKE PRESEN
- [SDR YENA2008087](https://openairdocs.org/sdr/YENA2008087.md): Unknown · odor · Sep 8, 2008 · N184JB · Emb ERJ190100IGW · Air Distribution System
  > STRONG PLASTIC BURNING ODOR, AFTER TAKEOFF UNTIL 3000 FEET. ODOR RETURNED ON DOWN WIND AT 3000 FEET UNTIL TOUCHDOWN. PERFORMED FIM TASK 21-20-00-801A. NO FURTHER DEFECT NOTED. RAN AIR CONDITIONER (CREW) CAN NOT DUPLICATE ON THE GROUND. ACFT OK TO CONTINUE. (
- [SDR YENA2007056](https://openairdocs.org/sdr/YENA2007056.md): Battery · overtemp · Jun 24, 2007 · N184JB · Emb ERJ190100IGW · Battery/Charger System
  > ON TAKEOFF ROLL BATTERY NR 2 OVERTEMP EICAS MESSAGE. T/S TSM 24-36-810-804-A. REMOVED AND REPLACED NR 2 MAIN BATTERY, GROUND CHECK OK.
- [SDR YENA200605](https://openairdocs.org/sdr/YENA200605.md): Pitot Head · unknown · Feb 4, 2006 · N184JB · Emb ERJ190100IGW · Pitot/Static System
  > AIRCRAFT EXPERIENCED LOSS OF ADS SYSTEM NR 3 & NR 4. CMC SHOWED NR 3 & NR 4 (SMART PROBES) PITOT/STATIC AOA SENSOR. REMOVED & REPLACED NR 3 AND NR 4 INTEGRATED PITOT/STATIC AOA SENSOR IAW AMM 34-13-01, OPS CHECK. NO FAULT NOTED.

## 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 = 'N184JB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N184JB/reports

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